Date:
February 21st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3218)
---------------------------------------
Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6342873
58 A = 6718953
96 meter
Y = 1845060
83 meter E =
0022367
Z = 1148600
13 I = 51
60624
XDOT = -2338
800492 Wp = 188
07975
YDOT = -4386
871511 meter/sec RA = 351
70056 deg
ZDOT = -5904
152459 TA = 339
29511
MA = 339
38559
Ha = 186
766 n
mi
Hp = 175
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20809952
70 X = -6368613
47
Y = 6053349
18 feet Y = 1773987
44 meter
Z = 3768373
15 Z = 1117724
52
XDOT = -7673
229961 XDOT = -2260
891400
YDOT = -14392
623066 feet/sec YDOT = -4412
590098 meter/sec
ZDOT = -19370
578935 ZDOT = -5915
324535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20906322
01 X = -6372246
95
Y = -5786337
71 feet Y = -1763675
74 meter
Z = 3652642
85 Z = 1113325
54
XDOT = 696
926989 XDOT = 212
423346
YDOT = -14696
630742 feet/sec YDOT = -4479
533050 meter/sec
ZDOT = -19413
088385 ZDOT = -5917
109340
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 07050
53377715
00020000 00000-0 20000-3 0 9009
2 25544 51
6348 352
0191 0020867 225
8056 134
1396 15
78470295 32191
Satellite: ISS
Catalog Number: 25544
Epoch time: 07050
53377715 = yrday
fracday
Element set: 900
Inclination: 51
6348 deg
RA of node: 352
0191 deg
Eccentricity:
0020867
Arg of perigee: 225
8056 deg
Mean anomaly: 134
1396 deg
Mean motion: 15
78470295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3219
Checksum: 292
Coasting Arc #2 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 537541
10 A = 6707238
69 meter
Y = 4156885
52 meter E =
0018431
Z = 5246999
71 I = 51
53929
XDOT = -7545
964159 Wp = 226
61354
YDOT = 1473
779717 meter/sec RA = 346
53384 deg
ZDOT = -407
864555 TA = 227
18804
MA = 227
34312
Ha = 186
325 n
mi
Hp = 175
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1763586
27 X = 465529
71
Y = 13638075
86 feet Y = 4162494
34 meter
Z = 17214565
98 Z = 5249435
84
XDOT = -24757
100260 XDOT = -7559
902046
YDOT = 4835
235292 feet/sec YDOT = 1389
318571 meter/sec
ZDOT = -1338
138303 ZDOT = -444
556184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5526209
34 X = -1684388
61
Y = 12579161
32 feet Y = 3834128
37 meter
Z = 17224237
07 Z = 5249947
46
XDOT = -22833
685869 XDOT = -6959
707453
YDOT = -8070
367203 feet/sec YDOT = -2459
847924 meter/sec
ZDOT = -1475
753243 ZDOT = -449
809589
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 07051
54670221
00020000 00000-0 20000-3 0 9010
2 25544 51
6349 346
7824 0020898 230
0598 129
8732 15
78548380 32352
Satellite: ISS
Catalog Number: 25544
Epoch time: 07051
54670221 = yrday
fracday
Element set: 901
Inclination: 51
6349 deg
RA of node: 346
7824 deg
Eccentricity:
0020898
Arg of perigee: 230
0598 deg
Mean anomaly: 129
8732 deg
Mean motion: 15
78548380 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 304
Coasting Arc #3 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6432397
28 A = 6717617
95 meter
Y = -612142
95 meter E =
0007798
Z = 1856246
49 I = 51
54688
XDOT = -1140
531656 Wp = 208
68332
YDOT = 5111
258800 meter/sec RA = 341
37683 deg
ZDOT = 5640
856767 TA = 171
96191
MA = 171
94941
Ha = 186
033 n
mi
Hp = 175
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21103665
61 X = 6429747
08
Y = -2008343
02 feet Y = -540227
01 meter
Z = 6090047
53 Z = 1887488
29
XDOT = -3741
901758 XDOT = -1225
003646
YDOT = 16769
221786 feet/sec YDOT = 5098
032735 meter/sec
ZDOT = 18506
747923 ZDOT = 5635
110678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19296194
49 X = 5881480
08
Y = 8695580
84 feet Y = 2650413
04 meter
Z = 6207300
11 Z = 1891985
07
XDOT = -11014
679461 XDOT = -3357
274300
YDOT = 11253
441996 feet/sec YDOT = 3430
049120 meter/sec
ZDOT = 18485
808982 ZDOT = 5634
474578
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 07052
55959858
00020000 00000-0 20000-3 0 9029
2 25544 51
6346 341
5440 0020868 233
9056 126
0178 15
78578240 32513
Satellite: ISS
Catalog Number: 25544
Epoch time: 07052
55959858 = yrday
fracday
Element set: 902
Inclination: 51
6346 deg
RA of node: 341
5440 deg
Eccentricity:
0020868
Arg of perigee: 233
9056 deg
Mean anomaly: 126
0178 deg
Mean motion: 15
78578240 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 304
Coasting Arc #4 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2409523
79 A = 6711507
73 meter
Y = -4683329
84 meter E =
0017197
Z = -4160547
94 I = 51
50003
XDOT = 6771
297101 Wp = 215
59687
YDOT = 201
571605 meter/sec RA = 336
15439 deg
ZDOT = 3673
236388 TA = 92
02423
MA = 91
82728
Ha = 185
703 n
mi
Hp = 175
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7905261
78 X = 2481925
36
Y = -15365255
39 feet Y = -4655980
50 meter
Z = -13650091
66 Z = -4148666
59
XDOT = 22215
541670 XDOT = 6750
696103
YDOT = 661
324165 feet/sec YDOT = 277
176950 meter/sec
ZDOT = 12051
300485 ZDOT = 3706
080972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14382214
71 X = 4383699
04
Y = -9640351
28 feet Y = -2938379
07 meter
Z = -13606056
24 Z = -4147125
94
XDOT = 18403
219817 XDOT = 5609
301400
YDOT = 10173
163119 feet/sec YDOT = 3100
780119 meter/sec
ZDOT = 12174
673391 ZDOT = 3710
840450
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 07053
50916092
00020000 00000-0 20000-3 0 9039
2 25544 51
6349 336
6333 0020844 237
4989 122
4162 15
78632389 32664
Satellite: ISS
Catalog Number: 25544
Epoch time: 07053
50916092 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 336
6333 deg
Eccentricity:
0020844
Arg of perigee: 237
4989 deg
Mean anomaly: 122
4162 deg
Mean motion: 15
78632389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3266
Checksum: 305
Coasting Arc #5 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5053834
53 A = 6710770
74 meter
Y = -1084812
02 meter E =
0012127
Z = -4266993
97 I = 51
47314
XDOT = 4139
907579 Wp = 235
39871
YDOT = -5485
762247 meter/sec RA = 331
02293 deg
ZDOT = -3508
410328 TA = 359
06583
MA = 359
06809
Ha = 185
186 n
mi
Hp = 175
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16580821
93 X = -5020600
33
Y = -3559094
54 feet Y = -1141141
01 meter
Z = -13999324
05 Z = -4291464
51
XDOT = 13582
373946 XDOT = 4217
985512
YDOT = -17997
907635 feet/sec YDOT = -5439
030945 meter/sec
ZDOT = -11510
532572 ZDOT = -3488
109204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12950981
92 X = -3947459
29
Y = -10829475
24 feet Y = -3300824
05 meter
Z = -14091359
66 Z = -4295046
42
XDOT = 19664
038551 XDOT = 5993
598950
YDOT = -8635
995001 feet/sec YDOT = -2632
251276 meter/sec
ZDOT = -11434
973205 ZDOT = -3485
379833
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 07054
52199812
00020000 00000-0 20000-3 0 9046
2 25544 51
6354 331
3956 0020786 241
5332 118
3740 15
78689295 32828
Satellite: ISS
Catalog Number: 25544
Epoch time: 07054
52199812 = yrday
fracday
Element set: 904
Inclination: 51
6354 deg
RA of node: 331
3956 deg
Eccentricity:
0020786
Arg of perigee: 241
5332 deg
Mean anomaly: 118
3740 deg
Mean motion: 15
78689295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 306
Coasting Arc #6 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4515624
16 A = 6717652
17 meter
Y = 4673892
83 meter E =
0016311
Z = 1667070
14 I = 51
47160
XDOT = -4581
076664 Wp = 202
20819
YDOT = -2396
407778 meter/sec RA = 325
79881 deg
ZDOT = -5723
134753 TA = 319
27306
MA = 319
39489
Ha = 185
082 n
mi
Hp = 175
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14815039
88 X = -4575650
90
Y = 15334294
05 feet Y = 4623060
94 meter
Z = 5469390
23 Z = 1644987
81
XDOT = -15029
779083 XDOT = -4526
137640
YDOT = -7862
230242 feet/sec YDOT = -2447
328666 meter/sec
ZDOT = -18776
688823 ZDOT = -5745
255913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20157960
01 X = -6144146
21
Y = 7012609
92 feet Y = 2137443
50 meter
Z = 5387036
36 Z = 1641968
68
XDOT = -9278
598765 XDOT = -2828
116903
YDOT = -12267
867359 feet/sec YDOT = -3739
245971 meter/sec
ZDOT = -18860
067049 ZDOT = -5748
548437
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 07055
53480591
00020000 00000-0 20000-3 0 9056
2 25544 51
6352 326
1575 0020855 245
2248 114
6748 15
78702288 32981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07055
53480591 = yrday
fracday
Element set: 905
Inclination: 51
6352 deg
RA of node: 326
1575 deg
Eccentricity:
0020855
Arg of perigee: 245
2248 deg
Mean anomaly: 114
6748 deg
Mean motion: 15
78702288 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3298
Checksum: 309
Coasting Arc #7 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2759464
57 A = 6706480
48 meter
Y = 3154947
02 meter E =
0018827
Z = 5250194
15 I = 51
41194
XDOT = -5890
878998 Wp = 245
88401
YDOT = 4951
177647 meter/sec RA = 320
62901 deg
ZDOT = 113
687557 TA = 202
99090
MA = 203
07528
Ha = 184
678 n
mi
Hp = 175
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9053361
46 X = 2698476
38
Y = 10350876
06 feet Y = 3185463
77 meter
Z = 17225046
44 Z = 5263451
33
XDOT = -19327
030833 XDOT = -5946
358217
YDOT = 16244
021152 feet/sec YDOT = 4884
992347 meter/sec
ZDOT = 372
990674 ZDOT = 84
935546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3568606
94 X = 1087711
39
Y = 13215053
13 feet Y = 4027948
19 meter
Z = 17275231
67 Z = 5265490
61
XDOT = -23504
075315 XDOT = -7164
042156
YDOT = 5968
817477 feet/sec YDOT = 1819
295567 meter/sec
ZDOT = 265
617360 ZDOT = 80
960171
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 07056
54758130
00020000 00000-0 20000-3 0 9066
2 25544 51
6353 320
9187 0020960 249
4423 110
4494 15
78795435 33148
Satellite: ISS
Catalog Number: 25544
Epoch time: 07056
54758130 = yrday
fracday
Element set: 906
Inclination: 51
6353 deg
RA of node: 320
9187 deg
Eccentricity:
0020960
Arg of perigee: 249
4423 deg
Mean anomaly: 110
4494 deg
Mean motion: 15
78795435 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3314
Checksum: 296
Coasting Arc #8 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5427391
28 A = 6717521
93 meter
Y = -3665946
96 meter E =
0007539
Z = 1497908
57 I = 51
42835
XDOT = 1668
004096 Wp = 274
33203
YDOT = 4817
819737 meter/sec RA = 315
45391 deg
ZDOT = 5772
775204 TA = 102
23664
MA = 102
15221
Ha = 184
422 n
mi
Hp = 175
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17806401
84 X = 5460704
65
Y = -12027385
03 feet Y = -3605068
60 meter
Z = 4914398
19 Z = 1524355
07
XDOT = 5472
454383 XDOT = 1585
964124
YDOT = 15806
495201 feet/sec YDOT = 4836
013463 meter/sec
ZDOT = 18939
551193 ZDOT = 5780
679010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21182611
01 X = 6456459
84
Y = -3470058
61 feet Y = -1057673
86 meter
Z = 5013275
40 Z = 1528046
34
XDOT = -2003
797573 XDOT = -610
757500
YDOT = 15055
930355 feet/sec YDOT = 4589
047572 meter/sec
ZDOT = 18969
841439 ZDOT = 5782
007671
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 07057
56032950
00020000 00000-0 20000-3 0 9075
2 25544 51
6356 315
6794 0020862 253
5709 106
3163 15
78804026 33302
Satellite: ISS
Catalog Number: 25544
Epoch time: 07057
56032950 = yrday
fracday
Element set: 907
Inclination: 51
6356 deg
RA of node: 315
6794 deg
Eccentricity:
0020862
Arg of perigee: 253
5709 deg
Mean anomaly: 106
3163 deg
Mean motion: 15
78804026 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3330
Checksum: 289
Coasting Arc #9 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -200588
58 A = 6710157
19 meter
Y = -5117722
33 meter E =
0014346
Z = -4329584
62 I = 51
38465
XDOT = 6184
380434 Wp = 236
78842
YDOT = -3121
737914 meter/sec RA = 310
22547 deg
ZDOT = 3387
660833 TA = 67
49733
MA = 67
34552
Ha = 184
182 n
mi
Hp = 175
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -658099
03 X = -122314
80
Y = -16790427
58 feet Y = -5119527
74 meter
Z = -14204673
94 Z = -4330368
96
XDOT = 20289
962055 XDOT = 6202
372323
YDOT = -10241
922290 feet/sec YDOT = -3052
480144 meter/sec
ZDOT = 11114
372813 ZDOT = 3417
747419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6242988
45 X = 1902862
88
Y = -15597262
20 feet Y = -4754045
52 meter
Z = -14208265
96 Z = -4330679
46
XDOT = 21503
162159 XDOT = 6554
163826
YDOT = -1667
569593 feet/sec YDOT = -508
275212 meter/sec
ZDOT = 11226
993177 ZDOT = 3421
987520
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 07058
50975167
00020000 00000-0 20000-3 0 9087
2 25544 51
6359 310
7682 0020966 257
2948 102
5874 15
78862951 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 07058
50975167 = yrday
fracday
Element set: 908
Inclination: 51
6359 deg
RA of node: 310
7682 deg
Eccentricity:
0020966
Arg of perigee: 257
2948 deg
Mean anomaly: 102
5874 deg
Mean motion: 15
78862951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3345
Checksum: 331
Coasting Arc #10 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2007/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5071705
76 A = 6710687
05 meter
Y = 1487731
57 meter E =
0013322
Z = -4123179
91 I = 51
36942
XDOT = 1066
388101 Wp = 267
86668
YDOT = -6679
141791 meter/sec RA = 305
08427 deg
ZDOT = -3711
890880 TA = 324
07376
MA = 324
16326
Ha = 183
892 n
mi
Hp = 174
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16639454
58 X = -5067935
78
Y = 4881009
09 feet Y = 1431037
94 meter
Z = -13527493
16 Z = -4147808
39
XDOT = 3498
648624 XDOT = 1159
027125
YDOT = -21913
194851 feet/sec YDOT = -6666
698926 meter/sec
ZDOT = -12178
119685 ZDOT = -3706
485411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17161061
21 X = -5230691
46
Y = -1920226
95 feet Y = -585285
17 meter
Z = -13619819
24 Z = -4151320
90
XDOT = 11640
622305 XDOT = 3548
061679
YDOT = -17566
630310 feet/sec YDOT = -5354
308918 meter/sec
ZDOT = -12158
666330 ZDOT = -3705
961497
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 07059
52243993
00020000 00000-0 20000-3 0 9096
2 25544 51
6358 305
5297 0021072 261
4000 98
4778 15
78908721 33610
Satellite: ISS
Catalog Number: 25544
Epoch time: 07059
52243993 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 305
5297 deg
Eccentricity:
0021072
Arg of perigee: 261
4000 deg
Mean anomaly: 98
4778 deg
Mean motion: 15
78908721 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3361
Checksum: 308
Coasting Arc #11 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2007/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1888744
42 A = 6716787
83 meter
Y = 6185229
54 meter E =
0011091
Z = 1802625
05 I = 51
37433
XDOT = -5234
705529 Wp = 225
53684
YDOT = 41
556981 meter/sec RA = 299
84933 deg
ZDOT = -5656
369251 TA = 294
36174
MA = 294
47748
Ha = 183
846 n
mi
Hp = 174
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6196668
04 X = -1966524
73
Y = 20292747
82 feet Y = 6163673
72 meter
Z = 5914124
19 Z = 1793260
65
XDOT = -17174
230737 XDOT = -5207
304380
YDOT = 136
341802 feet/sec YDOT = -16
827431 meter/sec
ZDOT = -18557
641899 ZDOT = -5681
732129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13325325
67 X = -4061559
26
Y = 16523784
92 feet Y = 5036449
64 meter
Z = 5879745
02 Z = 1792146
28
XDOT = -14693
685201 XDOT = -4478
635249
YDOT = -5246
147104 feet/sec YDOT = -1599
025637 meter/sec
ZDOT = -18652
913722 ZDOT = -5685
408103
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 07060
53509984
00020000 00000-0 20000-3 0 9106
2 25544 51
6355 300
2908 0020917 264
9480 94
9298 15
78926669 33771
Satellite: ISS
Catalog Number: 25544
Epoch time: 07060
53509984 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 300
2908 deg
Eccentricity:
0020917
Arg of perigee: 264
9480 deg
Mean anomaly: 94
9298 deg
Mean motion: 15
78926669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3377
Checksum: 329
Coasting Arc #12 (Orbit 3392)
---------------------------------------
Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3900221
57 A = 6705899
06 meter
Y = 1562350
57 meter E =
0018659
Z = 5242554
29 I = 51
32490
XDOT = -3075
309555 Wp = 267
69279
YDOT = 7051
716251 meter/sec RA = 294
67257 deg
ZDOT = 186
214903 TA = 180
53003
MA = 180
53201
Ha = 183
723 n
mi
Hp = 174
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12796002
52 X = 3856994
62
Y = 5125822
07 feet Y = 1605723
65 meter
Z = 17199981
26 Z = 5261395
93
XDOT = -10089
598278 XDOT = -3154
838866
YDOT = 23135
552005 feet/sec YDOT = 7016
881762 meter/sec
ZDOT = 610
941282 ZDOT = 171
081875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10046907
45 X = 3062297
39
Y = 9307226
45 feet Y = 2836842
62 meter
Z = 17270966
23 Z = 5264190
51
XDOT = -16982
250548 XDOT = -5176
189967
YDOT = 17300
948220 feet/sec YDOT = 5273
329018 meter/sec
ZDOT = 555
014299 ZDOT = 169
168358
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 07061
54772688
00020000 00000-0 20000-3 0 9112
2 25544 51
6353 295
0507 0021038 269
2399 90
6356 15
79003334 33939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07061
54772688 = yrday
fracday
Element set: 911
Inclination: 51
6353 deg
RA of node: 295
0507 deg
Eccentricity:
0021038
Arg of perigee: 269
2399 deg
Mean anomaly: 90
6356 deg
Mean motion: 15
79003334 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3393
Checksum: 303
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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