Date:
January 24th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
There are no maneuvers
Coasting Arc #1 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2007/017/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -361285
55 A = 6711404
87 meter
Y = -4202788
60 meter E =
0025560
Z = 5197985
53 I = 51
70991
XDOT = 7476
346615 Wp = 97
51688
YDOT = -1737
160566 meter/sec RA = 161
69921 deg
ZDOT = -884
537799 TA =
87248
MA =
86803
Ha = 193
670 n
mi
Hp = 170
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1185320
05 X = -339512
91
Y = -13788676
51 feet Y = -4206707
73 meter
Z = 17053758
29 Z = 5196282
69
XDOT = 24528
696242 XDOT = 7499
512978
YDOT = -5699
345688 feet/sec YDOT = -1653
426237 meter/sec
ZDOT = -2902
026901 ZDOT = -848
162380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12300800
52 X = 3749284
00
Y = -6360737
18 feet Y = -1938752
69 meter
Z = 17046835
02 Z = 5195875
31
XDOT = 14029
416168 XDOT = 4276
166048
YDOT = 19715
072155 feet/sec YDOT = 6009
153993 meter/sec
ZDOT = -2765
853244 ZDOT = -843
032069
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 07017
53576275
00020000 00000-0 20000-3 0 9004
2 25544 51
6299 162
4378 0023049 102
2819 258
0928 15
77130963 26987
Satellite: ISS
Catalog Number: 25544
Epoch time: 07017
53576275 = yrday
fracday
Element set: 900
Inclination: 51
6299 deg
RA of node: 162
4378 deg
Eccentricity:
0023049
Arg of perigee: 102
2819 deg
Mean anomaly: 258
0928 deg
Mean motion: 15
77130963 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2698
Checksum: 313
Coasting Arc #2 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2007/018/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6356630
15 A = 6721680
32 meter
Y = 1226755
06 meter E =
0034862
Z = 1779776
37 I = 51
77372
XDOT = 625
516525 Wp = 91
06272
YDOT = -5159
280356 meter/sec RA = 156
57094 deg
ZDOT = 5694
296898 TA = 288
65797
MA = 289
03614
Ha = 193
441 n
mi
Hp = 170
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20855085
80 X = -6378521
08
Y = 4024786
96 feet Y = 1155549
05 meter
Z = 5839161
33 Z = 1748843
61
XDOT = 2052
219569 XDOT = 655
500658
YDOT = -16926
772820 feet/sec YDOT = -5152
118604 meter/sec
ZDOT = 18682
076437 ZDOT = 5697
407713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11873987
51 X = -3619191
39
Y = -17648835
99 feet Y = -5379365
21 meter
Z = 5723314
39 Z = 1744466
23
XDOT = 15053
472793 XDOT = 4588
298507
YDOT = -3961
743602 feet/sec YDOT = -1207
539450 meter/sec
ZDOT = 18693
079918 ZDOT = 5697
650759
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 07018
54953816
00020000 00000-0 20000-3 0 9017
2 25544 51
6315 157
2065 0022938 106
4365 253
9324 15
77233373 27141
Satellite: ISS
Catalog Number: 25544
Epoch time: 07018
54953816 = yrday
fracday
Element set: 901
Inclination: 51
6315 deg
RA of node: 157
2065 deg
Eccentricity:
0022938
Arg of perigee: 106
4365 deg
Mean anomaly: 253
9324 deg
Mean motion: 15
77233373 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 290
Coasting Arc #3 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2007/019/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1421551
27 A = 6714195
18 meter
Y = 4809788
92 meter E =
0032716
Z = -4496094
58 I = 51
77510
XDOT = -6927
721850 Wp = 110
18227
YDOT = 922
503939 meter/sec RA = 151
38088 deg
ZDOT = 3184
857338 TA = 191
64042
MA = 191
71624
Ha = 193
344 n
mi
Hp = 170
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4663882
12 X = -1453388
78
Y = 15780147
37 feet Y = 4793714
83 meter
Z = -14750966
48 Z = -4503077
08
XDOT = -22728
746227 XDOT = -6952
993555
YDOT = 3026
587727 feet/sec YDOT = 844
892641 meter/sec
ZDOT = 10449
007014 ZDOT = 3151
142151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16279157
26 X = -4961887
13
Y = 2235827
34 feet Y = 681480
17 meter
Z = -14776534
60 Z = -4503887
75
XDOT = -11873
754889 XDOT = -3619
120490
YDOT = -18395
957774 feet/sec YDOT = -5607
087930 meter/sec
ZDOT = 10322
670416 ZDOT = 3146
349943
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 07019
49993211
00020000 00000-0 20000-3 0 9026
2 25544 51
6322 152
3021 0022828 109
5711 250
7921 15
77232874 27293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07019
49993211 = yrday
fracday
Element set: 902
Inclination: 51
6322 deg
RA of node: 152
3021 deg
Eccentricity:
0022828
Arg of perigee: 109
5711 deg
Mean anomaly: 250
7921 deg
Mean motion: 15
77232874 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2729
Checksum: 281
Coasting Arc #4 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2007/020/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5619715
68 A = 6717051
79 meter
Y = -265503
16 meter E =
0027664
Z = -3685159
27 I = 51
81004
XDOT = -2552
284848 Wp = 107
08200
YDOT = 5813
318072 meter/sec RA = 146
27971 deg
ZDOT = -4345
576128 TA = 117
11722
MA = 116
83479
Ha = 193
281 n
mi
Hp = 170
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18437387
39 X = 5640168
20
Y = -871073
36 feet Y = -202545
71 meter
Z = -12090417
56 Z = -3657809
87
XDOT = -8373
637954 XDOT = -2595
991125
YDOT = 19072
565852 feet/sec YDOT = 5784
532980 meter/sec
ZDOT = -14257
139527 ZDOT = -4358
080439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8608730
53 X = 2623941
07
Y = 16402900
89 feet Y = 4999604
19 meter
Z = -11987861
37 Z = -3653900
15
XDOT = -19594
953212 XDOT = -5972
541739
YDOT = -85
656400 feet/sec YDOT = -26
108071 meter/sec
ZDOT = -14303
288920 ZDOT = -4359
642463
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 07020
51365912
00020000 00000-0 20000-3 0 9033
2 25544 51
6327 147
0691 0022784 113
4049 246
9515 15
77274059 27456
Satellite: ISS
Catalog Number: 25544
Epoch time: 07020
51365912 = yrday
fracday
Element set: 903
Inclination: 51
6327 deg
RA of node: 147
0691 deg
Eccentricity:
0022784
Arg of perigee: 113
4049 deg
Mean anomaly: 246
9515 deg
Mean motion: 15
77274059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2745
Checksum: 291
Coasting Arc #5 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2007/021/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2887762
14 A = 6718996
44 meter
Y = -5288839
05 meter E =
0035671
Z = 2928135
17 I = 51
84058
XDOT = 5839
950206 Wp = 110
03814
YDOT = 376
713885 meter/sec RA = 141
08214 deg
ZDOT = -5041
882335 TA = 36
19278
MA = 35
95193
Ha = 193
146 n
mi
Hp = 170
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9474285
23 X = 2932464
12
Y = -17351834
16 feet Y = -5256296
69 meter
Z = 9606742
69 Z = 2942271
82
XDOT = 19159
941620 XDOT = 5859
795546
YDOT = 1235
937944 feet/sec YDOT = 442
130678 meter/sec
ZDOT = -16541
608710 ZDOT = -5013
464457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19725326
17 X = 6012279
42
Y = 866799
81 feet Y = 264200
58 meter
Z = 9659083
81 Z = 2944088
74
XDOT = 7386
108242 XDOT = 2251
285792
YDOT = 16408
825149 feet/sec YDOT = 5001
409905 meter/sec
ZDOT = -16434
951884 ZDOT = -5009
373334
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 07021
52736027
00020000 00000-0 20000-3 0 9045
2 25544 51
6332 141
8374 0022817 117
0848 243
2648 15
77307014 27619
Satellite: ISS
Catalog Number: 25544
Epoch time: 07021
52736027 = yrday
fracday
Element set: 904
Inclination: 51
6332 deg
RA of node: 141
8374 deg
Eccentricity:
0022817
Arg of perigee: 117
0848 deg
Mean anomaly: 243
2648 deg
Mean motion: 15
77307014 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2761
Checksum: 276
Coasting Arc #6 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2007/022/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4471161
27 A = 6712144
88 meter
Y = -1017609
94 meter E =
0029272
Z = 4885469
03 I = 51
84053
XDOT = 3918
946314 Wp = 121
24195
YDOT = -6255
703189 meter/sec RA = 135
97817 deg
ZDOT = 2258
803255 TA = 306
77708
MA = 307
04540
Ha = 193
039 n
mi
Hp = 170
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14669164
29 X = -4483182
04
Y = -3338615
29 feet Y = -1067676
30 meter
Z = 16028441
69 Z = 4863719
44
XDOT = 12857
435413 XDOT = 3977
634629
YDOT = -20523
960594 feet/sec YDOT = -6211
551267 meter/sec
ZDOT = 7410
771835 ZDOT = 2277
983397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3716978
60 X = -1132935
08
Y = -14667247
29 feet Y = -4470576
97 meter
Z = 15946711
35 Z = 4860557
62
XDOT = 23034
686064 XDOT = 7020
972312
YDOT = 2385
962281 feet/sec YDOT = 727
241303 meter/sec
ZDOT = 7481
908446 ZDOT = 2280
485694
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 07022
54103245
00020000 00000-0 20000-3 0 9059
2 25544 51
6340 136
6056 0022625 120
8030 239
5365 15
77404676 27772
Satellite: ISS
Catalog Number: 25544
Epoch time: 07022
54103245 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 136
6056 deg
Eccentricity:
0022625
Arg of perigee: 120
8030 deg
Mean anomaly: 239
5365 deg
Mean motion: 15
77404676 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2777
Checksum: 273
Coasting Arc #7 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2007/023/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3810715
16 A = 6722155
65 meter
Y = 5474052
66 meter E =
0025538
Z = -883472
26 I = 51
89414
XDOT = -4371
950809 Wp = 100
78900
YDOT = -2102
410045 meter/sec RA = 130
80614 deg
ZDOT = 5971
406456 TA = 249
60471
MA = 249
87919
Ha = 192
870 n
mi
Hp = 170
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12502346
32 X = -3867351
91
Y = 17959490
36 feet Y = 5431122
47 meter
Z = -2898531
04 Z = -902121
82
XDOT = -14343
670633 XDOT = -4377
123870
YDOT = -6897
670752 feet/sec YDOT = -2151
328664 meter/sec
ZDOT = 19591
228531 ZDOT = 5950
155338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21717056
18 X = -6619358
72
Y = -2610588
72 feet Y = -795707
44 meter
Z = -2967783
22 Z = -904580
33
XDOT = -871
959469 XDOT = -265
773246
YDOT = -14415
824097 feet/sec YDOT = -4393
943185 meter/sec
ZDOT = 19511
222338 ZDOT = 5947
020569
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 07023
49132918
00020000 00000-0 20000-3 0 9064
2 25544 51
6341 131
7005 0022596 123
8183 236
5137 15
77395802 27923
Satellite: ISS
Catalog Number: 25544
Epoch time: 07023
49132918 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 131
7005 deg
Eccentricity:
0022596
Arg of perigee: 123
8183 deg
Mean anomaly: 236
5137 deg
Mean motion: 15
77395802 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2792
Checksum: 289
Coasting Arc #8 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2007/024/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140906
44 A = 6710336
46 meter
Y = 2740769
70 meter E =
0035844
Z = -5287174
68 I = 51
87229
XDOT = -4692
792989 Wp = 113
87247
YDOT = 6071
314642 meter/sec RA = 125
66734 deg
ZDOT = 347
121247 TA = 159
49301
MA = 159
34875
Ha = 192
707 n
mi
Hp = 171
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10304811
17 X = 3135709
09
Y = 8992026
57 feet Y = 2775864
13 meter
Z = -17346373
61 Z = -5271928
94
XDOT = -15396
302458 XDOT = -4762
020741
YDOT = 19919
011294 feet/sec YDOT = 6018
450137 meter/sec
ZDOT = 1138
849235 ZDOT = 324
155981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2836459
51 X = -864552
86
Y = 13453392
12 feet Y = 4100593
92 meter
Z = -17288814
03 Z = -5269630
52
XDOT = -23903
691499 XDOT = -7285
845169
YDOT = -3633
813241 feet/sec YDOT = -1107
586276 meter/sec
ZDOT = 1053
476179 ZDOT = 321
099539
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 07024
50495174
00020000 00000-0 20000-3 0 9074
2 25544 51
6341 126
4679 0022495 127
6046 232
7165 15
77451261 28088
Satellite: ISS
Catalog Number: 25544
Epoch time: 07024
50495174 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 126
4679 deg
Eccentricity:
0022495
Arg of perigee: 127
6046 deg
Mean anomaly: 232
7165 deg
Mean motion: 15
77451261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2808
Checksum: 294
Coasting Arc #9 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2007/025/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271022
56 A = 6721371
60 meter
Y = -4961792
66 meter E =
0030896
Z = -1477201
88 I = 51
92506
XDOT = 2850
496532 Wp = 134
71862
YDOT = 4162
119283 meter/sec RA = 120
54007 deg
ZDOT = -5833
591128 TA = 61
51774
MA = 61
20689
Ha = 192
655 n
mi
Hp = 171
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14012541
20 X = 4333364
49
Y = -16278847
32 feet Y = -4913683
08 meter
Z = -4846462
87 Z = -1456302
27
XDOT = 9352
022742 XDOT = 2832
081481
YDOT = 13655
246992 feet/sec YDOT = 4193
892399 meter/sec
ZDOT = -19139
078505 ZDOT = -5819
788131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21112204
37 X = 6434999
89
Y = 4046584
17 feet Y = 1233398
86 meter
Z = -4768686
01 Z = -1453495
49
XDOT = -6821
406475 XDOT = -2079
164694
YDOT = 13469
873161 feet/sec YDOT = 4105
617340 meter/sec
ZDOT = -19086
748094 ZDOT = -5817
640819
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 07025
51854851
00020000 00000-0 20000-3 0 9088
2 25544 51
6337 121
2347 0022521 131
4925 228
8178 15
77479157 28249
Satellite: ISS
Catalog Number: 25544
Epoch time: 07025
51854851 = yrday
fracday
Element set: 908
Inclination: 51
6337 deg
RA of node: 121
2347 deg
Eccentricity:
0022521
Arg of perigee: 131
4925 deg
Mean anomaly: 228
8178 deg
Mean motion: 15
77479157 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2824
Checksum: 299
Coasting Arc #10 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2007/026/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1894090
62 A = 6712762
52 meter
Y = -4459504
41 meter E =
0026230
Z = 4620647
38 I = 51
91054
XDOT = 4972
048601 Wp = 117
64574
YDOT = -5140
787010 meter/sec RA = 115
36155 deg
ZDOT = -2922
812750 TA = 1
08593
MA = 1
08024
Ha = 192
495 n
mi
Hp = 171
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6214208
06 X = -1866529
07
Y = -14630919
99 feet Y = -4480531
39 meter
Z = 15159604
27 Z = 4611512
63
XDOT = 16312
495410 XDOT = 5043
362429
YDOT = -16866
099115 feet/sec YDOT = -5084
787865 meter/sec
ZDOT = -9589
280677 ZDOT = -2898
485903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9317545
14 X = 2839987
76
Y = -12919711
41 feet Y = -3937928
04 meter
Z = 15124754
97 Z = 4610025
31
XDOT = 21935
383238 XDOT = 6685
904811
YDOT = 4697
589201 feet/sec YDOT = 1431
825188 meter/sec
ZDOT = -9498
654426 ZDOT = -2895
189869
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 07026
53211848
00020000 00000-0 20000-3 0 9095
2 25544 51
6341 116
0018 0022370 134
7783 225
5206 15
77545108 28405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07026
53211848 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 116
0018 deg
Eccentricity:
0022370
Arg of perigee: 134
7783 deg
Mean anomaly: 225
5206 deg
Mean motion: 15
77545108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2840
Checksum: 272
Coasting Arc #11 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2007/027/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4311620
94 A = 6716742
80 meter
Y = 3777668
25 meter E =
0032114
Z = 3493935
04 I = 51
93527
XDOT = -1564
364904 Wp = 122
38455
YDOT = -6028
396379 meter/sec RA = 110
26691 deg
ZDOT = 4540
523422 TA = 278
99498
MA = 279
35832
Ha = 192
322 n
mi
Hp = 171
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14145738
01 X = -4370515
62
Y = 12393924
72 feet Y = 3729123
70 meter
Z = 11463041
48 Z = 3472846
72
XDOT = -5132
430789 XDOT = -1518
895031
YDOT = -19778
203342 feet/sec YDOT = -6045
636152 meter/sec
ZDOT = 14896
730388 ZDOT = 4533
033731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18030337
91 X = -5495647
00
Y = -5515013
64 feet Y = -1680976
16 meter
Z = 11384381
10 Z = 3469959
36
XDOT = 13634
195260 XDOT = 4155
702715
YDOT = -13563
353230 feet/sec YDOT = -4134
110065 meter/sec
ZDOT = 14867
858389 ZDOT = 4531
723237
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 07027
54566224
00020000 00000-0 20000-3 0 9100
2 25544 51
6341 110
7689 0022358 138
8108 221
4749 15
77587687 28564
Satellite: ISS
Catalog Number: 25544
Epoch time: 07027
54566224 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 110
7689 deg
Eccentricity:
0022358
Arg of perigee: 138
8108 deg
Mean anomaly: 221
4749 deg
Mean motion: 15
77587687 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2856
Checksum: 316
Coasting Arc #12 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2007/028/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 463808
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 882659
46 A = 6717876
41 meter
Y = 5932917
43 meter E =
0024201
Z = -3060183
09 I = 51
94794
XDOT = -4889
138558 Wp = 132
21609
YDOT = 3272
731336 meter/sec RA = 105
07523 deg
ZDOT = 4943
706011 TA = 192
53558
MA = 192
59588
Ha = 192
121 n
mi
Hp = 171
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2895864
36 X = 831116
71
Y = 19464952
20 feet Y = 5942499
96 meter
Z = -10039970
78 Z = -3056019
77
XDOT = -16040
480834 XDOT = -4949
386579
YDOT = 10737
307532 feet/sec YDOT = 3217
720876 meter/sec
ZDOT = 16219
507911 ZDOT = 4919
808962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14744134
15 X = -4494012
09
Y = 13046431
60 feet Y = 3976552
35 meter
Z = -10023599
08 Z = -3055193
00
XDOT = -16822
936450 XDOT = -5127
631030
YDOT = -6641
657946 feet/sec YDOT = -2024
377342 meter/sec
ZDOT = 16130
230146 ZDOT = 4916
494148
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 07028
49583766
00020000 00000-0 20000-3 0 9116
2 25544 51
6339 105
8633 0022214 142
1711 218
1020 15
77602432 28712
Satellite: ISS
Catalog Number: 25544
Epoch time: 07028
49583766 = yrday
fracday
Element set: 911
Inclination: 51
6339 deg
RA of node: 105
8633 deg
Eccentricity:
0022214
Arg of perigee: 142
1711 deg
Mean anomaly: 218
1020 deg
Mean motion: 15
77602432 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2871
Checksum: 270
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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