ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 29062.56
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 122.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.135
ET - UTC (sec) : 67.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
There are no maneuvers.
Coasting Arc #1 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2013/140/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4096210.22 A = 6798690.47 meter
Y = -5049224.92 meter E = .0013821
Z = -1957272.03 I = 51.34015
XDOT = 2831.499510 Wp = 1.21401
YDOT = -4448.759654 meter/sec RA = 244.88454 deg
ZDOT = 5565.044248 TA = 337.12285
MA = 337.18436
Ha = 228.113 n.mi
Hp = 221.048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13439009.90 X = -4029936.22
Y = -16565698.55 feet Y = -5094660.73 meter
Z = -6421496.15 Z = -1977010.45
XDOT = 9289.696554 XDOT = 2854.002179
YDOT = -14595.668155 feet/sec YDOT = -4416.970323 meter/sec
ZDOT = 18258.019186 ZDOT = 5578.854196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21044743.09 X = -6414437.69
Y = -3330547.98 feet Y = -1015151.03 meter
Z = -6503168.98 Z = -1982165.91
XDOT = -3200.686475 XDOT = -975.569238
YDOT = -15449.385979 feet/sec YDOT = -4708.972846 meter/sec
ZDOT = 18316.182675 ZDOT = 5582.772479
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13140.46110433 .00016717 00000-0 10270-3 0 9008
2 25544 51.6485 245.8109 0009551 334.4780 25.5898 15.50344770 30409
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140.46110433 = yrday.fracday
Element set: 900
Inclination: 51.6485 deg
RA of node: 245.8109 deg
Eccentricity: .0009551
Arg of perigee: 334.4780 deg
Mean anomaly: 25.5898 deg
Mean motion: 15.50344770 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 291
Coasting Arc #2 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2013/141/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4307777.40 A = 6799237.47 meter
Y = 5041753.40 meter E = .0009009
Z = 1500263.33 I = 51.35629
XDOT = -2879.715261 Wp = 75.33802
YDOT = 4176.397852 meter/sec RA = 239.90995 deg
ZDOT = -5735.204822 TA = 88.25152
MA = 88.14833
Ha = 228.252 n.mi
Hp = 220.741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14133127.96 X = 4243791.26
Y = 16541185.70 feet Y = 5089567.88 meter
Z = 4922123.79 Z = 1521035.22
XDOT = -9447.884713 XDOT = -2898.342029
YDOT = 13702.092690 feet/sec YDOT = 4144.091060 meter/sec
ZDOT = -18816.288786 ZDOT = -5749.239612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21596311.95 X = 6582555.88
Y = 2470125.78 feet Y = 752894.34 meter
Z = 5008115.60 Z = 1526473.64
XDOT = 2706.792936 XDOT = 825.030487
YDOT = 14808.075194 feet/sec YDOT = 4513.501319 meter/sec
ZDOT = -18875.354952 ZDOT = -5753.208190
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13141.49242995 .00016717 00000-0 10270-3 0 9012
2 25544 51.6485 240.6991 0009483 338.1802 21.8944 15.50388494 30560
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141.49242995 = yrday.fracday
Element set: 901
Inclination: 51.6485 deg
RA of node: 240.6991 deg
Eccentricity: .0009483
Arg of perigee: 338.1802 deg
Mean anomaly: 21.8944 deg
Mean motion: 15.50388494 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 326
Coasting Arc #3 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2013/142/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507372.94 A = 6799671.34 meter
Y = -4967901.66 meter E = .0016998
Z = -1045503.78 I = 51.37494
XDOT = 2976.007807 Wp = 10.30065
YDOT = -3929.797461 meter/sec RA = 234.93639 deg
ZDOT = 5874.196553 TA = 338.33062
MA = 338.40246
Ha = 228.381 n.mi
Hp = 220.467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14787968.97 X = -4446406.91
Y = -16298889.96 feet Y = -5017965.02 meter
Z = -3430130.51 Z = -1067252.79
XDOT = 9763.805140 XDOT = 2991.194595
YDOT = -12893.036290 feet/sec YDOT = -3896.433209 meter/sec
ZDOT = 19272.298402 ZDOT = 5888.690758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21944763.96 X = -6688764.06
Y = -1462552.63 feet Y = -445786.04 meter
Z = -3520214.48 Z = -1072961.37
XDOT = -2127.414589 XDOT = -648.435967
YDOT = -14372.416006 feet/sec YDOT = -4380.712399 meter/sec
ZDOT = 19333.251595 ZDOT = 5892.775086
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13142.45927491 .00016717 00000-0 10270-3 0 9021
2 25544 51.6493 235.9067 0009736 342.3494 17.7317 15.50411827 30717
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142.45927491 = yrday.fracday
Element set: 902
Inclination: 51.6493 deg
RA of node: 235.9067 deg
Eccentricity: .0009736
Arg of perigee: 342.3494 deg
Mean anomaly: 17.7317 deg
Mean motion: 15.50411827 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 312
Coasting Arc #4 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2013/143/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4683261.20 A = 6799868.85 meter
Y = 4900348.22 meter E = .0007889
Z = 543021.22 I = 51.39407
XDOT = -3131.021020 Wp = 81.73003
YDOT = 3660.143888 meter/sec RA = 229.96508 deg
ZDOT = -5951.060232 TA = 92.40482
MA = 92.31449
Ha = 228.477 n.mi
Hp = 220.176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15365030.20 X = 4625478.47
Y = 16077257.92 feet Y = 4952396.28 meter
Z = 1781565.70 Z = 565632.59
XDOT = -10272.378673 XDOT = -3142.807532
YDOT = 12008.346089 feet/sec YDOT = 3625.065351 meter/sec
ZDOT = -19524.475827 ZDOT = -5966.299172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22225137.81 X = 6774222.00
Y = 512824.49 feet Y = 156308.90 meter
Z = 1875263.21 Z = 571580.23
XDOT = 1348.532715 XDOT = 411.032771
YDOT = 14047.713844 feet/sec YDOT = 4281.743180 meter/sec
ZDOT = -19588.505997 ZDOT = -5970.576628
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13143.49055334 .00016717 00000-0 10270-3 0 9035
2 25544 51.6490 230.7952 0009628 346.0400 14.0484 15.50460440 30875
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143.49055334 = yrday.fracday
Element set: 903
Inclination: 51.6490 deg
RA of node: 230.7952 deg
Eccentricity: .0009628
Arg of perigee: 346.0400 deg
Mean anomaly: 14.0484 deg
Mean motion: 15.50460440 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3087
Checksum: 284
Coasting Arc #5 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2013/144/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829535.19 A = 6799953.92 meter
Y = -4769189.73 meter E = .0019379
Z = -52650.41 I = 51.41541
XDOT = 3332.010901 Wp = 20.59919
YDOT = -3432.733188 meter/sec RA = 224.99440 deg
ZDOT = 5995.372676 TA = 338.83224
MA = 338.91233
Ha = 228.618 n.mi
Hp = 219.901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15844931.72 X = -4775590.37
Y = -15646947.92 feet Y = -4822895.00 meter
Z = -172737.55 Z = -75981.80
XDOT = 10931.794293 XDOT = 3341.024294
YDOT = -11262.247991 feet/sec YDOT = -3395.422735 meter/sec
ZDOT = 19669.857862 ZDOT = 6011.581192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22261507.68 X = -6785307.54
Y = 520905.66 feet Y = 158772.04 meter
Z = -269465.23 Z = -82133.00
XDOT = -548.347092 XDOT = -167.136194
YDOT = -13975.279015 feet/sec YDOT = -4259.665044 meter/sec
ZDOT = 19737.910910 ZDOT = 6016.115245
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13144.45735455 .00016717 00000-0 10270-3 0 9042
2 25544 51.6495 226.0026 0009878 350.1116 9.9839 15.50481794 31027
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144.45735455 = yrday.fracday
Element set: 904
Inclination: 51.6495 deg
RA of node: 226.0026 deg
Eccentricity: .0009878
Arg of perigee: 350.1116 deg
Mean anomaly: 9.9839 deg
Mean motion: 15.50481794 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 313
Coasting Arc #6 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2013/145/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4941019.76 A = 6799717.09 meter
Y = 4648775.73 meter E = .0006532
Z = -479237.28 I = 51.43622
XDOT = -3581.295513 Wp = 77.49371
YDOT = 3198.846465 meter/sec RA = 220.02595 deg
ZDOT = -5961.432640 TA = 107.67672
MA = 107.60539
Ha = 228.688 n.mi
Hp = 219.635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16210694.75 X = 4890996.96
Y = 15251888.86 feet Y = 4703749.69 meter
Z = -1572300.79 Z = -455354.77
XDOT = -11749.657195 XDOT = -3587.839999
YDOT = 10494.903100 feet/sec YDOT = 3158.762296 meter/sec
ZDOT = -19558.506038 ZDOT = -5978.846066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22217329.73 X = 6771842.10
Y = -1448680.36 feet Y = -441557.77 meter
Z = -1473245.67 Z = -449045.28
XDOT = -370.550824 XDOT = -112.943891
YDOT = 14040.795422 feet/sec YDOT = 4279.634445 meter/sec
ZDOT = -19631.565264 ZDOT = -5983.701092
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13145.48858686 .00016717 00000-0 10270-3 0 9059
2 25544 51.6482 220.8908 0009785 353.8243 6.2785 15.50529644 31186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145.48858686 = yrday.fracday
Element set: 905
Inclination: 51.6482 deg
RA of node: 220.8908 deg
Eccentricity: .0009785
Arg of perigee: 353.8243 deg
Mean anomaly: 6.2785 deg
Mean motion: 15.50529644 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 339
Coasting Arc #7 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2013/146/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5005966.21 A = 6799356.00 meter
Y = -4474096.74 meter E = .0020626
Z = 987888.49 I = 51.45942
XDOT = 3870.410438 Wp = 31.59708
YDOT = -3020.436783 meter/sec RA = 215.05772 deg
ZDOT = 5894.628438 TA = 339.12900
MA = 339.21308
Ha = 228.822 n.mi
Hp = 219.354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16423773.67 X = -4960362.79
Y = -14678795.08 feet Y = -4529821.76 meter
Z = 3241103.98 Z = 963679.84
XDOT = 12698.196975 XDOT = 3875.263109
YDOT = -9909.569499 feet/sec YDOT = -2977.129073 meter/sec
ZDOT = 19339.332147 ZDOT = 5913.442151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21913055.44 X = -6679099.30
Y = 2380428.60 feet Y = 725554.64 meter
Z = 3140649.97 Z = 957270.11
XDOT = 1239.882052 XDOT = 377.916050
YDOT = -14378.595545 feet/sec YDOT = -4382.595922 meter/sec
ZDOT = 19418.221683 ZDOT = 5918.673969
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13146.51979558 .00016717 00000-0 10270-3 0 9067
2 25544 51.6484 215.7781 0009984 357.9530 2.1578 15.50556136 31344
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146.51979558 = yrday.fracday
Element set: 906
Inclination: 51.6484 deg
RA of node: 215.7781 deg
Eccentricity: .0009984
Arg of perigee: 357.9530 deg
Mean anomaly: 2.1578 deg
Mean motion: 15.50556136 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 335
Coasting Arc #8 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2013/147/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5027641.51 A = 6798656.80 meter
Y = 4319016.76 meter E = .0006315
Z = -1527945.10 I = 51.48164
XDOT = -4187.919427 Wp = 57.81506
YDOT = 2850.582167 meter/sec RA = 210.09125 deg
ZDOT = -5736.645801 TA = 138.86980
MA = 138.82219
Ha = 228.883 n.mi
Hp = 219.110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16494886.83 X = 4986394.05
Y = 14170002.48 feet Y = 4375008.59 meter
Z = -5012943.24 Z = -1503620.73
XDOT = -13739.893134 XDOT = -4191.616755
YDOT = 9352.303699 feet/sec YDOT = 2803.730301 meter/sec
ZDOT = -18821.016409 ZDOT = -5756.999066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21539031.13 X = 6565096.69
Y = -3153182.78 feet Y = -961090.11 meter
Z = -4911968.84 Z = -1497168.10
XDOT = -2127.743989 XDOT = -648.536368
YDOT = 14843.680903 feet/sec YDOT = 4524.353939 meter/sec
ZDOT = -18906.319907 ZDOT = -5762.646308
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13147.48653223 .00016717 00000-0 10270-3 0 9073
2 25544 51.6469 210.9852 0009959 1.5684 358.5497 15.50598297 31495
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147.48653223 = yrday.fracday
Element set: 907
Inclination: 51.6469 deg
RA of node: 210.9852 deg
Eccentricity: .0009959
Arg of perigee: 1.5684 deg
Mean anomaly: 358.5497 deg
Mean motion: 15.50598297 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 352
Coasting Arc #9 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2013/148/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4988699.40 A = 6797830.23 meter
Y = -4124826.63 meter E = .0020548
Z = 2032532.53 I = 51.50637
XDOT = 4535.956186 Wp = 42.79706
YDOT = -2744.152107 meter/sec RA = 205.12496 deg
ZDOT = 5545.961490 TA = 339.70746
MA = 339.78900
Ha = 229.005 n.mi
Hp = 218.824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16367124.01 X = -4952077.44
Y = -13532895.77 feet Y = -4180408.89 meter
Z = 6668413.81 Z = 2008386.29
XDOT = 14881.746018 XDOT = 4539.363934
YDOT = -9003.123710 feet/sec YDOT = -2693.409796 meter/sec
ZDOT = 18195.411711 ZDOT = 5568.004750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20918330.90 X = -6375907.26
Y = 3843530.40 feet Y = 1171508.07 meter
Z = 6568140.21 Z = 2001969.14
XDOT = 2900.193358 XDOT = 883.978936
YDOT = -15571.080144 feet/sec YDOT = -4746.065228 meter/sec
ZDOT = 18287.765990 ZDOT = 5574.111074
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13148.51769569 .00016717 00000-0 10270-3 0 9080
2 25544 51.6472 205.8718 0010082 5.4901 354.6358 15.50630309 31659
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148.51769569 = yrday.fracday
Element set: 908
Inclination: 51.6472 deg
RA of node: 205.8718 deg
Eccentricity: .0010082
Arg of perigee: 5.4901 deg
Mean anomaly: 354.6358 deg
Mean motion: 15.50630309 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 313
Coasting Arc #10 (Orbit 3179)
---------------------------------------
Vector Time (GMT): 2013/149/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4903306.89 A = 6796718.21 meter
Y = 3962784.07 meter E = .0008703
Z = -2554976.25 I = 51.53029
XDOT = -4884.147317 Wp = 40.94876
YDOT = 2656.443166 meter/sec RA = 200.15994 deg
ZDOT = -5256.881267 TA = 167.71862
MA = 167.69739
Ha = 229.059 n.mi
Hp = 218.598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16086964.85 X = 4871041.14
Y = 13001260.06 feet Y = 4017435.79 meter
Z = -8382468.01 Z = -2531234.40
XDOT = -16024.105371 XDOT = -4887.952731
YDOT = 8715.364719 feet/sec YDOT = 2601.804805 meter/sec
ZDOT = -17246.985785 ZDOT = -5280.616993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20266421.32 X = 6177205.22
Y = -4328861.83 feet Y = -1319437.09 meter
Z = -8283845.31 Z = -2524916.05
XDOT = -3588.375939 XDOT = -1093.736986
YDOT = 16370.949854 feet/sec YDOT = 4989.865515 meter/sec
ZDOT = -17346.404144 ZDOT = -5287.183983
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13149.48439122 .00016717 00000-0 10270-3 0 9097
2 25544 51.6463 201.0780 0010134 9.3188 350.8149 15.50666934 31800
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149.48439122 = yrday.fracday
Element set: 909
Inclination: 51.6463 deg
RA of node: 201.0780 deg
Eccentricity: .0010134
Arg of perigee: 9.3188 deg
Mean anomaly: 350.8149 deg
Mean motion: 15.50666934 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3180
Checksum: 301
Coasting Arc #11 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2013/150/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747882.50 A = 6795504.99 meter
Y = -3780992.35 meter E = .0019162
Z = 3028707.21 I = 51.55598
XDOT = 5251.782196 Wp = 53.44384
YDOT = -2633.178097 meter/sec RA = 195.19549 deg
ZDOT = 4935.083445 TA = 341.31264
MA = 341.38290
Ha = 229.181 n.mi
Hp = 218.301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15577042.31 X = -4719962.40
Y = -12404830.55 feet Y = -3833930.31 meter
Z = 9936703.45 Z = 3005709.92
XDOT = 17230.256550 XDOT = 5256.863330
YDOT = -8639.035752 feet/sec YDOT = -2574.421351 meter/sec
ZDOT = 16191.218653 ZDOT = 4960.608267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19410810.84 X = -5916415.14
Y = 4651267.54 feet Y = 1417706.35 meter
Z = 9841152.20 Z = 2999583.19
XDOT = 4112.685793 XDOT = 1253.546630
YDOT = -17394.176411 feet/sec YDOT = -5301.744970 meter/sec
ZDOT = 16298.113113 ZDOT = 4967.664877
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13150.51551036 .00016717 00000-0 10270-3 0 9104
2 25544 51.6466 195.9643 0010203 13.1435 346.9980 15.50701872 31964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150.51551036 = yrday.fracday
Element set: 910
Inclination: 51.6466 deg
RA of node: 195.9643 deg
Eccentricity: .0010203
Arg of perigee: 13.1435 deg
Mean anomaly: 346.9980 deg
Mean motion: 15.50701872 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 292
Coasting Arc #12 (Orbit 3210)
---------------------------------------
Vector Time (GMT): 2013/151/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4550339.57 A = 6794123.21 meter
Y = 3645738.39 meter E = .0012837
Z = -3504513.22 I = 51.58155
XDOT = -5586.215177 Wp = 38.92189
YDOT = 2630.932450 meter/sec RA = 190.23179 deg
ZDOT = -4515.585871 TA = 182.18834
MA = 182.19396
Ha = 229.211 n.mi
Hp = 218.104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14928935.60 X = 4526257.96
Y = 11961083.96 feet Y = 3696488.75 meter
Z = -11497746.80 Z = -3482466.28
XDOT = -18327.477616 XDOT = -5593.284105
YDOT = 8631.668143 feet/sec YDOT = 2568.424651 meter/sec
ZDOT = -14814.914275 ZDOT = -4542.740258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18588722.58 X = 5665842.64
Y = -4743237.52 feet Y = -1445738.80 meter
Z = -11406135.17 Z = -3476590.00
XDOT = -4468.321183 XDOT = -1361.944296
YDOT = 18393.553509 feet/sec YDOT = 5606.355110 meter/sec
ZDOT = -14928.622258 ZDOT = -4550.244064
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13151.48216514 .00016717 00000-0 10270-3 0 9111
2 25544 51.6467 191.1702 0010286 17.0655 343.0840 15.50734319 32110
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151.48216514 = yrday.fracday
Element set: 911
Inclination: 51.6467 deg
RA of node: 191.1702 deg
Eccentricity: .0010286
Arg of perigee: 17.0655 deg
Mean anomaly: 343.0840 deg
Mean motion: 15.50734319 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3211
Checksum: 275
Coasting Arc #13 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2013/152/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4279240.11 A = 6792696.07 meter
Y = -3511894.99 meter E = .0016736
Z = 3917408.98 I = 51.60727
XDOT = 5928.770081 Wp = 62.11419
YDOT = -2686.126052 meter/sec RA = 185.26893 deg
ZDOT = 4062.702617 TA = 345.36276
MA = 345.41116
Ha = 229.345 n.mi
Hp = 217.787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14039501.68 X = -4258681.12
Y = -11521965.18 feet Y = -3559633.44 meter
Z = 12852391.66 Z = 3896670.42
XDOT = 19451.345410 XDOT = 5938.630664
YDOT = -8812.749514 feet/sec YDOT = -2619.771922 meter/sec
ZDOT = 13329.076827 ZDOT = 4091.527992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17630133.69 X = -5373664.75
Y = 4609698.80 feet Y = 1405036.19 meter
Z = 12766218.07 Z = 3891143.27
XDOT = 4640.014816 XDOT = 1414.276516
YDOT = -19553.387610 feet/sec YDOT = -5959.872543 meter/sec
ZDOT = 13449.779748 ZDOT = 4099.492867
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13152.51324043 .00016717 00000-0 10270-3 0 9124
2 25544 51.6465 186.0565 0010353 20.9814 339.1760 15.50770711 32273
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152.51324043 = yrday.fracday
Element set: 912
Inclination: 51.6465 deg
RA of node: 186.0565 deg
Eccentricity: .0010353
Arg of perigee: 20.9814 deg
Mean anomaly: 339.1760 deg
Mean motion: 15.50770711 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 281
Coasting Arc #14 (Orbit 3241)
---------------------------------------
Vector Time (GMT): 2013/153/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3979069.31 A = 6791278.82 meter
Y = 3437899.34 meter E = .0017301
Z = -4315908.71 I = 51.63410
XDOT = -6204.462776 Wp = 44.98810
YDOT = 2755.167470 meter/sec RA = 180.30648 deg
ZDOT = -3522.283668 TA = 189.02473
MA = 189.05587
Ha = 229.330 n.mi
Hp = 217.638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13054689.35 X = 3961295.95
Y = 11279197.30 feet Y = 3482296.70 meter
Z = -14159805.49 Z = -4296621.53
XDOT = -20355.849001 XDOT = -6217.700069
YDOT = 9039.263354 feet/sec YDOT = 2685.711465 meter/sec
ZDOT = -11556.048781 ZDOT = -3552.456635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16787378.76 X = 5116793.05
Y = -4253458.10 feet Y = -1296454.03 meter
Z = -14079677.05 Z = -4291485.57
XDOT = -4596.614130 XDOT = -1401.047987
YDOT = 20564.811011 feet/sec YDOT = 6268.154396 meter/sec
ZDOT = -11682.399845 ZDOT = -3560.795473
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13153.47985400 .00016717 00000-0 10270-3 0 9131
2 25544 51.6472 181.2621 0010396 24.6840 335.4807 15.50798999 32424
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153.47985400 = yrday.fracday
Element set: 913
Inclination: 51.6472 deg
RA of node: 181.2621 deg
Eccentricity: .0010396
Arg of perigee: 24.6840 deg
Mean anomaly: 335.4807 deg
Mean motion: 15.50798999 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3242
Checksum: 319
Coasting Arc #15 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2013/154/10:58:21.532
Vector Time (MET): N/A
Weight (LBS) : 879644.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3608161.49 A = 6789885.53 meter
Y = -3385273.32 meter E = .0013880
Z = 4636412.03 I = 51.65944
XDOT = 6478.142131 Wp = 66.07142
YDOT = -2866.197772 meter/sec RA = 175.34465 deg
ZDOT = 2947.220918 TA = 354.59714
MA = 354.61210
Ha = 229.470 n.mi
Hp = 217.304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11837800.15 X = -3592561.16
Y = -11106539.76 feet Y = -3425535.17 meter
Z = 15211325.57 Z = 4618921.35
XDOT = 21253.747149 XDOT = 6495.394131
YDOT = -9403.535997 feet/sec YDOT = -2793.658856 meter/sec
ZDOT = 9669.359968 ZDOT = 2978.733213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15889148.33 X = -4843012.41
Y = 3637064.61 feet Y = 1108577.29 meter
Z = 15138688.51 Z = 4614272.26
XDOT = 4385.422502 XDOT = 1336.676779
YDOT = -21658.062238 feet/sec YDOT = -6601.377370 meter/sec
ZDOT = 9801.332396 ZDOT = 2987.446114
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13154.51088519 .00016717 00000-0 10270-3 0 9143
2 25544 51.6461 176.1480 0010495 28.7597 331.4131 15.50838748 32582
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154.51088519 = yrday.fracday
Element set: 914
Inclination: 51.6461 deg
RA of node: 176.1480 deg
Eccentricity: .0010495
Arg of perigee: 28.7597 deg
Mean anomaly: 331.4131 deg
Mean motion: 15.50838748 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 319
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