Date:
October 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4574 66 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 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
There are no maneuvers
Coasting Arc #1 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2007/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6084333
80 A = 6723682
77 meter
Y = -754509
16 meter E =
0015569
Z = 2744863
15 I = 51
72332
XDOT = 2947
568608 Wp = 84
15401
YDOT = -4905
221192 meter/sec RA = 166
38090 deg
ZDOT = 5161
943106 TA = 307
21316
MA = 307
35515
Ha = 188
076 n
mi
Hp = 180
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19961725
07 X = -6088778
83
Y = -2475423
75 feet Y = -822572
34 meter
Z = 9005456
54 Z = 2715294
24
XDOT = 9670
500682 XDOT = 2977
124273
YDOT = -16093
245379 feet/sec YDOT = -4872
094291 meter/sec
ZDOT = 16935
508878 ZDOT = 5176
334663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18595977
70 X = 5668054
00
Y = -7797542
09 feet Y = -2376690
83 meter
Z = 8892940
39 Z = 2710568
23
XDOT = -879
329885 XDOT = -268
019749
YDOT = 17367
739741 feet/sec YDOT = 5293
687073 meter/sec
ZDOT = 16989
588281 ZDOT = 5178
426508
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 07295
55796267
00020000 00000-0 20000-3 0 9009
2 25544 51
6382 167
0477 0002285 114
6382 245
5021 15
75864522 30873
Satellite: ISS
Catalog Number: 25544
Epoch time: 07295
55796267 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 167
0477 deg
Eccentricity:
0002285
Arg of perigee: 114
6382 deg
Mean anomaly: 245
5021 deg
Mean motion: 15
75864522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3087
Checksum: 304
Coasting Arc #2 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2007/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2907988
99 A = 6719245
67 meter
Y = 4436151
21 meter E =
0010050
Z = -4135190
21 I = 51
73649
XDOT = -6658
219688 Wp = 112
69262
YDOT = -863
897191 meter/sec RA = 161
18861 deg
ZDOT = 3758
907508 TA = 195
76645
MA = 195
79777
Ha = 187
864 n
mi
Hp = 180
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9540646
28 X = -2937290
14
Y = 14554301
88 feet Y = 4403468
34 meter
Z = -13566897
01 Z = -4149388
97
XDOT = -21844
552781 XDOT = -6666
325078
YDOT = -2834
308368 feet/sec YDOT = -938
398254 meter/sec
ZDOT = 12332
373715 ZDOT = 3726
541573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 681033
46 X = 207579
00
Y = -17347499
78 feet Y = -5287517
93 meter
Z = -13620307
40 Z = -4151469
70
XDOT = 19011
366609 XDOT = 5794
664542
YDOT = -8830
866444 feet/sec YDOT = -2691
648092 meter/sec
ZDOT = 12209
203355 ZDOT = 3721
365183
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 07296
50916219
00020000 00000-0 20000-3 0 9017
2 25544 51
6378 162
1486 0002165 121
1642 238
9735 15
75910150 31028
Satellite: ISS
Catalog Number: 25544
Epoch time: 07296
50916219 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 162
1486 deg
Eccentricity:
0002165
Arg of perigee: 121
1642 deg
Mean anomaly: 238
9735 deg
Mean motion: 15
75910150 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3102
Checksum: 277
Coasting Arc #3 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2007/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5499523
39 A = 6720603
08 meter
Y = 821120
87 meter E =
0007535
Z = -3781112
35 I = 51
76689
XDOT = -3686
598103 Wp = 89
28561
YDOT = 5273
840025 meter/sec RA = 156
09777 deg
ZDOT = -4223
880549 TA = 136
42818
MA = 136
36865
Ha = 187
835 n
mi
Hp = 180
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18043055
74 X = 5508301
21
Y = 2693966
10 feet Y = 882668
50 meter
Z = -12405224
25 Z = -3754373
67
XDOT = -12095
138132 XDOT = -3724
777570
YDOT = 17302
624753 feet/sec YDOT = 5232
400666 meter/sec
ZDOT = -13857
875817 ZDOT = -4241
883590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16816971
26 X = -5125812
84
Y = 7246617
93 feet Y = 2208769
14 meter
Z = -12303451
08 Z = -3750091
89
XDOT = 1634
149969 XDOT = 498
088911
YDOT = -19810
978212 feet/sec YDOT = -6038
386159 meter/sec
ZDOT = -13925
648329 ZDOT = -4244
537611
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 07297
52375843
00020000 00000-0 20000-3 0 9023
2 25544 51
6368 156
9230 0002086 127
0399 233
0956 15
75916800 31187
Satellite: ISS
Catalog Number: 25544
Epoch time: 07297
52375843 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 156
9230 deg
Eccentricity:
0002086
Arg of perigee: 127
0399 deg
Mean anomaly: 233
0956 deg
Mean motion: 15
75916800 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3118
Checksum: 302
Coasting Arc #4 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2007/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3465952
55 A = 6722025
64 meter
Y = -4792476
45 meter E =
0014606
Z = 3179935
73 I = 51
79869
XDOT = 5912
961872 Wp = 97
69526
YDOT = 1059
971339 meter/sec RA = 150
90602 deg
ZDOT = -4830
449987 TA = 45
24833
MA = 45
12956
Ha = 187
604 n
mi
Hp = 180
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11371235
41 X = 3503837
08
Y = -15723347
92 feet Y = -4753506
25 meter
Z = 10432860
00 Z = 3196866
10
XDOT = 19399
481206 XDOT = 5924
135871
YDOT = 3477
596256 feet/sec YDOT = 1126
155709 meter/sec
ZDOT = -15847
933027 ZDOT = -4801
696774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1005658
14 X = -306524
60
Y = 19343803
74 feet Y = 5895991
38 meter
Z = 10496625
21 Z = 3199371
36
XDOT = -16860
267602 XDOT = -5139
009565
YDOT = 7693
546406 feet/sec YDOT = 2344
992944 meter/sec
ZDOT = -15738
465337 ZDOT = -4797
084235
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 07298
53833550
00020000 00000-0 20000-3 0 9030
2 25544 51
6369 151
6968 0001962 126
3374 233
7972 15
76001628 31342
Satellite: ISS
Catalog Number: 25544
Epoch time: 07298
53833550 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 151
6968 deg
Eccentricity:
0001962
Arg of perigee: 126
3374 deg
Mean anomaly: 233
7972 deg
Mean motion: 15
76001628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3134
Checksum: 304
Coasting Arc #5 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2007/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4791909
48 A = 6717605
13 meter
Y = -1094588
41 meter E =
0010569
Z = 4573217
84 I = 51
80617
XDOT = 4195
076066 Wp = 117
52858
YDOT = -5718
773098 meter/sec RA = 145
81360 deg
ZDOT = 3016
836513 TA = 302
55013
MA = 302
65217
Ha = 187
830 n
mi
Hp = 180
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15721487
79 X = -4801530
14
Y = -3591169
32 feet Y = -1148228
02 meter
Z = 15003995
54 Z = 4549914
54
XDOT = 13763
372920 XDOT = 4244
056682
YDOT = -18762
378931 feet/sec YDOT = -5671
587500 meter/sec
ZDOT = 9897
757590 ZDOT = 3037
335938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15137851
05 X = 4614017
00
Y = -5793320
79 feet Y = -1765804
18 meter
Z = 14915242
46 Z = 4546165
90
XDOT = -1398
766539 XDOT = -426
344041
YDOT = 22111
842349 feet/sec YDOT = 6739
689548 meter/sec
ZDOT = 9974
990805 ZDOT = 3040
377197
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 07299
55289756
00020000 00000-0 20000-3 0 9047
2 25544 51
6353 146
4698 0002029 129
7697 230
3646 15
75953612 31504
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
55289756 = yrday
fracday
Element set: 904
Inclination: 51
6353 deg
RA of node: 146
4698 deg
Eccentricity:
0002029
Arg of perigee: 129
7697 deg
Mean anomaly: 230
3646 deg
Mean motion: 15
75953612 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3150
Checksum: 323
Coasting Arc #6 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2007/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3793084
16 A = 6724638
75 meter
Y = 5169316
97 meter E =
0006623
Z = -2025133
01 I = 51
85272
XDOT = -5063
648387 Wp = 57
63934
YDOT = -1530
101724 meter/sec RA = 140
63402 deg
ZDOT = 5595
210633 TA = 279
84225
MA = 279
91702
Ha = 187
536 n
mi
Hp = 180
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12444501
83 X = -3840768
25
Y = 16959701
34 feet Y = 5126634
00 meter
Z = -6644137
17 Z = -2043676
13
XDOT = -16613
019644 XDOT = -5073
343692
YDOT = -5020
018780 feet/sec YDOT = -1586
780693 meter/sec
ZDOT = 18356
990265 ZDOT = 5570
586964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 534943
76 X = 163050
86
Y = -21006605
35 feet Y = -6402813
31 meter
Z = -6714016
75 Z = -2046432
30
XDOT = 15066
357940 XDOT = 4592
225900
YDOT = -5436
187793 feet/sec YDOT = -1656
950039 meter/sec
ZDOT = 18263
155661 ZDOT = 5566
609845
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 07300
50402938
00020000 00000-0 20000-3 0 9055
2 25544 51
6341 141
5692 0001963 138
5239 221
6075 15
76007320 31659
Satellite: ISS
Catalog Number: 25544
Epoch time: 07300
50402938 = yrday
fracday
Element set: 905
Inclination: 51
6341 deg
RA of node: 141
5692 deg
Eccentricity:
0001963
Arg of perigee: 138
5239 deg
Mean anomaly: 221
6075 deg
Mean motion: 15
76007320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3165
Checksum: 266
Coasting Arc #7 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2007/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045200
11 A = 6715122
74 meter
Y = 1656084
80 meter E =
0014787
Z = -5110574
66 I = 51
84130
XDOT = -4449
809081 Wp = 85
28009
YDOT = 6080
191836 meter/sec RA = 135
52849 deg
ZDOT = -1554
534499 TA = 169
84388
MA = 169
81397
Ha = 187
504 n
mi
Hp = 180
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13271653
90 X = 4051207
88
Y = 5433349
10 feet Y = 1701354
42 meter
Z = -16766977
24 Z = -5090907
78
XDOT = -14599
111159 XDOT = -4509
916099
YDOT = 19948
135945 feet/sec YDOT = 6030
095572 meter/sec
ZDOT = -5100
178803 ZDOT = -1576
297975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14023958
03 X = -4274502
41
Y = 3390614
66 feet Y = 1033459
35 meter
Z = -16691972
28 Z = -5087713
15
XDOT = 432
736345 XDOT = 131
898038
YDOT = -23679
264852 feet/sec YDOT = -7217
439927 meter/sec
ZDOT = -5182
213059 ZDOT = -1579
538540
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 07301
51855399
00020000 00000-0 20000-3 0 9061
2 25544 51
6331 136
3421 0002016 141
0150 219
1160 15
76039774 31814
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
51855399 = yrday
fracday
Element set: 906
Inclination: 51
6331 deg
RA of node: 136
3421 deg
Eccentricity:
0002016
Arg of perigee: 141
0150 deg
Mean anomaly: 219
1160 deg
Mean motion: 15
76039774 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3181
Checksum: 257
Coasting Arc #8 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2007/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3922181
47 A = 6725986
52 meter
Y = -5414472
66 meter E =
0015137
Z = 662271
74 I = 51
89933
XDOT = 4224
289854 Wp = 129
84409
YDOT = 2314
310774 meter/sec RA = 130
37390 deg
ZDOT = -6016
119086 TA = 42
95989
MA = 42
84178
Ha = 187
327 n
mi
Hp = 180
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12868049
45 X = 3979218
14
Y = -17764017
92 feet Y = -5370293
75 meter
Z = 2172807
56 Z = 681464
32
XDOT = 13859
218681 XDOT = 4227
322857
YDOT = 7592
883116 feet/sec YDOT = 2361
566573 meter/sec
ZDOT = -19737
923512 ZDOT = -5995
589443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 308849
46 X = 94137
31
Y = 21925601
07 feet Y = 6682923
21 meter
Z = 2245161
84 Z = 684325
33
XDOT = -14139
818370 XDOT = -4309
816639
YDOT = 2238
489900 feet/sec YDOT = 682
291722 meter/sec
ZDOT = -19659
549793 ZDOT = -5992
230777
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 07302
53305905
00020000 00000-0 20000-3 0 9078
2 25544 51
6340 131
1155 0001795 142
8638 217
2651 15
76108132 31970
Satellite: ISS
Catalog Number: 25544
Epoch time: 07302
53305905 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 131
1155 deg
Eccentricity:
0001795
Arg of perigee: 142
8638 deg
Mean anomaly: 217
2651 deg
Mean motion: 15
76108132 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3197
Checksum: 270
Coasting Arc #9 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2007/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3358212
42 A = 6714235
90 meter
Y = -2427676
37 meter E =
0003862
Z = 5279998
15 I = 51
87631
XDOT = 4474
357703 Wp = 116
04127
YDOT = -6275
846477 meter/sec RA = 125
24548 deg
ZDOT = -41
387925 TA = 334
34025
MA = 334
35941
Ha = 187
542 n
mi
Hp = 180
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11017757
28 X = -3356465
94
Y = -7964817
50 feet Y = -2465220
41 meter
Z = 17322828
56 Z = 5263687
72
XDOT = 14679
651255 XDOT = 4544
403676
YDOT = -20590
047497 feet/sec YDOT = -6225
420028 meter/sec
ZDOT = -135
787157 ZDOT = -19
481385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13665413
58 X = 4165218
06
Y = -491731
11 feet Y = -149879
64 meter
Z = 17260485
35 Z = 5260995
94
XDOT = 933
788902 XDOT = 284
618857
YDOT = 24272
408315 feet/sec YDOT = 7398
230054 meter/sec
ZDOT = -53
196345 ZDOT = -16
214246
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 07303
54754888
00020000 00000-0 20000-3 0 9089
2 25544 51
6334 125
8880 0002037 147
2896 212
8394 15
76058352 32135
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
54754888 = yrday
fracday
Element set: 908
Inclination: 51
6334 deg
RA of node: 125
8880 deg
Eccentricity:
0002037
Arg of perigee: 147
2896 deg
Mean anomaly: 212
8394 deg
Mean motion: 15
76058352 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3213
Checksum: 306
Coasting Arc #10 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2007/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3843430
83 A = 6725927
19 meter
Y = 5462567
38 meter E =
0013256
Z = 744882
01 I = 51
93182
XDOT = -3519
224441 Wp = 61
45524
YDOT = -3304
913629 meter/sec RA = 120
11911 deg
ZDOT = 6004
154649 TA = 306
63795
MA = 306
75976
Ha = 187
286 n
mi
Hp = 180
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12609681
20 X = -3907846
98
Y = 17921809
00 feet Y = 5419227
76 meter
Z = 2443838
61 Z = 726054
19
XDOT = -11546
011947 XDOT = -3511
174348
YDOT = -10842
892485 feet/sec YDOT = -3344
222910 meter/sec
ZDOT = 19698
670108 ZDOT = 5987
077387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1342859
77 X = -409303
66
Y = -21879989
64 feet Y = -6669020
84 meter
Z = 2372851
97 Z = 723245
28
XDOT = 14280
663936 XDOT = 4352
746368
YDOT = 1279
814591 feet/sec YDOT = 390
087487 meter/sec
ZDOT = 19633
298711 ZDOT = 5984
229447
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 07304
56201700
00020000 00000-0 20000-3 0 9093
2 25544 51
6332 120
6605 0002020 152
6140 207
5131 15
76121674 32290
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
56201700 = yrday
fracday
Element set: 909
Inclination: 51
6332 deg
RA of node: 120
6605 deg
Eccentricity:
0002020
Arg of perigee: 152
6140 deg
Mean anomaly: 207
5131 deg
Mean motion: 15
76121674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3229
Checksum: 235
Coasting Arc #11 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2007/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2825318
75 A = 6714879
10 meter
Y = 3374675
67 meter E =
0015050
Z = -5084721
10 I = 51
90866
XDOT = -4313
545782 Wp = 108
98581
YDOT = 6144
302708 meter/sec RA = 114
96568 deg
ZDOT = 1680
325067 TA = 177
13120
MA = 177
12256
Ha = 187
236 n
mi
Hp = 180
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9269418
48 X = 2812073
58
Y = 11071770
56 feet Y = 3406196
10 meter
Z = -16682155
84 Z = -5071027
59
XDOT = -14152
053091 XDOT = -4390
094518
YDOT = 20158
473453 feet/sec YDOT = 6095
638132 meter/sec
ZDOT = 5512
877515 ZDOT = 1659
183896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14274465
59 X = -4350857
11
Y = -2548531
20 feet Y = -776792
31 meter
Z = -16629647
21 Z = -5068716
47
XDOT = -2131
534394 XDOT = -649
691683
YDOT = -23530
038323 feet/sec YDOT = -7171
955681 meter/sec
ZDOT = 5433
160509 ZDOT = 1656
027323
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 07305
51306454
00020000 00000-0 20000-3 0 9103
2 25544 51
6336 115
7600 0002120 153
6954 206
4318 15
76154974 32440
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
51306454 = yrday
fracday
Element set: 910
Inclination: 51
6336 deg
RA of node: 115
7600 deg
Eccentricity:
0002120
Arg of perigee: 153
6954 deg
Mean anomaly: 206
4318 deg
Mean motion: 15
76154974 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3244
Checksum: 265
Coasting Arc #12 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2007/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682224
45 A = 6723869
15 meter
Y = -5186121
77 meter E =
0008138
Z = -2172831
85 I = 51
95081
XDOT = 2999
634956 Wp = 142
23259
YDOT = 4440
619973 meter/sec RA = 109
86722 deg
ZDOT = -5532
620985 TA = 62
00481
MA = 61
92249
Ha = 187
129 n
mi
Hp = 180
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12080788
88 X = 3750498
12
Y = -17014835
20 feet Y = -5144563
28 meter
Z = -7128713
40 Z = -2154777
64
XDOT = 9841
322034 XDOT = 2976
633111
YDOT = 14568
963165 feet/sec YDOT = 4474
035064 meter/sec
ZDOT = -18151
643651 ZDOT = -5518
104398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1885218
27 X = 574614
53
Y = 20805340
36 feet Y = 6341467
74 meter
Z = -7060622
93 Z = -2152077
87
XDOT = -15517
121156 XDOT = -4729
618528
YDOT = -4715
841474 feet/sec YDOT = -1437
388481 meter/sec
ZDOT = -18095
873489 ZDOT = -5515
622240
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 07306
52749589
00020000 00000-0 20000-3 0 9116
2 25544 51
6338 110
5329 0001918 154
6860 205
4398 15
76211693 32601
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
52749589 = yrday
fracday
Element set: 911
Inclination: 51
6338 deg
RA of node: 110
5329 deg
Eccentricity:
0001918
Arg of perigee: 154
6860 deg
Mean anomaly: 205
4398 deg
Mean motion: 15
76211693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3260
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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