ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 23680.6
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74
ET - UTC (sec) : 66.18
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 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4922221.80 A = 6720268.20 meter
Y = -2322063.96 meter E = .0003611
Z = 3938698.29 I = 51.69615
XDOT = 5144.124780 Wp = 18.92155
YDOT = -4090.661888 meter/sec RA = 170.39220 deg
ZDOT = 4019.328552 TA = 29.41841
MA = 29.39809
Ha = 187.233 n.mi
Hp = 183.190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16149021.64 X = -4915023.31
Y = -7618320.09 feet Y = -2377067.09 meter
Z = 12922238.50 Z = 3914804.03
XDOT = 16877.049804 XDOT = 5169.960213
YDOT = -13420.806718 feet/sec YDOT = -4032.992967 meter/sec
ZDOT = 13186.773463 ZDOT = 4044.380740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6877532.16 X = -2096271.80
Y = -16552117.00 feet Y = -5045085.26 meter
Z = 12827350.57 Z = 3909776.45
XDOT = 20250.799409 XDOT = 6172.443660
YDOT = 1875.886024 feet/sec YDOT = 571.770060 meter/sec
ZDOT = 13286.001569 ZDOT = 4049.573278
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 10039.55498280 .00016717 00000-0 10270-3 0 9001
2 25544 51.6441 171.1159 0011231 298.8801 61.1236 15.75843839 3210
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039.55498280 = yrday.fracday
Element set: 900
Inclination: 51.6441 deg
RA of node: 171.1159 deg
Eccentricity: .0011231
Arg of perigee: 298.8801 deg
Mean anomaly: 61.1236 deg
Mean motion: 15.75843839 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 321
Checksum: 295
Coasting Arc #2 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4718391.10 A = 6722909.95 meter
Y = 3708083.70 meter E = .0009130
Z = -3016943.92 I = 51.73522
XDOT = -5262.658732 Wp = 326.41875
YDOT = -2658.604806 meter/sec RA = 165.19855 deg
ZDOT = 4963.312465 TA = 358.68648
MA = 358.68887
Ha = 187.408 n.mi
Hp = 182.900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15480285.75 X = -4744849.47
Y = 12165628.93 feet Y = 3655172.04 meter
Z = -9898109.97 Z = -3039929.39
XDOT = -17265.940723 XDOT = -5256.648873
YDOT = -8722.456714 feet/sec YDOT = -2717.421576 meter/sec
ZDOT = 16283.833547 ZDOT = 4937.761606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19615087.08 X = -5978678.54
Y = -1038882.34 feet Y = -316651.34 meter
Z = -9989166.00 Z = -3044697.80
XDOT = -7362.249485 XDOT = -2244.013643
YDOT = -16580.638274 feet/sec YDOT = -5053.778546 meter/sec
ZDOT = 16182.346736 ZDOT = 4932.379285
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 10040.50621736 .00016717 00000-0 10270-3 0 9013
2 25544 51.6445 166.2187 0011310 303.5452 56.4632 15.75835825 3363
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040.50621736 = yrday.fracday
Element set: 901
Inclination: 51.6445 deg
RA of node: 166.2187 deg
Eccentricity: .0011310
Arg of perigee: 303.5452 deg
Mean anomaly: 56.4632 deg
Mean motion: 15.75835825 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 336
Checksum: 280
Coasting Arc #3 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216254.39 A = 6717462.24 meter
Y = 2382277.31 meter E = .0010520
Z = -4661119.36 I = 51.74646
XDOT = -5635.652584 Wp = 6.55699
YDOT = 4414.359495 meter/sec RA = 160.10284 deg
ZDOT = -2831.990806 TA = 235.45980
MA = 235.55914
Ha = 187.654 n.mi
Hp = 182.717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13832855.61 X = 4211944.21
Y = 7815870.43 feet Y = 2429402.00 meter
Z = -15292386.35 Z = -4640647.78
XDOT = -18489.673833 XDOT = -5670.838978
YDOT = 14482.806743 feet/sec YDOT = 4351.141634 meter/sec
ZDOT = -9291.308418 ZDOT = -2859.453356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5559592.71 X = 1694563.86
Y = 14966882.80 feet Y = 4561905.88 meter
Z = -15211053.66 Z = -4636329.16
XDOT = -22335.186569 XDOT = -6807.764866
YDOT = -1289.117103 feet/sec YDOT = -392.922893 meter/sec
ZDOT = -9400.113803 ZDOT = -2865.154687
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 10041.52084199 .00016717 00000-0 10270-3 0 9023
2 25544 51.6450 160.9944 0011319 307.2783 52.7348 15.75883317 3528
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041.52084199 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 160.9944 deg
Eccentricity: .0011319
Arg of perigee: 307.2783 deg
Mean anomaly: 52.7348 deg
Mean motion: 15.75883317 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 352
Checksum: 305
Coasting Arc #4 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5071386.66 A = 6725132.90 meter
Y = -4000216.64 meter E = .0004979
Z = 1872958.41 I = 51.80129
XDOT = 4360.748099 Wp = 67.61735
YDOT = 2873.610210 meter/sec RA = 154.92380 deg
ZDOT = -5656.402846 TA = 91.62716
MA = 91.57013
Ha = 187.764 n.mi
Hp = 182.343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16638407.66 X = 5106642.66
Y = -13124070.33 feet Y = -3943308.28 meter
Z = 6144876.69 Z = 1897680.03
XDOT = 14306.916334 XDOT = 4355.767715
YDOT = 9427.855021 feet/sec YDOT = 2922.346905 meter/sec
ZDOT = -18557.752118 ZDOT = -5635.231047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21159571.52 X = 6449437.40
Y = 370034.45 feet Y = 112786.50 meter
Z = 6242831.80 Z = 1902815.13
XDOT = 5203.170959 XDOT = 1585.926508
YDOT = 14885.509060 feet/sec YDOT = 4537.103161 meter/sec
ZDOT = -18473.610567 ZDOT = -5630.756501
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 10042.53544153 .00016717 00000-0 10270-3 0 9037
2 25544 51.6454 155.7700 0011236 311.5406 48.4793 15.75922245 3689
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042.53544153 = yrday.fracday
Element set: 903
Inclination: 51.6454 deg
RA of node: 155.7700 deg
Eccentricity: .0011236
Arg of perigee: 311.5406 deg
Mean anomaly: 48.4793 deg
Mean motion: 15.75922245 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 368
Checksum: 290
Coasting Arc #5 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3383825.10 A = 6715074.39 meter
Y = -2705355.29 meter E = .0006895
Z = 5133053.20 I = 51.79584
XDOT = 5914.317943 Wp = 322.55727
YDOT = -4727.402042 meter/sec RA = 149.81408 deg
ZDOT = 1413.645639 TA = 113.97204
MA = 113.89983
Ha = 187.949 n.mi
Hp = 182.018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11101788.39 X = -3378256.50
Y = -8875837.55 feet Y = -2743164.06 meter
Z = 16840725.73 Z = 5116628.64
XDOT = 19403.930259 XDOT = 5959.874011
YDOT = -15509.849219 feet/sec YDOT = -4661.009906 meter/sec
ZDOT = 4637.945009 ZDOT = 1442.487166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3278744.99 X = -999361.47
Y = -13909536.72 feet Y = -4239626.79 meter
Z = 16775424.29 Z = 5113149.32
XDOT = 23804.523695 XDOT = 7255.618822
YDOT = 94.957423 feet/sec YDOT = 28.943022 meter/sec
ZDOT = 4752.232161 ZDOT = 1448.480363
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 10043.55001386 .00016717 00000-0 10270-3 0 9047
2 25544 51.6464 150.5449 0011359 315.8069 44.2187 15.76005019 3842
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043.55001386 = yrday.fracday
Element set: 904
Inclination: 51.6464 deg
RA of node: 150.5449 deg
Eccentricity: .0011359
Arg of perigee: 315.8069 deg
Mean anomaly: 44.2187 deg
Mean motion: 15.76005019 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 384
Checksum: 293
Coasting Arc #6 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186588.31 A = 6726373.95 meter
Y = 4226579.23 meter E = .0017163
Z = -570150.42 I = 51.85965
XDOT = -3416.599353 Wp = 359.67568
YDOT = -3381.422398 meter/sec RA = 144.66003 deg
ZDOT = 6029.502148 TA = 354.12675
MA = 354.14685
Ha = 188.186 n.mi
Hp = 181.687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17016365.85 X = -5230695.59
Y = 13866729.76 feet Y = 4168333.09 meter
Z = -1870572.23 Z = -595453.32
XDOT = -11209.315461 XDOT = -3407.823086
YDOT = -11093.905505 feet/sec YDOT = -3419.579613 meter/sec
ZDOT = 19781.831195 ZDOT = 6012.926227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21930853.07 X = -6684524.02
Y = 703852.88 feet Y = 214534.36 meter
Z = -1970841.54 Z = -600712.50
XDOT = -2219.562592 XDOT = -676.522678
YDOT = -14090.610770 feet/sec YDOT = -4294.818163 meter/sec
ZDOT = 19715.895070 ZDOT = 6009.404817
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 10044.50115481 .00016717 00000-0 10270-3 0 9056
2 25544 51.6467 145.6473 0011469 320.5238 39.5089 15.75987312 3998
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044.50115481 = yrday.fracday
Element set: 905
Inclination: 51.6467 deg
RA of node: 145.6473 deg
Eccentricity: .0011469
Arg of perigee: 320.5238 deg
Mean anomaly: 39.5089 deg
Mean motion: 15.75987312 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 399
Checksum: 318
Coasting Arc #7 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2583354.89 A = 6714263.13 meter
Y = 3251924.36 meter E = .0012356
Z = -5282660.44 I = 51.84309
XDOT = -5924.866483 Wp = 42.83237
YDOT = 4913.893983 meter/sec RA = 139.53007 deg
ZDOT = 136.564357 TA = 228.40729
MA = 228.51325
Ha = 188.335 n.mi
Hp = 181.415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8475573.78 X = 2572460.77
Y = 10669043.19 feet Y = 3280751.83 meter
Z = -17331563.12 Z = -5270137.47
XDOT = -19438.538329 XDOT = -5980.037556
YDOT = 16121.699419 feet/sec YDOT = 4847.330140 meter/sec
ZDOT = 448.045792 ZDOT = 107.647964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 579622.14 X = 176668.83
Y = 13676739.89 feet Y = 4168670.32 meter
Z = -17281716.86 Z = -5267467.30
XDOT = -24216.689251 XDOT = -7381.246884
YDOT = 1409.998226 feet/sec YDOT = 429.767459 meter/sec
ZDOT = 333.453090 ZDOT = 101.636502
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 10045.51567929 .00016717 00000-0 10270-3 0 9067
2 25544 51.6465 140.4232 0011484 324.2054 35.8339 15.76049045 4155
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045.51567929 = yrday.fracday
Element set: 906
Inclination: 51.6465 deg
RA of node: 140.4232 deg
Eccentricity: .0011484
Arg of perigee: 324.2054 deg
Mean anomaly: 35.8339 deg
Mean motion: 15.76049045 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 415
Checksum: 296
Coasting Arc #8 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5113494.81 A = 6725971.24 meter
Y = -4291698.47 meter E = .0001747
Z = -829282.83 I = 51.90427
XDOT = 2507.300556 Wp = 19.80996
YDOT = 4143.028609 meter/sec RA = 134.40489 deg
ZDOT = -5982.586054 TA = 169.20209
MA = 169.19834
Ha = 188.399 n.mi
Hp = 181.139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16776557.79 X = 5165133.71
Y = -14080375.56 feet Y = -4234227.66 meter
Z = -2720744.19 Z = -804316.42
XDOT = 8226.051693 XDOT = 2489.847716
YDOT = 13592.613545 feet/sec YDOT = 4170.968795 meter/sec
ZDOT = -19627.907001 ZDOT = -5970.448532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21843931.48 X = 6658030.31
Y = -1755315.94 feet Y = -535020.30 meter
Z = -2621800.82 Z = -799124.89
XDOT = -1198.579953 XDOT = -365.327170
YDOT = 14318.645312 feet/sec YDOT = 4364.323091 meter/sec
ZDOT = -19579.552477 ZDOT = -5967.847595
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 10046.53017895 .00016717 00000-0 10270-3 0 9073
2 25544 51.6456 135.1982 0011409 328.4034 31.6444 15.76082618 4311
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046.53017895 = yrday.fracday
Element set: 907
Inclination: 51.6456 deg
RA of node: 135.1982 deg
Eccentricity: .0011409
Arg of perigee: 328.4034 deg
Mean anomaly: 31.6444 deg
Mean motion: 15.76082618 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 431
Checksum: 298
Coasting Arc #9 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2010/047/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1834332.67 A = 6714929.96 meter
Y = -4024510.21 meter E = .0013338
Z = 5056964.46 I = 51.88865
XDOT = 5730.163773 Wp = 355.37224
YDOT = -4835.369229 meter/sec RA = 129.24890 deg
ZDOT = -1756.934251 TA = 111.55484
MA = 111.41263
Ha = 188.522 n.mi
Hp = 180.735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6018151.80 X = -1813758.85
Y = -13203773.65 feet Y = -4044907.43 meter
Z = 16591090.74 Z = 5048103.70
XDOT = 18799.749911 XDOT = 5792.342542
YDOT = -15864.072272 feet/sec YDOT = -4770.943597 meter/sec
ZDOT = -5764.219982 ZDOT = -1728.946348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2413532.86 X = 735644.81
Y = -14349357.94 feet Y = -4373684.30 meter
Z = 16555750.29 Z = 5046192.69
XDOT = 23455.993667 XDOT = 7149.386870
YDOT = -2625.477742 feet/sec YDOT = -800.245616 meter/sec
ZDOT = -5653.296030 ZDOT = -1723.124630
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 10047.54465121 .00016717 00000-0 10270-3 0 9085
2 25544 51.6462 129.9721 0011596 332.2780 27.7765 15.76163206 4470
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047.54465121 = yrday.fracday
Element set: 908
Inclination: 51.6462 deg
RA of node: 129.9721 deg
Eccentricity: .0011596
Arg of perigee: 332.2780 deg
Mean anomaly: 27.7765 deg
Mean motion: 15.76163206 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 447
Checksum: 309
Coasting Arc #10 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2010/048/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4855212.15 A = 6723946.44 meter
Y = 4073448.21 meter E = .0017520
Z = 2210837.82 I = 51.93646
XDOT = -1762.065387 Wp = 30.12358
YDOT = -5095.658572 meter/sec RA = 124.15101 deg
ZDOT = 5515.189432 TA = 354.60662
MA = 354.62546
Ha = 188.765 n.mi
Hp = 180.418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15929173.72 X = -4911140.99
Y = 13364331.38 feet Y = 4018841.78 meter
Z = 7253404.93 Z = 2187115.47
XDOT = -5781.054418 XDOT = -1731.745213
YDOT = -16718.039934 feet/sec YDOT = -5115.193118 meter/sec
ZDOT = 18094.453518 ZDOT = 5506.703466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20691287.23 X = -6306704.35
Y = 2360030.28 feet Y = 719337.23 meter
Z = 7159378.59 Z = 2182178.59
XDOT = 4464.239119 XDOT = 1360.700083
YDOT = -15687.572565 feet/sec YDOT = -4781.572118 meter/sec
ZDOT = 18060.560879 ZDOT = 5504.858956
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 10048.55910059 .00016717 00000-0 10270-3 0 9093
2 25544 51.6455 124.7468 0011555 336.9383 23.1261 15.76166175 4635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048.55910059 = yrday.fracday
Element set: 909
Inclination: 51.6455 deg
RA of node: 124.7468 deg
Eccentricity: .0011555
Arg of perigee: 336.9383 deg
Mean anomaly: 23.1261 deg
Mean motion: 15.76166175 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 463
Checksum: 312
Coasting Arc #11 (Orbit 477)
---------------------------------------
Vector Time (GMT): 2010/049/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293084.88 A = 6717225.21 meter
Y = 4861880.80 meter E = .0009225
Z = -4451315.09 I = 51.92943
XDOT = -5385.961054 Wp = 34.82623
YDOT = 4424.582970 meter/sec RA = 118.97697 deg
ZDOT = 3278.804461 TA = 267.85108
MA = 267.95672
Ha = 188.835 n.mi
Hp = 180.056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4242404.48 X = 1260245.77
Y = 15951052.48 feet Y = 4876156.94 meter
Z = -14604052.13 Z = -4445113.44
XDOT = -17670.475900 XDOT = -5450.964866
YDOT = 14516.348326 feet/sec YDOT = 4363.990709 meter/sec
ZDOT = 10757.232484 ZDOT = 3252.481629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4900443.51 X = -1493655.18
Y = 15784287.61 feet Y = 4811050.86 meter
Z = -14579243.04 Z = -4443753.28
XDOT = -21601.548519 XDOT = -6584.151989
YDOT = 3100.576308 feet/sec YDOT = 945.055659 meter/sec
ZDOT = 10652.885888 ZDOT = 3246.999619
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 10049.51012277 .00016717 00000-0 10270-3 0 9107
2 25544 51.6444 119.8480 0011602 341.1812 18.8922 15.76227399 4787
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049.51012277 = yrday.fracday
Element set: 910
Inclination: 51.6444 deg
RA of node: 119.8480 deg
Eccentricity: .0011602
Arg of perigee: 341.1812 deg
Mean anomaly: 18.8922 deg
Mean motion: 15.76227399 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 478
Checksum: 298
Coasting Arc #12 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2010/050/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4542873.31 A = 6720649.22 meter
Y = -3543324.83 meter E = .0011674
Z = -3473453.61 I = 51.95417
XDOT = 1227.097845 Wp = 10.17296
YDOT = 6064.395179 meter/sec RA = 113.89499 deg
ZDOT = -4572.569294 TA = 210.79399
MA = 210.86253
Ha = 188.945 n.mi
Hp = 179.901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14904439.98 X = 4599031.00
Y = -11625081.45 feet Y = -3492209.90 meter
Z = -11395845.17 Z = -3451247.97
XDOT = 4025.911564 XDOT = 1181.405994
YDOT = 19896.309642 feet/sec YDOT = 6077.861608 meter/sec
ZDOT = -15001.867764 ZDOT = -4566.719404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18837148.63 X = 5741562.90
Y = -2108447.40 feet Y = -642654.77 meter
Z = -11307803.42 Z = -3446618.48
XDOT = -7022.722494 XDOT = -2140.525816
YDOT = 17746.817380 feet/sec YDOT = 5409.229937 meter/sec
ZDOT = -14978.417255 ZDOT = -4565.421579
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 10050.52452229 .00016717 00000-0 10270-3 0 9116
2 25544 51.6441 114.6214 0011639 345.2095 14.8727 15.76237020 4949
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050.52452229 = yrday.fracday
Element set: 911
Inclination: 51.6441 deg
RA of node: 114.6214 deg
Eccentricity: .0011639
Arg of perigee: 345.2095 deg
Mean anomaly: 14.8727 deg
Mean motion: 15.76237020 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 494
Checksum: 279
Coasting Arc #13 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2010/051/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -906112.44 A = 6720459.73 meter
Y = -5705337.50 meter E = .0015579
Z = 3437146.93 I = 51.96606
XDOT = 5019.693592 Wp = 40.72081
YDOT = -3586.547293 meter/sec RA = 108.71333 deg
ZDOT = -4606.830356 TA = 98.79933
MA = 98.62288
Ha = 189.028 n.mi
Hp = 179.434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2972809.86 X = -858943.89
Y = -18718298.89 feet Y = -5715206.34 meter
Z = 11276728.76 Z = 3432859.84
XDOT = 16468.810996 XDOT = 5081.804876
YDOT = -11766.887443 feet/sec YDOT = -3530.066973 meter/sec
ZDOT = -15114.272821 ZDOT = -4582.293916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6868590.67 X = 2093546.44
Y = -17675489.41 feet Y = -5387489.17 meter
Z = 11259505.29 Z = 3431897.21
XDOT = 18948.408405 XDOT = 5775.474882
YDOT = -2251.291097 feet/sec YDOT = -686.193526 meter/sec
ZDOT = -15016.966664 ZDOT = -4577.171439
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 10051.53889414 .00016717 00000-0 10270-3 0 9129
2 25544 51.6446 109.3948 0011864 348.8356 11.2544 15.76318459 5101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051.53889414 = yrday.fracday
Element set: 912
Inclination: 51.6446 deg
RA of node: 109.3948 deg
Eccentricity: .0011864
Arg of perigee: 348.8356 deg
Mean anomaly: 11.2544 deg
Mean motion: 15.76318459 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 510
Checksum: 314
Coasting Arc #14 (Orbit 525)
---------------------------------------
Vector Time (GMT): 2010/052/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244395.33 A = 6716873.64 meter
Y = 2637956.00 meter E = .0010844
Z = 4477656.54 I = 51.96226
XDOT = -914.401814 Wp = 40.41722
YDOT = -6943.491933 meter/sec RA = 103.63234 deg
ZDOT = 3227.670012 TA = 17.49932
MA = 17.46199
Ha = 189.264 n.mi
Hp = 179.125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13925181.53 X = -4295329.40
Y = 8654711.29 feet Y = 2590207.94 meter
Z = 14690474.22 Z = 4456913.71
XDOT = -3000.005951 XDOT = -852.369778
YDOT = -22780.485344 feet/sec YDOT = -6953.370425 meter/sec
ZDOT = 10589.468543 ZDOT = 3223.378678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16456428.42 X = -5015919.38
Y = 641494.08 feet Y = 195527.39 meter
Z = 14608189.14 Z = 4452576.05
XDOT = 8588.753548 XDOT = 2617.852082
YDOT = -20138.927195 feet/sec YDOT = -6138.345009 meter/sec
ZDOT = 10572.195323 ZDOT = 3222.405134
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 10052.55324261 .00016717 00000-0 10270-3 0 9137
2 25544 51.6443 104.1681 0011759 353.5378 6.5633 15.76333097 5263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052.55324261 = yrday.fracday
Element set: 913
Inclination: 51.6443 deg
RA of node: 104.1681 deg
Eccentricity: .0011759
Arg of perigee: 353.5378 deg
Mean anomaly: 6.5633 deg
Mean motion: 15.76333097 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 526
Checksum: 294
Coasting Arc #15 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2010/053/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 764580.8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 735096.03 A = 6723487.44 meter
Y = 6327688.25 meter E = .0017033
Z = -2121564.21 I = 51.99121
XDOT = -4757.767451 Wp = 12.57742
YDOT = 2411.202930 meter/sec RA = 98.46048 deg
ZDOT = 5567.569605 TA = 323.77987
MA = 323.89508
Ha = 189.285 n.mi
Hp = 178.812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2411732.37 X = 674590.10
Y = 20760132.04 feet Y = 6335570.22 meter
Z = -6960512.51 Z = -2118140.14
XDOT = -15609.473266 XDOT = -4811.422250
YDOT = 7910.770767 feet/sec YDOT = 2357.698757 meter/sec
ZDOT = 18266.304479 ZDOT = 5544.326335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7745862.88 X = -2360939.01
Y = 19416309.16 feet Y = 5918091.03 meter
Z = -6946712.65 Z = -2117358.02
XDOT = -16171.137898 XDOT = -4928.962831
YDOT = 22.175518 feet/sec YDOT = 6.759098 meter/sec
ZDOT = 18174.071245 ZDOT = 5539.456915
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 10053.50417101 .00016717 00000-0 10270-3 0 9140
2 25544 51.6447 99.2683 0011839 357.4912 2.6191 15.76367404 5411
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053.50417101 = yrday.fracday
Element set: 914
Inclination: 51.6447 deg
RA of node: 99.2683 deg
Eccentricity: .0011839
Arg of perigee: 357.4912 deg
Mean anomaly: 2.6191 deg
Mean motion: 15.76367404 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 541
Checksum: 295
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