Date:
January 20th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 2209)
---------------------------------------
Vector Time (GMT): 2009/016/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128696
28 A = 6737721
70 meter
Y = -2863364
79 meter E =
0003320
Z = -3298061
42 I = 51
66039
XDOT = 4980
607130 Wp = 273
61080
YDOT = -3487
405150 meter/sec RA = 2
81148 deg
ZDOT = -4713
137898 TA = 305
01228
MA = 305
04344
Ha = 193
230 n
mi
Hp = 192
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16826431
37 X = -5080275
32
Y = -9394241
44 feet Y = -2920445
98 meter
Z = -10820411
48 Z = -3322858
80
XDOT = 16340
574575 XDOT = 5042
128965
YDOT = -11441
617947 feet/sec YDOT = -3431
364932 meter/sec
ZDOT = -15463
050848 ZDOT = -4688
793142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1190467
95 X = -362854
63
Y = -19179707
81 feet Y = -5845974
94 meter
Z = -10917117
93 Z = -3327537
55
XDOT = 17121
298143 XDOT = 5218
571674
YDOT = 7692
969203 feet/sec YDOT = 2344
817013 meter/sec
ZDOT = -15368
487999 ZDOT = -4684
315142
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 09016
54575237
00010596 00000-0 82463-4 0 9004
2 25544 51
6401 3
1542 0008078 273
4222 86
6015 15
70373981 22104
Satellite: ISS
Catalog Number: 25544
Epoch time: 09016
54575237 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 3
1542 deg
Eccentricity:
0008078
Arg of perigee: 273
4222 deg
Mean anomaly: 86
6015 deg
Mean motion: 15
70373981 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2210
Checksum: 278
Coasting Arc #2 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2009/017/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2780331
06 A = 6732747
47 meter
Y = 3880524
65 meter E =
0004905
Z = 4750979
18 I = 51
61404
XDOT = -7002
566046 Wp = 342
30696
YDOT = -1796
366683 meter/sec RA = 357
65834 deg
ZDOT = -2626
865306 TA = 133
54285
MA = 133
50210
Ha = 193
771 n
mi
Hp = 192
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9121821
06 X = -2846596
24
Y = 12731380
07 feet Y = 3849062
62 meter
Z = 15587202
03 Z = 4737311
71
XDOT = -22974
298052 XDOT = -6969
197628
YDOT = -5893
591479 feet/sec YDOT = -1874
486732 meter/sec
ZDOT = -8618
324495 ZDOT = -2660
802462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15704076
46 X = -4786602
51
Y = -571177
46 feet Y = -174094
89 meter
Z = 15534228
78 Z = 4734832
93
XDOT = -7898
088749 XDOT = -2407
337451
YDOT = -21182
686088 feet/sec YDOT = -6456
482719 meter/sec
ZDOT = -8750
543518 ZDOT = -2667
165664
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 09017
56392417
00010596 00000-0 82463-4 0 9015
2 25544 51
6400 357
9537 0008225 277
5404 82
4822 15
70397006 22269
Satellite: ISS
Catalog Number: 25544
Epoch time: 09017
56392417 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 357
9537 deg
Eccentricity:
0008225
Arg of perigee: 277
5404 deg
Mean anomaly: 82
4822 deg
Mean motion: 15
70397006 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2226
Checksum: 304
Coasting Arc #3 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2009/018/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6627567
02 A = 6741641
74 meter
Y = 92736
75 meter E =
0009494
Z = 1196501
39 I = 51
61550
XDOT = -1129
838128 Wp = 23
38647
YDOT = 4840
922699 meter/sec RA = 352
58041 deg
ZDOT = 5875
768692 TA = 349
71217
MA = 349
73159
Ha = 193
804 n
mi
Hp = 192
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21743986
29 X = 6620225
11
Y = 304254
42 feet Y = 166808
92 meter
Z = 3925529
50 Z = 1228680
00
XDOT = -3706
818004 XDOT = -1212
429321
YDOT = 15882
292318 feet/sec YDOT = 4827
826012 meter/sec
ZDOT = 19277
456337 ZDOT = 5870
079695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12143155
07 X = 3701233
67
Y = 18012165
38 feet Y = 5490108
01 meter
Z = 4050799
41 Z = 1234683
66
XDOT = -13908
480593 XDOT = -4239
304885
YDOT = 5040
912809 feet/sec YDOT = 1536
470224 meter/sec
ZDOT = 19255
597463 ZDOT = 5869
106107
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 09018
58208012
00010596 00000-0 82463-4 0 9026
2 25544 51
6402 352
7528 0008140 280
4070 79
6174 15
70449627 22425
Satellite: ISS
Catalog Number: 25544
Epoch time: 09018
58208012 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 352
7528 deg
Eccentricity:
0008140
Arg of perigee: 280
4070 deg
Mean anomaly: 79
6174 deg
Mean motion: 15
70449627 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2242
Checksum: 291
Coasting Arc #4 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2009/019/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -858073
70 A = 6730283
22 meter
Y = -4099562
39 meter E =
0007378
Z = -5274289
98 I = 51
54855
XDOT = 7514
868812 Wp = 73
99953
YDOT = -1632
662093 meter/sec RA = 347
45571 deg
ZDOT = 48
483893 TA = 196
44975
MA = 196
47371
Ha = 194
185 n
mi
Hp = 192
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2815202
43 X = -786546
63
Y = -13450007
84 feet Y = -4108757
50 meter
Z = -17304100
98 Z = -5278285
07
XDOT = 24655
081403 XDOT = 7532
331463
YDOT = -5356
502929 feet/sec YDOT = -1548
528836 meter/sec
ZDOT = 159
067889 ZDOT = 85
033082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9325022
02 X = 2842266
71
Y = -10066041
95 feet Y = -3068129
59 meter
Z = -17319894
63 Z = -5279103
88
XDOT = 18024
383283 XDOT = 5493
832025
YDOT = 16190
744961 feet/sec YDOT = 4934
939064 meter/sec
ZDOT = 301
250013 ZDOT = 91
821004
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 09019
53658978
00010596 00000-0 82463-4 0 9033
2 25544 51
6407 347
8767 0008206 285
3740 74
6514 15
70434464 22573
Satellite: ISS
Catalog Number: 25544
Epoch time: 09019
53658978 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 347
8767 deg
Eccentricity:
0008206
Arg of perigee: 285
3740 deg
Mean anomaly: 74
6514 deg
Mean motion: 15
70434464 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2257
Checksum: 336
Coasting Arc #5 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2009/020/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6013259
04 A = 6741769
52 meter
Y = 2833348
16 meter E =
0006120
Z = 1101915
07 I = 51
55944
XDOT = -2952
062691 Wp = 142
18981
YDOT = -3968
588605 meter/sec RA = 342
33170 deg
ZDOT = -5892
782444 TA = 25
75869
MA = 25
72823
Ha = 194
411 n
mi
Hp = 192
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19728540
16 X = -6049847
93
Y = 9295761
67 feet Y = 2765899
72 meter
Z = 3615206
93 Z = 1072614
37
XDOT = -9685
245048 XDOT = -2878
840112
YDOT = -13020
303823 feet/sec YDOT = -4001
190298 meter/sec
ZDOT = -19333
275736 ZDOT = -5906
945944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19266482
29 X = -5872423
80
Y = -10258639
87 feet Y = -3126833
43 meter
Z = 3501309
95 Z = 1067199
27
XDOT = 3953
754970 XDOT = 1205
104515
YDOT = -14057
313606 feet/sec YDOT = -4284
669187 meter/sec
ZDOT = -19388
645012 ZDOT = -5909
659000
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 09020
55471757
00010596 00000-0 82463-4 0 9046
2 25544 51
6411 342
6758 0008221 289
4748 70
5525 15
70461968 22735
Satellite: ISS
Catalog Number: 25544
Epoch time: 09020
55471757 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 342
6758 deg
Eccentricity:
0008221
Arg of perigee: 289
4748 deg
Mean anomaly: 70
5525 deg
Mean motion: 15
70461968 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2273
Checksum: 321
Coasting Arc #6 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2009/021/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051145
45 A = 6732033
17 meter
Y = 2436388
49 meter E =
0001655
Z = 4794511
41 I = 51
50033
XDOT = -5686
645206 Wp = 254
07379
YDOT = 4539
966694 meter/sec RA = 337
24550 deg
ZDOT = 2498
186707 TA = 171
41399
MA = 171
41116
Ha = 194
419 n
mi
Hp = 192
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13291159
60 X = 4000309
71
Y = 7993400
54 feet Y = 2481405
99 meter
Z = 15730024
30 Z = 4814068
39
XDOT = -18656
972462 XDOT = -5749
124792
YDOT = 14894
903853 feet/sec YDOT = 4476
025721 meter/sec
ZDOT = 8196
150612 ZDOT = 2470
410085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1759885
21 X = 536413
01
Y = 15331231
65 feet Y = 4672959
41 meter
Z = 15806301
91 Z = 4817760
82
XDOT = -22109
800263 XDOT = -6739
067120
YDOT = -5800
014346 feet/sec YDOT = -1767
844373 meter/sec
ZDOT = 8088
283828 ZDOT = 2465
308911
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 09021
57282820
00010596 00000-0 82463-4 0 9051
2 25544 51
6417 337
4752 0008330 292
4593 67
5686 15
70524395 22895
Satellite: ISS
Catalog Number: 25544
Epoch time: 09021
57282820 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 337
4752 deg
Eccentricity:
0008330
Arg of perigee: 292
4593 deg
Mean anomaly: 67
5686 deg
Mean motion: 15
70524395 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2289
Checksum: 326
Coasting Arc #7 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2009/022/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3577146
65 A = 6737872
46 meter
Y = -4746349
46 meter E =
0005605
Z = -3166133
01 I = 51
49259
XDOT = 5878
833905 Wp = 327
60583
YDOT = 1219
799173 meter/sec RA = 332
08209 deg
ZDOT = 4814
122802 TA = 355
46503
MA = 355
47010
Ha = 194
805 n
mi
Hp = 191
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11736045
44 X = 3645335
48
Y = -15572012
66 feet Y = -4705966
12 meter
Z = -10387575
51 Z = -3148590
43
XDOT = 19287
512812 XDOT = 5841
371253
YDOT = 4001
965792 feet/sec YDOT = 1285
329709 meter/sec
ZDOT = 15794
366148 ZDOT = 4842
590823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19527869
34 X = 5952094
57
Y = -541341
77 feet Y = -165000
97 meter
Z = -10319560
74 Z = -3145402
11
XDOT = 8848
980106 XDOT = 2697
169136
YDOT = 16054
670053 feet/sec YDOT = 4893
463432 meter/sec
ZDOT = 15905
267103 ZDOT = 4847
925413
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 09022
52729564
00010596 00000-0 82463-4 0 9069
2 25544 51
6414 332
5987 0008337 297
1595 62
8716 15
70498093 23044
Satellite: ISS
Catalog Number: 25544
Epoch time: 09022
52729564 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 332
5987 deg
Eccentricity:
0008337
Arg of perigee: 297
1595 deg
Mean anomaly: 62
8716 deg
Mean motion: 15
70498093 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2304
Checksum: 333
Coasting Arc #8 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2009/023/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772504
40 A = 6736788
66 meter
Y = 477921
44 meter E =
0005050
Z = -3442930
35 I = 51
46520
XDOT = 2241
380255 Wp = 336
21185
YDOT = -5778
148269 meter/sec RA = 327
01198 deg
ZDOT = -4553
168286 TA = 244
57153
MA = 244
62379
Ha = 194
864 n
mi
Hp = 191
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18938662
73 X = -5760694
80
Y = 1567983
73 feet Y = 413436
34 meter
Z = -11295703
25 Z = -3470943
85
XDOT = 7353
609762 XDOT = 2327
943875
YDOT = -18957
179361 feet/sec YDOT = -5752
599370 meter/sec
ZDOT = -14938
216163 ZDOT = -4542
070246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13265949
59 X = -4043461
44
Y = -13515581
74 feet Y = -4119549
31 meter
Z = -11404738
61 Z = -3476164
33
XDOT = 18350
485300 XDOT = 5593
227919
YDOT = -5423
707944 feet/sec YDOT = -1653
146181 meter/sec
ZDOT = -14895
353929 ZDOT = -4540
103878
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 09023
54537793
00010596 00000-0 82463-4 0 9074
2 25544 51
6423 327
3973 0008280 301
3322 58
7028 15
70548456 23201
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023
54537793 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 327
3973 deg
Eccentricity:
0008280
Arg of perigee: 301
3322 deg
Mean anomaly: 58
7028 deg
Mean motion: 15
70548456 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2320
Checksum: 305
Coasting Arc #9 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2009/024/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -265970
90 A = 6732770
81 meter
Y = 4894068
93 meter E =
0008313
Z = 4619369
60 I = 51
42762
XDOT = -6728
273038 Wp = 4
33768
YDOT = 2363
073128 meter/sec RA = 321
84236 deg
ZDOT = -2882
497257 TA = 114
34763
MA = 114
26082
Ha = 195
036 n
mi
Hp = 191
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -872607
95 X = -343116
93
Y = 16056656
60 feet Y = 4890662
90 meter
Z = 15155412
07 Z = 4617890
63
XDOT = -22074
386607 XDOT = -6740
194953
YDOT = 7752
864593 feet/sec YDOT = 2287
767294 meter/sec
ZDOT = -9457
011997 ZDOT = -2915
211128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12798772
11 X = -3901065
74
Y = 9743437
73 feet Y = 2969799
82 meter
Z = 15149951
63 Z = 4617705
26
XDOT = -19526
555942 XDOT = -5951
694251
YDOT = -10703
897237 feet/sec YDOT = -3262
547878 meter/sec
ZDOT = -9584
237032 ZDOT = -2921
275447
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 09024
56344515
00010596 00000-0 82463-4 0 9086
2 25544 51
6424 322
1965 0008264 304
8880 55
1504 15
70555025 23362
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024
56344515 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 322
1965 deg
Eccentricity:
0008264
Arg of perigee: 304
8880 deg
Mean anomaly: 55
1504 deg
Mean motion: 15
70555025 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2336
Checksum: 298
Coasting Arc #10 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2009/025/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5518481
88 A = 6740935
49 meter
Y = -3554552
54 meter E =
0013173
Z = 1494609
22 I = 51
43314
XDOT = 1559
481147 Wp = 26
38368
YDOT = 4851
428136 meter/sec RA = 316
75374 deg
ZDOT = 5772
061910 TA = 350
11198
MA = 350
13788
Ha = 195
119 n
mi
Hp = 191
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18105255
50 X = 5550558
99
Y = -11661917
77 feet Y = -3492662
44 meter
Z = 4903573
55 Z = 1521494
89
XDOT = 5116
407964 XDOT = 1477
076916
YDOT = 15916
758977 feet/sec YDOT = 4868
405951 meter/sec
ZDOT = 18937
210991 ZDOT = 5779
437896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20731178
00 X = 6318863
05
Y = 5743126
13 feet Y = 1750504
85 meter
Z = 5008033
29 Z = 1526448
55
XDOT = -8137
449723 XDOT = -2480
294676
YDOT = 12813
464913 feet/sec YDOT = 3905
544106 meter/sec
ZDOT = 18966
231616 ZDOT = 5780
907397
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 09025
58149668
00010596 00000-0 82463-4 0 9092
2 25544 51
6425 316
9946 0008328 308
9704 51
0715 15
70575315 23525
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025
58149668 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 316
9946 deg
Eccentricity:
0008328
Arg of perigee: 308
9704 deg
Mean anomaly: 51
0715 deg
Mean motion: 15
70575315 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2352
Checksum: 327
Coasting Arc #11 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2789235
47 A = 6729850
05 meter
Y = -3171905
47 meter E =
0009883
Z = -5246477
94 I = 51
37617
XDOT = 5369
525195 Wp = 61
87582
YDOT = -5484
595978 meter/sec RA = 311
60942 deg
ZDOT = 466
467376 TA = 212
54698
MA = 212
60794
Ha = 195
232 n
mi
Hp = 190
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9151035
02 X = -2728073
70
Y = -10406514
01 feet Y = -3202754
03 meter
Z = -17212854
14 Z = -5259879
29
XDOT = 17616
552476 XDOT = 5428
189831
YDOT = -17994
081294 feet/sec YDOT = -5424
222848 meter/sec
ZDOT = 1530
404776 ZDOT = 492
693942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1515827
91 X = 462024
35
Y = -13708872
54 feet Y = -4178464
35 meter
Z = -17265236
84 Z = -5262444
19
XDOT = 24164
746832 XDOT = 7365
414834
YDOT = 638
011907 feet/sec YDOT = 194
466029 meter/sec
ZDOT = 1632
172090 ZDOT = 497
486053
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 09026
53590543
00010596 00000-0 82463-4 0 9102
2 25544 51
6431 312
1185 0008312 312
5395 47
5064 15
70613122 23677
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026
53590543 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 312
1185 deg
Eccentricity:
0008312
Arg of perigee: 312
5395 deg
Mean anomaly: 47
5064 deg
Mean motion: 15
70613122 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 279
Coasting Arc #12 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3537973
32 A = 6741634
47 meter
Y = 5696142
75 meter E =
0005236
Z = 678613
26 I = 51
39724
XDOT = -4417
394355 Wp = 115
43390
YDOT = -2029
625093 meter/sec RA = 306
47953 deg
ZDOT = -5960
375638 TA = 57
16343
MA = 57
11303
Ha = 195
438 n
mi
Hp = 190
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11607524
02 X = -3604702
07
Y = 18688132
40 feet Y = 5656205
96 meter
Z = 2226421
45 Z = 661264
40
XDOT = -14492
763632 XDOT = -4365
416841
YDOT = -6658
874978 feet/sec YDOT = -2078
732121 meter/sec
ZDOT = -19555
038182 ZDOT = -5981
708554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21542271
63 X = -6566084
39
Y = 4495115
27 feet Y = 1370111
13 meter
Z = 2159243
02 Z = 658137
27
XDOT = -4782
039479 XDOT = -1457
565633
YDOT = -13429
435898 feet/sec YDOT = -4093
292062 meter/sec
ZDOT = -19638
235421 ZDOT = -5985
734156
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 09027
55392739
00010596 00000-0 82463-4 0 9113
2 25544 51
6431 306
9170 0008274 315
9930 44
0572 15
70615406 23832
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027
55392739 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 306
9170 deg
Eccentricity:
0008274
Arg of perigee: 315
9930 deg
Mean anomaly: 44
0572 deg
Mean motion: 15
70615406 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 305
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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