Date:
July 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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
202/01:19:27
227 -0
9 3
4 3
4
N/A 3
2 0
1 186
9
000/00:04:54
453 0
1 0
2 172
7
204/22:26:46
987 0
2 11
9 11
9
N/A -11
9 -0
0 187
4
000/00:21:33
973 -0
6 0
4 180
3
Coasting Arc #1 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2007/201/12:24:32
881
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4156344
58 A = 6705458
19 meter
Y = -825914
89 meter E =
0023118
Z = -5216698
40 I = 51
31422
XDOT = 2254
939753 Wp = 84
72265
YDOT = -7326
633228 meter/sec RA = 290
92193 deg
ZDOT = -636
959412 TA = 179
18974
MA = 179
18598
Ha = 185
099 n
mi
Hp = 172
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13636301
12 X = -4121458
66
Y = -2709694
54 feet Y = -872197
94 meter
Z = -17115152
24 Z = -5236805
06
XDOT = 7398
096303 XDOT = 2339
793856
YDOT = -24037
510589 feet/sec YDOT = -7300
942721 meter/sec
ZDOT = -2089
761850 ZDOT = -625
799591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5170650
84 X = 1576014
38
Y = 12803991
19 feet Y = 3902656
52 meter
Z = -17191328
29 Z = -5239916
86
XDOT = -23224
298633 XDOT = -7078
766223
YDOT = 6629
878396 feet/sec YDOT = 2020
786935 meter/sec
ZDOT = -2048
362320 ZDOT = -624
340835
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 07201
53395017
00020000 00000-0 20000-3 0 9002
2 25544 51
6345 291
4753 0008229 84
4384 275
7720 15
79200061 16041
Satellite: ISS
Catalog Number: 25544
Epoch time: 07201
53395017 = yrday
fracday
Element set: 900
Inclination: 51
6345 deg
RA of node: 291
4753 deg
Eccentricity:
0008229
Arg of perigee: 84
4384 deg
Mean anomaly: 275
7720 deg
Mean motion: 15
79200061 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1604
Checksum: 275
Coasting Arc #2 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2007/202/01:21:54
453
Vector Time (MET): N/A
Weight (LBS) : 508907
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3778777
25 A = 6707012
09 meter
Y = 1862417
34 meter E =
0013739
Z = 5207372
57 I = 51
30952
XDOT = -2796
078782 Wp = 80
46214
YDOT = 7175
349446 meter/sec RA = 288
10730 deg
ZDOT = -533
820994 TA = 14
64066
MA = 14
60091
Ha = 186
881 n
mi
Hp = 172
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12397563
15 X = 3732374
31
Y = 6110293
11 feet Y = 1904413
81 meter
Z = 17084555
68 Z = 5225617
19
XDOT = -9173
486816 XDOT = -2873
513602
YDOT = 23541
172724 feet/sec YDOT = 7143
649211 meter/sec
ZDOT = -1751
381214 ZDOT = -547
591640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5093159
90 X = 1552395
14
Y = 12756332
85 feet Y = 3888130
25 meter
Z = 17153803
98 Z = 5228479
45
XDOT = -21596
185010 XDOT = -6582
517191
YDOT = 11061
844508 feet/sec YDOT = 3371
650206 meter/sec
ZDOT = -1802
674987 ZDOT = -549
455336
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 07202
10348683
00020000 00000-0 20000-3 0 9014
2 25544 51
6351 288
5290 0011052 84
2621 275
9804 15
78633908 16135
Satellite: ISS
Catalog Number: 25544
Epoch time: 07202
10348683 = yrday
fracday
Element set: 901
Inclination: 51
6351 deg
RA of node: 288
5290 deg
Eccentricity:
0011052
Arg of perigee: 84
2621 deg
Mean anomaly: 275
9804 deg
Mean motion: 15
78633908 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 281
Coasting Arc #3 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2007/203/01:21:54
453
Vector Time (MET): N/A
Weight (LBS) : 508907
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2907110
04 A = 6717410
25 meter
Y = -5725448
47 meter E =
0024909
Z = 1939256
73 I = 51
33655
XDOT = 3717
127506 Wp = 76
22633
YDOT = 3799
376554 meter/sec RA = 282
93608 deg
ZDOT = 5590
936024 TA = 305
50538
MA = 305
73750
Ha = 187
013 n
mi
Hp = 172
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9537762
60 X = 2961496
28
Y = -18784279
76 feet Y = -5692635
65 meter
Z = 6362390
86 Z = 1953510
90
XDOT = 12195
300217 XDOT = 3647
206439
YDOT = 12465
146173 feet/sec YDOT = 3840
552024 meter/sec
ZDOT = 18342
965957 ZDOT = 5608
824302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19471959
88 X = 5935053
37
Y = -7998747
64 feet Y = -2438018
28 meter
Z = 6415677
18 Z = 1955498
40
XDOT = 414
806914 XDOT = 126
433147
YDOT = 15918
054192 feet/sec YDOT = 4851
822918 meter/sec
ZDOT = 18411
088310 ZDOT = 5611
699717
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 07203
11635127
00020000 00000-0 20000-3 0 9029
2 25544 51
6350 283
2908 0011103 87
3631 272
8805 15
78618001 16295
Satellite: ISS
Catalog Number: 25544
Epoch time: 07203
11635127 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 283
2908 deg
Eccentricity:
0011103
Arg of perigee: 87
3631 deg
Mean anomaly: 272
8805 deg
Mean motion: 15
78618001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1629
Checksum: 266
Coasting Arc #4 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2007/204/01:21:54
453
Vector Time (MET): N/A
Weight (LBS) : 508907
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2680815
07 A = 6711612
97 meter
Y = -4613174
72 meter E =
0018405
Z = -4089105
94 I = 51
31204
XDOT = 3792
739090 Wp = 98
49527
YDOT = -5533
475813 meter/sec RA = 277
69778 deg
ZDOT = 3767
908378 TA = 210
30814
MA = 210
41470
Ha = 186
916 n
mi
Hp = 172
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8795325
02 X = -2609166
56
Y = -15135087
65 feet Y = -4642751
99 meter
Z = -13415701
90 Z = -4101955
82
XDOT = 12443
369719 XDOT = 3836
029595
YDOT = -18154
448206 feet/sec YDOT = -5490
821680 meter/sec
ZDOT = 12361
904126 ZDOT = 3786
437924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3003687
63 X = 915523
99
Y = -17207127
45 feet Y = -5244732
45 meter
Z = -13464854
39 Z = -4104087
62
XDOT = 19878
007078 XDOT = 6058
816557
YDOT = -6227
745497 feet/sec YDOT = -1898
216827 meter/sec
ZDOT = 12431
391130 ZDOT = 3789
088016
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 07204
06589296
00020000 00000-0 20000-3 0 9030
2 25544 51
6348 278
3799 0010957 90
8930 269
3491 15
78655272 16442
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
06589296 = yrday
fracday
Element set: 903
Inclination: 51
6348 deg
RA of node: 278
3799 deg
Eccentricity:
0010957
Arg of perigee: 90
8930 deg
Mean anomaly: 269
3491 deg
Mean motion: 15
78655272 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 334
Coasting Arc #5 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2007/204/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3141393
65 A = 6718793
06 meter
Y = -4209247
18 meter E =
0009685
Z = -4200306
25 I = 51
30777
XDOT = 3213
898624 Wp = 118
30070
YDOT = -5991
939361 meter/sec RA = 273
09598 deg
ZDOT = 3602
807006 TA = 188
55114
MA = 188
56765
Ha = 187
416 n
mi
Hp = 180
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10306409
60 X = -3073687
49
Y = -13809866
06 feet Y = -4243996
87 meter
Z = -13780532
32 Z = -4215403
21
XDOT = 10544
286823 XDOT = 3263
160781
YDOT = -19658
593705 feet/sec YDOT = -5955
724795 meter/sec
ZDOT = 11820
232958 ZDOT = 3618
538915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11837303
38 X = 3608010
07
Y = -12458793
34 feet Y = -3797440
21 meter
Z = -13838145
37 Z = -4217866
71
XDOT = 20263
419500 XDOT = 6176
290264
YDOT = 6064
798573 feet/sec YDOT = 1848
550605 meter/sec
ZDOT = 11879
082265 ZDOT = 3620
744274
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 07204
95212718
00020000 00000-0 20000-3 0 9041
2 25544 51
6343 273
7963 0001882 156
0844 204
0408 15
75984216 16584
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
95212718 = yrday
fracday
Element set: 904
Inclination: 51
6343 deg
RA of node: 273
7963 deg
Eccentricity:
0001882
Arg of perigee: 156
0844 deg
Mean anomaly: 204
0408 deg
Mean motion: 15
75984216 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 297
Coasting Arc #6 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2007/205/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2768947
65 A = 6720535
75 meter
Y = 4903873
73 meter E =
0006288
Z = -3672428
19 I = 51
31415
XDOT = -3627
340297 Wp = 94
83036
YDOT = -5259
333744 meter/sec RA = 267
97284 deg
ZDOT = -4294
784708 TA = 129
57821
MA = 129
52266
Ha = 187
291 n
mi
Hp = 180
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9084473
91 X = -2805737
78
Y = 16088824
58 feet Y = 4872704
66 meter
Z = -12048648
90 Z = -3685968
28
XDOT = -11900
722759 XDOT = -3547
396867
YDOT = -17255
031969 feet/sec YDOT = -5299
449055 meter/sec
ZDOT = -14090
501012 ZDOT = -4312
212882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17506008
29 X = -5335831
33
Y = -5804633
25 feet Y = -1769252
21 meter
Z = -12099330
13 Z = -3687875
82
XDOT = 14278
927573 XDOT = 4352
217124
YDOT = -13600
545537 feet/sec YDOT = -4145
446280 meter/sec
ZDOT = -14157
062116 ZDOT = -4315
072533
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 07205
96667472
00020000 00000-0 20000-3 0 9055
2 25544 51
6348 268
5700 0001801 160
8213 199
3019 15
76010664 16744
Satellite: ISS
Catalog Number: 25544
Epoch time: 07205
96667472 = yrday
fracday
Element set: 905
Inclination: 51
6348 deg
RA of node: 268
5700 deg
Eccentricity:
0001801
Arg of perigee: 160
8213 deg
Mean anomaly: 199
3019 deg
Mean motion: 15
76010664 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 291
Coasting Arc #7 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2007/206/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3234254
11 A = 6721847
57 meter
Y = 4917930
56 meter E =
0013568
Z = 3232054
76 I = 51
32027
XDOT = -3159
097783 Wp = 99
56812
YDOT = 5198
549679 meter/sec RA = 262
74706 deg
ZDOT = -4734
295690 TA = 42
36721
MA = 42
26252
Ha = 187
242 n
mi
Hp = 180
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10611069
91 X = 3163320
09
Y = 16134942
79 feet Y = 4953700
66 meter
Z = 10603854
20 Z = 3247595
18
XDOT = -10364
494040 XDOT = -3193
995762
YDOT = 17055
609184 feet/sec YDOT = 5163
028538 meter/sec
ZDOT = -15532
466174 ZDOT = -4749
726375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13610252
30 X = -4148404
90
Y = 13653910
46 feet Y = 4161711
91 meter
Z = 10663239
14 Z = 3250155
29
XDOT = -17813
700418 XDOT = -5429
615887
YDOT = -5543
999082 feet/sec YDOT = -1689
810920 meter/sec
ZDOT = -15590
271099 ZDOT = -4751
914631
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 07206
98120840
00020000 00000-0 20000-3 0 9062
2 25544 51
6341 263
3438 0001827 162
1538 197
9691 15
76013768 16907
Satellite: ISS
Catalog Number: 25544
Epoch time: 07206
98120840 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 263
3438 deg
Eccentricity:
0001827
Arg of perigee: 162
1538 deg
Mean anomaly: 197
9691 deg
Mean motion: 15
76013768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 301
Coasting Arc #8 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2007/207/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2794646
62 A = 6717429
17 meter
Y = -4114871
25 meter E =
0009835
Z = 4510056
20 I = 51
31092
XDOT = 3815
727416 Wp = 121
88639
YDOT = 5955
815015 meter/sec RA = 257
62073 deg
ZDOT = 3059
535729 TA = 297
49196
MA = 297
59190
Ha = 187
131 n
mi
Hp = 180
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9168788
14 X = 2818543
24
Y = -13500233
75 feet Y = -4083487
10 meter
Z = 14796772
32 Z = 4523689
78
XDOT = 12518
790735 XDOT = 3733
982526
YDOT = 19540
075510 feet/sec YDOT = 5998
027039 meter/sec
ZDOT = 10037
846881 ZDOT = 3077
874791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15187384
36 X = 4629114
75
Y = 5843852
81 feet Y = 1781206
34 meter
Z = 14847902
17 Z = 4525640
58
XDOT = -15840
073234 XDOT = -4828
054322
YDOT = 15401
079179 feet/sec YDOT = 4694
248934 meter/sec
ZDOT = 10107
955105 ZDOT = 3080
904716
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 07207
99572579
00020000 00000-0 20000-3 0 9075
2 25544 51
6345 258
1171 0001717 166
9443 193
1766 15
76044794 17064
Satellite: ISS
Catalog Number: 25544
Epoch time: 07207
99572579 = yrday
fracday
Element set: 907
Inclination: 51
6345 deg
RA of node: 258
1171 deg
Eccentricity:
0001717
Arg of perigee: 166
9443 deg
Mean anomaly: 193
1766 deg
Mean motion: 15
76044794 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 321
Coasting Arc #9 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2007/208/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3431724
81 A = 6724394
00 meter
Y = -5407714
14 meter E =
0005559
Z = -2045738
93 I = 51
34228
XDOT = 3317
795455 Wp = 52
91204
YDOT = -4195
729561 meter/sec RA = 252
40472 deg
ZDOT = 5539
047946 TA = 284
15575
MA = 284
21751
Ha = 187
038 n
mi
Hp = 180
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11258939
66 X = -3361062
23
Y = -17741844
29 feet Y = -5445694
18 meter
Z = -6711741
91 Z = -2062239
25
XDOT = 10885
155692 XDOT = 3337
558892
YDOT = -13765
516934 feet/sec YDOT = -4158
518532 meter/sec
ZDOT = 18172
729482 ZDOT = 5555
212835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14531878
57 X = 4429316
59
Y = -15149597
43 feet Y = -4617597
30 meter
Z = -6774839
01 Z = -2064970
93
XDOT = 14845
678130 XDOT = 4524
962694
YDOT = 6106
257185 feet/sec YDOT = 1861
187190 meter/sec
ZDOT = 18233
433532 ZDOT = 5557
550541
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 07208
94682225
00020000 00000-0 20000-3 0 9082
2 25544 51
6344 253
2170 0001632 174
0175 186
1009 15
76081888 17210
Satellite: ISS
Catalog Number: 25544
Epoch time: 07208
94682225 = yrday
fracday
Element set: 908
Inclination: 51
6344 deg
RA of node: 253
2170 deg
Eccentricity:
0001632
Arg of perigee: 174
0175 deg
Mean anomaly: 186
1009 deg
Mean motion: 15
76081888 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1721
Checksum: 284
Coasting Arc #10 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2007/209/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3067976
28 A = 6714911
08 meter
Y = 3178622
55 meter E =
0013521
Z = -5068946
70 I = 51
31985
XDOT = -4024
223030 Wp = 84
51834
YDOT = -6369
597178 meter/sec RA = 247
26277 deg
ZDOT = -1560
869857 TA = 170
43270
MA = 170
40692
Ha = 186
921 n
mi
Hp = 180
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10065538
97 X = -3078668
58
Y = 10428551
69 feet Y = 3144255
70 meter
Z = -16630402
55 Z = -5083876
10
XDOT = -13202
831463 XDOT = -3945
115904
YDOT = -20897
628537 feet/sec YDOT = -6414
155756 meter/sec
ZDOT = -5120
964099 ZDOT = -1580
227947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12637973
20 X = -3852054
23
Y = -6962811
14 feet Y = -2122264
84 meter
Z = -16686549
93 Z = -5086060
42
XDOT = 16310
563442 XDOT = 4971
459737
YDOT = -17172
804440 feet/sec YDOT = -5234
270793 meter/sec
ZDOT = -5195
009132 ZDOT = -1583
438783
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 07209
96131084
00020000 00000-0 20000-3 0 9098
2 25544 51
6338 247
9901 0001534 180
0487 180
0677 15
76115269 17371
Satellite: ISS
Catalog Number: 25544
Epoch time: 07209
96131084 = yrday
fracday
Element set: 909
Inclination: 51
6338 deg
RA of node: 247
9901 deg
Eccentricity:
0001534
Arg of perigee: 180
0487 deg
Mean anomaly: 180
0677 deg
Mean motion: 15
76115269 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1737
Checksum: 301
Coasting Arc #11 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2007/210/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3583119
66 A = 6726077
73 meter
Y = 5645735
43 meter E =
0014468
Z = 652375
12 I = 51
36930
XDOT = -3765
518038 Wp = 133
65251
YDOT = 3088
401058 meter/sec RA = 242
07015 deg
ZDOT = -5973
085324 TA = 39
20720
MA = 39
10248
Ha = 186
976 n
mi
Hp = 180
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11755641
92 X = 3516552
86
Y = 18522754
03 feet Y = 5685431
61 meter
Z = 2140338
31 Z = 669620
53
XDOT = -12354
061804 XDOT = -3770
757665
YDOT = 10132
549403 feet/sec YDOT = 3046
264384 meter/sec
ZDOT = -19596
736626 ZDOT = -5991
390106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14610728
47 X = -4453350
04
Y = 16356263
93 feet Y = 4985389
25 meter
Z = 2206314
92 Z = 672484
79
XDOT = -11898
965791 XDOT = -3626
804773
YDOT = -7945
258034 feet/sec YDOT = -2421
714649 meter/sec
ZDOT = -19665
675514 ZDOT = -5994
097897
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 07210
97578648
00020000 00000-0 20000-3 0 9104
2 25544 51
6335 242
7633 0001722 181
7023 178
4135 15
76078461 17536
Satellite: ISS
Catalog Number: 25544
Epoch time: 07210
97578648 = yrday
fracday
Element set: 910
Inclination: 51
6335 deg
RA of node: 242
7633 deg
Eccentricity:
0001722
Arg of perigee: 181
7023 deg
Mean anomaly: 178
4135 deg
Mean motion: 15
76078461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1753
Checksum: 292
Coasting Arc #12 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2007/211/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3555635
38 A = 6713983
52 meter
Y = -2223164
04 meter E =
0002561
Z = 5241492
56 I = 51
34348
XDOT = 4159
915685 Wp = 123
83632
YDOT = 6487
228972 meter/sec RA = 236
90323 deg
ZDOT = -71
776294 TA = 326
83901
MA = 326
85506
Ha = 186
690 n
mi
Hp = 180
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11665470
41 X = 3554769
28
Y = -7293845
27 feet Y = -2183408
28 meter
Z = 17196497
91 Z = 5258763
09
XDOT = 13648
017340 XDOT = 4087
414029
YDOT = 21283
559619 feet/sec YDOT = 6533
342120 meter/sec
ZDOT = -235
486529 ZDOT = -51
743382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10332171
86 X = 3149245
98
Y = 8960212
72 feet Y = 2731072
84 meter
Z = 17261625
99 Z = 5261343
60
XDOT = -15764
314860 XDOT = -4804
963169
YDOT = 18475
385943 feet/sec YDOT = 5631
297635 meter/sec
ZDOT = -158
836105 ZDOT = -48
413245
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 07211
99024421
00020000 00000-0 20000-3 0 9113
2 25544 51
6331 237
5357 0001531 189
1726 170
9410 15
76147724 17696
Satellite: ISS
Catalog Number: 25544
Epoch time: 07211
99024421 = yrday
fracday
Element set: 911
Inclination: 51
6331 deg
RA of node: 237
5357 deg
Eccentricity:
0001531
Arg of perigee: 189
1726 deg
Mean anomaly: 170
9410 deg
Mean motion: 15
76147724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1769
Checksum: 281
Coasting Arc #13 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2007/212/22:37:33
973
Vector Time (MET): N/A
Weight (LBS) : 508072
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3622290
95 A = 6725711
02 meter
Y = -5605726
33 meter E =
0012289
Z = 785550
13 I = 51
39948
XDOT = 4449
288139 Wp = 57
63463
YDOT = -2032
292311 meter/sec RA = 231
73894 deg
ZDOT = 5952
689024 TA = 310
96747
MA = 311
07374
Ha = 186
662 n
mi
Hp = 180
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11884156
66 X = -3563153
65
Y = -18391490
59 feet Y = -5645902
23 meter
Z = 2577264
21 Z = 768096
69
XDOT = 14597
402032 XDOT = 4442
766420
YDOT = -6667
625691 feet/sec YDOT = -1982
574747 meter/sec
ZDOT = 19529
819633 ZDOT = 5974
287197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13867089
73 X = 4226688
95
Y = -16956524
81 feet Y = -5168348
76 meter
Z = 2510475
08 Z = 765192
81
XDOT = 9545
491543 XDOT = 2909
465822
YDOT = 10740
334700 feet/sec YDOT = 3273
654016 meter/sec
ZDOT = 19611
360401 ZDOT = 5977
542650
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 07213
00468749
00020000 00000-0 20000-3 0 9123
2 25544 51
6324 232
3074 0001549 196
7595 163
3518 15
76188221 17854
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
00468749 = yrday
fracday
Element set: 912
Inclination: 51
6324 deg
RA of node: 232
3074 deg
Eccentricity:
0001549
Arg of perigee: 196
7595 deg
Mean anomaly: 163
3518 deg
Mean motion: 15
76188221 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1785
Checksum: 299
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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