Date:
February 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2008/049/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 395095
15 A = 6722818
83 meter
Y = -6699035
77 meter E =
0020016
Z = 193466
09 I = 51
33147
XDOT = 4800
565648 Wp = 48
15843
YDOT = 467
984245 meter/sec RA = 272
05329 deg
ZDOT = 6015
935791 TA = 313
95678
MA = 314
12172
Ha = 187
451 n
mi
Hp = 176
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1296243
95 X = 469035
65
Y = -21978463
80 feet Y = -6694204
17 meter
Z = 634731
28 Z = 195564
88
XDOT = 15749
887296 XDOT = 4765
752393
YDOT = 1535
381381 feet/sec YDOT = 521
472147 meter/sec
ZDOT = 19737
322149 ZDOT = 6039
171645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1548356
75 X = -471939
14
Y = -21961930
42 feet Y = -6693996
39 meter
Z = 642033
47 Z = 195691
80
XDOT = 14103
775326 XDOT = 4298
830719
YDOT = -378
236477 feet/sec YDOT = -115
286478 meter/sec
ZDOT = 19826
287424 ZDOT = 6043
052407
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 08049
67465245
00020000 00000-0 20000-3 0 9009
2 25544 51
6357 272
4618 0007359 50
2007 309
9805 15
77293225 9676
Satellite: ISS
Catalog Number: 25544
Epoch time: 08049
67465245 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 272
4618 deg
Eccentricity:
0007359
Arg of perigee: 50
2007 deg
Mean anomaly: 309
9805 deg
Mean motion: 15
77293225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 967
Checksum: 307
Coasting Arc #2 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2008/050/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157650
80 A = 6711328
72 meter
Y = -1451414
10 meter E =
0019708
Z = -5081087
17 I = 51
29312
XDOT = 792
401010 Wp = 85
63943
YDOT = -7502
633767 meter/sec RA = 266
85366 deg
ZDOT = 1501
218874 TA = 198
80696
MA = 198
87986
Ha = 187
432 n
mi
Hp = 176
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13640586
61 X = -4116429
67
Y = -4761857
28 feet Y = -1497676
89 meter
Z = -16670233
50 Z = -5101184
23
XDOT = 2599
740845 XDOT = 868
945316
YDOT = -24614
940180 feet/sec YDOT = -7493
344690 meter/sec
ZDOT = 4925
258772 ZDOT = 1505
254229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14095420
76 X = -4296284
25
Y = -2735790
42 feet Y = -833868
92 meter
Z = -16747302
38 Z = -5104577
76
XDOT = -1244
346870 XDOT = -379
276926
YDOT = -23699
015194 feet/sec YDOT = -7223
459831 meter/sec
ZDOT = 4939
870405 ZDOT = 1505
672499
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 08050
62498546
00020000 00000-0 20000-3 0 9017
2 25544 51
6353 267
5565 0007384 54
8174 305
3682 15
77347462 9824
Satellite: ISS
Catalog Number: 25544
Epoch time: 08050
62498546 = yrday
fracday
Element set: 901
Inclination: 51
6353 deg
RA of node: 267
5565 deg
Eccentricity:
0007384
Arg of perigee: 54
8174 deg
Mean anomaly: 305
3682 deg
Mean motion: 15
77347462 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 982
Checksum: 313
Coasting Arc #3 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2008/051/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1028551
05 A = 6719946
57 meter
Y = 6199573
10 meter E =
0010346
Z = -2389365
19 I = 51
32584
XDOT = -4745
015982 Wp = 88
93582
YDOT = -2842
925475 meter/sec RA = 261
70240 deg
ZDOT = -5353
585481 TA = 118
14279
MA = 118
03821
Ha = 187
393 n
mi
Hp = 176
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3374511
31 X = -1086192
45
Y = 20339806
76 feet Y = 6187748
88 meter
Z = -7839124
63 Z = -2394501
97
XDOT = -15567
637735 XDOT = -4686
867363
YDOT = -9327
183316 feet/sec YDOT = -2895
662027 meter/sec
ZDOT = -17564
256826 ZDOT = -5376
494692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 25887
14 X = 7890
40
Y = 20610598
68 feet Y = 6282110
48 meter
Z = -7858084
52 Z = -2395144
16
XDOT = -15277
018778 XDOT = -4656
435324
YDOT = -6686
314117 feet/sec YDOT = -2037
988543 meter/sec
ZDOT = -17652
250565 ZDOT = -5380
405972
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 08051
63864320
00020000 00000-0 20000-3 0 9027
2 25544 51
6353 262
3241 0007485 57
4446 302
7441 15
77422835 9980
Satellite: ISS
Catalog Number: 25544
Epoch time: 08051
63864320 = yrday
fracday
Element set: 902
Inclination: 51
6353 deg
RA of node: 262
3241 deg
Eccentricity:
0007485
Arg of perigee: 57
4446 deg
Mean anomaly: 302
7441 deg
Mean motion: 15
77422835 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 998
Checksum: 289
Coasting Arc #4 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2008/052/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139318
49 A = 6715264
85 meter
Y = 3412513
09 meter E =
0017850
Z = 4028900
47 I = 51
31484
XDOT = -1598
677938 Wp = 70
89589
YDOT = 6494
331756 meter/sec RA = 256
46967 deg
ZDOT = -3838
671063 TA = 58
81209
MA = 58
63722
Ha = 187
297 n
mi
Hp = 176
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13580441
24 X = 4081280
48
Y = 11195909
08 feet Y = 3458477
04 meter
Z = 13218177
40 Z = 4048867
54
XDOT = -5245
006359 XDOT = -1652
532693
YDOT = 21306
862716 feet/sec YDOT = 6476
153078 meter/sec
ZDOT = -12594
065168 ZDOT = -3846
568425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15297819
16 X = 4662775
28
Y = 8585867
15 feet Y = 2616972
31 meter
Z = 13294983
74 Z = 4052311
04
XDOT = -633
138657 XDOT = -192
980663
YDOT = 20774
266438 feet/sec YDOT = 6331
996410 meter/sec
ZDOT = -12623
546207 ZDOT = -3847
656884
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 08052
65227067
00020000 00000-0 20000-3 0 9032
2 25544 51
6345 257
0908 0007313 62
1140 298
0764 15
77426941 10143
Satellite: ISS
Catalog Number: 25544
Epoch time: 08052
65227067 = yrday
fracday
Element set: 903
Inclination: 51
6345 deg
RA of node: 257
0908 deg
Eccentricity:
0007313
Arg of perigee: 62
1140 deg
Mean anomaly: 298
0764 deg
Mean motion: 15
77426941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1014
Checksum: 277
Coasting Arc #5 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2008/053/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1824262
88 A = 6714652
84 meter
Y = -4951116
71 meter E =
0016560
Z = 4138344
99 I = 51
32211
XDOT = 4747
206145 Wp = 89
29621
YDOT = 4838
695681 meter/sec RA = 251
33538 deg
ZDOT = 3683
895094 TA = 322
93734
MA = 323
05160
Ha = 187
181 n
mi
Hp = 175
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5985114
43 X = 1859388
58
Y = -16243821
22 feet Y = -4930520
05 meter
Z = 13577247
33 Z = 4147292
74
XDOT = 15574
823310 XDOT = 4674
851000
YDOT = 15874
985831 feet/sec YDOT = 4891
377365 meter/sec
ZDOT = 12086
269994 ZDOT = 3706
780375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2598333
53 X = 791972
06
Y = -17088490
94 feet Y = -5208572
04 meter
Z = 13610918
70 Z = 4148608
02
XDOT = 17078
969838 XDOT = 5205
670007
YDOT = 12326
243569 feet/sec YDOT = 3757
039040 meter/sec
ZDOT = 12174
416011 ZDOT = 3710
762000
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 08053
66586464
00020000 00000-0 20000-3 0 9044
2 25544 51
6349 251
8577 0007233 65
9901 294
2020 15
77518045 10306
Satellite: ISS
Catalog Number: 25544
Epoch time: 08053
66586464 = yrday
fracday
Element set: 904
Inclination: 51
6349 deg
RA of node: 251
8577 deg
Eccentricity:
0007233
Arg of perigee: 65
9901 deg
Mean anomaly: 294
2020 deg
Mean motion: 15
77518045 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1030
Checksum: 292
Coasting Arc #6 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2008/054/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4083385
42 A = 6719932
59 meter
Y = -4857035
89 meter E =
0013041
Z = -2208507
49 I = 51
35222
XDOT = 2682
761114 Wp = 57
79054
YDOT = -4724
572520 meter/sec RA = 246
10547 deg
ZDOT = 5460
520565 TA = 277
31945
MA = 277
46765
Ha = 187
225 n
mi
Hp = 175
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13396933
81 X = -4018041
48
Y = -15935157
11 feet Y = -4902333
45 meter
Z = -7245759
49 Z = -2228185
12
XDOT = 8801
709692 XDOT = 2708
866886
YDOT = -15500
566012 feet/sec YDOT = -4694
425960 meter/sec
ZDOT = 17915
093717 ZDOT = 5473
616961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16449669
47 X = -5013859
25
Y = -12716528
47 feet Y = -3875997
88 meter
Z = -7321637
54 Z = -2231635
12
XDOT = 4262
963573 XDOT = 1299
351297
YDOT = -15801
063982 feet/sec YDOT = -4816
164302 meter/sec
ZDOT = 17964
665051 ZDOT = 5475
629907
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 08054
61608172
00020000 00000-0 20000-3 0 9052
2 25544 51
6362 246
9519 0007349 69
5909 290
6045 15
77542120 10452
Satellite: ISS
Catalog Number: 25544
Epoch time: 08054
61608172 = yrday
fracday
Element set: 905
Inclination: 51
6362 deg
RA of node: 246
9519 deg
Eccentricity:
0007349
Arg of perigee: 69
5909 deg
Mean anomaly: 290
6045 deg
Mean motion: 15
77542120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1045
Checksum: 296
Coasting Arc #7 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2008/055/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2942254
22 A = 6710346
78 meter
Y = 3179474
09 meter E =
0021633
Z = -5143721
09 I = 51
33382
XDOT = -4501
711489 Wp = 78
01246
YDOT = -6117
519697 meter/sec RA = 240
95250 deg
ZDOT = -1206
234981 TA = 180
39829
MA = 180
40001
Ha = 187
196 n
mi
Hp = 175
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9653065
03 X = -2952601
99
Y = 10431345
43 feet Y = 3146513
89 meter
Z = -16875725
37 Z = -5158039
73
XDOT = -14769
394649 XDOT = -4427
110272
YDOT = -20070
602679 feet/sec YDOT = -6167
443373 meter/sec
ZDOT = -3957
463850 ZDOT = -1227
922341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6898501
26 X = -2102663
19
Y = 12351732
40 feet Y = 3764808
03 meter
Z = -16930154
33 Z = -5160311
04
XDOT = -18071
202756 XDOT = -5508
102600
YDOT = -15632
666847 feet/sec YDOT = -4764
836855 meter/sec
ZDOT = -4041
186605 ZDOT = -1231
753677
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 08055
62961388
00020000 00000-0 20000-3 0 9066
2 25544 51
6366 241
7195 0007397 72
6170 287
5803 15
77608473 10616
Satellite: ISS
Catalog Number: 25544
Epoch time: 08055
62961388 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 241
7195 deg
Eccentricity:
0007397
Arg of perigee: 72
6170 deg
Mean anomaly: 287
5803 deg
Mean motion: 15
77608473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1061
Checksum: 314
Coasting Arc #8 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/056/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3663280
34 A = 6721764
66 meter
Y = 5628064
82 meter E =
0016790
Z = -173328
47 I = 51
38793
XDOT = -4109
625798 Wp = 114
01720
YDOT = 2503
892421 meter/sec RA = 235
75893 deg
ZDOT = -6018
041841 TA = 67
87513
MA = 67
69699
Ha = 187
093 n
mi
Hp = 175
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12018636
27 X = 3600916
17
Y = 18464779
61 feet Y = 5668681
01 meter
Z = -568662
97 Z = -155684
26
XDOT = -13483
024273 XDOT = -4108
085026
YDOT = 8214
870148 feet/sec YDOT = 2457
944502 meter/sec
ZDOT = -19744
231763 ZDOT = -6038
002593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16209432
17 X = 4940634
93
Y = 14923904
38 feet Y = 4548806
06 meter
Z = -500467
81 Z = -152542
59
XDOT = -9839
639197 XDOT = -2999
122027
YDOT = 10080
575147 feet/sec YDOT = 3072
559305 meter/sec
ZDOT = -19820
336183 ZDOT = -6041
238469
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 08056
64311259
00020000 00000-0 20000-3 0 9076
2 25544 51
6362 236
4848 0007295 75
3682 284
8291 15
77662812 10778
Satellite: ISS
Catalog Number: 25544
Epoch time: 08056
64311259 = yrday
fracday
Element set: 907
Inclination: 51
6362 deg
RA of node: 236
4848 deg
Eccentricity:
0007295
Arg of perigee: 75
3682 deg
Mean anomaly: 284
8291 deg
Mean motion: 15
77662812 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 316
Coasting Arc #9 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/057/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239997
30 A = 6710462
86 meter
Y = -1200982
16 meter E =
0011964
Z = 5052022
80 I = 51
36853
XDOT = 3751
173158 Wp = 69
52049
YDOT = 6552
633606 meter/sec RA = 230
56215 deg
ZDOT = -1583
375991 TA = 35
75199
MA = 35
67195
Ha = 187
008 n
mi
Hp = 175
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13910752
29 X = 4228570
15
Y = -3940230
19 feet Y = -1153631
78 meter
Z = 16574877
94 Z = 5072592
81
XDOT = 12306
998549 XDOT = 3685
313487
YDOT = 21498
141751 feet/sec YDOT = 6594
213058 meter/sec
ZDOT = -5194
803119 ZDOT = -1565
313198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12289265
72 X = 3745768
19
Y = -7442906
11 feet Y = -2268597
78 meter
Z = 16653471
68 Z = 5075978
17
XDOT = 17024
045842 XDOT = 5188
929173
YDOT = 16589
893262 feet/sec YDOT = 5056
599466 meter/sec
ZDOT = -5124
892463 ZDOT = -1562
067223
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 08057
65657992
00020000 00000-0 20000-3 0 9086
2 25544 51
6373 231
2519 0007383 79
1940 281
0056 15
77669595 10936
Satellite: ISS
Catalog Number: 25544
Epoch time: 08057
65657992 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 231
2519 deg
Eccentricity:
0007383
Arg of perigee: 79
1940 deg
Mean anomaly: 281
0056 deg
Mean motion: 15
77669595 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 324
Coasting Arc #10 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2008/058/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2698450
24 A = 6718705
36 meter
Y = -5602215
48 meter E =
0021063
Z = 2520216
64 I = 51
41778
XDOT = 5610
904680 Wp = 78
45290
YDOT = -311
199967 meter/sec RA = 225
41620 deg
ZDOT = 5282
988332 TA = 310
26544
MA = 310
44943
Ha = 186
923 n
mi
Hp = 175
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8853183
20 X = -2647847
49
Y = -18379972
04 feet Y = -5632108
09 meter
Z = 8268427
30 Z = 2507230
73
XDOT = 18408
479922 XDOT = 5588
303975
YDOT = -1020
997267 feet/sec YDOT = -248
581875 meter/sec
ZDOT = 17332
638884 ZDOT = 5310
190976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13692693
27 X = -4173532
91
Y = -15150669
88 feet Y = -4617924
18 meter
Z = 8218057
44 Z = 2504863
91
XDOT = 16185
863342 XDOT = 4933
451147
YDOT = -5111
187613 feet/sec YDOT = -1557
889985 meter/sec
ZDOT = 17436
732162 ZDOT = 5314
715963
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 08058
67000896
00020000 00000-0 20000-3 0 9095
2 25544 51
6382 226
0187 0007228 83
0307 277
1680 15
77782102 11095
Satellite: ISS
Catalog Number: 25544
Epoch time: 08058
67000896 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 226
0187 deg
Eccentricity:
0007228
Arg of perigee: 83
0307 deg
Mean anomaly: 277
1680 deg
Mean motion: 15
77782102 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 292
Coasting Arc #11 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2008/059/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5467940
79 A = 6714794
73 meter
Y = -582484
48 meter E =
0013567
Z = -3866304
60 I = 51
42631
XDOT = -2222
824221 Wp = 95
48666
YDOT = -6136
247599 meter/sec RA = 220
18867 deg
ZDOT = 4079
081254 TA = 217
14780
MA = 217
24176
Ha = 186
849 n
mi
Hp = 175
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17939438
28 X = -5442239
35
Y = -1911038
32 feet Y = -643486
44 meter
Z = -12684726
37 Z = -3892805
15
XDOT = -7292
730384 XDOT = -2173
857789
YDOT = -20132
045927 feet/sec YDOT = -6160
830665 meter/sec
ZDOT = 13382
812514 ZDOT = 4068
401875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17629960
89 X = -5373612
08
Y = 3474792
23 feet Y = 1059116
67 meter
Z = -12786246
29 Z = -3897247
87
XDOT = -12755
094144 XDOT = -3887
752695
YDOT = -15754
783407 feet/sec YDOT = -4802
057983 meter/sec
ZDOT = 13341
204690 ZDOT = 4066
399190
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 08059
62007056
00020000 00000-0 20000-3 0 9108
2 25544 51
6382 221
1129 0007151 84
4728 275
7252 15
77786934 11247
Satellite: ISS
Catalog Number: 25544
Epoch time: 08059
62007056 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 221
1129 deg
Eccentricity:
0007151
Arg of perigee: 84
4728 deg
Mean anomaly: 275
7252 deg
Mean motion: 15
77786934 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1124
Checksum: 287
Coasting Arc #12 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2008/060/14:40:48
045
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 989087
94 A = 6712831
70 meter
Y = 4982431
49 meter E =
0016214
Z = -4404063
72 I = 51
44345
XDOT = -6779
679412 Wp = 77
79886
YDOT = -1555
204380 meter/sec RA = 215
05930 deg
ZDOT = -3288
863720 TA = 159
09899
MA = 159
03263
Ha = 186
781 n
mi
Hp = 175
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3245039
17 X = 954693
99
Y = 16346560
01 feet Y = 4993299
73 meter
Z = -14449027
96 Z = -4399342
33
XDOT = -22243
042690 XDOT = -6745
808488
YDOT = -5102
376574 feet/sec YDOT = -1630
829237 meter/sec
ZDOT = -10790
235302 ZDOT = -3321
716726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8276305
54 X = 2522617
93
Y = 14483857
55 feet Y = 4414679
78 meter
Z = -14430362
07 Z = -4398374
36
XDOT = -21607
795152 XDOT = -6586
055962
YDOT = 1493
423530 feet/sec YDOT = 455
195492 meter/sec
ZDOT = -10916
201711 ZDOT = -3327
258282
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 08060
63343439
00020000 00000-0 20000-3 0 9110
2 25544 51
6384 215
8786 0007120 88
3381 271
8600 15
77843983 11402
Satellite: ISS
Catalog Number: 25544
Epoch time: 08060
63343439 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 215
8786 deg
Eccentricity:
0007120
Arg of perigee: 88
3381 deg
Mean anomaly: 271
8600 deg
Mean motion: 15
77843983 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 294
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 may contain past, current and future orbital data 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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