Date:
April 3rd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 3388)
---------------------------------------
Vector Time (GMT): 2009/091/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350011
20 A = 6731697
46 meter
Y = -1280280
97 meter E =
0008985
Z = -3878850
08 I = 51
52487
XDOT = 4154
608771 Wp = 143
36276
YDOT = -5029
838244 meter/sec RA = 339
37671 deg
ZDOT = -4082
108035 TA = 84
03580
MA = 83
93340
Ha = 195
150 n
mi
Hp = 186
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17552530
17 X = -5316454
48
Y = -4200396
88 feet Y = -1339920
25 meter
Z = -12725886
07 Z = -3904758
96
XDOT = 13630
606203 XDOT = 4230
374646
YDOT = -16502
093978 feet/sec YDOT = -4982
955319 meter/sec
ZDOT = -13392
742897 ZDOT = -4061
740939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17970219
48 X = -5477322
90
Y = 467778
93 feet Y = 142579
02 meter
Z = -12827128
29 Z = -3909708
70
XDOT = 9002
275974 XDOT = 2743
893717
YDOT = -18178
046431 feet/sec YDOT = -5540
668552 meter/sec
ZDOT = -13313
534887 ZDOT = -4057
965434
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 09091
53941688
00010596 00000-0 82463-4 0 9003
2 25544 51
6437 339
7443 0009246 186
9335 173
1700 15
71839154 33893
Satellite: ISS
Catalog Number: 25544
Epoch time: 09091
53941688 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 339
7443 deg
Eccentricity:
0009246
Arg of perigee: 186
9335 deg
Mean anomaly: 173
1700 deg
Mean motion: 15
71839154 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3389
Checksum: 336
Coasting Arc #2 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2009/092/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2472227
54 A = 6731079
95 meter
Y = 4768792
56 meter E =
0011046
Z = 4044043
53 I = 51
49605
XDOT = -6666
426820 Wp = 126
31152
YDOT = -184
798226 meter/sec RA = 334
19720 deg
ZDOT = -3856
587675 TA = 3
46184
MA = 3
45421
Ha = 194
988 n
mi
Hp = 186
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8110982
76 X = -2545014
39
Y = 15645644
87 feet Y = 4740739
68 meter
Z = 13267859
35 Z = 4031856
72
XDOT = -21871
479068 XDOT = -6645
130386
YDOT = -606
293392 feet/sec YDOT = -259
227006 meter/sec
ZDOT = -12652
846703 ZDOT = -3888
921308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3560867
68 X = -1085352
47
Y = 17295864
96 feet Y = 5271779
64 meter
Z = 13220575
37 Z = 4029631
37
XDOT = -19860
394802 XDOT = -6053
448336
YDOT = 5681
363666 feet/sec YDOT = 1731
679646 meter/sec
ZDOT = -12779
110124 ZDOT = -3895
072766
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 09092
55663294
00010596 00000-0 82463-4 0 9011
2 25544 51
6438 334
5372 0009082 190
6387 169
4585 15
71906706 34051
Satellite: ISS
Catalog Number: 25544
Epoch time: 09092
55663294 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 334
5372 deg
Eccentricity:
0009082
Arg of perigee: 190
6387 deg
Mean anomaly: 169
4585 deg
Mean motion: 15
71906706 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3405
Checksum: 332
Coasting Arc #3 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2009/093/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6036517
14 A = 6734700
84 meter
Y = -1002236
20 meter E =
0012851
Z = 2812313
59 I = 51
48159
XDOT = -1453
100873 Wp = 120
82229
YDOT = 5586
486037 meter/sec RA = 329
11535 deg
ZDOT = 5086
233757 TA = 271
43597
MA = 271
58319
Ha = 194
836 n
mi
Hp = 186
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19804846
25 X = 6033614
06
Y = -3288176
51 feet Y = -934748
54 meter
Z = 9226750
61 Z = 2841631
71
XDOT = -4767
391316 XDOT = -1540
169698
YDOT = 18328
366264 feet/sec YDOT = 5569
749866 meter/sec
ZDOT = 16687
118624 ZDOT = 5078
963078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17930578
70 X = 5465240
39
Y = -8911448
77 feet Y = -2716209
58 meter
Z = 9341166
69 Z = 2847187
61
XDOT = 49
543249 XDOT = 15
100782
YDOT = 17642
486311 feet/sec YDOT = 5377
429827 meter/sec
ZDOT = 16659
086119 ZDOT = 5077
689449
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 09093
57383650
00010596 00000-0 82463-4 0 9020
2 25544 51
6433 329
3292 0009077 194
9181 165
1715 15
71882015 34214
Satellite: ISS
Catalog Number: 25544
Epoch time: 09093
57383650 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 329
3292 deg
Eccentricity:
0009077
Arg of perigee: 194
9181 deg
Mean anomaly: 165
1715 deg
Mean motion: 15
71882015 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3421
Checksum: 314
Coasting Arc #4 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2009/094/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 74794
10 A = 6728252
85 meter
Y = -4757733
75 meter E =
0014622
Z = -4768705
54 I = 51
43477
XDOT = 6824
229887 Wp = 146
71999
YDOT = -2455
575307 meter/sec RA = 323
93882 deg
ZDOT = 2548
631112 TA = 148
41216
MA = 148
32431
Ha = 194
656 n
mi
Hp = 187
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 245387
46 X = 151155
60
Y = -15609362
71 feet Y = -4756470
60 meter
Z = -15645359
40 Z = -4768156
52
XDOT = 22389
205665 XDOT = 6838
800679
YDOT = -8056
349432 feet/sec YDOT = -2379
181214 meter/sec
ZDOT = 8361
650630 ZDOT = 2581
818391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4494048
86 X = -1369786
09
Y = -14952368
21 feet Y = -4557481
83 meter
Z = -15643525
81 Z = -4768146
67
XDOT = 17677
043016 XDOT = 5387
962711
YDOT = -14225
131874 feet/sec YDOT = -4335
820195 meter/sec
ZDOT = 8491
080248 ZDOT = 2588
081259
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 09094
52745042
00010596 00000-0 82463-4 0 9034
2 25544 51
6427 324
4467 0009145 199
0856 160
9965 15
71924450 34364
Satellite: ISS
Catalog Number: 25544
Epoch time: 09094
52745042 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 324
4467 deg
Eccentricity:
0009145
Arg of perigee: 199
0856 deg
Mean anomaly: 160
9965 deg
Mean motion: 15
71924450 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3436
Checksum: 328
Coasting Arc #5 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2009/095/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5668269
84 A = 6736972
28 meter
Y = 3243539
09 meter E =
0014795
Z = -1616500
49 I = 51
44048
XDOT = -1228
833527 Wp = 175
24800
YDOT = -4995
405627 meter/sec RA = 318
84096 deg
ZDOT = -5732
701618 TA = 22
64675
MA = 22
58154
Ha = 194
482 n
mi
Hp = 187
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18596685
83 X = -5696265
76
Y = 10641532
45 feet Y = 3179996
55 meter
Z = -5303479
31 Z = -1644104
94
XDOT = -4031
606061 XDOT = -1145
034533
YDOT = -16389
126074 feet/sec YDOT = -5008
678996 meter/sec
ZDOT = -18808
076174 ZDOT = -5738
467365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14104633
52 X = -4299092
30
Y = 16093031
10 feet Y = 4905155
88 meter
Z = -5411052
84 Z = -1649288
91
XDOT = -7858
148679 XDOT = -2395
163717
YDOT = -13199
134595 feet/sec YDOT = -4023
096224 meter/sec
ZDOT = -18830
921889 ZDOT = -5739
664992
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 09095
54462649
00010596 00000-0 82463-4 0 9047
2 25544 51
6423 319
2401 0009266 203
3015 156
7728 15
71902680 34529
Satellite: ISS
Catalog Number: 25544
Epoch time: 09095
54462649 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 319
2401 deg
Eccentricity:
0009266
Arg of perigee: 203
3015 deg
Mean anomaly: 156
7728 deg
Mean motion: 15
71902680 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3452
Checksum: 306
Coasting Arc #6 (Orbit 3467)
---------------------------------------
Vector Time (GMT): 2009/096/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2131984
80 A = 6726356
41 meter
Y = 3742598
32 meter E =
0006038
Z = 5166223
77 I = 51
38328
XDOT = -5865
347014 Wp = 188
92930
YDOT = 4861
394748 meter/sec RA = 313
67962 deg
ZDOT = -1107
321512 TA = 271
64464
MA = 271
71380
Ha = 194
223 n
mi
Hp = 187
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6994700
78 X = 2064879
51
Y = 12278865
89 feet Y = 3766064
65 meter
Z = 16949553
04 Z = 5176417
59
XDOT = -19243
264480 XDOT = -5913
892872
YDOT = 15949
457836 feet/sec YDOT = 4795
533490 meter/sec
ZDOT = -3632
944594 ZDOT = -1135
933568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10669476
46 X = 3252056
42
Y = 9192343
67 feet Y = 2801826
35 meter
Z = 16989609
31 Z = 5178432
92
XDOT = -11962
788400 XDOT = -3646
257904
YDOT = 20768
925776 feet/sec YDOT = 6330
368577 meter/sec
ZDOT = -3744
337113 ZDOT = -1141
273952
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 09096
56178735
00010596 00000-0 82463-4 0 9051
2 25544 51
6418 314
0319 0009155 207
3868 152
6813 15
71954858 34682
Satellite: ISS
Catalog Number: 25544
Epoch time: 09096
56178735 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 314
0319 deg
Eccentricity:
0009155
Arg of perigee: 207
3868 deg
Mean anomaly: 152
6813 deg
Mean motion: 15
71954858 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3468
Checksum: 343
Coasting Arc #7 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/097/12:23:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4392461
18 A = 6737874
69 meter
Y = -5098234
84 meter E =
0004959
Z = 322664
75 I = 51
40136
XDOT = 3449
565751 Wp = 81
84160
YDOT = 3356
714330 meter/sec RA = 308
55353 deg
ZDOT = 6000
256481 TA = 281
67172
MA = 281
72736
Ha = 194
095 n
mi
Hp = 187
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14410961
87 X = 4447576
59
Y = -16726492
24 feet Y = -5048807
58 meter
Z = 1058611
38 Z = 344137
68
XDOT = 11317
472936 XDOT = 3382
625828
YDOT = 11012
842291 feet/sec YDOT = 3394
915645 meter/sec
ZDOT = 19685
880844 ZDOT = 6016
851592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7483332
15 X = 2280919
64
Y = -20766977
60 feet Y = -6329774
77 meter
Z = 1142105
14 Z = 348113
65
XDOT = 12882
680650 XDOT = 3926
641062
YDOT = 5741
511600 feet/sec YDOT = 1750
012736 meter/sec
ZDOT = 19750
906375 ZDOT = 6020
076263
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 09097
57893449
00010596 00000-0 82463-4 0 9060
2 25544 51
6403 308
8228 0009149 211
5643 148
4971 15
71980102 34844
Satellite: ISS
Catalog Number: 25544
Epoch time: 09097
57893449 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 308
8228 deg
Eccentricity:
0009149
Arg of perigee: 211
5643 deg
Mean anomaly: 148
4971 deg
Mean motion: 15
71980102 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3484
Checksum: 334
Coasting Arc #8 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2009/098/12:27:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2636716
16 A = 6726366
37 meter
Y = -3465222
11 meter E =
0013231
Z = -5136195
58 I = 51
34398
XDOT = 4990
006825 Wp = 138
63118
YDOT = -5708
736917 meter/sec RA = 303
38430 deg
ZDOT = 1281
930422 TA = 143
73981
MA = 143
65006
Ha = 193
878 n
mi
Hp = 187
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8650643
56 X = -2572820
61
Y = -11368838
96 feet Y = -3494350
59 meter
Z = -16851035
37 Z = -5148849
34
XDOT = 16371
413469 XDOT = 5047
244578
YDOT = -18729
451826 feet/sec YDOT = -5652
615607 meter/sec
ZDOT = 4205
808471 ZDOT = 1306
311554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12303676
15 X = -3750160
49
Y = -7143397
52 feet Y = -2177307
56 meter
Z = -16900679
01 Z = -5151326
96
XDOT = 7246
847747 XDOT = 2208
839193
YDOT = -22717
863556 feet/sec YDOT = -6924
404812 meter/sec
ZDOT = 4300
610085 ZDOT = 1310
825954
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 09098
53249747
00010596 00000-0 82463-4 0 9074
2 25544 51
6390 303
9390 0009134 214
8396 145
2169 15
72005496 34995
Satellite: ISS
Catalog Number: 25544
Epoch time: 09098
53249747 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 303
9390 deg
Eccentricity:
0009134
Arg of perigee: 214
8396 deg
Mean anomaly: 145
2169 deg
Mean motion: 15
72005496 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3499
Checksum: 339
Coasting Arc #9 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2009/099/12:27:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3519577
19 A = 6737666
72 meter
Y = 5711957
38 meter E =
0015433
Z = -494973
61 I = 51
36739
XDOT = -3874
932754 Wp = 174
02450
YDOT = -2904
031302 meter/sec RA = 298
26016 deg
ZDOT = -5990
896421 TA = 11
37998
MA = 11
34513
Ha = 193
584 n
mi
Hp = 188
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11547169
26 X = -3580783
15
Y = 18740017
66 feet Y = 5672257
16 meter
Z = -1623929
17 Z = -512220
99
XDOT = -12713
033969 XDOT = -3813
068364
YDOT = -9527
661752 feet/sec YDOT = -2947
017584 meter/sec
ZDOT = -19655
171986 ZDOT = -6009
570583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2958973
65 X = -901895
17
Y = 21807061
74 feet Y = 6646792
42 meter
Z = -1690875
28 Z = -515378
78
XDOT = -13788
240348 XDOT = -4202
655658
YDOT = -3392
822548 feet/sec YDOT = -1034
132313 meter/sec
ZDOT = -19728
281677 ZDOT = -6013
180255
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 09099
54961704
00010596 00000-0 82463-4 0 9081
2 25544 51
6393 298
7315 0009049 219
5916 140
4586 15
72034034 35150
Satellite: ISS
Catalog Number: 25544
Epoch time: 09099
54961704 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 298
7315 deg
Eccentricity:
0009049
Arg of perigee: 219
5916 deg
Mean anomaly: 140
4586 deg
Mean motion: 15
72034034 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3515
Checksum: 331
Coasting Arc #10 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2009/100/12:27:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938426
07 A = 6725821
61 meter
Y = 1482169
76 meter E =
0007926
Z = 5250124
60 I = 51
31347
XDOT = -2902
596627 Wp = 207
83752
YDOT = 7125
154092 meter/sec RA = 293
11338 deg
ZDOT = 159
083096 TA = 240
60531
MA = 240
68446
Ha = 193
489 n
mi
Hp = 188
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12921345
36 X = 3896054
95
Y = 4862761
67 feet Y = 1525974
89 meter
Z = 17224818
23 Z = 5269154
75
XDOT = -9522
954812 XDOT = -2982
828373
YDOT = 23376
489804 feet/sec YDOT = 7092
246973 meter/sec
ZDOT = 521
926167 ZDOT = 144
786832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13677519
31 X = 4168907
89
Y = -982067
47 feet Y = -299334
17 meter
Z = 17299219
32 Z = 5272802
05
XDOT = 1120
541116 XDOT = 341
540932
YDOT = 24217
305810 feet/sec YDOT = 7381
434811 meter/sec
ZDOT = 466
599068 ZDOT = 142
219396
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 09100
56672430
00010596 00000-0 82463-4 0 9092
2 25544 51
6385 293
5220 0009072 222
5607 137
4852 15
71996488 35315
Satellite: ISS
Catalog Number: 25544
Epoch time: 09100
56672430 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 293
5220 deg
Eccentricity:
0009072
Arg of perigee: 222
5607 deg
Mean anomaly: 137
4852 deg
Mean motion: 15
71996488 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3531
Checksum: 317
Coasting Arc #11 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2009/101/12:27:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1480944
74 A = 6737449
61 meter
Y = -6527922
27 meter E =
0001775
Z = -755280
38 I = 51
34259
XDOT = 4864
546188 Wp = 2
90927
YDOT = 415
996610 meter/sec RA = 287
96043 deg
ZDOT = 5945
224856 TA = 348
83564
MA = 348
83958
Ha = 193
323 n
mi
Hp = 188
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4858742
57 X = 1557500
06
Y = -21417067
82 feet Y = -6510933
46 meter
Z = -2477954
02 Z = -747899
71
XDOT = 15959
797204 XDOT = 4830
651623
YDOT = 1364
818275 feet/sec YDOT = 470
205448 meter/sec
ZDOT = 19505
330894 ZDOT = 5968
774842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4957750
14 X = -1511122
24
Y = -21397632
51 feet Y = -6521998
39 meter
Z = -2449584
88 Z = -746633
47
XDOT = 13294
583696 XDOT = 4052
189111
YDOT = -5322
893423 feet/sec YDOT = -1622
417915 meter/sec
ZDOT = 19597
306444 ZDOT = 5973
259004
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 09101
52024636
00010596 00000-0 82463-4 0 9100
2 25544 51
6382 288
6378 0009159 226
2437 133
7968 15
72061682 35462
Satellite: ISS
Catalog Number: 25544
Epoch time: 09101
52024636 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 288
6378 deg
Eccentricity:
0009159
Arg of perigee: 226
2437 deg
Mean anomaly: 133
7968 deg
Mean motion: 15
72061682 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3546
Checksum: 322
Coasting Arc #12 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2009/102/12:27:04
881
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4349288
40 A = 6726314
44 meter
Y = 779743
05 meter E =
0007345
Z = -5076452
25 I = 51
29771
XDOT = 446
553467 Wp = 114
50615
YDOT = -7524
111780 meter/sec RA = 282
83710 deg
ZDOT = -1543
046340 TA = 140
62873
MA = 140
57532
Ha = 192
985 n
mi
Hp = 188
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14269318
91 X = -4333023
53
Y = 2558212
10 feet Y = 731197
69 meter
Z = -16655027
07 Z = -5097541
89
XDOT = 1465
070429 XDOT = 538
152105
YDOT = -24685
406102 feet/sec YDOT = -7518
606010 meter/sec
ZDOT = -5062
487992 ZDOT = -1540
654427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11489629
18 X = -3502038
97
Y = 8683228
92 feet Y = 2646648
17 meter
Z = -16737317
43 Z = -5101534
35
XDOT = -9182
460877 XDOT = -2798
814075
YDOT = -21861
457010 feet/sec YDOT = -6663
372097 meter/sec
ZDOT = -5053
663980 ZDOT = -1540
356781
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 09102
53732427
00010596 00000-0 82463-4 0 9117
2 25544 51
6384 283
4296 0009001 229
5289 130
5089 15
72095101 35623
Satellite: ISS
Catalog Number: 25544
Epoch time: 09102
53732427 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 283
4296 deg
Eccentricity:
0009001
Arg of perigee: 229
5289 deg
Mean anomaly: 130
5089 deg
Mean motion: 15
72095101 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3562
Checksum: 300
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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