Date:
February 19th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 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
050/23:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
9
000/00:00:00
000 0
0 0
0 180
0
051/00:07:43
194 0
5 0
2 1
0
N/A -0
7 0
2 190
9
000/00:57:22
387 -0
6 -1
0 179
9
051/02:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
8
000/00:00:00
000 0
0 0
0 179
9
051/21:26:36
217 3
9 8
8 8
8
N/A 4
8 -0
2 191
2
000/00:25:12
435 -6
2 -0
3 185
7
Coasting Arc #1 (Orbit 479)
---------------------------------------
Vector Time (GMT): 2010/049/14:27:57
868
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2114104
55 A = 6727168
83 meter
Y = -6228695
64 meter E =
0011386
Z = 1419815
99 I = 51
95731
XDOT = 5001
725162 Wp = 59
11595
YDOT = 357
976546 meter/sec RA = 118
47191 deg
ZDOT = -5837
071978 TA = 105
34407
MA = 105
21822
Ha = 190
717 n
mi
Hp = 180
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6936038
56 X = 2176700
68
Y = -20435353
15 feet Y = -6204704
39 meter
Z = 4658188
95 Z = 1430238
62
XDOT = 16409
859455 XDOT = 5025
705553
YDOT = 1174
463735 feet/sec YDOT = 414
042523 meter/sec
ZDOT = -19150
498616 ZDOT = -5812
715679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5224260
99 X = 1592354
75
Y = -20929270
28 feet Y = -6379241
58 meter
Z = 4699335
71 Z = 1432357
53
XDOT = 15036
664625 XDOT = 4583
175378
YDOT = -554
096348 feet/sec YDOT = -168
888567 meter/sec
ZDOT = -19053
777477 ZDOT = -5807
591375
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
63727875
00016717 00000-0 10270-3 0 9006
2 25544 51
6447 119
2057 0012947 348
8779 11
2097 15
75445760 4809
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
63727875 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 119
2057 deg
Eccentricity:
0012947
Arg of perigee: 348
8779 deg
Mean anomaly: 11
2097 deg
Mean motion: 15
75445760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 480
Checksum: 329
Coasting Arc #2 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2010/050/14:27:57
868
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208268
44 A = 6716254
82 meter
Y = -535523
63 meter E =
0010857
Z = 5203905
77 I = 51
93349
XDOT = 2239
369707 Wp = 8
37707
YDOT = -7295
833899 meter/sec RA = 113
36921 deg
ZDOT = 1070
356812 TA = 71
52089
MA = 71
40293
Ha = 190
928 n
mi
Hp = 180
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13806654
98 X = -4227246
74
Y = -1756967
29 feet Y = -582688
84 meter
Z = 17073181
66 Z = 5183416
13
XDOT = 7347
013473 XDOT = 2315
587033
YDOT = -23936
462923 feet/sec YDOT = -7270
365732 meter/sec
ZDOT = 3511
669330 ZDOT = 1081
421048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14012103
39 X = -4270889
11
Y = -379145
84 feet Y = -115563
65 meter
Z = 16991803
76 Z = 5179101
79
XDOT = 4906
873696 XDOT = 1495
615103
YDOT = -23519
508357 feet/sec YDOT = -7168
746147 meter/sec
ZDOT = 3555
335810 ZDOT = 1083
666355
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
65217531
00016717 00000-0 10270-3 0 9014
2 25544 51
6441 113
9825 0012930 353
1871 6
9115 15
75480702 4965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
65217531 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 113
9825 deg
Eccentricity:
0012930
Arg of perigee: 353
1871 deg
Mean anomaly: 6
9115 deg
Mean motion: 15
75480702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 283
Coasting Arc #3 (Orbit 500)
---------------------------------------
Vector Time (GMT): 2010/050/23:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010367
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2247470
75 A = 6727894
12 meter
Y = 6319759
73 meter E =
0022603
Z = -285324
50 I = 51
97918
XDOT = -4565
084403 Wp = 16
46366
YDOT = -1355
689299 meter/sec RA = 111
48268 deg
ZDOT = 6068
036240 TA = 340
44384
MA = 340
53040
Ha = 190
917 n
mi
Hp = 180
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7373591
70 X = -2316586
35
Y = 20734119
85 feet Y = 6294240
72 meter
Z = -936103
99 Z = -296410
76
XDOT = -14977
311032 XDOT = -4579
062708
YDOT = -4447
799538 feet/sec YDOT = -1406
816678 meter/sec
ZDOT = 19908
255381 ZDOT = 6045
825373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19391441
88 X = 5910511
49
Y = -10400079
45 feet Y = -3169944
22 meter
Z = -979898
11 Z = -298672
94
XDOT = 7428
612518 XDOT = 2264
241096
YDOT = 12024
018246 feet/sec YDOT = 3664
920761 meter/sec
ZDOT = 19820
012106 ZDOT = 6041
139690
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
96932451
00016717 00000-0 10270-3 0 9024
2 25544 51
6461 112
3513 0013231 353
2450 6
8534 15
75495071 5019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
96932451 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 112
3513 deg
Eccentricity:
0013231
Arg of perigee: 353
2450 deg
Mean anomaly: 6
8534 deg
Mean motion: 15
75495071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 501
Checksum: 267
Coasting Arc #4 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2010/051/00:36:24
387
Vector Time (MET): N/A
Weight (LBS) : 1009454
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 803232
42 A = 6722183
65 meter
Y = 5639596
26 meter E =
0013087
Z = -3560638
45 I = 51
96130
XDOT = -5148
750314 Wp = 17
62109
YDOT = 3559
957684 meter/sec RA = 111
17072 deg
ZDOT = 4493
480768 TA = 300
08166
MA = 300
21136
Ha = 190
857 n
mi
Hp = 179
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2635276
96 X = 757406
53
Y = 18502612
40 feet Y = 5648322
10 meter
Z = -11681884
67 Z = -3556847
93
XDOT = -16892
225440 XDOT = -5210
004044
YDOT = 11679
651195 feet/sec YDOT = 3502
039004 meter/sec
ZDOT = 14742
390970 ZDOT = 4468
319438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4368301
44 X = 1331458
28
Y = -18181458
61 feet Y = -5541708
58 meter
Z = -11666631
26 Z = -3555989
21
XDOT = 18778
014988 XDOT = 5723
538968
YDOT = -4849
519268 feet/sec YDOT = -1478
133473 meter/sec
ZDOT = 14642
608009 ZDOT = 4463
066921
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
03275286
00016717 00000-0 10270-3 0 9030
2 25544 51
6460 112
0255 0013243 354
0359 6
0645 15
75572105 5028
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
03275286 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 112
0255 deg
Eccentricity:
0013243
Arg of perigee: 354
0359 deg
Mean anomaly: 6
0645 deg
Mean motion: 15
75572105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 262
Coasting Arc #5 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2010/051/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797416
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990907
49 A = 6716611
15 meter
Y = 3267031
50 meter E =
0015460
Z = -5056571
89 I = 51
94113
XDOT = -3935
673375 Wp = 49
80806
YDOT = 6365
791837 meter/sec RA = 110
88291 deg
ZDOT = 1798
340695 TA = 237
37836
MA = 237
52766
Ha = 190
845 n
mi
Hp = 179
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9812688
60 X = 2978716
36
Y = 10718607
29 feet Y = 3300409
23 meter
Z = -16589802
80 Z = -5042071
95
XDOT = -12912
314223 XDOT = -4015
300216
YDOT = 20885
143822 feet/sec YDOT = 6321
335658 meter/sec
ZDOT = 5900
067897 ZDOT = 1779
027698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9746405
54 X = -2970704
41
Y = -10867193
20 feet Y = -3312320
49 meter
Z = -16532109
60 Z = -5038987
01
XDOT = 12469
377515 XDOT = 3800
666267
YDOT = -19975
930431 feet/sec YDOT = -6088
663595 meter/sec
ZDOT = 5823
607166 ZDOT = 1775
035464
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
09617843
00016717 00000-0 10270-3 0 9046
2 25544 51
6439 111
6975 0013166 354
4065 5
6950 15
75585747 5031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
09617843 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 111
6975 deg
Eccentricity:
0013166
Arg of perigee: 354
4065 deg
Mean anomaly: 5
6950 deg
Mean motion: 15
75585747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 311
Coasting Arc #6 (Orbit 515)
---------------------------------------
Vector Time (GMT): 2010/051/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335587
72 A = 6722391
71 meter
Y = -492934
18 meter E =
0013117
Z = -5124083
85 I = 51
94976
XDOT = -981
980969 Wp = 48
55639
YDOT = 7470
522299 meter/sec RA = 106
71534 deg
ZDOT = -1543
584401 TA = 206
64471
MA = 206
71218
Ha = 191
211 n
mi
Hp = 185
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14224369
16 X = 4365669
22
Y = -1617238
11 feet Y = -444283
00 meter
Z = -16811298
72 Z = -5102948
67
XDOT = -3221
722338 XDOT = -1057
946306
YDOT = 24509
587594 feet/sec YDOT = 7459
116419 meter/sec
ZDOT = -5064
253284 ZDOT = -1548
539538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7463414
81 X = -2274848
84
Y = -12331254
35 feet Y = -3758566
32 meter
Z = -16727387
94 Z = -5098507
84
XDOT = 22696
444800 XDOT = 6917
876375
YDOT = -6814
251838 feet/sec YDOT = -2076
983960 meter/sec
ZDOT = -5083
673420 ZDOT = -1549
503658
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
92074097
00016717 00000-0 10270-3 0 9057
2 25544 51
6453 107
4553 0006947 328
0139 32
0602 15
73476627 5166
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
92074097 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 107
4553 deg
Eccentricity:
0006947
Arg of perigee: 328
0139 deg
Mean anomaly: 32
0602 deg
Mean motion: 15
73476627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 516
Checksum: 297
Coasting Arc #7 (Orbit 531)
---------------------------------------
Vector Time (GMT): 2010/052/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 153218
31 A = 6732688
68 meter
Y = -6561048
38 meter E =
0009090
Z = 1493234
14 I = 51
99198
XDOT = 4890
350283 Wp = 93
84688
YDOT = -1216
581607 meter/sec RA = 101
58035 deg
ZDOT = -5817
684209 TA = 69
79900
MA = 69
70127
Ha = 191
287 n
mi
Hp = 185
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 502684
73 X = 219319
94
Y = -21525749
29 feet Y = -6558965
40 meter
Z = 4899062
14 Z = 1494139
09
XDOT = 16044
456310 XDOT = 4931
851810
YDOT = -3991
409472 feet/sec YDOT = -1161
662817 meter/sec
ZDOT = -19086
890449 ZDOT = -5793
826325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19597701
95 X = -5973379
55
Y = 8916699
63 feet Y = 2717810
05 meter
Z = 4902441
28 Z = 1494264
10
XDOT = -9958
938460 XDOT = -3035
484443
YDOT = -11393
085465 feet/sec YDOT = -3472
612450 meter/sec
ZDOT = -18992
183916 ZDOT = -5788
817658
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
93691219
00016717 00000-0 10270-3 0 9061
2 25544 51
6453 102
2412 0006902 331
5061 28
5723 15
73479194 5321
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
93691219 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 102
2412 deg
Eccentricity:
0006902
Arg of perigee: 331
5061 deg
Mean anomaly: 28
5723 deg
Mean motion: 15
73479194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 532
Checksum: 286
Coasting Arc #8 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2010/053/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148687
04 A = 6722543
20 meter
Y = 1612280
98 meter E =
0003575
Z = 5035708
14 I = 51
96380
XDOT = -625
002134 Wp = 27
86207
YDOT = -7445
191661 meter/sec RA = 96
50140 deg
ZDOT = 1871
375104 TA = 44
18444
MA = 44
15589
Ha = 191
480 n
mi
Hp = 185
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13611177
94 X = -4190869
72
Y = 5289635
77 feet Y = 1565652
03 meter
Z = 16521352
16 Z = 5015451
65
XDOT = -2050
531936 XDOT = -550
792900
YDOT = -24426
481828 feet/sec YDOT = -7451
765887 meter/sec
ZDOT = 6139
682099 ZDOT = 1868
519111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10887253
07 X = 3318434
74
Y = 9867234
11 feet Y = 3007532
96 meter
Z = 16440951
93 Z = 5011202
15
XDOT = -20162
099531 XDOT = -6145
407937
YDOT = 12049
657350 feet/sec YDOT = 3672
735560 meter/sec
ZDOT = 6128
106422 ZDOT = 1867
846837
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
95305639
00016717 00000-0 10270-3 0 9073
2 25544 51
6458 97
0268 0006992 335
5572 24
5258 15
73543911 5481
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
95305639 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 97
0268 deg
Eccentricity:
0006992
Arg of perigee: 335
5572 deg
Mean anomaly: 24
5258 deg
Mean motion: 15
73543911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 328
Coasting Arc #9 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2010/054/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1230655
58 A = 6731997
87 meter
Y = 6370025
68 meter E =
0012702
Z = -1768440
57 I = 51
99886
XDOT = -4531
565888 Wp = 9
50245
YDOT = 2459
410320 meter/sec RA = 91
36197 deg
ZDOT = 5723
444551 TA = 331
00181
MA = 331
07231
Ha = 191
474 n
mi
Hp = 184
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4037583
92 X = 1167923
96
Y = 20899034
39 feet Y = 6383436
87 meter
Z = -5801970
39 Z = -1762614
48
XDOT = -14867
342152 XDOT = -4586
533589
YDOT = 8068
931495 feet/sec YDOT = 2408
428271 meter/sec
ZDOT = 18777
705219 ZDOT = 5701
297128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16611719
01 X = 5063251
96
Y = -13318885
98 feet Y = -4059596
45 meter
Z = -5778637
40 Z = -1761328
68
XDOT = 13135
044815 XDOT = 4003
561660
YDOT = 8299
266720 feet/sec YDOT = 2529
616496 meter/sec
ZDOT = 18689
811030 ZDOT = 5696
654402
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 10054
90566899
00016717 00000-0 10270-3 0 9087
2 25544 51
6464 92
1384 0007074 339
0616 21
0256 15
73588083 5639
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
90566899 = yrday
fracday
Element set: 908
Inclination: 51
6464 deg
RA of node: 92
1384 deg
Eccentricity:
0007074
Arg of perigee: 339
0616 deg
Mean anomaly: 21
0256 deg
Mean motion: 15
73588083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 320
Coasting Arc #10 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2010/055/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3716099
97 A = 6722645
33 meter
Y = -2629763
95 meter E =
0014397
Z = -4958523
95 I = 51
96726
XDOT = 2137
324479 Wp = 44
34299
YDOT = 7069
923414 meter/sec RA = 86
28726 deg
ZDOT = -2141
419133 TA = 204
91857
MA = 204
98814
Ha = 191
526 n
mi
Hp = 184
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12191929
05 X = 3769317
31
Y = -8627834
48 feet Y = -2587910
75 meter
Z = -16268123
21 Z = -4940342
32
XDOT = 7012
219418 XDOT = 2068
510866
YDOT = 23195
286791 feet/sec YDOT = 7093
439490 meter/sec
ZDOT = -7025
653323 ZDOT = -2131
203395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13466897
40 X = -4104710
33
Y = -6638332
22 feet Y = -2023363
66 meter
Z = -16195978
33 Z = -4936534
20
XDOT = 16479
396378 XDOT = 5022
920016
YDOT = -16338
620813 feet/sec YDOT = -4980
011624 meter/sec
ZDOT = -6984
865342 ZDOT = -2128
986956
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 10055
92176341
00016717 00000-0 10270-3 0 9090
2 25544 51
6464 86
9241 0007182 342
8142 17
2768 15
73636324 5792
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
92176341 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 86
9241 deg
Eccentricity:
0007182
Arg of perigee: 342
8142 deg
Mean anomaly: 17
2768 deg
Mean motion: 15
73636324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 316
Coasting Arc #11 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2010/056/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2476658
69 A = 6731566
89 meter
Y = -5942182
11 meter E =
0011591
Z = 1960828
83 I = 51
99392
XDOT = 3909
685051 Wp = 82
43955
YDOT = -3497
984486 meter/sec RA = 81
14380 deg
ZDOT = -5632
567277 TA = 75
85800
MA = 75
72923
Ha = 191
623 n
mi
Hp = 184
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8125520
63 X = -2419553
17
Y = -19495348
15 feet Y = -5969558
25 meter
Z = 6433165
46 Z = 1948936
39
XDOT = 12827
050693 XDOT = 3975
870783
YDOT = -11476
327055 feet/sec YDOT = -3453
894114 meter/sec
ZDOT = -18479
551435 ZDOT = -5613
413735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12898815
62 X = -3931559
00
Y = 16742791
52 feet Y = 5103202
86 meter
Z = 6385749
01 Z = 1946376
30
XDOT = -15154
101994 XDOT = -4618
970288
YDOT = -4618
280338 feet/sec YDOT = -1407
651847 meter/sec
ZDOT = -18403
565210 ZDOT = -5609
406676
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 10056
93783375
00016717 00000-0 10270-3 0 9105
2 25544 51
6462 81
7094 0007049 347
3292 12
7693 15
73636345 5955
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
93783375 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 81
7094 deg
Eccentricity:
0007049
Arg of perigee: 347
3292 deg
Mean anomaly: 12
7693 deg
Mean motion: 15
73636345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 324
Coasting Arc #12 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2010/057/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079750
34 A = 6722781
61 meter
Y = 3442532
39 meter E =
0005790
Z = 4879483
33 I = 51
95881
XDOT = -3493
824233 Wp = 52
23805
YDOT = -6452
456694 meter/sec RA = 76
06994 deg
ZDOT = 2348
698852 TA = 14
99754
MA = 14
98038
Ha = 191
810 n
mi
Hp = 184
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10104167
79 X = -3141719
40
Y = 11294397
59 feet Y = 3407746
55 meter
Z = 16008803
58 Z = 4864371
66
XDOT = -11462
677930 XDOT = -3432
821262
YDOT = -21169
477343 feet/sec YDOT = -6491
185508 meter/sec
ZDOT = 7705
704895 ZDOT = 2331
874857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14915990
40 X = 4546393
87
Y = 3014333
67 feet Y = 918768
90 meter
Z = 15948869
51 Z = 4861215
43
XDOT = -12124
013646 XDOT = -3695
399359
YDOT = 19605
260650 feet/sec YDOT = 5975
683446 meter/sec
ZDOT = 7638
680415 ZDOT = 2328
269790
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 10057
95387572
00016717 00000-0 10270-3 0 9118
2 25544 51
6460 76
4938 0007183 351
0363 9
0671 15
73683872 6112
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
95387572 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 76
4938 deg
Eccentricity:
0007183
Arg of perigee: 351
0363 deg
Mean anomaly: 9
0671 deg
Mean motion: 15
73683872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 314
Coasting Arc #13 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2010/058/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587974
30 A = 6731005
83 meter
Y = 5272220
62 meter E =
0012515
Z = -2132738
89 I = 51
97774
XDOT = -3094
192759 Wp = 15
37706
YDOT = 4345
712657 meter/sec RA = 70
92165 deg
ZDOT = 5556
484504 TA = 320
88178
MA = 320
97219
Ha = 191
793 n
mi
Hp = 183
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11771569
23 X = 3539112
90
Y = 17297311
75 feet Y = 5312070
11 meter
Z = -6997174
84 Z = -2115428
11
XDOT = -10151
551047 XDOT = -3169
548966
YDOT = 14257
587458 feet/sec YDOT = 4310
690668 meter/sec
ZDOT = 18229
936036 ZDOT = 5541
269953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8529595
95 X = 2599820
84
Y = -19130411
13 feet Y = -5830949
31 meter
Z = -6928250
50 Z = -2111730
75
XDOT = 16125
119562 XDOT = 4914
936443
YDOT = 632
338140 feet/sec YDOT = 192
736665 meter/sec
ZDOT = 18169
618226 ZDOT = 5538
099635
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 10058
90639038
00016717 00000-0 10270-3 0 9122
2 25544 51
6453 71
6040 0007291 353
1561 6
9502 15
73728527 6260
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
90639038 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 71
6040 deg
Eccentricity:
0007291
Arg of perigee: 353
1561 deg
Mean anomaly: 6
9502 deg
Mean motion: 15
73728527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 296
Coasting Arc #14 (Orbit 641)
---------------------------------------
Vector Time (GMT): 2010/059/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2313422
90 A = 6722754
87 meter
Y = -4081422
37 meter E =
0015346
Z = -4828590
57 I = 51
93852
XDOT = 4648
892696 Wp = 44
88503
YDOT = 5593
361138 meter/sec RA = 65
84807 deg
ZDOT = -2494
688689 TA = 200
74851
MA = 200
81088
Ha = 191
740 n
mi
Hp = 183
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7589970
14 X = 2382346
03
Y = -13390493
34 feet Y = -4055167
43 meter
Z = -15841832
59 Z = -4817184
40
XDOT = 15252
272624 XDOT = 4598
119687
YDOT = 18350
922369 feet/sec YDOT = 5645
063673 meter/sec
ZDOT = -8184
674176 ZDOT = -2472
228801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15420183
77 X = -4700072
01
Y = 748893
74 feet Y = 228262
81 meter
Z = -15796636
00 Z = -4814814
65
XDOT = 7260
888648 XDOT = 2213
118860
YDOT = -21655
202956 feet/sec YDOT = -6600
505861 meter/sec
ZDOT = -8095
287587 ZDOT = -2467
443656
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 10059
92238064
00016717 00000-0 10270-3 0 9130
2 25544 51
6443 66
3879 0007243 356
6739 3
4375 15
73779463 6425
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
92238064 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 66
3879 deg
Eccentricity:
0007243
Arg of perigee: 356
6739 deg
Mean anomaly: 3
4375 deg
Mean motion: 15
73779463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 642
Checksum: 329
Coasting Arc #15 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2010/060/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4503740
40 A = 6730528
68 meter
Y = -4480760
63 meter E =
0013680
Z = 2216133
02 I = 51
95249
XDOT = 2175
371113 Wp = 78
20048
YDOT = -4923
706416 meter/sec RA = 60
69650 deg
ZDOT = -5503
101018 TA = 77
07574
MA = 76
92299
Ha = 191
789 n
mi
Hp = 183
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14776051
19 X = -4464066
40
Y = -14700658
24 feet Y = -4530902
06 meter
Z = 7270777
62 Z = 2194351
09
XDOT = 7137
044333 XDOT = 2256
999813
YDOT = -16153
892440 feet/sec YDOT = -4898
924321 meter/sec
ZDOT = -18054
793365 ZDOT = -5492
334431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4039976
21 X = -1231384
75
Y = 20478579
71 feet Y = 6241871
10 meter
Z = 7184122
35 Z = 2189720
49
XDOT = -15969
628758 XDOT = -4867
542845
YDOT = 3204
702978 feet/sec YDOT = 976
793468 meter/sec
ZDOT = -18012
158937 ZDOT = -5490
106044
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 10060
93834376
00016717 00000-0 10270-3 0 9142
2 25544 51
6450 61
1720 0007308 1
0501 359
0677 15
73847670 6589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
93834376 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 61
1720 deg
Eccentricity:
0007308
Arg of perigee: 1
0501 deg
Mean anomaly: 359
0677 deg
Mean motion: 15
73847670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 295
Coasting Arc #16 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2010/061/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1477760
73 A = 6722735
27 meter
Y = 4479358
96 meter E =
0007857
Z = 4782864
23 I = 51
90956
XDOT = -5608
500840 Wp = 62
61423
YDOT = -4609
672105 meter/sec RA = 55
62110 deg
ZDOT = 2584
620384 TA = 2
16389
MA = 2
16049
Ha = 191
975 n
mi
Hp = 183
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4848296
34 X = -1550973
91
Y = 14696059
59 feet Y = 4462424
90 meter
Z = 15691811
78 Z = 4775507
06
XDOT = -18400
593306 XDOT = -5569
093305
YDOT = -15123
596146 feet/sec YDOT = -4672
169089 meter/sec
ZDOT = 8479
725670 ZDOT = 2557
470796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14902817
92 X = 4542378
90
Y = -4277710
07 feet Y = -1303846
03 meter
Z = 15662704
63 Z = 4773992
37
XDOT = -2285
186265 XDOT = -696
524773
YDOT = 22687
852085 feet/sec YDOT = 6915
257315 meter/sec
ZDOT = 8371
752479 ZDOT = 2551
710156
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 10061
95428129
00016717 00000-0 10270-3 0 9151
2 25544 51
6442 55
9551 0007244 5
3016 354
8223 15
73826674 6749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
95428129 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 55
9551 deg
Eccentricity:
0007244
Arg of perigee: 5
3016 deg
Mean anomaly: 354
8223 deg
Mean motion: 15
73826674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 304
Coasting Arc #17 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2010/062/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5242641
09 A = 6730245
05 meter
Y = 3536534
68 meter E =
0012450
Z = -2286998
07 I = 51
91680
XDOT = -1191
631823 Wp = 23
78487
YDOT = 5289
871850 meter/sec RA = 50
46518 deg
ZDOT = 5469
802089 TA = 310
61647
MA = 310
72470
Ha = 191
888 n
mi
Hp = 183
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17200266
03 X = 5213815
02
Y = 11602804
07 feet Y = 3594999
64 meter
Z = -7503274
51 Z = -2261599
84
XDOT = -3909
553226 XDOT = -1277
266649
YDOT = 17355
222604 feet/sec YDOT = 5276
067965 meter/sec
ZDOT = 17945
544912 ZDOT = 5463
804739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -597611
35 X = -182151
94
Y = -20775520
02 feet Y = -6332378
50 meter
Z = -7402294
99 Z = -2256219
51
XDOT = 14936
240986 XDOT = 4552
566253
YDOT = -6789
839924 feet/sec YDOT = -2069
543209 meter/sec
ZDOT = 17921
853436 ZDOT = 5462
580927
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 10062
90669444
00016717 00000-0 10270-3 0 9165
2 25544 51
6436 51
0645 0007109 7
7873 352
3399 15
73898849 6896
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
90669444 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 51
0645 deg
Eccentricity:
0007109
Arg of perigee: 7
7873 deg
Mean anomaly: 352
3399 deg
Mean motion: 15
73898849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 345
Coasting Arc #18 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2010/063/21:39:12
435
Vector Time (MET): N/A
Weight (LBS) : 796372
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628042
55 A = 6722451
09 meter
Y = -4702877
93 meter E =
0016373
Z = -4777345
99 I = 51
87035
XDOT = 6328
825863 Wp = 49
63984
YDOT = 3499
678824 meter/sec RA = 45
38841 deg
ZDOT = -2608
588491 TA = 194
78320
MA = 194
83114
Ha = 191
841 n
mi
Hp = 182
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2060507
05 X = 703791
62
Y = -15429389
52 feet Y = -4695431
54 meter
Z = -15673707
31 Z = -4774110
69
XDOT = 20763
864379 XDOT = 6301
893423
YDOT = 11481
885904 feet/sec YDOT = 3570
300764 meter/sec
ZDOT = -8558
361191 ZDOT = -2577
908905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13674912
22 X = -4168113
24
Y = 7463764
69 feet Y = 2274955
48 meter
Z = -15660965
60 Z = -4773462
32
XDOT = -2634
517663 XDOT = -803
000984
YDOT = -22559
966315 feet/sec YDOT = -6876
277733 meter/sec
ZDOT = -8436
410176 ZDOT = -2571
417822
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 10063
92257633
00016717 00000-0 10270-3 0 9172
2 25544 51
6430 45
8483 0007072 12
6043 347
5295 15
73947103 7052
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
92257633 = yrday
fracday
Element set: 917
Inclination: 51
6430 deg
RA of node: 45
8483 deg
Eccentricity:
0007072
Arg of perigee: 12
6043 deg
Mean anomaly: 347
5295 deg
Mean motion: 15
73947103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 298
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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