Date:
April 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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 7)
---------------------------------------
Vector Time (GMT): 2007/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716836
55 A = 6714922
07 meter
Y = -5321639
49 meter E =
0018848
Z = -3088843
35 I = 51
95668
XDOT = 3598
317961 Wp = 62
43275
YDOT = 4686
856929 meter/sec RA = 93
18434 deg
ZDOT = -4924
077421 TA = 153
23675
MA = 153
13937
Ha = 188
490 n
mi
Hp = 171
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8913505
74 X = 2791147
00
Y = -17459447
13 feet Y = -5290842
75 meter
Z = -10134000
51 Z = -3075464
56
XDOT = 11805
505120 XDOT = 3569
561680
YDOT = 15376
827195 feet/sec YDOT = 4726
934637 meter/sec
ZDOT = -16155
109650 ZDOT = -4906
666569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8179469
89 X = 2493102
42
Y = -17843305
50 feet Y = -5438639
52 meter
Z = -10084322
80 Z = -3073701
59
XDOT = 11270
455951 XDOT = 3435
234974
YDOT = 14232
733819 feet/sec YDOT = 4338
137268 meter/sec
ZDOT = -16088
942342 ZDOT = -4903
909626
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 07100
48378295
00020000 00000-0 20000-3 0 9003
2 25544 51
6313 93
7753 0015867 51
2531 309
0049 15
78625473 80
Satellite: ISS
Catalog Number: 25544
Epoch time: 07100
48378295 = yrday
fracday
Element set: 900
Inclination: 51
6313 deg
RA of node: 93
7753 deg
Eccentricity:
0015867
Arg of perigee: 51
2531 deg
Mean anomaly: 309
0049 deg
Mean motion: 15
78625473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 8
Checksum: 285
Coasting Arc #2 (Orbit 23)
---------------------------------------
Vector Time (GMT): 2007/101/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2686604
13 A = 6714423
17 meter
Y = -5251299
90 meter E =
0027257
Z = 3195124
34 I = 51
95541
XDOT = 3610
605912 Wp = 71
80892
YDOT = -4809
661138 meter/sec RA = 87
98511 deg
ZDOT = -4827
202574 TA = 70
97781
MA = 70
68272
Ha = 188
475 n
mi
Hp = 171
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8814318
01 X = -2643204
95
Y = -17228674
21 feet Y = -5281100
37 meter
Z = 10482691
42 Z = 3182178
25
XDOT = 11845
819921 XDOT = 3687
569487
YDOT = -15779
728142 feet/sec YDOT = -4768
854967 meter/sec
ZDOT = -15837
278786 ZDOT = -4809
475396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9922574
02 X = -3024400
56
Y = -16646196
60 feet Y = -5073760
72 meter
Z = 10433259
32 Z = 3180057
44
XDOT = 9719
867968 XDOT = 2962
615757
YDOT = -15764
822077 feet/sec YDOT = -4805
117769 meter/sec
ZDOT = -15771
155320 ZDOT = -4807
048142
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 07101
49661897
00020000 00000-0 20000-3 0 9019
2 25544 51
6308 88
5366 0015926 54
5189 305
7460 15
78698947 241
Satellite: ISS
Catalog Number: 25544
Epoch time: 07101
49661897 = yrday
fracday
Element set: 901
Inclination: 51
6308 deg
RA of node: 88
5366 deg
Eccentricity:
0015926
Arg of perigee: 54
5189 deg
Mean anomaly: 305
7460 deg
Mean motion: 15
78698947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 24
Checksum: 322
Coasting Arc #3 (Orbit 39)
---------------------------------------
Vector Time (GMT): 2007/102/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3550017
00 A = 6708190
35 meter
Y = 2796095
88 meter E =
0019272
Z = 4940301
76 I = 51
93141
XDOT = -2544
308417 Wp = 75
18042
YDOT = -6977
491446 meter/sec RA = 82
87735 deg
ZDOT = 2118
841462 TA = 354
41469
MA = 354
43615
Ha = 188
592 n
mi
Hp = 171
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11647037
40 X = -3605018
49
Y = 9173542
90 feet Y = 2756090
13 meter
Z = 16208339
12 Z = 4922922
23
XDOT = -8347
468561 XDOT = -2476
388905
YDOT = -22892
032304 feet/sec YDOT = -7005
563545 meter/sec
ZDOT = 6951
579600 ZDOT = 2106
646329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10974886
86 X = -3345145
51
Y = 10072968
38 feet Y = 3070240
76 meter
Z = 16143258
45 Z = 4920465
17
XDOT = -9435
833723 XDOT = -2876
042119
YDOT = -21356
817832 feet/sec YDOT = -6509
558075 meter/sec
ZDOT = 6904
748589 ZDOT = 2104
567370
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 07102
50943406
00020000 00000-0 20000-3 0 9022
2 25544 51
6301 83
2980 0015857 58
4994 301
7718 15
78699275 403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07102
50943406 = yrday
fracday
Element set: 902
Inclination: 51
6301 deg
RA of node: 83
2980 deg
Eccentricity:
0015857
Arg of perigee: 58
4994 deg
Mean anomaly: 301
7718 deg
Mean motion: 15
78699275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 40
Checksum: 297
Coasting Arc #4 (Orbit 54)
---------------------------------------
Vector Time (GMT): 2007/103/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1668530
34 A = 6718564
95 meter
Y = 6490242
01 meter E =
0027064
Z = -317661
79 I = 51
96231
XDOT = -4541
285309 Wp = 54
24301
YDOT = 1446
131678 meter/sec RA = 77
70778 deg
ZDOT = 6065
161838 TA = 302
31035
MA = 302
57218
Ha = 188
390 n
mi
Hp = 171
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5474180
90 X = 1597374
64
Y = 21293444
93 feet Y = 6508502
59 meter
Z = -1042197
46 Z = -309729
15
XDOT = -14899
230018 XDOT = -4586
582001
YDOT = 4744
526501 feet/sec YDOT = 1395
095423 meter/sec
ZDOT = 19898
824928 ZDOT = 6042
990280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7503471
69 X = 2287058
17
Y = 20667328
06 feet Y = 6299401
59 meter
Z = -1011480
44 Z = -308299
24
XDOT = -12976
628450 XDOT = -3955
276352
YDOT = 5619
521990 feet/sec YDOT = 1712
830302 meter/sec
ZDOT = 19815
520829 ZDOT = 6039
770749
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 07103
45892634
00020000 00000-0 20000-3 0 9034
2 25544 51
6301 78
3875 0015832 62
9218 297
3561 15
78781022 557
Satellite: ISS
Catalog Number: 25544
Epoch time: 07103
45892634 = yrday
fracday
Element set: 903
Inclination: 51
6301 deg
RA of node: 78
3875 deg
Eccentricity:
0015832
Arg of perigee: 62
9218 deg
Mean anomaly: 297
3561 deg
Mean motion: 15
78781022 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 55
Checksum: 293
Coasting Arc #5 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2007/104/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4328014
85 A = 6707339
54 meter
Y = 348215
29 meter E =
0028351
Z = -5135414
69 I = 51
91633
XDOT = 1135
304331 Wp = 82
21873
YDOT = 7460
301852 meter/sec RA = 72
54655 deg
ZDOT = 1473
301653 TA = 201
81084
MA = 201
93178
Ha = 188
460 n
mi
Hp = 171
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14199523
77 X = 4348746
30
Y = 1142438
63 feet Y = 396729
22 meter
Z = -16848473
38 Z = -5114338
85
XDOT = 3724
751741 XDOT = 1044
640746
YDOT = 24476
055944 feet/sec YDOT = 7472
490615 meter/sec
ZDOT = 4833
666839 ZDOT = 1478
596333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14330609
21 X = 4367969
69
Y = -484674
84 feet Y = -147728
89 meter
Z = -16769061
59 Z = -5111209
97
XDOT = 6412
547694 XDOT = 1954
544537
YDOT = 22854
226327 feet/sec YDOT = 6965
968185 meter/sec
ZDOT = 4854
574634 ZDOT = 1479
674348
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 07104
47169595
00020000 00000-0 20000-3 0 9041
2 25544 51
6299 73
1475 0015819 65
8028 294
4789 15
78745522 711
Satellite: ISS
Catalog Number: 25544
Epoch time: 07104
47169595 = yrday
fracday
Element set: 904
Inclination: 51
6299 deg
RA of node: 73
1475 deg
Eccentricity:
0015819
Arg of perigee: 65
8028 deg
Mean anomaly: 294
4789 deg
Mean motion: 15
78745522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 71
Checksum: 324
Coasting Arc #6 (Orbit 86)
---------------------------------------
Vector Time (GMT): 2007/105/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -174437
91 A = 6715100
99 meter
Y = -6114513
81 meter E =
0019237
Z = -2791072
37 I = 51
93380
XDOT = 5279
390250 Wp = 80
15942
YDOT = 2188
964906 meter/sec RA = 67
42922 deg
ZDOT = -5152
081593 TA = 131
66110
MA = 131
49625
Ha = 188
396 n
mi
Hp = 170
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -572302
86 X = -92492
96
Y = -20060740
85 feet Y = -6116006
48 meter
Z = -9157061
58 Z = -2791720
36
XDOT = 17320
834155 XDOT = 5279
548583
YDOT = 7181
643394 feet/sec YDOT = 2248
002561 meter/sec
ZDOT = -16903
154832 ZDOT = -5126
433922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3132868
89 X = -954898
44
Y = -19821372
52 feet Y = -6041554
35 meter
Z = -9160292
28 Z = -2792057
09
XDOT = 16757
223685 XDOT = 5107
601779
YDOT = 5077
900781 feet/sec YDOT = 1547
744158 meter/sec
ZDOT = -16806
289906 ZDOT = -5122
557163
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 07105
48444192
00020000 00000-0 20000-3 0 9053
2 25544 51
6303 67
9073 0015883 69
5706 290
7164 15
78814524 879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07105
48444192 = yrday
fracday
Element set: 905
Inclination: 51
6303 deg
RA of node: 67
9073 deg
Eccentricity:
0015883
Arg of perigee: 69
5706 deg
Mean anomaly: 290
7164 deg
Mean motion: 15
78814524 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 87
Checksum: 304
Coasting Arc #7 (Orbit 102)
---------------------------------------
Vector Time (GMT): 2007/106/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4751472
01 A = 6713338
90 meter
Y = -3258511
88 meter E =
0027962
Z = 3427232
97 I = 51
91579
XDOT = 853
524206 Wp = 80
06163
YDOT = -6129
973476 meter/sec RA = 62
22736 deg
ZDOT = -4608
594115 TA = 59
43290
MA = 59
15730
Ha = 188
375 n
mi
Hp = 170
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15588818
92 X = -4731330
80
Y = -10690655
79 feet Y = -3311532
70 meter
Z = 11244202
66 Z = 3404199
14
XDOT = 2800
276268 XDOT = 944
395020
YDOT = -20111
461535 feet/sec YDOT = -6119
921069 meter/sec
ZDOT = -15120
059431 ZDOT = -4604
226564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17056461
98 X = -5198809
61
Y = -8266249
37 feet Y = -2519552
81 meter
Z = 11157047
82 Z = 3400668
18
XDOT = -715
075711 XDOT = -217
955077
YDOT = -19073
043197 feet/sec YDOT = -5813
463567 meter/sec
ZDOT = -15104
398147 ZDOT = -4603
820555
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 07106
49716386
00020000 00000-0 20000-3 0 9063
2 25544 51
6303 62
6681 0015730 73
0458 287
2430 15
78854788 1033
Satellite: ISS
Catalog Number: 25544
Epoch time: 07106
49716386 = yrday
fracday
Element set: 906
Inclination: 51
6303 deg
RA of node: 62
6681 deg
Eccentricity:
0015730
Arg of perigee: 73
0458 deg
Mean anomaly: 287
2430 deg
Mean motion: 15
78854788 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 103
Checksum: 298
Coasting Arc #8 (Orbit 118)
---------------------------------------
Vector Time (GMT): 2007/107/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1766273
08 A = 6707948
51 meter
Y = 4269404
74 meter E =
0020942
Z = 4845172
94 I = 51
88475
XDOT = -5425
893987 Wp = 89
93424
YDOT = -4954
817030 meter/sec RA = 57
11846 deg
ZDOT = 2379
321036 TA = 336
96758
MA = 337
06133
Ha = 188
248 n
mi
Hp = 170
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5794859
20 X = -1837420
31
Y = 14007233
41 feet Y = 4249255
64 meter
Z = 15896236
68 Z = 4836419
28
XDOT = -17801
489460 XDOT = -5381
643759
YDOT = -16255
961383 feet/sec YDOT = -5015
244923 meter/sec
ZDOT = 7806
171378 ZDOT = 2353
069222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3500037
28 X = -1066811
36
Y = 14783858
61 feet Y = 4506120
11 meter
Z = 15863813
70 Z = 4835290
42
XDOT = -19196
812094 XDOT = -5851
188326
YDOT = -12845
241376 feet/sec YDOT = -3915
229572 meter/sec
ZDOT = 7706
690471 ZDOT = 2348
999255
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 07107
50986151
00020000 00000-0 20000-3 0 9076
2 25544 51
6313 57
4296 0015555 77
1309 283
1593 15
78914003 1192
Satellite: ISS
Catalog Number: 25544
Epoch time: 07107
50986151 = yrday
fracday
Element set: 907
Inclination: 51
6313 deg
RA of node: 57
4296 deg
Eccentricity:
0015555
Arg of perigee: 77
1309 deg
Mean anomaly: 283
1593 deg
Mean motion: 15
78914003 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 119
Checksum: 290
Coasting Arc #9 (Orbit 133)
---------------------------------------
Vector Time (GMT): 2007/108/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4427653
22 A = 6718090
97 meter
Y = 5019889
32 meter E =
0025406
Z = -499277
57 I = 51
90250
XDOT = -3291
428603 Wp = 64
26892
YDOT = 3479
443289 meter/sec RA = 51
93966 deg
ZDOT = 6041
340577 TA = 290
30733
MA = 290
58019
Ha = 188
237 n
mi
Hp = 170
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14526421
33 X = 4373616
47
Y = 16469453
15 feet Y = 5069099
68 meter
Z = -1638049
76 Z = -477898
85
XDOT = -10798
650272 XDOT = -3359
439934
YDOT = 11415
496354 feet/sec YDOT = 3442
256404 meter/sec
ZDOT = 19820
671185 ZDOT = 6025
185308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17281422
00 X = 5267377
43
Y = 13559921
30 feet Y = 4133064
01 meter
Z = -1556919
68 Z = -474549
12
XDOT = -7668
733203 XDOT = -2337
429880
YDOT = 11944
446897 feet/sec YDOT = 3640
667414 meter/sec
ZDOT = 19760
269203 ZDOT = 6022
930053
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 07108
45924566
00020000 00000-0 20000-3 0 9084
2 25544 51
6315 52
5177 0015692 80
9310 279
3630 15
78926518 1344
Satellite: ISS
Catalog Number: 25544
Epoch time: 07108
45924566 = yrday
fracday
Element set: 908
Inclination: 51
6315 deg
RA of node: 52
5177 deg
Eccentricity:
0015692
Arg of perigee: 80
9310 deg
Mean anomaly: 279
3630 deg
Mean motion: 15
78926518 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 134
Checksum: 300
Coasting Arc #10 (Orbit 149)
---------------------------------------
Vector Time (GMT): 2007/109/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3972062
40 A = 6706673
67 meter
Y = -1690530
73 meter E =
0029380
Z = -5157908
35 I = 51
84625
XDOT = 4365
670053 Wp = 91
70735
YDOT = 6183
394649 meter/sec RA = 46
77612 deg
ZDOT = 1341
002183 TA = 191
07756
MA = 191
14239
Ha = 188
150 n
mi
Hp = 170
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13031700
78 X = 4015727
58
Y = -5546360
66 feet Y = -1645868
57 meter
Z = -16922271
48 Z = -5138505
72
XDOT = 14323
064479 XDOT = 4289
687509
YDOT = 20286
727852 feet/sec YDOT = 6231
789126 meter/sec
ZDOT = 4399
613460 ZDOT = 1362
026656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11765623
72 X = 3586162
11
Y = -8038532
85 feet Y = -2450144
81 meter
Z = -16849412
51 Z = -5135700
93
XDOT = 17450
459360 XDOT = 5318
900013
YDOT = 16191
126555 feet/sec YDOT = 4935
055374 meter/sec
ZDOT = 4479
545386 ZDOT = 1365
365434
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 07109
47189770
00020000 00000-0 20000-3 0 9098
2 25544 51
6326 47
2780 0015560 84
3913 275
9027 15
78944133 1501
Satellite: ISS
Catalog Number: 25544
Epoch time: 07109
47189770 = yrday
fracday
Element set: 909
Inclination: 51
6326 deg
RA of node: 47
2780 deg
Eccentricity:
0015560
Arg of perigee: 84
3913 deg
Mean anomaly: 275
9027 deg
Mean motion: 15
78944133 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 150
Checksum: 301
Coasting Arc #11 (Orbit 165)
---------------------------------------
Vector Time (GMT): 2007/110/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2863880
59 A = 6714657
53 meter
Y = -5427267
53 meter E =
0019698
Z = -2739854
25 I = 51
85400
XDOT = 5678
358398 Wp = 95
36601
YDOT = -396
921309 meter/sec RA = 41
65206 deg
ZDOT = -5182
656067 TA = 115
85912
MA = 115
65587
Ha = 188
046 n
mi
Hp = 170
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9395933
68 X = -2789669
35
Y = -17805995
83 feet Y = -5458877
94 meter
Z = -8989023
14 Z = -2753587
25
XDOT = 18629
784769 XDOT = 5707
551546
YDOT = -1302
235267 feet/sec YDOT = -333
259179 meter/sec
ZDOT = -17003
464787 ZDOT = -5154
999340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12956919
63 X = -3949269
10
Y = -15378912
35 feet Y = -4687492
48 meter
Z = -9041398
28 Z = -2755818
20
XDOT = 16884
470926 XDOT = 5146
386738
YDOT = -4354
327550 feet/sec YDOT = -1327
199037 meter/sec
ZDOT = -16899
357619 ZDOT = -5150
924202
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 07110
48452557
00020000 00000-0 20000-3 0 9109
2 25544 51
6333 42
0383 0015538 88
1665 272
1280 15
79000960 1661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07110
48452557 = yrday
fracday
Element set: 910
Inclination: 51
6333 deg
RA of node: 42
0383 deg
Eccentricity:
0015538
Arg of perigee: 88
1665 deg
Mean anomaly: 272
1280 deg
Mean motion: 15
79000960 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 166
Checksum: 272
Coasting Arc #12 (Orbit 181)
---------------------------------------
Vector Time (GMT): 2007/111/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5696287
85 A = 6712838
34 meter
Y = -862872
66 meter E =
0028011
Z = 3421097
42 I = 51
82581
XDOT = -1892
083018 Wp = 90
55068
YDOT = -5899
096192 meter/sec RA = 36
44362 deg
ZDOT = -4606
402759 TA = 48
94717
MA = 48
70544
Ha = 188
063 n
mi
Hp = 170
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18688608
43 X = -5702834
93
Y = -2830947
05 feet Y = -926608
59 meter
Z = 11224072
89 Z = 3393408
66
XDOT = -6207
621449 XDOT = -1803
600595
YDOT = -19353
990130 feet/sec YDOT = -5919
759462 meter/sec
ZDOT = -15112
869944 ZDOT = -4615
380072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18896312
03 X = -5759595
91
Y = 1593772
00 feet Y = 485781
71 meter
Z = 11119687
10 Z = 3389280
63
XDOT = -10327
642343 XDOT = -3147
865386
YDOT = -16028
745380 feet/sec YDOT = -4885
561592 meter/sec
ZDOT = -15147
387793 ZDOT = -4616
923799
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 07111
49712939
00020000 00000-0 20000-3 0 9115
2 25544 51
6336 36
7991 0015470 92
0014 268
2923 15
79041493 1820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07111
49712939 = yrday
fracday
Element set: 911
Inclination: 51
6336 deg
RA of node: 36
7991 deg
Eccentricity:
0015470
Arg of perigee: 92
0014 deg
Mean anomaly: 268
2923 deg
Mean motion: 15
79041493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 182
Checksum: 287
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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