Date:
June 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 458)
---------------------------------------
Vector Time (GMT): 2009/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6496924
65 A = 6733253
96 meter
Y = 1593703
27 meter E =
0020919
Z = 701120
66 I = 51
60724
XDOT = -1768
315953 Wp = 112
40261
YDOT = -4518
432288 meter/sec RA = 350
98125 deg
ZDOT = -5981
652778 TA = 59
95470
MA = 59
74736
Ha = 193
964 n
mi
Hp = 181
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21315369
58 X = -6517668
77
Y = 5228685
25 feet Y = 1520934
73 meter
Z = 2300264
63 Z = 669508
36
XDOT = -5801
561525 XDOT = -1688
600719
YDOT = -14824
252914 feet/sec YDOT = -4537
759724 meter/sec
ZDOT = -19624
845072 ZDOT = -5990
050577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5543
00 X = 1689
51
Y = 21959924
27 feet Y = 6693384
92 meter
Z = 2176474
74 Z = 663389
50
XDOT = -14150
626919 XDOT = -4313
111085
YDOT = 1997
827132 feet/sec YDOT = 608
937710 meter/sec
ZDOT = -19657
915734 ZDOT = -5991
732716
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 09159
53310193
00010596 00000-0 82463-4 0 9009
2 25544 51
6395 351
3192 0008765 89
4139 270
8028 15
73555513 4590
Satellite: ISS
Catalog Number: 25544
Epoch time: 09159
53310193 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 351
3192 deg
Eccentricity:
0008765
Arg of perigee: 89
4139 deg
Mean anomaly: 270
8028 deg
Mean motion: 15
73555513 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 459
Checksum: 319
Coasting Arc #2 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2009/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2062314
83 A = 6721776
03 meter
Y = 3730129
82 meter E =
0012049
Z = 5187820
67 I = 51
53810
XDOT = -7187
888683 Wp = 101
42020
YDOT = 2610
598074 meter/sec RA = 345
85846 deg
ZDOT = 976
083819 TA = 339
25007
MA = 339
29895
Ha = 194
022 n
mi
Hp = 181
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6766124
77 X = 1995249
09
Y = 12237958
72 feet Y = 3752815
82 meter
Z = 17020409
03 Z = 5197677
25
XDOT = -23582
311951 XDOT = -7221
288254
YDOT = 8564
954312 feet/sec YDOT = 2530
031967 meter/sec
ZDOT = 3202
374734 ZDOT = 941
084392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13409560
93 X = 4087234
17
Y = -3796168
41 feet Y = -1157072
13 meter
Z = 17059167
12 Z = 5199634
14
XDOT = 2857
761191 XDOT = 871
045611
YDOT = 23932
340362 feet/sec YDOT = 7294
577342 meter/sec
ZDOT = 3065
348460 ZDOT = 934
318211
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 09160
54923634
00010596 00000-0 82463-4 0 9013
2 25544 51
6385 346
1034 0008872 94
3229 265
8948 15
73508803 4753
Satellite: ISS
Catalog Number: 25544
Epoch time: 09160
54923634 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 346
1034 deg
Eccentricity:
0008872
Arg of perigee: 94
3229 deg
Mean anomaly: 265
8948 deg
Mean motion: 15
73508803 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 475
Checksum: 326
Coasting Arc #3 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2009/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5980860
87 A = 6732954
94 meter
Y = -2924730
41 meter E =
0016258
Z = -986968
22 I = 51
54774
XDOT = 2903
442925 Wp = 66
02732
YDOT = 3966
613563 meter/sec RA = 340
70109 deg
ZDOT = 5922
975931 TA = 283
18019
MA = 283
36154
Ha = 193
941 n
mi
Hp = 181
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19622246
95 X = 6017915
69
Y = -9595572
21 feet Y = -2857641
56 meter
Z = -3238084
70 Z = -957823
79
XDOT = 9525
731381 XDOT = 2830
099106
YDOT = 13013
824026 feet/sec YDOT = 3998
670350 meter/sec
ZDOT = 19432
335732 ZDOT = 5936
903430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5380497
97 X = -1639975
78
Y = -21186873
13 feet Y = -6457758
93 meter
Z = -3124007
45 Z = -952197
47
XDOT = 13117
782545 XDOT = 3998
300120
YDOT = -6163
039048 feet/sec YDOT = -1878
494302 meter/sec
ZDOT = 19487
055857 ZDOT = 5939
654625
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 09161
50183788
00010596 00000-0 82463-4 0 9029
2 25544 51
6384 341
2136 0008787 98
5511 261
6647 15
73585474 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 09161
50183788 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 341
2136 deg
Eccentricity:
0008787
Arg of perigee: 98
5511 deg
Mean anomaly: 261
6647 deg
Mean motion: 15
73585474 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 490
Checksum: 331
Coasting Arc #4 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2009/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2945641
90 A = 6721638
13 meter
Y = -3173783
17 meter E =
0022845
Z = -5160814
86 I = 51
48256
XDOT = 6446
185029 Wp = 88
60088
YDOT = -3997
675992 meter/sec RA = 335
57939 deg
ZDOT = -1224
933829 TA = 169
66576
MA = 169
61872
Ha = 193
883 n
mi
Hp = 181
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9664179
47 X = -2884862
99
Y = -10412674
45 feet Y = -3206382
32 meter
Z = -16931807
28 Z = -5174977
66
XDOT = 21148
901013 XDOT = 6496
359105
YDOT = -13115
734883 feet/sec YDOT = -3925
310234 meter/sec
ZDOT = -4018
811774 ZDOT = -1193
497212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12021399
00 X = -3664122
41
Y = 7444439
76 feet Y = 2269065
24 meter
Z = -16987422
84 Z = -5177766
48
XDOT = -8372
075339 XDOT = -2551
808563
YDOT = -22378
409428 feet/sec YDOT = -6820
939194 meter/sec
ZDOT = -3895
794699 ZDOT = -1187
438224
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 09162
51792567
00010596 00000-0 82463-4 0 9033
2 25544 51
6386 335
9983 0008909 102
1437 258
0725 15
73626951 5060
Satellite: ISS
Catalog Number: 25544
Epoch time: 09162
51792567 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 335
9983 deg
Eccentricity:
0008909
Arg of perigee: 102
1437 deg
Mean anomaly: 258
0725 deg
Mean motion: 15
73626951 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 506
Checksum: 333
Coasting Arc #5 (Orbit 521)
---------------------------------------
Vector Time (GMT): 2009/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5252102
69 A = 6732507
66 meter
Y = 4036091
29 meter E =
0022178
Z = 1152190
85 I = 51
49308
XDOT = -3788
920399 Wp = 115
54277
YDOT = -3229
315587 meter/sec RA = 330
41392 deg
ZDOT = -5880
810733 TA = 51
80698
MA = 51
60746
Ha = 193
661 n
mi
Hp = 181
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17231308
03 X = -5302441
70
Y = 13241769
34 feet Y = 3977077
57 meter
Z = 3780153
70 Z = 1126554
61
XDOT = -12430
841203 XDOT = -3723
960265
YDOT = -10594
867413 feet/sec YDOT = -3271
321366 meter/sec
ZDOT = -19293
998467 ZDOT = -5899
059949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10106043
54 X = 3080322
07
Y = 19258204
86 feet Y = 5869900
84 meter
Z = 3679867
28 Z = 1121623
55
XDOT = -11136
205761 XDOT = -3394
315516
YDOT = 9594
690599 feet/sec YDOT = 2924
461695 meter/sec
ZDOT = -19365
631308 ZDOT = -5902
644423
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 09163
53398814
00010596 00000-0 82463-4 0 9044
2 25544 51
6385 330
7821 0008605 104
8993 255
3123 15
73693773 5228
Satellite: ISS
Catalog Number: 25544
Epoch time: 09163
53398814 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 330
7821 deg
Eccentricity:
0008605
Arg of perigee: 104
8993 deg
Mean anomaly: 255
3123 deg
Mean motion: 15
73693773 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 522
Checksum: 322
Coasting Arc #6 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2009/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3635765
37 A = 6721663
84 meter
Y = 2426073
73 meter E =
0013131
Z = 5097324
31 I = 51
43120
XDOT = -5501
008602 Wp = 114
21423
YDOT = 5205
249876 meter/sec RA = 325
29115 deg
ZDOT = 1438
047782 TA = 321
93570
MA = 322
02840
Ha = 193
619 n
mi
Hp = 181
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11928364
07 X = 3583604
60
Y = 7959559
47 feet Y = 2466438
61 meter
Z = 16723504
97 Z = 5114860
45
XDOT = -18047
928484 XDOT = -5565
791490
YDOT = 17077
591456 feet/sec YDOT = 5143
371960 meter/sec
ZDOT = 4718
004533 ZDOT = 1411
167356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9681998
52 X = 2951073
15
Y = -10468674
91 feet Y = -3190852
11 meter
Z = 16792314
47 Z = 5118297
45
XDOT = 13336
564668 XDOT = 4064
984911
YDOT = 19776
749799 feet/sec YDOT = 6027
953339 meter/sec
ZDOT = 4612
894818 ZDOT = 1406
010340
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 09164
55003110
00010596 00000-0 82463-4 0 9050
2 25544 51
6384 325
5665 0008764 109
1741 251
0372 15
73677842 5385
Satellite: ISS
Catalog Number: 25544
Epoch time: 09164
55003110 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 325
5665 deg
Eccentricity:
0008764
Arg of perigee: 109
1741 deg
Mean anomaly: 251
0372 deg
Mean motion: 15
73677842 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 538
Checksum: 305
Coasting Arc #7 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2009/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4312151
01 A = 6732186
97 meter
Y = -4993431
06 meter E =
0013995
Z = -1338639
83 I = 51
44447
XDOT = 4468
623246 Wp = 74
72405
YDOT = 2312
773673 meter/sec RA = 320
11904 deg
ZDOT = 5821
725556 TA = 270
54528
MA = 270
70563
Ha = 193
650 n
mi
Hp = 181
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14147477
07 X = 4374170
77
Y = -16382647
82 feet Y = -4944863
12 meter
Z = -4391862
96 Z = -1317541
42
XDOT = 14660
837422 XDOT = 4414
148449
YDOT = 7587
840133 feet/sec YDOT = 2362
439100 meter/sec
ZDOT = 19100
149461 ZDOT = 5843
302080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14294489
69 X = -4356960
46
Y = -16276587
78 feet Y = -4961103
96 meter
Z = -4309405
06 Z = -1313506
66
XDOT = 8316
527426 XDOT = 2534
877560
YDOT = -12335
217065 feet/sec YDOT = -3759
774161 meter/sec
ZDOT = 19184
787004 ZDOT = 5847
523079
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 09165
50254753
00010596 00000-0 82463-4 0 9068
2 25544 51
6396 320
6771 0008825 113
2466 246
9627 15
73729534 5539
Satellite: ISS
Catalog Number: 25544
Epoch time: 09165
50254753 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 320
6771 deg
Eccentricity:
0008825
Arg of perigee: 113
2466 deg
Mean anomaly: 246
9627 deg
Mean motion: 15
73729534 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 553
Checksum: 327
Coasting Arc #8 (Orbit 568)
---------------------------------------
Vector Time (GMT): 2009/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112496
27 A = 6721526
36 meter
Y = -1625326
98 meter E =
0021431
Z = -5080276
64 I = 51
38728
XDOT = 4356
843564 Wp = 92
58634
YDOT = -6132
592912 meter/sec RA = 314
99592 deg
ZDOT = -1571
541686 TA = 162
27978
MA = 162
20492
Ha = 193
513 n
mi
Hp = 180
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13492441
83 X = -4069336
82
Y = -5332437
59 feet Y = -1671073
38 meter
Z = -16667574
29 Z = -5100150
56
XDOT = 14294
106181 XDOT = 4432
729728
YDOT = -20120
055487 feet/sec YDOT = -6083
447650 meter/sec
ZDOT = -5155
976661 ZDOT = -1550
192500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6894736
90 X = -2101515
81
Y = 12662516
74 feet Y = 3859535
10 meter
Z = -16745512
32 Z = -5104032
15
XDOT = -17341
600204 XDOT = -5285
719742
YDOT = -16121
970426 feet/sec YDOT = -4913
976586 meter/sec
ZDOT = -5072
589956 ZDOT = -1546
125419
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 09166
51854259
00010596 00000-0 82463-4 0 9078
2 25544 51
6398 315
4621 0008795 116
2975 243
9093 15
73778478 5693
Satellite: ISS
Catalog Number: 25544
Epoch time: 09166
51854259 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 315
4621 deg
Eccentricity:
0008795
Arg of perigee: 116
2975 deg
Mean anomaly: 243
9093 deg
Mean motion: 15
73778478 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 569
Checksum: 361
Coasting Arc #9 (Orbit 584)
---------------------------------------
Vector Time (GMT): 2009/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3280986
98 A = 6731916
54 meter
Y = 5693770
09 meter E =
0022656
Z = 1410363
74 I = 51
40142
XDOT = -4888
661752 Wp = 119
57015
YDOT = -1365
931414 meter/sec RA = 309
81692 deg
ZDOT = -5799
705947 TA = 44
85489
MA = 44
67200
Ha = 193
395 n
mi
Hp = 181
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10764392
99 X = -3351263
17
Y = 18680348
07 feet Y = 5656687
07 meter
Z = 4627177
61 Z = 1394254
58
XDOT = -16038
916509 XDOT = -4844
850238
YDOT = -4481
402277 feet/sec YDOT = -1420
353624 meter/sec
ZDOT = -19027
906651 ZDOT = -5823
348966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17477696
70 X = 5327201
95
Y = 12646562
75 feet Y = 3854672
33 meter
Z = 4564307
37 Z = 1391200
89
XDOT = -5166
435629 XDOT = -1574
729580
YDOT = 14111
283872 feet/sec YDOT = 4301
119324 meter/sec
ZDOT = -19120
600929 ZDOT = -5827
959163
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 09167
53451379
00010596 00000-0 82463-4 0 9088
2 25544 51
6390 310
2449 0008643 120
4655 239
7363 15
73798311 5859
Satellite: ISS
Catalog Number: 25544
Epoch time: 09167
53451379 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 310
2449 deg
Eccentricity:
0008643
Arg of perigee: 120
4655 deg
Mean anomaly: 239
7363 deg
Mean motion: 15
73798311 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 585
Checksum: 327
Coasting Arc #10 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2009/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4380617
90 A = 6721392
19 meter
Y = 746430
28 meter E =
0013598
Z = 5035085
52 I = 51
34963
XDOT = -3108
980547 Wp = 124
34354
YDOT = 6849
995289 meter/sec RA = 304
69142 deg
ZDOT = 1678
596157 TA = 309
40376
MA = 309
52408
Ha = 193
094 n
mi
Hp = 181
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14372105
97 X = 4347485
83
Y = 2448918
24 feet Y = 795231
00 meter
Z = 16519309
46 Z = 5056286
40
XDOT = -10200
067413 XDOT = -3193
501687
YDOT = 22473
737825 feet/sec YDOT = 6814
756051 meter/sec
ZDOT = 5507
205238 ZDOT = 1663
288157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3657123
59 X = 1114691
27
Y = -14015266
84 feet Y = -4271853
33 meter
Z = 16602408
20 Z = 5060414
02
XDOT = 20497
904332 XDOT = 6247
761240
YDOT = 11843
534921 feet/sec YDOT = 3609
909444 meter/sec
ZDOT = 5447
526412 ZDOT = 1660
406050
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 09168
55046070
00010596 00000-0 82463-4 0 9090
2 25544 51
6400 305
0290 0008505 124
2395 235
9574 15
73865039 6010
Satellite: ISS
Catalog Number: 25544
Epoch time: 09168
55046070 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 305
0290 deg
Eccentricity:
0008505
Arg of perigee: 124
2395 deg
Mean anomaly: 235
9574 deg
Mean motion: 15
73865039 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 601
Checksum: 300
Coasting Arc #11 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2009/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2136586
38 A = 6731572
92 meter
Y = -6206463
24 meter E =
0012011
Z = -1498592
38 I = 51
36879
XDOT = 5083
664163 Wp = 82
44007
YDOT = 368
449485 meter/sec RA = 299
50913 deg
ZDOT = 5762
996783 TA = 261
00540
MA = 261
14136
Ha = 193
194 n
mi
Hp = 181
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7009797
85 X = 2213109
30
Y = -20362412
20 feet Y = -6182142
60 meter
Z = -4916641
65 Z = -1488027
75
XDOT = 16678
688199 XDOT = 5051
170311
YDOT = 1208
823769 feet/sec YDOT = 425
115453 meter/sec
ZDOT = 18907
469761 ZDOT = 5787
614673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19836046
62 X = -6046027
01
Y = -8408271
35 feet Y = -2562841
11 meter
Z = -4875519
37 Z = -1486058
30
XDOT = 1721
286285 XDOT = 524
648060
YDOT = -15001
419759 feet/sec YDOT = -4572
432742 meter/sec
ZDOT = 19003
940830 ZDOT = 5792
401165
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 09169
50289098
00010596 00000-0 82463-4 0 9107
2 25544 51
6408 300
1392 0008552 126
9684 233
2264 15
73871309 6169
Satellite: ISS
Catalog Number: 25544
Epoch time: 09169
50289098 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 300
1392 deg
Eccentricity:
0008552
Arg of perigee: 126
9684 deg
Mean anomaly: 233
2264 deg
Mean motion: 15
73871309 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 616
Checksum: 316
Coasting Arc #12 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2009/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462722
65 A = 6721309
43 meter
Y = 69214
40 meter E =
0019761
Z = -5041750
14 I = 51
32120
XDOT = 1801
481589 Wp = 96
98612
YDOT = -7276
356486 meter/sec RA = 294
38179 deg
ZDOT = -1702
558721 TA = 156
57683
MA = 156
48669
Ha = 193
009 n
mi
Hp = 181
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14641478
50 X = -4438672
69
Y = 227081
35 feet Y = 19444
97 meter
Z = -16541174
99 Z = -5063371
92
XDOT = 5910
372667 XDOT = 1890
983985
YDOT = -23872
560650 feet/sec YDOT = -7255
710536 meter/sec
ZDOT = -5585
822574 ZDOT = -1693
590862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -514055
90 X = -156684
24
Y = 14537896
50 feet Y = 4431150
85 meter
Z = -16625890
67 Z = -5067571
48
XDOT = -22479
011379 XDOT = -6851
602668
YDOT = -7112
951048 feet/sec YDOT = -2168
027479 meter/sec
ZDOT = -5551
001179 ZDOT = -1691
945159
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 09170
51879269
00010596 00000-0 82463-4 0 9116
2 25544 51
6410 294
9230 0008399 130
6174 229
5721 15
73908088 6327
Satellite: ISS
Catalog Number: 25544
Epoch time: 09170
51879269 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 294
9230 deg
Eccentricity:
0008399
Arg of perigee: 130
6174 deg
Mean anomaly: 229
5721 deg
Mean motion: 15
73908088 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 632
Checksum: 323
Coasting Arc #13 (Orbit 647)
---------------------------------------
Vector Time (GMT): 2009/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1000980
35 A = 6731427
15 meter
Y = 6477699
61 meter E =
0022290
Z = 1480962
10 I = 51
34456
XDOT = -5079
298799 Wp = 124
28273
YDOT = 546
130377 meter/sec RA = 289
19633 deg
ZDOT = -5772
533384 TA = 39
32472
MA = 39
16306
Ha = 192
932 n
mi
Hp = 181
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3284056
26 X = -1080535
02
Y = 21252295
30 feet Y = 6466060
95 meter
Z = 4858799
55 Z = 1475907
36
XDOT = -16664
366138 XDOT = -5056
985962
YDOT = 1791
766328 feet/sec YDOT = 489
456619 meter/sec
ZDOT = -18938
757821 ZDOT = -5797
154608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21128579
19 X = 6439990
94
Y = 4027106
05 feet Y = 1227461
92 meter
Z = 4839273
95 Z = 1475010
70
XDOT = 1525
744105 XDOT = 465
046803
YDOT = 15064
423240 feet/sec YDOT = 4591
636204 meter/sec
ZDOT = -19035
210851 ZDOT = -5801
932267
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 09171
53467154
00010596 00000-0 82463-4 0 9126
2 25544 51
6412 289
7062 0008439 134
4692 225
7162 15
73933530 6480
Satellite: ISS
Catalog Number: 25544
Epoch time: 09171
53467154 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 289
7062 deg
Eccentricity:
0008439
Arg of perigee: 134
4692 deg
Mean anomaly: 225
7162 deg
Mean motion: 15
73933530 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 648
Checksum: 316
Coasting Arc #14 (Orbit 663)
---------------------------------------
Vector Time (GMT): 2009/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4369404
26 A = 6721007
98 meter
Y = -875876
84 meter E =
0013383
Z = 5025098
57 I = 51
30261
XDOT = -471
193840 Wp = 132
95512
YDOT = 7500
519269 meter/sec RA = 284
06700 deg
ZDOT = 1705
186563 TA = 300
50882
MA = 300
64088
Ha = 192
601 n
mi
Hp = 181
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14335315
81 X = 4354462
53
Y = -2873611
68 feet Y = -827100
29 meter
Z = 16486543
87 Z = 5046288
80
XDOT = -1545
911550 XDOT = -563
314443
YDOT = 24608
002852 feet/sec YDOT = 7494
734645 meter/sec
ZDOT = 5594
444103 ZDOT = 1702
675423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2637533
87 X = -803920
32
Y = -14284909
17 feet Y = -4354040
32 meter
Z = 16569545
48 Z = 5050397
46
XDOT = 23536
977820 XDOT = 7174
070839
YDOT = 2177
270010 feet/sec YDOT = 663
631899 meter/sec
ZDOT = 5584
930135 ZDOT = 1702
286705
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 09172
55052511
00010596 00000-0 82463-4 0 9137
2 25544 51
6421 284
4899 0008262 138
0662 222
1135 15
74016863 6642
Satellite: ISS
Catalog Number: 25544
Epoch time: 09172
55052511 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 284
4899 deg
Eccentricity:
0008262
Arg of perigee: 138
0662 deg
Mean anomaly: 222
1135 deg
Mean motion: 15
74016863 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 664
Checksum: 299
Coasting Arc #15 (Orbit 678)
---------------------------------------
Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -168079
39 A = 6731233
18 meter
Y = -6567288
93 meter E =
0010296
Z = -1474406
51 I = 51
33096
XDOT = 4892
026409 Wp = 87
34747
YDOT = -1412
116666 meter/sec RA = 278
88077 deg
ZDOT = 5767
318759 TA = 256
36392
MA = 256
47860
Ha = 192
660 n
mi
Hp = 181
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -551441
56 X = -87467
96
Y = -21546223
51 feet Y = -6568717
42 meter
Z = -4837291
70 Z = -1475028
79
XDOT = 16049
955411 XDOT = 4879
436769
YDOT = -4632
928695 feet/sec YDOT = -1357
482927 meter/sec
ZDOT = 18921
649473 ZDOT = 5791
053312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21545955
56 X = -6567207
25
Y = 537797
50 feet Y = 163920
68 meter
Z = -4840020
59 Z = -1475238
27
XDOT = -4604
057329 XDOT = -1403
316674
YDOT = -14365
551258 feet/sec YDOT = -4378
620024 meter/sec
ZDOT = 19014
607183 ZDOT = 5795
652269
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 09173
50286956
00010596 00000-0 82463-4 0 9146
2 25544 51
6422 279
5999 0008116 140
2766 219
8993 15
73995562 6799
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
50286956 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 279
5999 deg
Eccentricity:
0008116
Arg of perigee: 140
2766 deg
Mean anomaly: 219
8993 deg
Mean motion: 15
73995562 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 679
Checksum: 365
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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