Date:
August 17th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 1513)
---------------------------------------
Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -770577
05 A = 6721591
31 meter
Y = -4223596
84 meter E =
0013899
Z = -5182229
90 I = 51
66183
XDOT = 7606
143377 Wp = 48
58163
YDOT = 22
972771 meter/sec RA = 6
99634 deg
ZDOT = -1142
680586 TA = 210
45980
MA = 210
54061
Ha = 191
342 n
mi
Hp = 185
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2528139
91 X = -698116
50
Y = -13856945
01 feet Y = -4231808
35 meter
Z = -17002066
60 Z = -5185797
67
XDOT = 24954
538639 XDOT = 7610
872110
YDOT = 75
369985 feet/sec YDOT = 108
055654 meter/sec
ZDOT = -3748
952055 ZDOT = -1105
718522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6557354
67 X = -1998681
70
Y = 12446865
44 feet Y = 3793804
58 meter
Z = -17016266
50 Z = -5186558
03
XDOT = -18801
406867 XDOT = -5730
668813
YDOT = -14863
179935 feet/sec YDOT = -4530
297244 meter/sec
ZDOT = -3603
579970 ZDOT = -1098
371175
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 09226
51773491
00010596 00000-0 82463-4 0 9006
2 25544 51
6400 7
3976 0007945 331
7541 28
3190 15
73618790 15140
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
51773491 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 7
3976 deg
Eccentricity:
0007945
Arg of perigee: 331
7541 deg
Mean anomaly: 28
3190 deg
Mean motion: 15
73618790 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1514
Checksum: 306
Coasting Arc #2 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6608976
56 A = 6732779
64 meter
Y = 655261
96 meter E =
0008080
Z = 1097422
51 I = 51
66920
XDOT = -1454
231130 Wp = 92
22353
YDOT = -4717
248823 meter/sec RA = 1
84454 deg
ZDOT = -5904
179403 TA = 75
78136
MA = 75
69163
Ha = 191
500 n
mi
Hp = 185
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21682993
96 X = -6621143
67
Y = 2149809
59 feet Y = 581288
38 meter
Z = 3600467
57 Z = 1065286
80
XDOT = -4771
099509 XDOT = -1372
692699
YDOT = -15476
538133 feet/sec YDOT = -4733
054454 meter/sec
ZDOT = -19370
667332 ZDOT = -5911
046383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18678665
55 X = 5693257
26
Y = 11259456
15 feet Y = 3431882
24 meter
Z = 3474100
68 Z = 1058905
89
XDOT = -4703
677608 XDOT = -1433
680935
YDOT = 13827
061765 feet/sec YDOT = 4214
488426 meter/sec
ZDOT = -19397
861105 ZDOT = -5912
468065
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 09227
53382142
00010596 00000-0 82463-4 0 9019
2 25544 51
6396 2
1811 0008006 334
9357 25
1416 15
73615920 15300
Satellite: ISS
Catalog Number: 25544
Epoch time: 09227
53382142 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 2
1811 deg
Eccentricity:
0008006
Arg of perigee: 334
9357 deg
Mean anomaly: 25
1416 deg
Mean motion: 15
73615920 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1530
Checksum: 279
Coasting Arc #3 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1759204
80 A = 6721665
54 meter
Y = 3970726
81 meter E =
0005057
Z = 5128806
47 I = 51
60359
XDOT = -7424
474343 Wp = 5
52677
YDOT = 1516
867579 meter/sec RA = 356
73337 deg
ZDOT = 1377
102827 TA = 71
31319
MA = 71
25831
Ha = 191
572 n
mi
Hp = 184
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5771669
30 X = 1689758
18
Y = 13027318
92 feet Y = 3990010
50 meter
Z = 16826792
87 Z = 5137184
27
XDOT = -24358
511625 XDOT = -7447
574054
YDOT = 4976
599670 feet/sec YDOT = 1433
713468 meter/sec
ZDOT = 4518
053895 ZDOT = 1340
979167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3007549
96 X = 916701
23
Y = -13887496
00 feet Y = -4232908
78 meter
Z = 16859900
98 Z = 5138897
82
XDOT = 21684
166361 XDOT = 6609
333907
YDOT = 9989
476921 feet/sec YDOT = 3044
792565 meter/sec
ZDOT = 4376
030527 ZDOT = 1333
814105
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 09228
54990000
00010596 00000-0 82463-4 0 9020
2 25544 51
6409 356
9658 0008099 338
4738 21
6083 15
73653353 15468
Satellite: ISS
Catalog Number: 25544
Epoch time: 09228
54990000 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 356
9658 deg
Eccentricity:
0008099
Arg of perigee: 338
4738 deg
Mean anomaly: 21
6083 deg
Mean motion: 15
73653353 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1546
Checksum: 328
Coasting Arc #4 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6289122
96 A = 6732534
51 meter
Y = -1982059
87 meter E =
0015294
Z = -1311693
94 I = 51
61074
XDOT = 2571
378374 Wp = 11
32286
YDOT = 4304
780676 meter/sec RA = 351
57512 deg
ZDOT = 5850
250472 TA = 334
26412
MA = 334
34015
Ha = 191
857 n
mi
Hp = 184
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20633605
51 X = 6317191
14
Y = -6502821
11 feet Y = -1911574
17 meter
Z = -4303457
82 Z = -1281073
88
XDOT = 8436
280756 XDOT = 2494
631493
YDOT = 14123
296180 feet/sec YDOT = 4333
105755 meter/sec
ZDOT = 19193
735145 ZDOT = 5862
555946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20678532
25 X = -6302816
63
Y = -6438331
91 feet Y = -1962403
57 meter
Z = -4183096
24 Z = -1275007
73
XDOT = 746
185025 XDOT = 227
437196
YDOT = -14841
209645 feet/sec YDOT = -4523
600700 meter/sec
ZDOT = 19242
309257 ZDOT = 5865
055862
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 09229
50246863
00010596 00000-0 82463-4 0 9039
2 25544 51
6415 352
0771 0008151 343
0902 16
9989 15
73625909 15617
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
50246863 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 352
0771 deg
Eccentricity:
0008151
Arg of perigee: 343
0902 deg
Mean anomaly: 16
9989 deg
Mean motion: 15
73625909 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1561
Checksum: 316
Coasting Arc #5 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2688880
34 A = 6721928
11 meter
Y = -3502554
60 meter E =
0015824
Z = -5080610
99 I = 51
54626
XDOT = 6909
594795 Wp = 46
50498
YDOT = -2971
115031 meter/sec RA = 346
46421 deg
ZDOT = -1600
994533 TA = 208
03435
MA = 208
11967
Ha = 191
897 n
mi
Hp = 184
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8821785
89 X = -2624834
17
Y = -11491320
85 feet Y = -3532264
86 meter
Z = -16668671
24 Z = -5093517
92
XDOT = 22669
274261 XDOT = 6950
081955
YDOT = -9747
752725 feet/sec YDOT = -2893
621425 meter/sec
ZDOT = -5252
606734 ZDOT = -1567
330253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 861842
73 X = 262689
66
Y = 14402488
89 feet Y = 4389878
61 meter
Z = -16719584
41 Z = -5096129
33
XDOT = -23236
800467 XDOT = -7082
576782
YDOT = -4582
398599 feet/sec YDOT = -1396
715093 meter/sec
ZDOT = -5120
310138 ZDOT = -1560
670530
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 09230
51853376
00010596 00000-0 82463-4 0 9046
2 25544 51
6419 346
8625 0008204 346
5569 13
5374 15
73644606 15779
Satellite: ISS
Catalog Number: 25544
Epoch time: 09230
51853376 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 346
8625 deg
Eccentricity:
0008204
Arg of perigee: 346
5569 deg
Mean anomaly: 13
5374 deg
Mean motion: 15
73644606 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1577
Checksum: 325
Coasting Arc #6 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5743264
77 A = 6732262
54 meter
Y = 3183626
25 meter E =
0011051
Z = 1478658
67 I = 51
55246
XDOT = -3524
689292 Wp = 83
04867
YDOT = -3654
590501 meter/sec RA = 341
29797 deg
ZDOT = -5783
549352 TA = 80
66159
MA = 80
53665
Ha = 192
040 n
mi
Hp = 184
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18842732
17 X = -5785620
66
Y = 10444968
02 feet Y = 3119164
84 meter
Z = 4851242
35 Z = 1450655
71
XDOT = -11563
941247 XDOT = -3455
466273
YDOT = -11990
126317 feet/sec YDOT = -3693
618481 meter/sec
ZDOT = -18974
899450 ZDOT = -5800
503840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21520322
68 X = 6559394
35
Y = 1441160
28 feet Y = 439265
65 meter
Z = 4741227
03 Z = 1445126
00
XDOT = 3238
082099 XDOT = 986
967424
YDOT = 14713
556151 feet/sec YDOT = 4484
691915 meter/sec
ZDOT = -19041
745481 ZDOT = -5803
924023
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 09231
53459203
00010596 00000-0 82463-4 0 9051
2 25544 51
6420 341
6473 0008145 350
8800 9
2214 15
73650525 15935
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53459203 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 341
6473 deg
Eccentricity:
0008145
Arg of perigee: 350
8800 deg
Mean anomaly: 9
2214 deg
Mean motion: 15
73650525 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 286
Coasting Arc #7 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3442261
15 A = 6721955
86 meter
Y = 2846034
46 meter E =
0006241
Z = 5019117
48 I = 51
49128
XDOT = -6150
678136 Wp = 34
06967
YDOT = 4277
464413 meter/sec RA = 336
18514 deg
ZDOT = 1796
845958 TA = 38
61225
MA = 38
56763
Ha = 192
025 n
mi
Hp = 183
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11293507
71 X = 3385799
01
Y = 9337383
39 feet Y = 2884212
20 meter
Z = 16466920
87 Z = 5035702
47
XDOT = -20179
390210 XDOT = -6206
780920
YDOT = 14033
675895 feet/sec YDOT = 4208
370249 meter/sec
ZDOT = 5895
163903 ZDOT = 1766
830267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4593529
79 X = -1400107
88
Y = -13837364
56 feet Y = -4217628
72 meter
Z = 16532282
18 Z = 5039039
61
XDOT = 23565
583218 XDOT = 7182
789765
YDOT = -936
189609 feet/sec YDOT = -285
350593 meter/sec
ZDOT = 5777
285998 ZDOT = 1760
916772
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 09232
55064117
00010596 00000-0 82463-4 0 9061
2 25544 51
6428 336
4320 0008260 354
5520 5
5552 15
73703742 16096
Satellite: ISS
Catalog Number: 25544
Epoch time: 09232
55064117 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 336
4320 deg
Eccentricity:
0008260
Arg of perigee: 354
5520 deg
Mean anomaly: 5
5552 deg
Mean motion: 15
73703742 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1609
Checksum: 287
Coasting Arc #8 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4938972
77 A = 6732013
16 meter
Y = -4248270
07 meter E =
0015486
Z = -1662560
44 I = 51
49766
XDOT = 4329
755328 Wp = 16
81930
YDOT = 2805
193784 meter/sec RA = 331
01268 deg
ZDOT = 5722
228110 TA = 324
76104
MA = 324
86333
Ha = 192
410 n
mi
Hp = 183
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16203978
90 X = 4994186
87
Y = -13937893
94 feet Y = -4192730
91 meter
Z = -5454594
63 Z = -1638433
05
XDOT = 14205
234017 XDOT = 4270
268263
YDOT = 9203
391680 feet/sec YDOT = 2853
279220 meter/sec
ZDOT = 18773
714273 ZDOT = 5743
117148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21084052
26 X = -6426419
13
Y = 3649765
89 feet Y = 1112448
64 meter
Z = -5359885
39 Z = -1633693
07
XDOT = -7122
194292 XDOT = -2170
844820
YDOT = -13588
894147 feet/sec YDOT = -4141
894936 meter/sec
ZDOT = 18856
003974 ZDOT = 5747
310011
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 09233
50318309
00010596 00000-0 82463-4 0 9073
2 25544 51
6428 331
5438 0008514 358
3799 1
7335 15
73648932 16247
Satellite: ISS
Catalog Number: 25544
Epoch time: 09233
50318309 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 331
5438 deg
Eccentricity:
0008514
Arg of perigee: 358
3799 deg
Mean anomaly: 1
7335 deg
Mean motion: 15
73648932 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1624
Checksum: 320
Coasting Arc #9 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060005
33 A = 6722295
55 meter
Y = -2036079
99 meter E =
0017387
Z = -4970363
00 I = 51
43929
XDOT = 5127
154669 Wp = 47
55062
YDOT = -5376
201488 meter/sec RA = 325
89956 deg
ZDOT = -1978
606886 TA = 203
19421
MA = 203
27277
Ha = 192
386 n
mi
Hp = 183
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13320227
45 X = -4012790
90
Y = -6680052
45 feet Y = -2081217
55 meter
Z = -16306965
21 Z = -4989971
54
XDOT = 16821
373585 XDOT = 5196
502835
YDOT = -17638
456326 feet/sec YDOT = -5318
478962 meter/sec
ZDOT = -6491
492407 ZDOT = -1953
530769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8147792
87 X = 2483447
27
Y = 12375004
07 feet Y = 3771901
24 meter
Z = -16384182
01 Z = -4993898
68
XDOT = -22497
815509 XDOT = -6857
334167
YDOT = 6317
531305 feet/sec YDOT = 1925
583542 meter/sec
ZDOT = -6393
111191 ZDOT = -1948
620291
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 09234
51921956
00010596 00000-0 82463-4 0 9084
2 25544 51
6423 326
3291 0008381 1
9038 358
2156 15
73674849 16405
Satellite: ISS
Catalog Number: 25544
Epoch time: 09234
51921956 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 326
3291 deg
Eccentricity:
0008381
Arg of perigee: 1
9038 deg
Mean anomaly: 358
2156 deg
Mean motion: 15
73674849 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1640
Checksum: 319
Coasting Arc #10 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3995388
74 A = 6731683
55 meter
Y = 5111331
11 meter E =
0014062
Z = 1790496
93 I = 51
44622
XDOT = -4889
016652 Wp = 79
44709
YDOT = -1825
844808 meter/sec RA = 320
72010 deg
ZDOT = -5657
179497 TA = 80
66406
MA = 80
50508
Ha = 192
547 n
mi
Hp = 183
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13108230
76 X = -4060945
44
Y = 16769459
02 feet Y = 5066285
84 meter
Z = 5874333
76 Z = 1770928
02
XDOT = -16040
080880 XDOT = -4840
754955
YDOT = -5990
304487 feet/sec YDOT = -1880
247006 meter/sec
ZDOT = -18560
300186 ZDOT = -5680
812935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19603233
18 X = 5975065
47
Y = -8345614
09 feet Y = -2543743
17 meter
Z = 5797606
50 Z = 1767110
46
XDOT = 10454
378709 XDOT = 3186
494631
YDOT = 11505
613535 feet/sec YDOT = 3506
911006 meter/sec
ZDOT = -18653
334811 ZDOT = -5685
536451
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 09235
53524910
00010596 00000-0 82463-4 0 9097
2 25544 51
6415 321
1140 0008465 7
0180 353
1100 15
73696724 16566
Satellite: ISS
Catalog Number: 25544
Epoch time: 09235
53524910 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 321
1140 deg
Eccentricity:
0008465
Arg of perigee: 7
0180 deg
Mean anomaly: 353
1100 deg
Mean motion: 15
73696724 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1656
Checksum: 283
Coasting Arc #11 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4444849
02 A = 6722315
61 meter
Y = 1131723
51 meter E =
0008277
Z = 4907167
55 I = 51
39311
XDOT = -3952
603679 Wp = 52
84967
YDOT = 6260
313008 meter/sec RA = 315
60426 deg
ZDOT = 2138
879806 TA = 16
35997
MA = 16
33327
Ha = 192
451 n
mi
Hp = 182
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14582837
98 X = 4408025
44
Y = 3713003
65 feet Y = 1181222
63 meter
Z = 16099631
08 Z = 4928671
13
XDOT = -12967
859840 XDOT = -4032
704085
YDOT = 20539
084672 feet/sec YDOT = 6215
664849 meter/sec
ZDOT = 7017
322199 ZDOT = 2119
483399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11072775
40 X = -3374981
94
Y = -10055208
71 feet Y = -3064827
62 meter
Z = 16184254
79 Z = 4932960
86
XDOT = 20367
404986 XDOT = 6207
985040
YDOT = -11269
109183 feet/sec YDOT = -3434
824479 meter/sec
ZDOT = 6941
329914 ZDOT = 2115
717358
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 09236
55126937
00010596 00000-0 82463-4 0 9109
2 25544 51
6418 315
8980 0008505 10
0138 350
1193 15
73736790 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55126937 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 315
8980 deg
Eccentricity:
0008505
Arg of perigee: 10
0138 deg
Mean anomaly: 350
1193 deg
Mean motion: 15
73736790 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1672
Checksum: 307
Coasting Arc #12 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2867542
08 A = 6731432
04 meter
Y = -5762550
55 meter E =
0015329
Z = -1945787
12 I = 51
40211
XDOT = 5244
310031 Wp = 24
41468
YDOT = 730
350445 meter/sec RA = 310
41930 deg
ZDOT = 5595
059245 TA = 313
85420
MA = 313
98076
Ha = 192
805 n
mi
Hp = 182
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9407946
46 X = 2941219
07
Y = -18906005
75 feet Y = -5730072
07 meter
Z = -6383816
00 Z = -1931677
62
XDOT = 17205
741573 XDOT = 5208
573571
YDOT = 2396
162877 feet/sec YDOT = 788
795604 meter/sec
ZDOT = 18356
493586 ZDOT = 5620
449296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16972916
10 X = -5173344
83
Y = 12592403
57 feet Y = 3838164
61 meter
Z = -6328594
46 Z = -1928955
59
XDOT = -13248
947205 XDOT = -4038
279108
YDOT = -8631
073347 feet/sec YDOT = -2630
751156 meter/sec
ZDOT = 18456
382740 ZDOT = 5625
505459
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 09237
50378394
00010596 00000-0 82463-4 0 9112
2 25544 51
6411 311
0092 0008745 13
2224 346
9167 15
73691578 16874
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237
50378394 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 311
0092 deg
Eccentricity:
0008745
Arg of perigee: 13
2224 deg
Mean anomaly: 346
9167 deg
Mean motion: 15
73691578 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1687
Checksum: 316
Coasting Arc #13 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4654642
10 A = 6722620
53 meter
Y = -157715
07 meter E =
0018663
Z = -4864609
95 I = 51
35354
XDOT = 2621
284027 Wp = 50
56803
YDOT = -6856
511257 meter/sec RA = 305
30302 deg
ZDOT = -2280
005758 TA = 197
07937
MA = 197
14227
Ha = 192
840 n
mi
Hp = 182
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15271135
51 X = -4628901
18
Y = -517437
91 feet Y = -209622
03 meter
Z = -15960006
41 Z = -4887159
67
XDOT = 8600
013212 XDOT = 2708
835745
YDOT = -22495
115671 feet/sec YDOT = -6826
708961 meter/sec
ZDOT = -7480
333852 ZDOT = -2267
058995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13427658
30 X = 4092750
25
Y = 7094672
10 feet Y = 2162456
06 meter
Z = -16048699
22 Z = -4891643
52
XDOT = -17082
961174 XDOT = -5206
886566
YDOT = 15482
122980 feet/sec YDOT = 4718
951084 meter/sec
ZDOT = -7429
736983 ZDOT = -2264
583832
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 09238
51979201
00010596 00000-0 82463-4 0 9129
2 25544 51
6403 305
7933 0008678 17
6905 342
4559 15
73716295 17037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51979201 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 305
7933 deg
Eccentricity:
0008678
Arg of perigee: 17
6905 deg
Mean anomaly: 342
4559 deg
Mean motion: 15
73716295 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1703
Checksum: 326
Coasting Arc #14 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1703259
04 A = 6731031
81 meter
Y = 6182571
76 meter E =
0016709
Z = 2037420
20 I = 51
36659
XDOT = -5332
624682 Wp = 78
69355
YDOT = 370
057785 meter/sec RA = 300
11245 deg
ZDOT = -5539
342234 TA = 78
49993
MA = 78
31235
Ha = 192
936 n
mi
Hp = 182
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5588120
21 X = -1782164
42
Y = 20284028
08 feet Y = 6163083
68 meter
Z = 6684449
47 Z = 2028954
29
XDOT = -17495
487801 XDOT = -5309
457340
YDOT = 1214
100346 feet/sec YDOT = 310
554924 meter/sec
ZDOT = -18173
694992 ZDOT = -5565
191779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13647380
47 X = 4159721
57
Y = -16026790
98 feet Y = -4884965
89 meter
Z = 6651445
30 Z = 2027360
53
XDOT = 15114
012817 XDOT = 4606
751107
YDOT = 5228
535660 feet/sec YDOT = 1593
657669 meter/sec
ZDOT = -18275
343352 ZDOT = -5570
324654
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 09239
53579154
00010596 00000-0 82463-4 0 9136
2 25544 51
6407 300
5774 0008930 21
4905 338
6627 15
73775493 17196
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239
53579154 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 300
5774 deg
Eccentricity:
0008930
Arg of perigee: 21
4905 deg
Mean anomaly: 338
6627 deg
Mean motion: 15
73775493 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1719
Checksum: 332
Coasting Arc #15 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4621246
28 A = 6722641
66 meter
Y = -810618
54 meter E =
0010677
Z = 4804628
04 I = 51
32418
XDOT = -1237
720758 Wp = 65
39272
YDOT = 7217
131153 meter/sec RA = 294
99540 deg
ZDOT = 2408
330785 TA = 1
01794
MA = 1
01577
Ha = 192
863 n
mi
Hp = 182
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15161569
15 X = 4606627
40
Y = -2659509
64 feet Y = -759022
94 meter
Z = 15763215
34 Z = 4827042
39
XDOT = -4060
763643 XDOT = -1330
031142
YDOT = 23678
251813 feet/sec YDOT = 7202
774019 meter/sec
ZDOT = 7901
347720 ZDOT = 2402
093985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14853048
47 X = -4527209
17
Y = -3680658
92 feet Y = -1121864
84 meter
Z = 15851335
27 Z = 4831486
99
XDOT = 13088
205643 XDOT = 3989
285080
YDOT = -18895
190412 feet/sec YDOT = -5759
254038 meter/sec
ZDOT = 7877
163489 ZDOT = 2400
959432
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 09240
55178450
00010596 00000-0 82463-4 0 9145
2 25544 51
6404 295
3617 0008855 25
5891 334
5709 15
73772077 17354
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240
55178450 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 295
3617 deg
Eccentricity:
0008855
Arg of perigee: 25
5891 deg
Mean anomaly: 334
5709 deg
Mean motion: 15
73772077 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1735
Checksum: 329
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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