Date:
August 18th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10604 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
237/22:06:55
000 0
0 0
0 0
0
016/23:30:13
047 0
0 0
0 185
5
000/00:00:00
000 0
0 0
0 183
5
Coasting Arc #1 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2007/227/22:06:55
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1508607
27 A = 6714208
47 meter
Y = -3883205
07 meter E =
0006020
Z = 5269892
03 I = 51
75030
XDOT = 7038
757014 Wp = 241
27082
YDOT = -3111
701574 meter/sec RA = 154
50120 deg
ZDOT = -281
007225 TA = 211
37440
MA = 211
41033
Ha = 186
081 n
mi
Hp = 183
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4949498
93 X = -1490672
41
Y = -12740174
12 feet Y = -3899974
90 meter
Z = 17289672
02 Z = 5262606
88
XDOT = 23093
034823 XDOT = 7074
394452
YDOT = -10208
994665 feet/sec YDOT = -3032
790965 meter/sec
ZDOT = -921
939715 ZDOT = -246
726858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9427169
05 X = 2873401
13
Y = -9945352
26 feet Y = -3031343
37 meter
Z = 17261540
69 Z = 5261317
60
XDOT = 18266
621705 XDOT = 5567
666296
YDOT = 15957
188987 feet/sec YDOT = 4863
751203 meter/sec
ZDOT = -792
355806 ZDOT = -241
510050
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 07227
96862197
00020000 00000-0 20000-3 0 9005
2 25544 51
6324 155
2280 0008397 246
1859 113
8425 15
76077156 20212
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
96862197 = yrday
fracday
Element set: 900
Inclination: 51
6324 deg
RA of node: 155
2280 deg
Eccentricity:
0008397
Arg of perigee: 246
1859 deg
Mean anomaly: 113
8425 deg
Mean motion: 15
76077156 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2021
Checksum: 299
Coasting Arc #2 (Orbit 2036)
---------------------------------------
Vector Time (GMT): 2007/228/22:11:44
263
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6077213
83 A = 6723211
56 meter
Y = 1224231
91 meter E =
0005454
Z = 2597128
29 I = 51
80775
XDOT = 1148
467212 Wp = 88
69658
YDOT = -5498
235764 meter/sec RA = 149
36707 deg
ZDOT = 5269
797486 TA = 300
75192
MA = 300
80562
Ha = 185
807 n
mi
Hp = 183
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19938365
59 X = -6103067
97
Y = 4016508
88 feet Y = 1156128
52 meter
Z = 8520762
09 Z = 2567542
66
XDOT = 3767
937046 XDOT = 1184
264457
YDOT = -18038
831246 feet/sec YDOT = -5485
192803 meter/sec
ZDOT = 17289
361830 ZDOT = 5275
463638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12684890
02 X = -3866354
48
Y = -15958101
21 feet Y = -4864029
25 meter
Z = 8408729
00 Z = 2562980
60
XDOT = 16565
506159 XDOT = 5049
166277
YDOT = -4030
198356 feet/sec YDOT = -1228
404459 meter/sec
ZDOT = 17310
132973 ZDOT = 5276
128530
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 07228
98309479
00020000 00000-0 20000-3 0 9018
2 25544 51
6333 150
0013 0008540 249
2965 110
7284 15
76149233 20373
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
98309479 = yrday
fracday
Element set: 901
Inclination: 51
6333 deg
RA of node: 150
0013 deg
Eccentricity:
0008540
Arg of perigee: 249
2965 deg
Mean anomaly: 110
7284 deg
Mean motion: 15
76149233 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2037
Checksum: 283
Coasting Arc #3 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2007/229/22:16:36
086
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206574
47 A = 6722399
35 meter
Y = 5139314
66 meter E =
0004018
Z = -2911990
31 I = 51
82931
XDOT = -5767
483216 Wp = 263
18953
YDOT = -732
810888 meter/sec RA = 144
16422 deg
ZDOT = 5051
228221 TA = 63
36837
MA = 63
32721
Ha = 185
551 n
mi
Hp = 183
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10520257
45 X = -3249658
89
Y = 16861268
55 feet Y = 5103216
05 meter
Z = -9553773
99 Z = -2927672
38
XDOT = -18922
189028 XDOT = -5783
397984
YDOT = -2404
235196 feet/sec YDOT = -797
395153 meter/sec
ZDOT = 16572
271067 ZDOT = 5023
171280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19826689
22 X = -6043174
87
Y = -868045
18 feet Y = -264580
17 meter
Z = -9612579
45 Z = -2929914
22
XDOT = -7279
106033 XDOT = -2218
671519
YDOT = -16310
343914 feet/sec YDOT = -4971
392825 meter/sec
ZDOT = 16465
775575 ZDOT = 5018
768395
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 07229
93415143
00020000 00000-0 20000-3 0 9021
2 25544 51
6334 145
1016 0008497 254
4033 105
6193 15
76122471 20521
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
93415143 = yrday
fracday
Element set: 902
Inclination: 51
6334 deg
RA of node: 145
1016 deg
Eccentricity:
0008497
Arg of perigee: 254
4033 deg
Mean anomaly: 105
6193 deg
Mean motion: 15
76122471 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2052
Checksum: 264
Coasting Arc #4 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2007/230/22:21:29
612
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3253302
10 A = 6714067
69 meter
Y = 2642528
06 meter E =
0006453
Z = -5250632
57 I = 51
82446
XDOT = -5444
061434 Wp = 93
51463
YDOT = 5406
275290 meter/sec RA = 139
03857 deg
ZDOT = -653
363868 TA = 170
29527
MA = 170
28279
Ha = 185
344 n
mi
Hp = 184
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10673563
31 X = 3249017
72
Y = 8669711
48 feet Y = 2678884
46 meter
Z = -17226484
81 Z = -5234838
43
XDOT = -17861
093943 XDOT = -5500
936677
YDOT = 17737
123654 feet/sec YDOT = 5345
078732 meter/sec
ZDOT = -2143
582244 ZDOT = -679
949096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1756606
25 X = -535413
58
Y = 13714043
44 feet Y = 4180040
44 meter
Z = -17166245
28 Z = -5232271
56
XDOT = -23452
893584 XDOT = -7148
441964
YDOT = -5808
132927 feet/sec YDOT = -1770
318916 meter/sec
ZDOT = -2243
711530 ZDOT = -683
883274
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 07230
94859473
00020000 00000-0 20000-3 0 9033
2 25544 51
6336 139
8751 0008499 258
3170 101
7041 15
76172597 20686
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
94859473 = yrday
fracday
Element set: 903
Inclination: 51
6336 deg
RA of node: 139
8751 deg
Eccentricity:
0008499
Arg of perigee: 258
3170 deg
Mean anomaly: 101
7041 deg
Mean motion: 15
76172597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2068
Checksum: 311
Coasting Arc #5 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2007/231/22:26:02
512
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5395333
48 A = 6724593
12 meter
Y = -3583031
05 meter E =
0008101
Z = -1788845
72 I = 51
88124
XDOT = 1416
641003 Wp = 208
18980
YDOT = 4982
669346 meter/sec RA = 133
89595 deg
ZDOT = -5704
057515 TA = 351
58950
MA = 351
60307
Ha = 185
128 n
mi
Hp = 184
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17701225
33 X = 5443688
35
Y = -11755351
22 feet Y = -3522426
96 meter
Z = -5868916
41 Z = -1762517
90
XDOT = 4647
772321 XDOT = 1388
528010
YDOT = 16347
340375 feet/sec YDOT = 4998
354033 meter/sec
ZDOT = -18714
099460 ZDOT = -5697
243598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19613733
50 X = 5978265
97
Y = 8244995
81 feet Y = 2513074
72 meter
Z = -5769518
42 Z = -1758549
21
XDOT = -10371
065494 XDOT = -3161
100762
YDOT = 11586
515348 feet/sec YDOT = 3531
569878 meter/sec
ZDOT = -18687
619893 ZDOT = -5695
986543
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 07231
96302210
00020000 00000-0 20000-3 0 9049
2 25544 51
6337 134
6479 0008495 261
8497 98
1704 15
76194396 20848
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
96302210 = yrday
fracday
Element set: 904
Inclination: 51
6337 deg
RA of node: 134
6479 deg
Eccentricity:
0008495
Arg of perigee: 261
8497 deg
Mean anomaly: 98
1704 deg
Mean motion: 15
76194396 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2084
Checksum: 309
Coasting Arc #6 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2007/232/22:30:35
753
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 763278
24 A = 6720009
55 meter
Y = -5569405
09 meter E =
0003459
Z = 3679621
27 I = 51
88522
XDOT = 6017
083441 Wp = 81
16034
YDOT = -2052
018647 meter/sec RA = 128
70214 deg
ZDOT = -4350
072166 TA = 54
72505
MA = 54
69269
Ha = 184
665 n
mi
Hp = 184
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2504193
69 X = 807624
52
Y = -18272326
40 feet Y = -5560621
91 meter
Z = 12072248
25 Z = 3683436
70
XDOT = 19741
087405 XDOT = 6060
714047
YDOT = -6732
344643 feet/sec YDOT = -1984
488056 meter/sec
ZDOT = -14271
890307 ZDOT = -4320
735343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16247147
23 X = 4952130
48
Y = -8708990
08 feet Y = -2654500
18 meter
Z = 12086015
65 Z = 3683817
57
XDOT = 16416
979783 XDOT = 5003
895438
YDOT = 10956
866940 feet/sec YDOT = 3339
653043 meter/sec
ZDOT = -14160
873570 ZDOT = -4316
234264
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 07232
97743393
00020000 00000-0 20000-3 0 9053
2 25544 51
6338 129
4212 0008382 265
9477 94
0729 15
76199731 21003
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
97743393 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 129
4212 deg
Eccentricity:
0008382
Arg of perigee: 265
9477 deg
Mean anomaly: 94
0729 deg
Mean motion: 15
76199731 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2100
Checksum: 308
Coasting Arc #7 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2007/233/22:35:43
046
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4331355
63 A = 6714552
24 meter
Y = -693410
90 meter E =
0005303
Z = 5088152
57 I = 51
88494
XDOT = 3030
133263 Wp = 236
53434
YDOT = -6887
314795 meter/sec RA = 123
58817 deg
ZDOT = 1639
194877 TA = 197
75967
MA = 197
77821
Ha = 183
664 n
mi
Hp = 183
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14210484
34 X = -4347997
13
Y = -2274970
14 feet Y = -741939
94 meter
Z = 16693413
95 Z = 5067070
45
XDOT = 9941
382097 XDOT = 3098
960148
YDOT = -22596
177149 feet/sec YDOT = -6853
045413 meter/sec
ZDOT = 5377
935948 ZDOT = 1654
081950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7026258
10 X = -2141603
47
Y = -12665369
71 feet Y = -3860404
69 meter
Z = 16613353
99 Z = 5063750
30
XDOT = 22978
231760 XDOT = 7003
765040
YDOT = -5613
060296 feet/sec YDOT = -1710
860778 meter/sec
ZDOT = 5433
543885 ZDOT = 1656
144176
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 07233
99182694
00020000 00000-0 20000-3 0 9068
2 25544 51
6343 124
1934 0008548 270
2951 89
7234 15
76269487 21167
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
99182694 = yrday
fracday
Element set: 906
Inclination: 51
6343 deg
RA of node: 124
1934 deg
Eccentricity:
0008548
Arg of perigee: 270
2951 deg
Mean anomaly: 89
7234 deg
Mean motion: 15
76269487 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2116
Checksum: 317
Coasting Arc #8 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2007/234/22:40:11
614
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3797242
29 A = 6725399
57 meter
Y = 5462860
19 meter E =
0009024
Z = 942439
00 I = 51
93638
XDOT = -3456
653687 Wp = 17
67433
YDOT = -3433
679287 meter/sec RA = 118
43440 deg
ZDOT = 5969
548808 TA = 352
58729
MA = 352
60062
Ha = 184
792 n
mi
Hp = 184
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12458144
01 X = -3862624
76
Y = 17922769
66 feet Y = 5420031
65 meter
Z = 3091991
47 Z = 923833
70
XDOT = -11340
727320 XDOT = -3446
999671
YDOT = -11265
351990 feet/sec YDOT = -3472
279995 meter/sec
ZDOT = 19585
133885 ZDOT = 5952
779690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21742861
69 X = -6627224
24
Y = 2026420
81 feet Y = 617653
06 meter
Z = 3022088
72 Z = 921132
64
XDOT = 1371
303593 XDOT = 417
973335
YDOT = -14430
971712 feet/sec YDOT = -4398
560178 meter/sec
ZDOT = 19521
087391 ZDOT = 5950
027437
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 07235
00620712
00020000 00000-0 20000-3 0 9071
2 25544 51
6343 118
9665 0008493 275
1838 84
8357 15
76257415 21324
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
00620712 = yrday
fracday
Element set: 907
Inclination: 51
6343 deg
RA of node: 118
9665 deg
Eccentricity:
0008493
Arg of perigee: 275
1838 deg
Mean anomaly: 84
8357 deg
Mean motion: 15
76257415 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2132
Checksum: 297
Coasting Arc #9 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2007/235/22:45:10
534
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1342740
01 A = 6718107
70 meter
Y = 5109972
10 meter E =
0001708
Z = -4149609
42 I = 51
92452
XDOT = -5091
263978 Wp = 214
38661
YDOT = 4391
500490 meter/sec RA = 113
25020 deg
ZDOT = 3758
277443 TA = 93
92596
MA = 93
90644
Ha = 184
943 n
mi
Hp = 183
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4405315
00 X = 1305657
59
Y = 16765000
34 feet Y = 5124780
34 meter
Z = -13614204
14 Z = -4143176
16
XDOT = -16703
621974 XDOT = -5158
248835
YDOT = 14407
810006 feet/sec YDOT = 4334
192302 meter/sec
ZDOT = 12330
306571 ZDOT = 3733
381955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9358421
99 X = -2852447
02
Y = 14614145
22 feet Y = 4454391
46 meter
Z = -13589160
68 Z = -4141976
18
XDOT = -20883
564020 XDOT = -6365
310313
YDOT = -1988
481432 feet/sec YDOT = -606
089141 meter/sec
ZDOT = 12236
394849 ZDOT = 3729
653150
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 07235
95717239
00020000 00000-0 20000-3 0 9087
2 25544 51
6338 114
0666 0008481 278
6334 81
3869 15
76316582 21479
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
95717239 = yrday
fracday
Element set: 908
Inclination: 51
6338 deg
RA of node: 114
0666 deg
Eccentricity:
0008481
Arg of perigee: 278
6334 deg
Mean anomaly: 81
3869 deg
Mean motion: 15
76316582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2147
Checksum: 318
Coasting Arc #10 (Orbit 2162)
---------------------------------------
Vector Time (GMT): 2007/236/22:49:49
084
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4452472
68 A = 6715721
82 meter
Y = -1519388
89 meter E =
0006172
Z = -4796987
03 I = 51
92591
XDOT = -276
039287 Wp = 26
01209
YDOT = 7260
148069 meter/sec RA = 108
14639 deg
ZDOT = -2551
582303 TA = 219
07276
MA = 219
11736
Ha = 185
223 n
mi
Hp = 183
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14607849
99 X = 4492434
35
Y = -4984871
70 feet Y = -1469375
10 meter
Z = -15738146
41 Z = -4775260
26
XDOT = -905
640705 XDOT = -344
807882
YDOT = 23819
383427 feet/sec YDOT = 7256
676894 meter/sec
ZDOT = -8371
333016 ZDOT = -2553
089873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13861898
50 X = 4225106
66
Y = 6976265
85 feet Y = 2126365
83 meter
Z = -15655892
33 Z = -4771915
98
XDOT = -17068
634116 XDOT = -5202
519678
YDOT = 15086
975568 feet/sec YDOT = 4598
510153 meter/sec
ZDOT = -8376
153161 ZDOT = -2553
051484
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 07236
97152063
00020000 00000-0 20000-3 0 9099
2 25544 51
6333 108
8390 0008593 282
9667 77
0538 15
76297319 21639
Satellite: ISS
Catalog Number: 25544
Epoch time: 07236
97152063 = yrday
fracday
Element set: 909
Inclination: 51
6333 deg
RA of node: 108
8390 deg
Eccentricity:
0008593
Arg of perigee: 282
9667 deg
Mean anomaly: 77
0538 deg
Mean motion: 15
76297319 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2163
Checksum: 320
Coasting Arc #11 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2007/237/22:06:55
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1134486
09 A = 6725529
90 meter
Y = 6602170
33 meter E =
0011096
Z = -506682
65 I = 51
96743
XDOT = -4770
535533 Wp = 355
45807
YDOT = -356
148807 meter/sec RA = 103
14198 deg
ZDOT = 6042
648871 TA = 359
04727
MA = 359
04938
Ha = 185
466 n
mi
Hp = 183
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3722067
21 X = -1205766
89
Y = 21660663
81 feet Y = 6589085
34 meter
Z = -1662344
65 Z = -512366
75
XDOT = -15651
363296 XDOT = -4795
552038
YDOT = -1168
467214 feet/sec YDOT = -409
635746 meter/sec
ZDOT = 19824
963488 ZDOT = 6019
413246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19908830
82 X = -6068211
63
Y = 9306297
63 feet Y = 2836559
52 meter
Z = -1683095
47 Z = -513007
50
XDOT = -7352
796733 XDOT = -2241
132444
YDOT = -12161
338195 feet/sec YDOT = -3706
775882 meter/sec
ZDOT = 19736
744122 ZDOT = 6015
759608
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 07237
92245666
00020000 00000-0 20000-3 0 9109
2 25544 51
6341 103
9375 0008636 287
9281 72
0942 15
76298036 21789
Satellite: ISS
Catalog Number: 25544
Epoch time: 07237
92245666 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 103
9375 deg
Eccentricity:
0008636
Arg of perigee: 287
9281 deg
Mean anomaly: 72
0942 deg
Mean motion: 15
76298036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2178
Checksum: 310
Coasting Arc #12 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2007/238/22:11:33
219
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3476943
40 A = 6714957
16 meter
Y = 2966364
04 meter E =
0004081
Z = -4923150
31 I = 51
93676
XDOT = -2714
253989 Wp = 94
46984
YDOT = 6858
095421 meter/sec RA = 97
98135 deg
ZDOT = 2216
561121 TA = 196
96466
MA = 196
97831
Ha = 185
606 n
mi
Hp = 183
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11407294
63 X = 3467429
98
Y = 9732165
47 feet Y = 3005192
05 meter
Z = -16152067
94 Z = -4906282
72
XDOT = -8905
032771 XDOT = -2801
507947
YDOT = 22500
313060 feet/sec YDOT = 6827
255213 meter/sec
ZDOT = 7272
182154 ZDOT = 2203
163677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -871956
37 X = -265772
30
Y = 15038510
27 feet Y = 4583737
93 meter
Z = -16087685
20 Z = -4903526
45
XDOT = -22264
625953 XDOT = -6786
257990
YDOT = 6430
704133 feet/sec YDOT = 1960
078620 meter/sec
ZDOT = 7222
191009 ZDOT = 2201
323820
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 07238
93677333
00020000 00000-0 20000-3 0 9112
2 25544 51
6331 98
7099 0008581 291
7136 68
3115 15
76368430 21947
Satellite: ISS
Catalog Number: 25544
Epoch time: 07238
93677333 = yrday
fracday
Element set: 911
Inclination: 51
6331 deg
RA of node: 98
7099 deg
Eccentricity:
0008581
Arg of perigee: 291
7136 deg
Mean anomaly: 68
3115 deg
Mean motion: 15
76368430 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2194
Checksum: 311
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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