Date:
July 27th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 2965)
---------------------------------------
Vector Time (GMT): 2010/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5717102
70 A = 6739607
78 meter
Y = -3526312
96 meter E =
0018564
Z = -418678
88 I = 51
82705
XDOT = 2815
697421 Wp = 143
30493
YDOT = -3866
323319 meter/sec RA = 28
85763 deg
ZDOT = -6035
887764 TA = 41
23371
MA = 41
09364
Ha = 196
258 n
mi
Hp = 186
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18756898
62 X = -5675212
10
Y = -11569268
23 feet Y = -3590010
75 meter
Z = -1373618
38 Z = -446350
53
XDOT = 9237
852431 XDOT = 2888
042646
YDOT = -12684
787793 feet/sec YDOT = -3834
431385 meter/sec
ZDOT = -19802
781379 ZDOT = -6022
034101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 622730
00 X = 189808
10
Y = 22021926
81 feet Y = 6712283
29 meter
Z = -1484246
41 Z = -452398
31
XDOT = -14132
740932 XDOT = -4307
659436
YDOT = -900
344301 feet/sec YDOT = -274
424943 meter/sec
ZDOT = -19747
336617 ZDOT = -6018
988201
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 10207
53098269
00016717 00000-0 10270-3 0 9009
2 25544 51
6423 29
2368 0007425 151
8329 208
3235 15
71362563 29665
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
53098269 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 29
2368 deg
Eccentricity:
0007425
Arg of perigee: 151
8329 deg
Mean anomaly: 208
3235 deg
Mean motion: 15
71362563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 308
Coasting Arc #2 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2010/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1123075
04 A = 6727891
37 meter
Y = 4035216
39 meter E =
0009794
Z = 5260631
19 I = 51
75928
XDOT = -7190
339566 Wp = 143
68097
YDOT = -2705
907320 meter/sec RA = 23
75270 deg
ZDOT = 532
308459 TA = 301
22216
MA = 301
31810
Ha = 196
414 n
mi
Hp = 186
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3684629
38 X = -1193668
71
Y = 13238898
91 feet Y = 4022262
35 meter
Z = 17259288
68 Z = 5255004
28
XDOT = -23590
352906 XDOT = -7162
133015
YDOT = -8877
648689 feet/sec YDOT = -2786
156327 meter/sec
ZDOT = 1746
418828 ZDOT = 497
446870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13072276
65 X = 3984429
92
Y = -4328765
63 feet Y = -1319407
76 meter
Z = 17236744
33 Z = 5253759
67
XDOT = 5642
824603 XDOT = 1719
932939
YDOT = 23547
393545 feet/sec YDOT = 7177
245553 meter/sec
ZDOT = 1607
028774 ZDOT = 489
822370
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 10208
54854054
00016717 00000-0 10270-3 0 9014
2 25544 51
6416 24
0311 0007644 155
3537 204
7991 15
71295665 29826
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
54854054 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 24
0311 deg
Eccentricity:
0007644
Arg of perigee: 155
3537 deg
Mean anomaly: 204
7991 deg
Mean motion: 15
71295665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 304
Coasting Arc #3 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2010/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6517634
00 A = 6738981
46 meter
Y = 1098314
22 meter E =
0008177
Z = -1321691
16 I = 51
76954
XDOT = 341
100511 Wp = 90
28639
YDOT = 4978
381138 meter/sec RA = 18
62891 deg
ZDOT = 5850
071472 TA = 255
25843
MA = 255
34906
Ha = 196
238 n
mi
Hp = 186
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21383313
65 X = 6511288
45
Y = 3603393
10 feet Y = 1171162
90 meter
Z = -4336257
10 Z = -1290044
49
XDOT = 1119
096165 XDOT = 256
987990
YDOT = 16333
271451 feet/sec YDOT = 4981
724853 meter/sec
ZDOT = 19193
147874 ZDOT = 5851
524520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9419779
08 X = -2871148
66
Y = -19559646
42 feet Y = -5961780
23 meter
Z = -4209710
65 Z = -1283119
81
XDOT = 11328
936970 XDOT = 3453
059988
YDOT = -9565
443565 feet/sec YDOT = -2915
547199 meter/sec
ZDOT = 19198
909115 ZDOT = 5851
827498
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 10209
50248946
00016717 00000-0 10270-3 0 9029
2 25544 51
6422 19
1509 0007736 159
5539 200
5934 15
71358465 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
50248946 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 19
1509 deg
Eccentricity:
0007736
Arg of perigee: 159
5539 deg
Mean anomaly: 200
5934 deg
Mean motion: 15
71358465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 325
Coasting Arc #4 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2010/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1718202
59 A = 6729422
56 meter
Y = -4351186
72 meter E =
0014425
Z = -4847961
29 I = 51
70932
XDOT = 7295
871754 Wp = 104
67117
YDOT = -201
893970 meter/sec RA = 13
55218 deg
ZDOT = -2414
120677 TA = 141
79554
MA = 141
69323
Ha = 196
109 n
mi
Hp = 186
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5637147
59 X = -1645869
01
Y = -14275546
98 feet Y = -4369996
01 meter
Z = -15905384
81 Z = -4856132
70
XDOT = 23936
587121 XDOT = 7309
314282
YDOT = -662
381790 feet/sec YDOT = -120
231887 meter/sec
ZDOT = -7920
343428 ZDOT = -2378
645306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8234257
24 X = -2509801
61
Y = 12912261
24 feet Y = 3935657
23 meter
Z = -15938019
26 Z = -4857908
27
XDOT = -13775
723376 XDOT = -4198
840485
YDOT = -18347
559987 feet/sec YDOT = -5592
336284 meter/sec
ZDOT = -7778
478224 ZDOT = -2370
880163
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 10210
52002812
00016717 00000-0 10270-3 0 9034
2 25544 51
6428 13
9464 0007696 162
2144 197
9288 15
71383182 30133
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
52002812 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 13
9464 deg
Eccentricity:
0007696
Arg of perigee: 162
2144 deg
Mean anomaly: 197
9288 deg
Mean motion: 15
71383182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 291
Coasting Arc #5 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2010/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5920550
09 A = 6736212
59 meter
Y = 1410107
92 meter E =
0017867
Z = 2861476
45 I = 51
70158
XDOT = -3551
465572 Wp = 122
42921
YDOT = -4578
343086 meter/sec RA = 8
39855 deg
ZDOT = -5078
493356 TA = 24
74023
MA = 24
65466
Ha = 196
106 n
mi
Hp = 186
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19424376
95 X = -5949778
50
Y = 4626338
30 feet Y = 1343737
24 meter
Z = 9388046
10 Z = 2832643
88
XDOT = -11651
789934 XDOT = -3475
335684
YDOT = -15020
810649 feet/sec YDOT = -4617
631818 meter/sec
ZDOT = -16661
723610 ZDOT = -5095
561418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15471528
13 X = 4715721
77
Y = 12707988
60 feet Y = 3873394
92 meter
Z = 9272738
47 Z = 2826330
68
XDOT = -4040
545496 XDOT = -1231
558267
YDOT = 17159
447071 feet/sec YDOT = 5230
199467 meter/sec
ZDOT = -16729
930024 ZDOT = -5099
282671
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 10211
53755768
00016717 00000-0 10270-3 0 9042
2 25544 51
6423 8
7406 0007692 167
3042 192
8315 15
71368007 30296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53755768 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 8
7406 deg
Eccentricity:
0007692
Arg of perigee: 167
3042 deg
Mean anomaly: 192
8315 deg
Mean motion: 15
71368007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 302
Coasting Arc #6 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2010/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4337835
94 A = 6732834
31 meter
Y = 3348907
03 meter E =
0015483
Z = 3908350
50 I = 51
66173
XDOT = -5882
049451 Wp = 128
05631
YDOT = 2866
879436 meter/sec RA = 3
33521 deg
ZDOT = 4051
686861 TA = 279
69856
MA = 279
87341
Ha = 195
814 n
mi
Hp = 186
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14231745
20 X = 4281079
57
Y = 10987227
80 feet Y = 3397097
81 meter
Z = 12822672
23 Z = 3929285
78
XDOT = -19298
062504 XDOT = -5933
352423
YDOT = 9405
772428 feet/sec YDOT = 2800
815824 meter/sec
ZDOT = 13292
935896 ZDOT = 4022
987648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -127284
93 X = -38796
45
Y = -17919056
55 feet Y = -5461728
44 meter
Z = 12906350
39 Z = 3933855
60
XDOT = 18072
021443 XDOT = 5508
352136
YDOT = 9410
782346 feet/sec YDOT = 2868
406459 meter/sec
ZDOT = 13178
152437 ZDOT = 4016
700863
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 10212
55507786
00016717 00000-0 10270-3 0 9051
2 25544 51
6432 3
5357 0007722 171
2386 188
8912 15
71416642 30458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55507786 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 3
5357 deg
Eccentricity:
0007722
Arg of perigee: 171
2386 deg
Mean anomaly: 188
8912 deg
Mean motion: 15
71416642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 303
Coasting Arc #7 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2010/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4115211
54 A = 6732322
12 meter
Y = -3395199
69 meter E =
0012864
Z = -4120154
45 I = 51
63041
XDOT = 6084
912859 Wp = 141
38263
YDOT = 2793
534815 meter/sec RA = 358
16976 deg
ZDOT = 3772
075210 TA = 167
39289
MA = 167
36068
Ha = 195
789 n
mi
Hp = 187
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13501350
20 X = 4172886
27
Y = -11139106
59 feet Y = -3348858
26 meter
Z = -13517567
10 Z = -4100022
95
XDOT = 19963
624867 XDOT = 6034
898856
YDOT = 9165
140469 feet/sec YDOT = 2861
300125 meter/sec
ZDOT = 12375
574837 ZDOT = 3801
514179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17216897
16 X = -5247710
26
Y = -3480688
69 feet Y = -1060913
91 meter
Z = -13437039
53 Z = -4095609
65
XDOT = -5726
319508 XDOT = -1745
382186
YDOT = -19949
977308 feet/sec YDOT = -6080
753084 meter/sec
ZDOT = 12493
255185 ZDOT = 3807
944180
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 10213
50899645
00016717 00000-0 10270-3 0 9066
2 25544 51
6443 358
6566 0007655 173
9550 186
1705 15
71404052 30603
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50899645 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 358
6566 deg
Eccentricity:
0007655
Arg of perigee: 173
9550 deg
Mean anomaly: 186
1705 deg
Mean motion: 15
71404052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 313
Coasting Arc #8 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6049016
24 A = 6736444
56 meter
Y = -1360457
74 meter E =
0011284
Z = -2622243
02 I = 51
61443
XDOT = 3293
031267 Wp = 157
07799
YDOT = -4578
700180 meter/sec RA = 353
10025 deg
ZDOT = -5238
631389 TA = 52
71996
MA = 52
61713
Ha = 195
541 n
mi
Hp = 187
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19845853
80 X = -6020615
45
Y = -4463444
01 feet Y = -1427942
50 meter
Z = -8603159
53 Z = -2651560
12
XDOT = 10803
908355 XDOT = 3369
434599
YDOT = -15021
982217 feet/sec YDOT = -4541
448026 meter/sec
ZDOT = -17187
110856 ZDOT = -5222
448602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9366246
25 X = 2854831
86
Y = 18000647
31 feet Y = 5486597
30 meter
Z = -8720362
78 Z = -2657966
58
XDOT = -17200
618449 XDOT = -5242
748503
YDOT = 682
891107 feet/sec YDOT = 208
145210 meter/sec
ZDOT = -17122
360293 ZDOT = -5218
895417
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 10214
52649983
00016717 00000-0 10270-3 0 9078
2 25544 51
6441 353
4514 0007580 178
0177 182
1017 15
71425866 30760
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52649983 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 353
4514 deg
Eccentricity:
0007580
Arg of perigee: 178
0177 deg
Mean anomaly: 182
1017 deg
Mean motion: 15
71425866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 312
Coasting Arc #9 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2010/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496167
34 A = 6729061
38 meter
Y = 4321425
33 meter E =
0006638
Z = 4930487
39 I = 51
55963
XDOT = -7401
477532 Wp = 128
06011
YDOT = -142
308443 meter/sec RA = 347
94169 deg
ZDOT = -2123
356482 TA = 342
53867
MA = 342
56148
Ha = 195
599 n
mi
Hp = 187
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4908685
49 X = -1568330
44
Y = 14177904
63 feet Y = 4304290
43 meter
Z = 16176139
73 Z = 4923044
08
XDOT = -24283
062770 XDOT = -7389
021273
YDOT = -466
891218 feet/sec YDOT = -225
006382 meter/sec
ZDOT = -6966
392656 ZDOT = -2159
282488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13966078
23 X = 4256860
65
Y = -5569581
68 feet Y = -1697608
50 meter
Z = 16146333
58 Z = 4921402
48
XDOT = 15204
316387 XDOT = 4634
275635
YDOT = 17533
581828 feet/sec YDOT = 5344
235741 meter/sec
ZDOT = -7110
030131 ZDOT = -2167
137184
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 10215
54399600
00016717 00000-0 10270-3 0 9080
2 25544 51
6445 348
2467 0007580 180
9853 179
1295 15
71400042 30927
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54399600 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 348
2467 deg
Eccentricity:
0007580
Arg of perigee: 180
9853 deg
Mean anomaly: 179
1295 deg
Mean motion: 15
71400042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 311
Coasting Arc #10 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554646
76 A = 6738885
65 meter
Y = -1146125
32 meter E =
0010852
Z = 1055822
22 I = 51
56506
XDOT = -96
766025 Wp = 89
40371
YDOT = 4932
133879 meter/sec RA = 342
84783 deg
ZDOT = 5902
640220 TA = 282
13692
MA = 282
25847
Ha = 195
339 n
mi
Hp = 187
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504746
57 X = 6561846
81
Y = -3760253
68 feet Y = -1072787
18 meter
Z = 3463983
66 Z = 1087681
93
XDOT = -317
473834 XDOT = -180
584674
YDOT = 16181
541598 feet/sec YDOT = 4930
582581 meter/sec
ZDOT = 19365
617520 ZDOT = 5901
966996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17209253
56 X = -5245380
48
Y = -13399119
96 feet Y = -4084051
76 meter
Z = 3591377
45 Z = 1094651
85
XDOT = 11306
866546 XDOT = 3446
332923
YDOT = -9288
045795 feet/sec YDOT = -2830
996358 meter/sec
ZDOT = 19362
871628 ZDOT = 5901
803272
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 10216
56147967
00016717 00000-0 10270-3 0 9091
2 25544 51
6455 343
0416 0007534 185
5420 174
5660 15
71463538 31087
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56147967 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 343
0416 deg
Eccentricity:
0007534
Arg of perigee: 185
5420 deg
Mean anomaly: 174
5660 deg
Mean motion: 15
71463538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 312
Coasting Arc #11 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1284284
09 A = 6727320
82 meter
Y = -4000825
73 meter E =
0015906
Z = -5265866
71 I = 51
49772
XDOT = 7191
381002 Wp = 119
64434
YDOT = -2698
776336 meter/sec RA = 337
71199 deg
ZDOT = 289
469965 TA = 153
15511
MA = 153
07271
Ha = 195
133 n
mi
Hp = 187
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4213530
47 X = -1213870
25
Y = -13126068
67 feet Y = -4014793
10 meter
Z = -17276465
59 Z = -5271935
11
XDOT = 23593
769690 XDOT = 7219
618549
YDOT = -8854
253070 feet/sec YDOT = -2618
200161 meter/sec
ZDOT = 949
704609 ZDOT = 324
473725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6764273
74 X = -2061750
64
Y = 11977257
12 feet Y = 3650667
97 meter
Z = -17300684
78 Z = -5273248
72
XDOT = -21718
991687 XDOT = -6619
948666
YDOT = -10658
527337 feet/sec YDOT = -3248
719132 meter/sec
ZDOT = 1089
688393 ZDOT = 332
137022
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 10217
51536466
00016717 00000-0 10270-3 0 9105
2 25544 51
6455 338
1627 0007382 189
3638 170
7388 15
71484010 31230
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51536466 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 338
1627 deg
Eccentricity:
0007382
Arg of perigee: 189
3638 deg
Mean anomaly: 170
7388 deg
Mean motion: 15
71484010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 309
Coasting Arc #12 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5734380
41 A = 6739269
09 meter
Y = 3474821
86 meter E =
0017705
Z = 558498
45 I = 51
51050
XDOT = -2924
758820 Wp = 151
24239
YDOT = -3852
901734 meter/sec RA = 332
58324 deg
ZDOT = -5995
042757 TA = 22
66993
MA = 22
59183
Ha = 195
022 n
mi
Hp = 187
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18813584
01 X = -5775523
36
Y = 11400334
17 feet Y = 3410466
48 meter
Z = 1832343
98 Z = 530541
62
XDOT = -9595
665419 XDOT = -2852
335122
YDOT = -12640
753720 feet/sec YDOT = -3885
202517 meter/sec
ZDOT = -19668
775448 ZDOT = -6009
075580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21290697
82 X = 6489404
70
Y = 5569742
07 feet Y = 1697657
38 meter
Z = 1720525
08 Z = 524416
04
XDOT = -2064
648018 XDOT = -629
304716
YDOT = 14053
606487 feet/sec YDOT = 4283
539257 meter/sec
ZDOT = -19724
843408 ZDOT = -6012
132271
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 10218
53283329
00016717 00000-0 10270-3 0 9116
2 25544 51
6458 332
9571 0007425 193
5613 166
5350 15
71471717 31390
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53283329 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 332
9571 deg
Eccentricity:
0007425
Arg of perigee: 193
5613 deg
Mean anomaly: 166
5350 deg
Mean motion: 15
71471717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 310
Coasting Arc #13 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2010/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3654135
45 A = 6727936
54 meter
Y = 2471708
16 meter E =
0009891
Z = 5080459
37 I = 51
44753
XDOT = -5597
960108 Wp = 170
07917
YDOT = 5045
769099 meter/sec RA = 327
47390 deg
ZDOT = 1561
476271 TA = 264
82822
MA = 264
94111
Ha = 194
701 n
mi
Hp = 187
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11988633
37 X = 3601545
26
Y = 8109278
74 feet Y = 2512276
30 meter
Z = 16668173
79 Z = 5098083
38
XDOT = -18366
010854 XDOT = -5661
552003
YDOT = 16554
360560 feet/sec YDOT = 4982
813634 meter/sec
ZDOT = 5122
953646 ZDOT = 1534
127934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2703646
39 X = -824071
42
Y = -14135934
19 feet Y = -4308632
74 meter
Z = 16738620
32 Z = 5101931
47
XDOT = 23685
748538 XDOT = 7219
416154
YDOT = 1445
338570 feet/sec YDOT = 440
539196 meter/sec
ZDOT = 5013
551478 ZDOT = 1528
130490
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 10219
55029146
00016717 00000-0 10270-3 0 9125
2 25544 51
6466 327
7521 0007325 198
0553 162
0350 15
71525668 31552
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
55029146 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 327
7521 deg
Eccentricity:
0007325
Arg of perigee: 198
0553 deg
Mean anomaly: 162
0350 deg
Mean motion: 15
71525668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 301
Coasting Arc #14 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2010/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843956
98 A = 6737441
30 meter
Y = -5110363
73 meter E =
0002324
Z = -2126341
96 I = 51
45423
XDOT = 5135
368494 Wp = 137
96150
YDOT = 1573
616602 meter/sec RA = 322
31289 deg
ZDOT = 5503
420279 TA = 198
24538
MA = 198
25371
Ha = 194
656 n
mi
Hp = 188
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12611407
42 X = 3911145
47
Y = -16766285
20 feet Y = -5067002
45 meter
Z = -6976187
55 Z = -2107505
68
XDOT = 16848
321832 XDOT = 5090
656335
YDOT = 5162
784126 feet/sec YDOT = 1630
792887 meter/sec
ZDOT = 18055
840812 ZDOT = 5528
258875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20742087
28 X = -6322188
20
Y = 3311727
17 feet Y = 1009414
44 meter
Z = -6900825
13 Z = -2103371
50
XDOT = -8243
879593 XDOT = -2512
734500
YDOT = -13814
649438 feet/sec YDOT = -4210
705149 meter/sec
ZDOT = 18155
149517 ZDOT = 5533
689573
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 10220
50415291
00016717 00000-0 10270-3 0 9133
2 25544 51
6468 322
8728 0007111 202
1638 157
9217 15
71477871 31707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
50415291 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 322
8728 deg
Eccentricity:
0007111
Arg of perigee: 202
1638 deg
Mean anomaly: 157
9217 deg
Mean motion: 15
71477871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 294
Coasting Arc #15 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2010/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5056720
53 A = 6730618
35 meter
Y = -151789
49 meter E =
0006710
Z = -4442785
75 I = 51
40838
XDOT = 3017
216952 Wp = 117
35900
YDOT = -6298
662667 meter/sec RA = 317
22464 deg
ZDOT = -3225
721929 TA = 120
23095
MA = 120
16450
Ha = 194
432 n
mi
Hp = 188
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16590290
45 X = -5033065
66
Y = -497997
01 feet Y = -208204
25 meter
Z = -14576068
74 Z = -4467293
24
XDOT = 9899
005747 XDOT = 3103
095084
YDOT = -20664
903763 feet/sec YDOT = -6264
441989 meter/sec
ZDOT = -10583
077195 ZDOT = -3210
856420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11749573
49 X = 3581270
00
Y = 11600292
18 feet Y = 3535769
06 meter
Z = -14674067
67 Z = -4472655
83
XDOT = -20519
133678 XDOT = -6254
231945
YDOT = 7498
992019 feet/sec YDOT = 2285
692767 meter/sec
ZDOT = -10523
592672 ZDOT = -3207
591046
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 10221
52159565
00016717 00000-0 10270-3 0 9146
2 25544 51
6467 317
6682 0007238 205
7480 154
3322 15
71503628 31866
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52159565 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 317
6682 deg
Eccentricity:
0007238
Arg of perigee: 205
7480 deg
Mean anomaly: 154
3322 deg
Mean motion: 15
71503628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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