Date:
January 4th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 2476)
---------------------------------------
Vector Time (GMT): 2007/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3433436
04 A = 6724446
52 meter
Y = 5740936
38 meter E =
0025655
Z = -752118
67 I = 51
39644
XDOT = -4478
400757 Wp = 74
10782
YDOT = 1919
901198 meter/sec RA = 233
96771 deg
ZDOT = -5950
696174 TA = 114
11219
MA = 113
84364
Ha = 194
301 n
mi
Hp = 172
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11264553
92 X = 3372638
50
Y = 18835093
11 feet Y = 5778991
17 meter
Z = -2467580
93 Z = -735585
93
XDOT = -14692
915869 XDOT = -4470
629546
YDOT = 6298
888445 feet/sec YDOT = 1869
865743 meter/sec
ZDOT = -19523
281411 ZDOT = -5972
432710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16078211
79 X = -4900638
95
Y = 14948146
89 feet Y = 4556195
17 meter
Z = -2404968
53 Z = -733034
41
XDOT = -8103
973281 XDOT = -2470
091056
YDOT = -11783
345246 feet/sec YDOT = -3591
563631 meter/sec
ZDOT = -19604
439941 ZDOT = -5975
433294
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 07003
53039150
00020000 00000-0 20000-3 0 9005
2 25544 51
6339 234
6827 0023528 49
6103 310
7110 15
76633068 24772
Satellite: ISS
Catalog Number: 25544
Epoch time: 07003
53039150 = yrday
fracday
Element set: 900
Inclination: 51
6339 deg
RA of node: 234
6827 deg
Eccentricity:
0023528
Arg of perigee: 49
6103 deg
Mean anomaly: 310
7110 deg
Mean motion: 15
76633068 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2477
Checksum: 269
Coasting Arc #2 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2007/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4364290
78 A = 6713452
43 meter
Y = -1052219
70 meter E =
0029087
Z = 4976362
36 I = 51
37770
XDOT = 3719
308852 Wp = 53
47271
YDOT = 6501
702570 meter/sec RA = 228
76995 deg
ZDOT = -1862
485466 TA = 54
65339
MA = 54
38186
Ha = 194
095 n
mi
Hp = 171
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14318539
29 X = 4351558
69
Y = -3452164
38 feet Y = -1003487
77 meter
Z = 16326648
15 Z = 4997532
58
XDOT = 12202
456862 XDOT = 3655
376912
YDOT = 21331
045176 feet/sec YDOT = 6542
936787 meter/sec
ZDOT = -6110
516620 ZDOT = -1844
571653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6561436
48 X = 1999925
84
Y = 13087959
34 feet Y = 3989210
01 meter
Z = 16405801
35 Z = 5000488
25
XDOT = -17081
120802 XDOT = -5206
325621
YDOT = 16238
558168 feet/sec YDOT = 4949
512530 meter/sec
ZDOT = -6042
622911 ZDOT = -1841
791463
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 07004
54449439
00020000 00000-0 20000-3 0 9013
2 25544 51
6334 229
4525 0023546 52
9257 307
4055 15
76732286 24932
Satellite: ISS
Catalog Number: 25544
Epoch time: 07004
54449439 = yrday
fracday
Element set: 901
Inclination: 51
6334 deg
RA of node: 229
4525 deg
Eccentricity:
0023546
Arg of perigee: 52
9257 deg
Mean anomaly: 307
4055 deg
Mean motion: 15
76732286 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2493
Checksum: 297
Coasting Arc #3 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2007/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2956209
05 A = 6721848
82 meter
Y = -5500076
02 meter E =
0037004
Z = 2433500
36 I = 51
42457
XDOT = 5546
950188 Wp = 63
44954
YDOT = -597
795804 meter/sec RA = 223
63293 deg
ZDOT = 5341
435815 TA = 324
22666
MA = 324
47398
Ha = 194
215 n
mi
Hp = 171
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9698848
60 X = -2906307
96
Y = -18044868
83 feet Y = -5532855
31 meter
Z = 7983925
05 Z = 2419259
86
XDOT = 18198
655471 XDOT = 5527
275412
YDOT = -1961
272324 feet/sec YDOT = -535
877463 meter/sec
ZDOT = 17524
395720 ZDOT = 5368
334439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15158373
58 X = 4620272
27
Y = -13811894
69 feet Y = -4209865
50 meter
Z = 7929898
49 Z = 2417033
06
XDOT = 5266
940429 XDOT = 1605
363443
YDOT = 15986
575528 feet/sec YDOT = 4872
708221 meter/sec
ZDOT = 17625
068806 ZDOT = 5372
120972
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 07005
55857810
00020000 00000-0 20000-3 0 9022
2 25544 51
6323 224
2225 0023501 56
7058 303
6354 15
76741962 25091
Satellite: ISS
Catalog Number: 25544
Epoch time: 07005
55857810 = yrday
fracday
Element set: 902
Inclination: 51
6323 deg
RA of node: 224
2225 deg
Eccentricity:
0023501
Arg of perigee: 56
7058 deg
Mean anomaly: 303
6354 deg
Mean motion: 15
76741962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2509
Checksum: 275
Coasting Arc #4 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2007/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5288829
31 A = 6716674
95 meter
Y = 38476
81 meter E =
0029356
Z = -4158399
17 I = 51
42840
XDOT = -2924
818454 Wp = 72
82307
YDOT = -6078
523895 meter/sec RA = 218
41300 deg
ZDOT = 3693
615085 TA = 234
93979
MA = 235
21550
Ha = 194
156 n
mi
Hp = 171
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17351802
20 X = -5268666
19
Y = 126236
25 feet Y = -20552
62 meter
Z = -13643041
90 Z = -4184042
75
XDOT = -9595
861071 XDOT = -2874
572675
YDOT = -19942
663697 feet/sec YDOT = -6110
950315 meter/sec
ZDOT = 12118
159728 ZDOT = 3679
528001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4581295
56 X = -1396378
89
Y = -16657809
22 feet Y = -5077300
25 meter
Z = -13739093
51 Z = -4187675
70
XDOT = 15558
012124 XDOT = 4742
082095
YDOT = -14149
054518 feet/sec YDOT = -4312
631817 meter/sec
ZDOT = 12064
621549 ZDOT = 3677
296648
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 07006
50926156
00020000 00000-0 20000-3 0 9039
2 25544 51
6314 219
3185 0023468 60
3514 299
9983 15
76767959 25247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07006
50926156 = yrday
fracday
Element set: 903
Inclination: 51
6314 deg
RA of node: 219
3185 deg
Eccentricity:
0023468
Arg of perigee: 60
3514 deg
Mean anomaly: 299
9983 deg
Mean motion: 15
76767959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2524
Checksum: 318
Coasting Arc #5 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2007/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2009599
67 A = 6717527
06 meter
Y = 5078762
67 meter E =
0030176
Z = -3943633
05 I = 51
45363
XDOT = -6545
704993 Wp = 66
39820
YDOT = -497
137905 meter/sec RA = 213
29268 deg
ZDOT = -3988
029840 TA = 162
06033
MA = 161
95360
Ha = 194
197 n
mi
Hp = 171
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6593174
77 X = 1971815
93
Y = 16662607
17 feet Y = 5101024
22 meter
Z = -12938428
63 Z = -3933961
94
XDOT = -21475
410081 XDOT = -6520
286717
YDOT = -1631
029873 feet/sec YDOT = -570
193145 meter/sec
ZDOT = -13084
087402 ZDOT = -4019
766517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14190822
11 X = -4325362
58
Y = 10985716
26 feet Y = 3348446
32 meter
Z = -12901549
24 Z = -3932392
21
XDOT = -3509
993263 XDOT = -1069
845947
YDOT = -19992
340579 feet/sec YDOT = -6093
665408 meter/sec
ZDOT = -13203
040722 ZDOT = -4024
286812
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 07007
52330299
00020000 00000-0 20000-3 0 9040
2 25544 51
6305 214
0879 0023449 64
2001 296
1579 15
76794011 25409
Satellite: ISS
Catalog Number: 25544
Epoch time: 07007
52330299 = yrday
fracday
Element set: 904
Inclination: 51
6305 deg
RA of node: 214
0879 deg
Eccentricity:
0023449
Arg of perigee: 64
2001 deg
Mean anomaly: 296
1579 deg
Mean motion: 15
76794011 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2540
Checksum: 281
Coasting Arc #6 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2007/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6091284
98 A = 6720755
53 meter
Y = 814612
26 meter E =
0035533
Z = 2699266
94 I = 51
49091
XDOT = 1581
548773 Wp = 79
92402
YDOT = 5502
078497 meter/sec RA = 208
07330 deg
ZDOT = -5165
873569 TA = 69
15092
MA = 68
77076
Ha = 194
014 n
mi
Hp = 171
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19984530
76 X = 6068610
84
Y = 2672612
40 feet Y = 882601
42 meter
Z = 8855862
67 Z = 2728802
86
XDOT = 5188
808311 XDOT = 1545
000640
YDOT = 18051
438639 feet/sec YDOT = 5519
560279 meter/sec
ZDOT = -16948
404097 ZDOT = -5158
278917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3248368
54 X = 990102
73
Y = 19849394
06 feet Y = 6050095
31 meter
Z = 8966620
75 Z = 2733026
00
XDOT = -14283
447813 XDOT = -4353
594893
YDOT = 10073
556046 feet/sec YDOT = 3070
419883 meter/sec
ZDOT = -16919
241527 ZDOT = -5156
984817
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 07008
53732122
00020000 00000-0 20000-3 0 9054
2 25544 51
6313 208
8566 0023349 67
5112 292
8522 15
76876557 25564
Satellite: ISS
Catalog Number: 25544
Epoch time: 07008
53732122 = yrday
fracday
Element set: 905
Inclination: 51
6313 deg
RA of node: 208
8566 deg
Eccentricity:
0023349
Arg of perigee: 67
5112 deg
Mean anomaly: 292
8522 deg
Mean motion: 15
76876557 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2556
Checksum: 300
Coasting Arc #7 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2007/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -674988
38 A = 6713619
43 meter
Y = -4516480
62 meter E =
0027887
Z = 4896319
41 I = 51
49093
XDOT = 7317
124439 Wp = 82
27335
YDOT = 1241
986766 meter/sec RA = 202
94545 deg
ZDOT = 2147
681116 TA = 346
88294
MA = 346
95531
Ha = 194
226 n
mi
Hp = 171
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2214528
81 X = -648219
39
Y = -14817849
80 feet Y = -4523879
36 meter
Z = 16064040
07 Z = 4893105
09
XDOT = 24006
313775 XDOT = 7292
259647
YDOT = 4074
759731 feet/sec YDOT = 1323
671759 meter/sec
ZDOT = 7046
197886 ZDOT = 2183
166888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13390828
51 X = 4081524
53
Y = -6750118
68 feet Y = -2057436
17 meter
Z = 16051411
26 Z = 4892470
15
XDOT = 3003
149879 XDOT = 915
360083
YDOT = 23081
694774 feet/sec YDOT = 7035
300567 meter/sec
ZDOT = 7179
310677 ZDOT = 2188
253895
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 07009
55132222
00020000 00000-0 20000-3 0 9063
2 25544 51
6302 203
6257 0023452 71
7942 288
5772 15
76828159 25727
Satellite: ISS
Catalog Number: 25544
Epoch time: 07009
55132222 = yrday
fracday
Element set: 906
Inclination: 51
6302 deg
RA of node: 203
6257 deg
Eccentricity:
0023452
Arg of perigee: 71
7942 deg
Mean anomaly: 288
5772 deg
Mean motion: 15
76828159 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2572
Checksum: 292
Coasting Arc #8 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2007/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6523325
11 A = 6723535
34 meter
Y = -1286545
86 meter E =
0031758
Z = -961762
12 I = 51
55152
XDOT = 117
779554 Wp = 65
12171
YDOT = -4911
404042 meter/sec RA = 197
75157 deg
ZDOT = 5936
591411 TA = 284
34576
MA = 284
69812
Ha = 194
056 n
mi
Hp = 170
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21401985
26 X = -6503781
93
Y = -4220951
00 feet Y = -1359383
98 meter
Z = -3155387
54 Z = -993404
72
XDOT = 386
415859 XDOT = 143
852227
YDOT = -16113
530323 feet/sec YDOT = -4909
941572 meter/sec
ZDOT = 19477
005943 ZDOT = 5937
226590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2933732
97 X = -894201
81
Y = -21598408
57 feet Y = -6583194
93 meter
Z = -3274115
00 Z = -997950
25
XDOT = 13759
981448 XDOT = 4194
042345
YDOT = -4742
507850 feet/sec YDOT = -1445
516393 meter/sec
ZDOT = 19478
746916 ZDOT = 5937
122060
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 07010
50192467
00020000 00000-0 20000-3 0 9078
2 25544 51
6298 198
7215 0023344 75
6085 284
7668 15
76885742 25879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07010
50192467 = yrday
fracday
Element set: 907
Inclination: 51
6298 deg
RA of node: 198
7215 deg
Eccentricity:
0023344
Arg of perigee: 75
6085 deg
Mean anomaly: 284
7668 deg
Mean motion: 15
76885742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2587
Checksum: 329
Coasting Arc #9 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2007/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -972476
27 A = 6711810
40 meter
Y = 4076354
69 meter E =
0038339
Z = -5275406
09 I = 51
53947
XDOT = -7482
223253 Wp = 84
08620
YDOT = -1717
656444 meter/sec RA = 192
59557 deg
ZDOT = 56
258046 TA = 186
42534
MA = 186
47464
Ha = 194
091 n
mi
Hp = 170
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3190538
93 X = -992359
58
Y = 13373867
09 feet Y = 4065369
13 meter
Z = -17307762
76 Z = -5280178
35
XDOT = -24547
976551 XDOT = -7462
733372
YDOT = -5635
355788 feet/sec YDOT = -1801
217860 meter/sec
ZDOT = 184
573643 ZDOT = 19
956877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13629063
03 X = -4154138
41
Y = 1639376
39 feet Y = 499681
93 meter
Z = -17325114
64 Z = -5280694
94
XDOT = -2931
624635 XDOT = -893
559189
YDOT = -24007
802619 feet/sec YDOT = -7317
578238 meter/sec
ZDOT = 48
325989 ZDOT = 14
729761
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 07011
51588088
00020000 00000-0 20000-3 0 9089
2 25544 51
6295 193
4901 0023429 79
6401 280
7403 15
76921554 26034
Satellite: ISS
Catalog Number: 25544
Epoch time: 07011
51588088 = yrday
fracday
Element set: 908
Inclination: 51
6295 deg
RA of node: 193
4901 deg
Eccentricity:
0023429
Arg of perigee: 79
6401 deg
Mean anomaly: 280
7403 deg
Mean motion: 15
76921554 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2603
Checksum: 295
Coasting Arc #10 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2007/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6416966
43 A = 6723170
96 meter
Y = 1696755
00 meter E =
0029639
Z = -1074278
29 I = 51
60701
XDOT = -2140
804632 Wp = 99
56453
YDOT = 4444
102341 meter/sec RA = 187
44263 deg
ZDOT = -5911
181822 TA = 92
19760
MA = 91
85819
Ha = 194
007 n
mi
Hp = 170
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21053039
48 X = 6402734
78
Y = 5566781
51 feet Y = 1768433
61 meter
Z = -3524535
07 Z = -1043139
24
XDOT = -7023
637244 XDOT = -2161
624794
YDOT = 14580
388258 feet/sec YDOT = 4420
046774 meter/sec
ZDOT = -19393
641149 ZDOT = -5921
631987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2306260
33 X = 702948
15
Y = 21672820
15 feet Y = 6605875
58 meter
Z = -3407624
53 Z = -1038643
96
XDOT = -14507
328701 XDOT = -4421
833788
YDOT = -1435
418105 feet/sec YDOT = -437
515438 meter/sec
ZDOT = -19432
225148 ZDOT = -5922
942225
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 07012
52981334
00020000 00000-0 20000-3 0 9093
2 25544 51
6297 188
2586 0023436 82
8687 277
5142 15
77001233 26192
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
52981334 = yrday
fracday
Element set: 909
Inclination: 51
6297 deg
RA of node: 188
2586 deg
Eccentricity:
0023436
Arg of perigee: 82
8687 deg
Mean anomaly: 277
5142 deg
Mean motion: 15
77001233 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2619
Checksum: 307
Coasting Arc #11 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2007/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716478
04 A = 6713343
54 meter
Y = -3737639
88 meter E =
0029347
Z = 4847047
90 I = 51
60145
XDOT = 7061
448995 Wp = 81
22222
YDOT = 2112
057961 meter/sec RA = 182
25260 deg
ZDOT = -2312
631557 TA = 31
32254
MA = 31
14804
Ha = 193
974 n
mi
Hp = 170
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8912329
53 X = 2734524
99
Y = -12262598
04 feet Y = -3707162
32 meter
Z = 15902388
13 Z = 4860287
94
XDOT = 23167
483579 XDOT = 7048
541140
YDOT = 6929
324018 feet/sec YDOT = 2190
951083 meter/sec
ZDOT = -7587
373875 ZDOT = -2278
358312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14666337
52 X = 4470299
68
Y = 3624123
48 feet Y = 1104632
84 meter
Z = 15951524
98 Z = 4862024
81
XDOT = 2473
985364 XDOT = 754
070739
YDOT = 23051
080485 feet/sec YDOT = 7025
969332 meter/sec
ZDOT = -7458
653505 ZDOT = -2273
397588
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 07013
54372580
00020000 00000-0 20000-3 0 9105
2 25544 51
6289 183
0271 0023408 87
3254 273
0590 15
76973364 26354
Satellite: ISS
Catalog Number: 25544
Epoch time: 07013
54372580 = yrday
fracday
Element set: 910
Inclination: 51
6289 deg
RA of node: 183
0271 deg
Eccentricity:
0023408
Arg of perigee: 87
3254 deg
Mean anomaly: 273
0590 deg
Mean motion: 15
76973364 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2635
Checksum: 291
Coasting Arc #12 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2007/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5720664
13 A = 6720015
64 meter
Y = -1991869
83 meter E =
0036770
Z = 2876163
04 I = 51
65317
XDOT = 4035
093211 Wp = 87
80288
YDOT = -4207
970881 meter/sec RA = 177
13540 deg
ZDOT = 5057
709930 TA = 305
35162
MA = 305
69473
Ha = 193
982 n
mi
Hp = 170
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18768583
11 X = -5711937
39
Y = -6535006
02 feet Y = -2055793
05 meter
Z = 9436230
45 Z = 2848393
15
XDOT = 13238
494786 XDOT = 4057
278136
YDOT = -13805
678744 feet/sec YDOT = -4162
724808 meter/sec
ZDOT = 16593
536517 ZDOT = 5077
365675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1283961
00 X = -391351
31
Y = -19881543
34 feet Y = -6059894
41 meter
Z = 9331888
30 Z = 2844359
55
XDOT = 16376
745274 XDOT = 4991
631960
YDOT = 6849
143115 feet/sec YDOT = 2087
618822 meter/sec
ZDOT = 16666
667197 ZDOT = 5080
000162
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 07014
55761338
00020000 00000-0 20000-3 0 9111
2 25544 51
6292 177
7959 0023404 91
2815 269
1031 15
77041188 26519
Satellite: ISS
Catalog Number: 25544
Epoch time: 07014
55761338 = yrday
fracday
Element set: 911
Inclination: 51
6292 deg
RA of node: 177
7959 deg
Eccentricity:
0023404
Arg of perigee: 91
2815 deg
Mean anomaly: 269
1031 deg
Mean motion: 15
77041188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2651
Checksum: 292
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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