Date:
August 5th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8794 11 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 1340)
---------------------------------------
Vector Time (GMT): 2009/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2680490
88 A = 6733616
90 meter
Y = -6154581
16 meter E =
0005859
Z = -474023
38 I = 51
95883
XDOT = 4530
320616 Wp = 181
27947
YDOT = -1508
312143 meter/sec RA = 63
29829 deg
ZDOT = -6038
713715 TA = 3
85175
MA = 3
84724
Ha = 189
683 n
mi
Hp = 187
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8794261
41 X = -2609167
40
Y = -20192195
41 feet Y = -6184157
14 meter
Z = -1555194
82 Z = -486872
43
XDOT = 14863
256613 XDOT = 4576
184537
YDOT = -4948
530652 feet/sec YDOT = -1457
394311 meter/sec
ZDOT = -19812
052871 ZDOT = -6016
594605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9324858
03 X = -2842216
73
Y = 19948688
91 feet Y = 6080360
38 meter
Z = -1606005
54 Z = -489510
49
XDOT = -12167
611368 XDOT = -3708
687945
YDOT = -7274
561224 feet/sec YDOT = -2217
286261 meter/sec
ZDOT = -19725
116378 ZDOT = -6012
215472
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 09215
53082382
00010596 00000-0 82463-4 0 9008
2 25544 51
6405 63
7812 0007945 288
7931 71
2370 15
73456696 13414
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
53082382 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 63
7812 deg
Eccentricity:
0007945
Arg of perigee: 288
7931 deg
Mean anomaly: 71
2370 deg
Mean motion: 15
73456696 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1341
Checksum: 312
Coasting Arc #2 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2009/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3734953
48 A = 6721652
83 meter
Y = 1835915
70 meter E =
0006217
Z = 5282636
00 I = 51
90346
XDOT = -3806
711498 Wp = 308
36628
YDOT = -6679
453263 meter/sec RA = 58
17816 deg
ZDOT = -366
590871 TA = 145
12387
MA = 145
08312
Ha = 189
945 n
mi
Hp = 187
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12253784
40 X = -3780866
96
Y = 6023345
48 feet Y = 1793892
02 meter
Z = 17331482
93 Z = 5264380
64
XDOT = -12489
210952 XDOT = -3729
956993
YDOT = -21914
216743 feet/sec YDOT = -6721
592949 meter/sec
ZDOT = -1202
725955 ZDOT = -384
897715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12780581
18 X = 3895521
14
Y = 5057056
22 feet Y = 1541390
74 meter
Z = 17259755
23 Z = 5260773
39
XDOT = -7389
003291 XDOT = -2252
168203
YDOT = 23064
923998 feet/sec YDOT = 7030
188834 meter/sec
ZDOT = -1275
028822 ZDOT = -388
628785
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 09216
54699042
00010596 00000-0 82463-4 0 9018
2 25544 51
6399 58
5655 0007960 293
0066 67
0257 15
73472226 13579
Satellite: ISS
Catalog Number: 25544
Epoch time: 09216
54699042 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 58
5655 deg
Eccentricity:
0007960
Arg of perigee: 293
0066 deg
Mean anomaly: 67
0257 deg
Mean motion: 15
73472226 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1357
Checksum: 327
Coasting Arc #3 (Orbit 1372)
---------------------------------------
Vector Time (GMT): 2009/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3933441
81 A = 6733597
40 meter
Y = 5452503
52 meter E =
0012382
Z = 168322
96 I = 51
92596
XDOT = -3943
339337 Wp = 9
38331
YDOT = 2656
072862 meter/sec RA = 53
06950 deg
ZDOT = 6061
076331 TA = 352
43862
MA = 352
45728
Ha = 190
085 n
mi
Hp = 187
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12904992
80 X = 3871360
97
Y = 17888791
08 feet Y = 5496142
45 meter
Z = 552240
69 Z = 187280
85
XDOT = -12937
465017 XDOT = -4002
189880
YDOT = 8714
149809 feet/sec YDOT = 2611
646592 meter/sec
ZDOT = 19885
421033 ZDOT = 6041
777280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4131018
29 X = 1259134
37
Y = -21665505
96 feet Y = -6603646
22 meter
Z = 627052
47 Z = 191125
59
XDOT = 13720
737196 XDOT = 4182
080697
YDOT = 3193
695904 feet/sec YDOT = 973
438511 meter/sec
ZDOT = 19809
621863 ZDOT = 6037
972744
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 09217
56314661
00010596 00000-0 82463-4 0 9023
2 25544 51
6387 53
3494 0008034 297
0243 63
0100 15
73497107 13730
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
56314661 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 53
3494 deg
Eccentricity:
0008034
Arg of perigee: 297
0243 deg
Mean anomaly: 63
0100 deg
Mean motion: 15
73497107 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1373
Checksum: 293
Coasting Arc #4 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2009/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3103391
74 A = 6721450
32 meter
Y = -2761304
41 meter E =
0009115
Z = -5291136
58 I = 51
86555
XDOT = 5137
228269 Wp = 64
29692
YDOT = 5728
331756 meter/sec RA = 47
95280 deg
ZDOT = 27
559083 TA = 205
94112
MA = 205
98683
Ha = 190
219 n
mi
Hp = 187
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10181731
44 X = 3159741
30
Y = -9059397
68 feet Y = -2726285
09 meter
Z = -17359371
97 Z = -5275923
92
XDOT = 16854
423455 XDOT = 5072
657400
YDOT = 18793
739357 feet/sec YDOT = 5785
418219 meter/sec
ZDOT = 90
416940 ZDOT = 52
358702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13667111
96 X = -4165735
72
Y = -1010069
53 feet Y = -307869
19 meter
Z = -17299651
64 Z = -5272933
82
XDOT = 1566
069481 XDOT = 477
337978
YDOT = -24193
858392 feet/sec YDOT = -7374
288038 meter/sec
ZDOT = 188
221082 ZDOT = 57
369786
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 09218
51578366
00010596 00000-0 82463-4 0 9034
2 25544 51
6379 48
4598 0007918 300
6166 59
4215 15
73526136 13883
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
51578366 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 48
4598 deg
Eccentricity:
0007918
Arg of perigee: 300
6166 deg
Mean anomaly: 59
4215 deg
Mean motion: 15
73526136 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1388
Checksum: 337
Coasting Arc #5 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2009/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4992885
76 A = 6733363
74 meter
Y = -4512399
96 meter E =
0004525
Z = 109413
60 I = 51
88598
XDOT = 3111
564396 Wp = 148
87428
YDOT = -3592
286976 meter/sec RA = 42
83699 deg
ZDOT = -6054
580022 TA = 29
94184
MA = 29
91597
Ha = 190
368 n
mi
Hp = 186
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16380858
79 X = -4942587
75
Y = -14804461
81 feet Y = -4567952
11 meter
Z = 358968
49 Z = 85280
63
XDOT = 10208
544605 XDOT = 3180
914195
YDOT = -11785
718424 feet/sec YDOT = -3557
103654 meter/sec
ZDOT = -19864
107683 ZDOT = -6039
296021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1260889
36 X = 384319
08
Y = 22044818
64 feet Y = 6719260
72 meter
Z = 263840
71 Z = 80418
65
XDOT = -14019
508881 XDOT = -4273
146307
YDOT = 1044
603324 feet/sec YDOT = 318
395093 meter/sec
ZDOT = -19804
143938 ZDOT = -6036
303072
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 09219
53191882
00010596 00000-0 82463-4 0 9042
2 25544 51
6385 43
2449 0008134 305
6489 54
3916 15
73580661 14046
Satellite: ISS
Catalog Number: 25544
Epoch time: 09219
53191882 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 43
2449 deg
Eccentricity:
0008134
Arg of perigee: 305
6489 deg
Mean anomaly: 54
3916 deg
Mean motion: 15
73580661 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1404
Checksum: 318
Coasting Arc #6 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2009/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2300004
05 A = 6721524
77 meter
Y = 3469876
23 meter E =
0005789
Z = 5280227
23 I = 51
82201
XDOT = -6215
565516 Wp = 319
72403
YDOT = -4533
287860 meter/sec RA = 37
72199 deg
ZDOT = 276
094582 TA = 127
68720
MA = 127
63469
Ha = 190
634 n
mi
Hp = 186
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7545945
05 X = -2364283
85
Y = 11384108
37 feet Y = 3443796
72 meter
Z = 17323580
16 Z = 5268897
93
XDOT = -20392
275316 XDOT = -6165
752758
YDOT = -14872
991667 feet/sec YDOT = -4602
515448 meter/sec
ZDOT = 905
822118 ZDOT = 246
020742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13390361
30 X = 4081382
12
Y = -2962128
72 feet Y = -902856
83 meter
Z = 17279168
31 Z = 5266690
50
XDOT = 4281
999533 XDOT = 1305
153458
YDOT = 23863
434362 feet/sec YDOT = 7273
574794 meter/sec
ZDOT = 787
327564 ZDOT = 239
977442
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 09220
54804733
00010596 00000-0 82463-4 0 9052
2 25544 51
6379 38
0286 0007863 308
9577 51
0885 15
73505619 14209
Satellite: ISS
Catalog Number: 25544
Epoch time: 09220
54804733 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 38
0286 deg
Eccentricity:
0007863
Arg of perigee: 308
9577 deg
Mean anomaly: 51
0885 deg
Mean motion: 15
73505619 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1420
Checksum: 321
Coasting Arc #7 (Orbit 1434)
---------------------------------------
Vector Time (GMT): 2009/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5809014
78 A = 6733356
26 meter
Y = 3366076
92 meter E =
0013901
Z = -373619
11 I = 51
83850
XDOT = -2101
340751 Wp = 7
60389
YDOT = 4292
801160 meter/sec RA = 32
59688 deg
ZDOT = 6042
809812 TA = 348
34381
MA = 348
37596
Ha = 190
640 n
mi
Hp = 186
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19058447
46 X = 5772757
95
Y = 11043559
46 feet Y = 3430834
02 meter
Z = -1225784
49 Z = -345487
28
XDOT = -6894
162570 XDOT = -2178
541957
YDOT = 14083
993308 feet/sec YDOT = 4268
871024 meter/sec
ZDOT = 19825
491509 ZDOT = 6032
414135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6539617
50 X = -1993275
41
Y = -21039899
83 feet Y = -6412961
47 meter
Z = -1114984
75 Z = -339847
35
XDOT = 13163
845787 XDOT = 4012
340196
YDOT = -5132
622168 feet/sec YDOT = -1564
423237 meter/sec
ZDOT = 19784
788471 ZDOT = 6030
403526
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 09221
50065425
00010596 00000-0 82463-4 0 9067
2 25544 51
6384 33
1389 0007866 311
8757 48
1734 15
73568559 14359
Satellite: ISS
Catalog Number: 25544
Epoch time: 09221
50065425 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 33
1389 deg
Eccentricity:
0007866
Arg of perigee: 311
8757 deg
Mean anomaly: 48
1734 deg
Mean motion: 15
73568559 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1435
Checksum: 326
Coasting Arc #8 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2009/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351976
80 A = 6721340
81 meter
Y = -3968779
58 meter E =
0011651
Z = -5261991
33 I = 51
77305
XDOT = 7000
166672 Wp = 54
60689
YDOT = 3140
589219 meter/sec RA = 27
48517 deg
ZDOT = -564
436276 TA = 210
00067
MA = 210
06748
Ha = 190
745 n
mi
Hp = 186
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4435619
42 X = 1421817
52
Y = -13020930
38 feet Y = -3953270
44 meter
Z = -17263751
08 Z = -5255253
86
XDOT = 22966
426088 XDOT = 6967
269707
YDOT = 10303
770405 feet/sec YDOT = 3218
685260 meter/sec
ZDOT = -1851
825053 ZDOT = -530
509580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12044982
29 X = -3671310
60
Y = 6711641
19 feet Y = 2045708
23 meter
Z = -17237422
18 Z = -5253966
28
XDOT = -9824
993858 XDOT = -2994
658128
YDOT = -22093
695624 feet/sec YDOT = -6734
158426 meter/sec
ZDOT = -1718
248563 ZDOT = -523
722162
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 09222
51675987
00010596 00000-0 82463-4 0 9070
2 25544 51
6389 27
9244 0007747 316
6159 43
4394 15
73597051 14519
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
51675987 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 27
9244 deg
Eccentricity:
0007747
Arg of perigee: 316
6159 deg
Mean anomaly: 43
4394 deg
Mean motion: 15
73597051 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1451
Checksum: 339
Coasting Arc #9 (Orbit 1466)
---------------------------------------
Vector Time (GMT): 2009/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6365144
94 A = 6733057
94 meter
Y = -2105656
23 meter E =
0005536
Z = 600928
56 I = 51
78567
XDOT = 986
487993 Wp = 112
13952
YDOT = -4708
436275 meter/sec RA = 22
35147 deg
ZDOT = -6007
452381 TA = 61
33624
MA = 61
28059
Ha = 190
910 n
mi
Hp = 185
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20883021
44 X = -6344045
25
Y = -6908320
96 feet Y = -2176717
05 meter
Z = 1971550
41 Z = 570058
00
XDOT = 3236
509163 XDOT = 1068
248249
YDOT = -15447
625574 feet/sec YDOT = -4696
947539 meter/sec
ZDOT = -19709
489438 ZDOT = -6002
461522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11341954
09 X = 3457027
61
Y = 18858682
50 feet Y = 5748126
43 meter
Z = 1850044
82 Z = 563893
66
XDOT = -11235
882391 XDOT = -3424
696953
YDOT = 8703
427070 feet/sec YDOT = 2652
804571 meter/sec
ZDOT = -19690
059394 ZDOT = -6001
530103
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 09223
53285274
00010596 00000-0 82463-4 0 9080
2 25544 51
6387 22
7083 0008061 320
5236 39
5339 15
73640413 14674
Satellite: ISS
Catalog Number: 25544
Epoch time: 09223
53285274 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 22
7083 deg
Eccentricity:
0008061
Arg of perigee: 320
5236 deg
Mean anomaly: 39
5339 deg
Mean motion: 15
73640413 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1467
Checksum: 304
Coasting Arc #10 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2009/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -362951
52 A = 6721431
82 meter
Y = 4208535
87 meter E =
0005218
Z = 5229211
23 I = 51
71853
XDOT = -7477
349642 Wp = 339
38992
YDOT = -1648
548080 meter/sec RA = 17
23910 deg
ZDOT = 812
816490 TA = 102
91084
MA = 102
85255
Ha = 191
132 n
mi
Hp = 185
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1190785
83 X = -435387
67
Y = 13807532
40 feet Y = 4204071
95 meter
Z = 17156204
82 Z = 5227272
21
XDOT = -24531
987016 XDOT = -7462
308074
YDOT = -5408
622311 feet/sec YDOT = -1732
080117 meter/sec
ZDOT = 2666
720769 ZDOT = 776
528021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9812220
67 X = 2990764
86
Y = -9800095
60 feet Y = -2987069
14 meter
Z = 17148753
23 Z = 5226939
98
XDOT = 14718
677896 XDOT = 4486
253023
YDOT = 19124
482387 feet/sec YDOT = 5829
142232 meter/sec
ZDOT = 2523
930569 ZDOT = 769
294037
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 09224
54893849
00010596 00000-0 82463-4 0 9096
2 25544 51
6392 17
4929 0007877 324
7899 35
2743 15
73598905 14833
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
54893849 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 17
4929 deg
Eccentricity:
0007877
Arg of perigee: 324
7899 deg
Mean anomaly: 35
2743 deg
Mean motion: 15
73598905 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1483
Checksum: 369
Coasting Arc #11 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2009/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6629832
73 A = 6732950
09 meter
Y = 759053
23 meter E =
0014915
Z = -820581
97 I = 51
73008
XDOT = 179
603985 Wp = 9
22474
YDOT = 4860
243280 meter/sec RA = 12
09837 deg
ZDOT = 5976
230024 TA = 341
83203
MA = 341
88527
Ha = 191
201 n
mi
Hp = 185
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21751419
72 X = 6624838
36
Y = 2490332
13 feet Y = 833164
03 meter
Z = -2692198
05 Z = -788386
33
XDOT = 589
251920 XDOT = 96
211119
YDOT = 15945
680052 feet/sec YDOT = 4861
785117 meter/sec
ZDOT = 19607
053883 ZDOT = 5976
900244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15427739
08 X = -4702374
87
Y = -15555603
39 feet Y = -4741347
91 meter
Z = -2565543
63 Z = -781977
70
XDOT = 8467
189627 XDOT = 2580
799398
YDOT = -11615
148633 feet/sec YDOT = -3540
297303 meter/sec
ZDOT = 19609
886818 ZDOT = 5977
093502
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 09225
50150589
00010596 00000-0 82463-4 0 9102
2 25544 51
6405 12
6041 0007812 328
1411 31
9278 15
73635393 14982
Satellite: ISS
Catalog Number: 25544
Epoch time: 09225
50150589 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 12
6041 deg
Eccentricity:
0007812
Arg of perigee: 328
1411 deg
Mean anomaly: 31
9278 deg
Mean motion: 15
73635393 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1498
Checksum: 294
Coasting Arc #12 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -661330
46 A = 6721371
30 meter
Y = -4222511
02 meter E =
0013996
Z = -5198003
34 I = 51
66224
XDOT = 7619
597982 Wp = 49
83020
YDOT = 101
419239 meter/sec RA = 6
98730 deg
ZDOT = -1044
800973 TA = 210
15667
MA = 210
23732
Ha = 191
277 n
mi
Hp = 185
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2169719
36 X = -588813
56
Y = -13853382
62 feet Y = -4229500
55 meter
Z = -17053816
73 Z = -5201040
25
XDOT = 24998
681042 XDOT = 7622
973032
YDOT = 332
740284 feet/sec YDOT = 186
645002 meter/sec
ZDOT = -3427
824714 ZDOT = -1007
776829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6838907
53 X = -2084499
02
Y = 12224564
50 feet Y = 3726047
26 meter
Z = -17065928
74 Z = -5201695
08
XDOT = -18693
574911 XDOT = -5697
801633
YDOT = -15072
088611 feet/sec YDOT = -4593
972609 meter/sec
ZDOT = -3282
205364 ZDOT = -1000
416195
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 09226
51756777
00010596 00000-0 82463-4 0 9116
2 25544 51
6407 7
3900 0007881 332
6276 27
4471 15
73671879 15147
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
51756777 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 7
3900 deg
Eccentricity:
0007881
Arg of perigee: 332
6276 deg
Mean anomaly: 27
4471 deg
Mean motion: 15
73671879 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1514
Checksum: 323
Coasting Arc #13 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6632834
54 A = 6732698
99 meter
Y = 573463
86 meter E =
0007979
Z = 993906
09 I = 51
67016
XDOT = -1303
415570 Wp = 93
54215
YDOT = -4731
122603 meter/sec RA = 1
83690 deg
ZDOT = -5928
308095 TA = 75
60868
MA = 75
52013
Ha = 191
425 n
mi
Hp = 184
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21761268
17 X = -6643582
33
Y = 1881443
10 feet Y = 499231
43 meter
Z = 3260846
76 Z = 961657
92
XDOT = -4276
297803 XDOT = -1221
615997
YDOT = -15522
055783 feet/sec YDOT = -4745
240264 meter/sec
ZDOT = -19449
829708 ZDOT = -5934
441785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18579275
90 X = 5662963
29
Y = 11520159
63 feet Y = 3511344
65 meter
Z = 3134034
35 Z = 955253
67
XDOT = -5108
778447 XDOT = -1557
155671
YDOT = 13574
543848 feet/sec YDOT = 4137
520965 meter/sec
ZDOT = -19474
139924 ZDOT = -5935
717849
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 09227
53361823
00010596 00000-0 82463-4 0 9124
2 25544 51
6403 2
1733 0007956 335
8013 24
2776 15
73675993 15309
Satellite: ISS
Catalog Number: 25544
Epoch time: 09227
53361823 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 2
1733 deg
Eccentricity:
0007956
Arg of perigee: 335
8013 deg
Mean anomaly: 24
2776 deg
Mean motion: 15
73675993 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1530
Checksum: 303
Coasting Arc #14 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1604356
43 A = 6721366
48 meter
Y = 4000790
50 meter E =
0005275
Z = 5155898
98 I = 51
60384
XDOT = -7470
410634 Wp = 4
24801
YDOT = 1409
038040 meter/sec RA = 356
72325 deg
ZDOT = 1236
287145 TA = 73
96278
MA = 73
90470
Ha = 191
497 n
mi
Hp = 184
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5263636
59 X = 1534453
53
Y = 13125953
10 feet Y = 4018340
04 meter
Z = 16915679
05 Z = 5163523
43
XDOT = -24509
221241 XDOT = -7491
617113
YDOT = 4622
828215 feet/sec YDOT = 1325
380840 meter/sec
ZDOT = 4056
060187 ZDOT = 1199
944918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3477886
11 X = 1060059
68
Y = -13670407
02 feet Y = -4166740
06 meter
Z = 16945825
23 Z = 5165087
53
XDOT = 21613
408741 XDOT = 6587
766984
YDOT = 10328
771714 feet/sec YDOT = 3148
209618 meter/sec
ZDOT = 3913
172915 ZDOT = 1192
735105
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 09228
54965688
00010596 00000-0 82463-4 0 9136
2 25544 51
6415 356
9578 0008055 339
3607 20
7229 15
73716871 15460
Satellite: ISS
Catalog Number: 25544
Epoch time: 09228
54965688 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 356
9578 deg
Eccentricity:
0008055
Arg of perigee: 339
3607 deg
Mean anomaly: 20
7229 deg
Mean motion: 15
73716871 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1546
Checksum: 346
Coasting Arc #15 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6349359
62 A = 6732483
82 meter
Y = -1876361
70 meter E =
0015680
Z = -1167459
58 I = 51
61194
XDOT = 2368
035594 Wp = 12
67604
YDOT = 4366
685772 meter/sec RA = 351
56698 deg
ZDOT = 5890
497291 TA = 334
52410
MA = 334
60131
Ha = 191
760 n
mi
Hp = 184
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20831232
36 X = 6375540
74
Y = -6156042
32 feet Y = -1805212
95 meter
Z = -3830247
98 Z = -1136551
47
XDOT = 7769
145650 XDOT = 2290
416084
YDOT = 14326
396890 feet/sec YDOT = 4392
732071 meter/sec
ZDOT = 19325
778515 ZDOT = 5901
812828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20640857
63 X = -6291333
40
Y = -6834330
57 feet Y = -2083103
96 meter
Z = -3708749
18 Z = -1130426
75
XDOT = 1381
783937 XDOT = 421
167744
YDOT = -14629
938585 feet/sec YDOT = -4459
205281 meter/sec
ZDOT = 19370
461282 ZDOT = 5904
116599
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 09229
50218427
00010596 00000-0 82463-4 0 9146
2 25544 51
6422 352
0689 0008109 343
9520 16
1385 15
73697015 15610
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
50218427 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 352
0689 deg
Eccentricity:
0008109
Arg of perigee: 343
9520 deg
Mean anomaly: 16
1385 deg
Mean motion: 15
73697015 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1561
Checksum: 306
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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