Date:
November 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
329/05:06:30
216 -1
6 2
1 2
1
N/A 0
4 0
1 190
2
000/00:04:56
433 1
3 0
1 188
9
Coasting Arc #1 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2010/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5564348
38 A = 6734659
75 meter
Y = 3615830
14 meter E =
0002027
Z = -1141622
46 I = 51
80079
XDOT = -3481
964970 Wp = 16
18753
YDOT = -3495
460197 meter/sec RA = 154
76363 deg
ZDOT = 5904
676137 TA = 331
35338
MA = 331
36451
Ha = 191
729 n
mi
Hp = 187
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18255736
17 X = -5598821
75
Y = 11862959
79 feet Y = 3553413
54 meter
Z = -3745480
50 Z = -1168738
46
XDOT = -11423
769588 XDOT = -3471
303989
YDOT = -11468
045266 feet/sec YDOT = -3534
338241 meter/sec
ZDOT = 19372
297037 ZDOT = 5887
786013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -257216
00 X = -78399
44
Y = -21751041
29 feet Y = -6629717
38 meter
Z = -3854398
13 Z = -1174820
55
XDOT = 14277
025699 XDOT = 4351
637433
YDOT = -3587
193235 feet/sec YDOT = -1093
376498 meter/sec
ZDOT = 19304
468077 ZDOT = 5884
001870
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 10323
50227481
00016717 00000-0 10270-3 0 9005
2 25544 51
6398 155
7875 0007486 223
4369 136
6204 15
72915274 7907
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50227481 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 155
7875 deg
Eccentricity:
0007486
Arg of perigee: 223
4369 deg
Mean anomaly: 136
6204 deg
Mean motion: 15
72915274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 316
Coasting Arc #2 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2010/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619803
45 A = 6724012
04 meter
Y = 2517629
88 meter E =
0008107
Z = -5082671
15 I = 51
79136
XDOT = -5720
688973 Wp = 105
30753
YDOT = 4867
370198 meter/sec RA = 149
67195 deg
ZDOT = -1667
498802 TA = 148
70596
MA = 148
65768
Ha = 191
564 n
mi
Hp = 187
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11875995
58 X = 3616073
24
Y = 8259940
55 feet Y = 2558088
16 meter
Z = -16675430
27 Z = -5065094
52
XDOT = -18768
664611 XDOT = -5766
590984
YDOT = 15969
062330 feet/sec YDOT = 4803
141466 meter/sec
ZDOT = -5470
796593 ZDOT = -1695
401933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13287310
41 X = -4049972
21
Y = 5921365
71 feet Y = 1804832
27 meter
Z = -16604838
87 Z = -5061154
89
XDOT = -3442
995366 XDOT = -1049
424987
YDOT = -23341
989367 feet/sec YDOT = -7114
638359 meter/sec
ZDOT = -5582
898012 ZDOT = -1701
667314
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 10324
51879091
00016717 00000-0 10270-3 0 9018
2 25544 51
6389 150
5750 0007398 226
5671 133
4876 15
72962585 8069
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
51879091 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 150
5750 deg
Eccentricity:
0007398
Arg of perigee: 226
5671 deg
Mean anomaly: 133
4876 deg
Mean motion: 15
72962585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 331
Coasting Arc #3 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2010/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4358157
52 A = 6733513
56 meter
Y = -4808390
02 meter E =
0012436
Z = 1765421
38 I = 51
85047
XDOT = 4698
595804 Wp = 146
45406
YDOT = 2159
033874 meter/sec RA = 144
52660 deg
ZDOT = -5709
756155 TA = 14
04634
MA = 14
01178
Ha = 191
097 n
mi
Hp = 187
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14298417
06 X = 4403025
58
Y = -15775557
80 feet Y = -4759403
76 meter
Z = 5792064
90 Z = 1786702
48
XDOT = 15415
340565 XDOT = 4701
841612
YDOT = 7083
444467 feet/sec YDOT = 2211
595041 meter/sec
ZDOT = -18732
795785 ZDOT = -5686
921661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6388508
39 X = 1947217
36
Y = 20285510
30 feet Y = 6183023
54 meter
Z = 5877584
76 Z = 1791487
84
XDOT = -12486
621461 XDOT = -3805
922221
YDOT = 9341
815982 feet/sec YDOT = 2847
385511 meter/sec
ZDOT = -18641
076352 ZDOT = -5681
800072
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 10325
53528005
00016717 00000-0 10270-3 0 9028
2 25544 51
6394 145
3624 0007425 232
9282 127
1202 15
73041689 8222
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
53528005 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 145
3624 deg
Eccentricity:
0007425
Arg of perigee: 232
9282 deg
Mean anomaly: 127
1202 deg
Mean motion: 15
73041689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 284
Coasting Arc #4 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2010/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4479615
70 A = 6724782
20 meter
Y = -1204530
06 meter E =
0007790
Z = 4871729
35 I = 51
84402
XDOT = 4185
239845 Wp = 181
32591
YDOT = -6014
954990 meter/sec RA = 139
44741 deg
ZDOT = 2353
638081 TA = 245
74705
MA = 245
82846
Ha = 191
095 n
mi
Hp = 187
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14696901
90 X = -4489480
04
Y = -3951870
29 feet Y = -1254679
49 meter
Z = 15983363
99 Z = 4849942
74
XDOT = 13731
101853 XDOT = 4240
755301
YDOT = -19734
104297 feet/sec YDOT = -5967
842967 meter/sec
ZDOT = 7721
909714 ZDOT = 2374
104697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10706435
77 X = 3263321
62
Y = -10944342
91 feet Y = -3335835
72 meter
Z = 15895839
71 Z = 4845051
94
XDOT = 9670
866291 XDOT = 2947
680046
YDOT = 20831
814820 feet/sec YDOT = 6349
537157 meter/sec
ZDOT = 7804
184970 ZDOT = 2378
715579
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 10326
55174834
00016717 00000-0 10270-3 0 9039
2 25544 51
6386 140
1489 0007352 235
2168 124
8303 15
73017411 8382
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55174834 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 140
1489 deg
Eccentricity:
0007352
Arg of perigee: 235
2168 deg
Mean anomaly: 124
8303 deg
Mean motion: 15
73017411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 295
Coasting Arc #5 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2010/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2916642
02 A = 6732422
48 meter
Y = 5602945
22 meter E =
0002138
Z = -2327337
33 I = 51
89355
XDOT = -5415
258610 Wp = 272
32760
YDOT = -558
000052 meter/sec RA = 134
29551 deg
ZDOT = 5438
913155 TA = 61
60863
MA = 61
58708
Ha = 190
830 n
mi
Hp = 187
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9569035
51 X = -2967772
41
Y = 18382366
20 feet Y = 5570043
96 meter
Z = -7635621
17 Z = -2341630
22
XDOT = -17766
596488 XDOT = -5435
038259
YDOT = -1830
708832 feet/sec YDOT = -618
667952 meter/sec
ZDOT = 17844
203266 ZDOT = 5412
557184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11631568
61 X = -3545302
11
Y = -17126099
72 feet Y = -5220035
20 meter
Z = -7693104
59 Z = -2344858
28
XDOT = 8868
928547 XDOT = 2703
249421
YDOT = -13997
759252 feet/sec YDOT = -4266
517020 meter/sec
ZDOT = 17738
302128 ZDOT = 5406
634489
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 10327
50466185
00016717 00000-0 10270-3 0 9049
2 25544 51
6392 135
2614 0007348 237
5845 122
4607 15
73073915 8535
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
50466185 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 135
2614 deg
Eccentricity:
0007348
Arg of perigee: 237
5845 deg
Mean anomaly: 122
4607 deg
Mean motion: 15
73073915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 308
Coasting Arc #6 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2010/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4879362
56 A = 6725476
58 meter
Y = -240056
78 meter E =
0003541
Z = -4625462
39 I = 51
89167
XDOT = -2462
642657 Wp = 87
37477
YDOT = 6669
907350 meter/sec RA = 129
22803 deg
ZDOT = -2945
750325 TA = 153
52686
MA = 153
50877
Ha = 190
628 n
mi
Hp = 187
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16008407
33 X = 4904154
27
Y = -787587
85 feet Y = -185353
66 meter
Z = -15175401
55 Z = -4601697
89
XDOT = -8079
536276 XDOT = -2522
733633
YDOT = 21882
898130 feet/sec YDOT = 6642
032951 meter/sec
ZDOT = -9664
535186 ZDOT = -2957
859223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6719760
25 X = -2048182
93
Y = 14650045
84 feet Y = 4465333
97 meter
Z = -15079893
61 Z = -4596351
57
XDOT = -14654
696630 XDOT = -4466
751533
YDOT = -16714
151455 feet/sec YDOT = -5094
473363 meter/sec
ZDOT = -9713
266591 ZDOT = -2960
603657
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 10328
52107903
00016717 00000-0 10270-3 0 9053
2 25544 51
6399 130
0493 0007168 241
8124 118
2315 15
73130095 8697
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52107903 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 130
0493 deg
Eccentricity:
0007168
Arg of perigee: 241
8124 deg
Mean anomaly: 118
2315 deg
Mean motion: 15
73130095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 294
Coasting Arc #7 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2010/329/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1728450
68 A = 6732735
16 meter
Y = 5953107
34 meter E =
0003978
Z = -2621787
44 I = 51
92943
XDOT = -5570
204351 Wp = 293
66528
YDOT = 703
483671 meter/sec RA = 125
53665 deg
ZDOT = 5264
893536 TA = 36
67806
MA = 36
65084
Ha = 190
176 n
mi
Hp = 188
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5670769
96 X = -1782154
65
Y = 19531192
05 feet Y = 5933478
77 meter
Z = -8601664
83 Z = -2630314
16
XDOT = -18274
948658 XDOT = -5603
233049
YDOT = 2308
017293 feet/sec YDOT = 641
009052 meter/sec
ZDOT = 17273
272755 ZDOT = 5237
753004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16758385
32 X = 5107955
85
Y = -11497380
59 feet Y = -3504401
60 meter
Z = -8635999
87 Z = -2632252
76
XDOT = 14811
317966 XDOT = 4514
489716
YDOT = 8684
712427 feet/sec YDOT = 2647
100348 meter/sec
ZDOT = 17164
181982 ZDOT = 5231
642668
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 10329
21985095
00016717 00000-0 10270-3 0 9067
2 25544 51
6434 126
4697 0007805 259
9050 100
1232 15
72746694 8806
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
21985095 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 126
4697 deg
Eccentricity:
0007805
Arg of perigee: 259
9050 deg
Mean anomaly: 100
1232 deg
Mean motion: 15
72746694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 317
Coasting Arc #8 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2010/330/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872475
46 A = 6727360
72 meter
Y = -1494742
35 meter E =
0002604
Z = -4393169
98 I = 51
92900
XDOT = -953
062400 Wp = 15
19431
YDOT = 6845
847730 meter/sec RA = 120
47763 deg
ZDOT = -3384
283348 TA = 220
83747
MA = 220
85699
Ha = 189
862 n
mi
Hp = 189
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15985811
87 X = 4910169
22
Y = -4904010
34 feet Y = -1440044
24 meter
Z = -14413287
34 Z = -4369407
87
XDOT = -3126
845144 XDOT = -1013
102734
YDOT = 22460
130349 feet/sec YDOT = 6834
854622 meter/sec
ZDOT = -11103
291825 ZDOT = -3389
058574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15629609
16 X = -4763904
87
Y = -6168919
69 feet Y = -1880286
72 meter
Z = -14317754
63 Z = -4364051
61
XDOT = 15929
693782 XDOT = 4855
370665
YDOT = -14529
251525 feet/sec YDOT = -4428
515865 meter/sec
ZDOT = -11122
565788 ZDOT = -3390
158052
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 10330
23648938
00016717 00000-0 10270-3 0 9074
2 25544 51
6441 121
2591 0007849 265
0067 95
0199 15
72787453 8963
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
23648938 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 121
2591 deg
Eccentricity:
0007849
Arg of perigee: 265
0067 deg
Mean anomaly: 95
0199 deg
Mean motion: 15
72787453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 331
Coasting Arc #9 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2010/331/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -49828
04 A = 6730931
30 meter
Y = -5879553
83 meter E =
0005035
Z = 3271322
16 I = 51
95553
XDOT = 5406
295011 Wp = 96
85232
YDOT = -2701
807767 meter/sec RA = 115
32388 deg
ZDOT = -4767
979477 TA = 45
02452
MA = 44
98371
Ha = 189
186 n
mi
Hp = 188
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -163477
81 X = 30
33
Y = -19289874
78 feet Y = -5879832
50 meter
Z = 10732684
24 Z = 3271200
78
XDOT = 17737
188357 XDOT = 5459
267466
YDOT = -8864
198712 feet/sec YDOT = -2641
054802 meter/sec
ZDOT = -15642
977286 ZDOT = -4741
587026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11568855
08 X = -3526187
03
Y = 15436855
76 feet Y = 4705153
64 meter
Z = 10732268
23 Z = 3271195
36
XDOT = -18414
692652 XDOT = -5612
798320
YDOT = -2985
893201 feet/sec YDOT = -910
100248 meter/sec
ZDOT = -15536
845863 ZDOT = -4735
630619
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 10331
25310405
00016717 00000-0 10270-3 0 9083
2 25544 51
6438 116
0481 0007770 269
1091 90
9181 15
72805656 9124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10331
25310405 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 116
0481 deg
Eccentricity:
0007770
Arg of perigee: 269
1091 deg
Mean anomaly: 90
9181 deg
Mean motion: 15
72805656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 291
Coasting Arc #10 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2010/332/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4446824
08 A = 6728890
49 meter
Y = 3174140
75 meter E =
0003521
Z = 3926223
96 I = 51
96119
XDOT = -1010
485855 Wp = 113
13563
YDOT = -6455
154651 meter/sec RA = 110
26979 deg
ZDOT = 4069
954150 TA = 294
67742
MA = 294
71408
Ha = 189
550 n
mi
Hp = 188
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14589317
83 X = -4501060
45
Y = 10413847
61 feet Y = 3124110
24 meter
Z = 12881312
20 Z = 3904489
53
XDOT = -3315
242308 XDOT = -957
999273
YDOT = -21178
328908 feet/sec YDOT = -6466
161246 meter/sec
ZDOT = 13352
867946 ZDOT = 4065
172339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17983561
49 X = 5481389
54
Y = 363957
56 feet Y = 110934
26 meter
Z = 12793891
97 Z = 3899578
27
XDOT = -9854
541577 XDOT = -3003
664273
YDOT = 17725
095297 feet/sec YDOT = 5402
609047 meter/sec
ZDOT = 13333
727303 ZDOT = 4064
120082
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 10332
26969256
00016717 00000-0 10270-3 0 9090
2 25544 51
6442 110
8361 0007821 274
0976 85
9293 15
72835409 9286
Satellite: ISS
Catalog Number: 25544
Epoch time: 10332
26969256 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 110
8361 deg
Eccentricity:
0007821
Arg of perigee: 274
0976 deg
Mean anomaly: 85
9293 deg
Mean motion: 15
72835409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 330
Coasting Arc #11 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2010/333/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1664856
40 A = 6729042
04 meter
Y = 5284783
40 meter E =
0001956
Z = -3817029
39 I = 51
97155
XDOT = -4621
141824 Wp = 256
78142
YDOT = 4495
050885 meter/sec RA = 105
11425 deg
ZDOT = 4205
711363 TA = 57
14735
MA = 57
12852
Ha = 190
001 n
mi
Hp = 188
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5462127
29 X = 1624179
87
Y = 17338528
23 feet Y = 5303173
53 meter
Z = -12523062
31 Z = -3809040
04
XDOT = -15161
226456 XDOT = -4691
493681
YDOT = 14747
542275 feet/sec YDOT = 4442
980988 meter/sec
ZDOT = 13798
265628 ZDOT = 4183
090876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5576899
38 X = 1699838
93
Y = -17325103
80 feet Y = -5280691
64 meter
Z = -12491015
04 Z = -3807261
38
XDOT = 19713
389694 XDOT = 6008
641179
YDOT = -3542
232836 feet/sec YDOT = -1079
672568 meter/sec
ZDOT = 13707
256992 ZDOT = 4177
971931
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 10333
22272033
00016717 00000-0 10270-3 0 9109
2 25544 51
6440 105
9502 0008036 278
1438 81
8813 15
72889282 9431
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
22272033 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 105
9502 deg
Eccentricity:
0008036
Arg of perigee: 278
1438 deg
Mean anomaly: 81
8813 deg
Mean motion: 15
72889282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 294
Coasting Arc #12 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2010/334/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3530641
06 A = 6730273
41 meter
Y = -4597109
78 meter E =
0003502
Z = -3419311
47 I = 51
98226
XDOT = 2698
380283 Wp = 299
19671
YDOT = 5521
910301 meter/sec RA = 100
06195 deg
ZDOT = -4632
513779 TA = 280
96319
MA = 281
00259
Ha = 190
183 n
mi
Hp = 188
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11583468
05 X = 3598395
05
Y = -15082381
16 feet Y = -4557249
07 meter
Z = -11218213
50 Z = -3401994
93
XDOT = 8852
953683 XDOT = 2658
936966
YDOT = 18116
503612 feet/sec YDOT = 5551
864831 meter/sec
ZDOT = -15198
536020 ZDOT = -4619
500464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18150914
82 X = -5532398
84
Y = 5810170
38 feet Y = 1770939
93 meter
Z = -11148519
13 Z = -3398068
63
XDOT = 3337
820511 XDOT = 1017
367692
YDOT = -18668
298327 feet/sec YDOT = -5690
097330 meter/sec
ZDOT = -15146
299090 ZDOT = -4616
591963
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 10334
23925979
00016717 00000-0 10270-3 0 9116
2 25544 51
6436 100
7385 0008134 281
8026 78
2224 15
72907686 9593
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
23925979 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 100
7385 deg
Eccentricity:
0008134
Arg of perigee: 281
8026 deg
Mean anomaly: 78
2224 deg
Mean motion: 15
72907686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 323
Coasting Arc #13 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2010/335/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2971932
48 A = 6727198
56 meter
Y = -4281442
86 meter E =
0005609
Z = 4255321
12 I = 51
97740
XDOT = 3342
832847 Wp = 18
56460
YDOT = -5916
909444 meter/sec RA = 94
90780 deg
ZDOT = -3612
092142 TA = 108
03403
MA = 107
97290
Ha = 190
336 n
mi
Hp = 188
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9750434
64 X = -2944507
70
Y = -14046728
54 feet Y = -4314523
65 meter
Z = 13961027
29 Z = 4240949
60
XDOT = 10967
299368 XDOT = 3426
295622
YDOT = -19412
432558 feet/sec YDOT = -5879
061044 meter/sec
ZDOT = -11850
696004 ZDOT = -3595
649872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 422800
28 X = 128869
52
Y = 17140912
09 feet Y = 5224550
00 meter
Z = 13903316
66 Z = 4237730
92
XDOT = -18683
248121 XDOT = -5694
654027
YDOT = 10036
807416 feet/sec YDOT = 3059
218901 meter/sec
ZDOT = -11784
483564 ZDOT = -3591
910590
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 10335
25577259
00016717 00000-0 10270-3 0 9124
2 25544 51
6439 95
5260 0008164 287
2809 72
7460 15
73010314 9754
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
25577259 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 95
5260 deg
Eccentricity:
0008164
Arg of perigee: 287
2809 deg
Mean anomaly: 72
7460 deg
Mean motion: 15
73010314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 312
Coasting Arc #14 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2010/336/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2246086
78 A = 6731417
57 meter
Y = 5642132
59 meter E =
0007501
Z = 2892753
07 I = 51
99221
XDOT = -3983
618442 Wp = 48
86403
YDOT = -4194
029095 meter/sec RA = 89
85153 deg
ZDOT = 5083
445772 TA = 344
21523
MA = 344
23860
Ha = 190
644 n
mi
Hp = 188
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7369051
13 X = -2323064
02
Y = 18510933
68 feet Y = 5616584
89 meter
Z = 9490659
67 Z = 2881654
73
XDOT = -13069
614311 XDOT = -3961
118973
YDOT = -13759
937976 feet/sec YDOT = -4238
450859 meter/sec
ZDOT = 16677
971693 ZDOT = 5064
147279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16228102
15 X = 4946325
54
Y = -11595404
56 feet Y = -3534279
31 meter
Z = 9445924
78 Z = 2879117
87
XDOT = 2836
533861 XDOT = 864
575521
YDOT = 17502
788046 feet/sec YDOT = 5334
849797 meter/sec
ZDOT = 16600
455848 ZDOT = 5059
818943
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 10336
27226247
00016717 00000-0 10270-3 0 9136
2 25544 51
6431 90
3130 0008175 291
3359 68
6930 15
73002276 9915
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
27226247 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 90
3130 deg
Eccentricity:
0008175
Arg of perigee: 291
3359 deg
Mean anomaly: 68
6930 deg
Mean motion: 15
73002276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 295
Coasting Arc #15 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2010/337/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3891945
16 A = 6725763
37 meter
Y = 2987622
42 meter E =
0002345
Z = -4602365
37 I = 51
97193
XDOT = -1723
183510 Wp = 93
29557
YDOT = 6872
933980 meter/sec RA = 84
70098 deg
ZDOT = 3005
541093 TA = 206
41670
MA = 206
42866
Ha = 190
787 n
mi
Hp = 188
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12768848
93 X = 3880605
72
Y = 9801910
84 feet Y = 3031081
53 meter
Z = -15099623
92 Z = -4583485
12
XDOT = -5653
489205 XDOT = -1814
510582
YDOT = 22548
995998 feet/sec YDOT = 6853
153385 meter/sec
ZDOT = 9860
699124 ZDOT = 2996
948482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5813376
09 X = -1771917
03
Y = -15086768
78 feet Y = -4598447
12 meter
Z = -15023770
10 Z = -4579245
13
XDOT = 15583
507286 XDOT = 4749
853021
YDOT = -15785
896278 feet/sec YDOT = -4811
541186 meter/sec
ZDOT = 9825
997549 ZDOT = 2994
964053
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 10337
22519738
00016717 00000-0 10270-3 0 9143
2 25544 51
6427 85
4258 0008157 294
8268 65
2046 15
73052607 10065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
22519738 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 85
4258 deg
Eccentricity:
0008157
Arg of perigee: 294
8268 deg
Mean anomaly: 65
2046 deg
Mean motion: 15
73052607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 312
Coasting Arc #16 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2010/338/05:08:58
433
Vector Time (MET): N/A
Weight (LBS) : 829737
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 738227
33 A = 6732400
48 meter
Y = -6257450
51 meter E =
0003140
Z = -2368916
14 I = 51
99037
XDOT = 4788
719166 Wp = 269
84768
YDOT = 2620
770974 meter/sec RA = 79
64042 deg
ZDOT = -5424
274242 TA = 296
68118
MA = 296
71332
Ha = 190
848 n
mi
Hp = 187
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2422005
69 X = 819652
46
Y = -20529693
29 feet Y = -6248739
66 meter
Z = -7772034
58 Z = -2365132
71
XDOT = 15711
020886 XDOT = 4785
408009
YDOT = 8598
329967 feet/sec YDOT = 2674
303441 meter/sec
ZDOT = -17796
175336 ZDOT = -5401
017876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12582248
11 X = -3835069
22
Y = 16409145
62 feet Y = 5001507
58 meter
Z = -7756668
89 Z = -2364232
68
XDOT = -8034
201458 XDOT = -2448
824604
YDOT = -14538
163262 feet/sec YDOT = -4431
232162 meter/sec
ZDOT = -17702
717360 ZDOT = -5395
788251
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 10338
24163759
00016717 00000-0 10270-3 0 9155
2 25544 51
6425 80
2142 0008204 298
8111 61
2228 15
73068486 10220
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
24163759 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 80
2142 deg
Eccentricity:
0008204
Arg of perigee: 298
8111 deg
Mean anomaly: 61
2228 deg
Mean motion: 15
73068486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 289
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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