Date:
March 6th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 3439)
---------------------------------------
Vector Time (GMT): 2007/064/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174890
66 A = 6705964
03 meter
Y = -413731
34 meter E =
0007292
Z = -5226839
46 I = 51
29709
XDOT = 1039
894085 Wp = 309
25172
YDOT = -7640
325793 meter/sec RA = 279
06696 deg
ZDOT = -221
068718 TA = 318
61615
MA = 318
67137
Ha = 183
894 n
mi
Hp = 174
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13697147
84 X = -4144563
33
Y = -1357386
28 feet Y = -460248
22 meter
Z = -17148423
43 Z = -5247047
05
XDOT = 3411
726001 XDOT = 1126
325910
YDOT = -25066
685673 feet/sec YDOT = -7628
213872 meter/sec
ZDOT = -725
291069 ZDOT = -215
806342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12755396
98 X = -3887845
00
Y = -4913555
63 feet Y = -1497651
76 meter
Z = -17224389
72 Z = -5249993
99
XDOT = 9578
808905 XDOT = 2919
620954
YDOT = -22334
841112 feet/sec YDOT = -6807
659571 meter/sec
ZDOT = -706
549511 ZDOT = -215
356291
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 07064
52309984
00020000 00000-0 20000-3 0 9006
2 25544 51
6325 279
6744 0021128 281
4554 78
4239 15
78973825 34405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07064
52309984 = yrday
fracday
Element set: 900
Inclination: 51
6325 deg
RA of node: 279
6744 deg
Eccentricity:
0021128
Arg of perigee: 281
4554 deg
Mean anomaly: 78
4239 deg
Mean motion: 15
78973825 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3440
Checksum: 313
Coasting Arc #2 (Orbit 3455)
---------------------------------------
Vector Time (GMT): 2007/065/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1587457
11 A = 6717145
12 meter
Y = 6361964
05 meter E =
0015410
Z = -1440860
74 I = 51
33155
XDOT = -4473
525322 Wp = 265
24468
YDOT = -2437
841993 meter/sec RA = 273
88247 deg
ZDOT = -5783
618172 TA = 290
71041
MA = 290
87552
Ha = 184
205 n
mi
Hp = 174
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5208192
62 X = -1651480
16
Y = 20872585
47 feet Y = 6343854
12 meter
Z = -4727233
39 Z = -1448728
60
XDOT = -14676
920349 XDOT = -4417
837079
YDOT = -7998
169269 feet/sec YDOT = -2487
556602 meter/sec
ZDOT = -18975
125235 ZDOT = -5805
214832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10204350
14 X = -3110285
92
Y = 18931170
00 feet Y = 5770220
61 meter
Z = -4755930
09 Z = -1449607
49
XDOT = -10747
116169 XDOT = -3275
721008
YDOT = -10622
772346 feet/sec YDOT = -3237
821011 meter/sec
ZDOT = -19056
582695 ZDOT = -5808
446405
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 07065
53573179
00020000 00000-0 20000-3 0 9018
2 25544 51
6324 274
4354 0021211 285
1931 74
6889 15
78973667 34567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07065
53573179 = yrday
fracday
Element set: 901
Inclination: 51
6324 deg
RA of node: 274
4354 deg
Eccentricity:
0021211
Arg of perigee: 285
1931 deg
Mean anomaly: 74
6889 deg
Mean motion: 15
78973667 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3456
Checksum: 317
Coasting Arc #3 (Orbit 3471)
---------------------------------------
Vector Time (GMT): 2007/066/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3554031
93 A = 6709643
75 meter
Y = 3715696
70 meter E =
0015055
Z = 4326215
11 I = 51
30621
XDOT = -2568
167446 Wp = 312
31851
YDOT = 6411
773056 meter/sec RA = 268
64514 deg
ZDOT = -3394
686786 TA = 172
10538
MA = 172
08166
Ha = 184
347 n
mi
Hp = 174
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11660209
74 X = 3491202
51
Y = 12190605
97 feet Y = 3755088
91 meter
Z = 14193619
11 Z = 4343327
57
XDOT = -8425
746214 XDOT = -2623
183279
YDOT = 21036
000841 feet/sec YDOT = 6382
746496 meter/sec
ZDOT = -11137
423839 ZDOT = -3407
296990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8441202
88 X = 2572878
64
Y = 14542150
62 feet Y = 4432447
51 meter
Z = 14258405
86 Z = 4345962
11
XDOT = -11949
887504 XDOT = -3642
325711
YDOT = 17910
120005 feet/sec YDOT = 5459
004578 meter/sec
ZDOT = -11183
926318 ZDOT = -3408
860742
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 07066
54834019
00020000 00000-0 20000-3 0 9024
2 25544 51
6324 269
1940 0021316 289
1506 70
7352 15
79038001 34722
Satellite: ISS
Catalog Number: 25544
Epoch time: 07066
54834019 = yrday
fracday
Element set: 902
Inclination: 51
6324 deg
RA of node: 269
1940 deg
Eccentricity:
0021316
Arg of perigee: 289
1506 deg
Mean anomaly: 70
7352 deg
Mean motion: 15
79038001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3472
Checksum: 278
Coasting Arc #4 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2007/067/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2871981
06 A = 6710139
01 meter
Y = -4394233
49 meter E =
0011264
Z = 4184420
76 I = 51
30894
XDOT = 3580
248734 Wp = 299
11630
YDOT = 5778
942506 meter/sec RA = 263
49546 deg
ZDOT = 3624
135895 TA = 113
87832
MA = 113
76025
Ha = 184
504 n
mi
Hp = 174
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9422510
04 X = 2900577
48
Y = -14416776
53 feet Y = -4361957
23 meter
Z = 13728414
57 Z = 4198442
52
XDOT = 11746
222881 XDOT = 3497
756357
YDOT = 18959
785125 feet/sec YDOT = 5818
517839 meter/sec
ZDOT = 11890
209629 ZDOT = 3641
327930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12226342
04 X = 3726589
06
Y = -12071084
38 feet Y = -3679266
52 meter
Z = 13780493
09 Z = 4200294
29
XDOT = 6451
383245 XDOT = 1966
381613
YDOT = 20135
466741 feet/sec YDOT = 6137
290263 meter/sec
ZDOT = 11955
576903 ZDOT = 3644
059840
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 07067
56092858
00020000 00000-0 20000-3 0 9035
2 25544 51
6313 263
9525 0021289 293
2526 66
6399 15
79047719 34886
Satellite: ISS
Catalog Number: 25544
Epoch time: 07067
56092858 = yrday
fracday
Element set: 903
Inclination: 51
6313 deg
RA of node: 263
9525 deg
Eccentricity:
0021289
Arg of perigee: 293
2526 deg
Mean anomaly: 66
6399 deg
Mean motion: 15
79047719 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3488
Checksum: 333
Coasting Arc #5 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2007/068/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2595108
58 A = 6716517
43 meter
Y = -5953441
04 meter E =
0021160
Z = -1660919
55 I = 51
33503
XDOT = 3976
293514 Wp = 317
94956
YDOT = -3334
637631 meter/sec RA = 258
25559 deg
ZDOT = 5713
700549 TA = 23
54935
MA = 23
45261
Ha = 184
630 n
mi
Hp = 174
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8514135
76 X = -2520275
05
Y = -19532286
86 feet Y = -5982042
65 meter
Z = -5449211
11 Z = -1673344
51
XDOT = 13045
582396 XDOT = 3985
530345
YDOT = -10940
412174 feet/sec YDOT = -3290
120592 meter/sec
ZDOT = 18745
736708 ZDOT = 5733
039905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4445951
14 X = -1355125
91
Y = -20825813
04 feet Y = -6347707
81 meter
Z = -5496696
21 Z = -1675393
01
XDOT = 13333
386512 XDOT = 4064
016209
YDOT = -7835
756651 feet/sec YDOT = -2388
338627 meter/sec
ZDOT = 18817
937418 ZDOT = 5735
707325
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 07068
51020842
00020000 00000-0 20000-3 0 9046
2 25544 51
6309 259
0389 0021186 296
6715 63
2281 15
79086045 35034
Satellite: ISS
Catalog Number: 25544
Epoch time: 07068
51020842 = yrday
fracday
Element set: 904
Inclination: 51
6309 deg
RA of node: 259
0389 deg
Eccentricity:
0021186
Arg of perigee: 296
6715 deg
Mean anomaly: 63
2281 deg
Mean motion: 15
79086045 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3503
Checksum: 292
Coasting Arc #6 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2007/069/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4008597
62 A = 6705497
24 meter
Y = 1222479
15 meter E =
0011160
Z = -5231994
67 I = 51
30506
XDOT = -2242
066614 Wp = 344
65907
YDOT = -7379
172092 meter/sec RA = 253
07392 deg
ZDOT = 4
259685 TA = 285
31983
MA = 285
44313
Ha = 184
739 n
mi
Hp = 174
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13151567
01 X = -3996553
64
Y = 4010758
37 feet Y = 1177719
97 meter
Z = -17165336
85 Z = -5251439
14
XDOT = -7355
861593 XDOT = -2159
405712
YDOT = -24209
882190 feet/sec YDOT = -7403
781953 meter/sec
ZDOT = 13
975343 ZDOT = -6
431248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13566528
68 X = -4135077
94
Y = 1578497
15 feet Y = 481125
93 meter
Z = -17238223
02 Z = -5254210
38
XDOT = -2731
544096 XDOT = -832
574640
YDOT = -24152
772202 feet/sec YDOT = -7361
764967 meter/sec
ZDOT = -27
191806 ZDOT = -8
288062
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 07069
52275229
00020000 00000-0 20000-3 0 9050
2 25544 51
6305 253
7986 0021018 300
7485 59
1611 15
79133793 35190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07069
52275229 = yrday
fracday
Element set: 905
Inclination: 51
6305 deg
RA of node: 253
7986 deg
Eccentricity:
0021018
Arg of perigee: 300
7485 deg
Mean anomaly: 59
1611 deg
Mean motion: 15
79133793 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3519
Checksum: 302
Coasting Arc #7 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2007/070/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1142675
17 A = 6716191
60 meter
Y = 6400446
39 meter E =
0013948
Z = -1688334
56 I = 51
35175
XDOT = -5154
496804 Wp = 295
54457
YDOT = -592
674989 meter/sec RA = 247
89255 deg
ZDOT = -5692
961911 TA = 263
22862
MA = 263
38735
Ha = 185
088 n
mi
Hp = 174
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3748934
28 X = 1079221
11
Y = 20998839
85 feet Y = 6412869
61 meter
Z = -5539155
37 Z = -1682937
69
XDOT = -16911
078754 XDOT = -5119
831121
YDOT = -1944
471749 feet/sec YDOT = -650
121708 meter/sec
ZDOT = -18677
696559 ZDOT = -5717
918094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 278669
24 X = 84938
38
Y = 21334525
06 feet Y = 6502763
24 meter
Z = -5518007
76 Z = -1681888
76
XDOT = -14703
380914 XDOT = -4481
590503
YDOT = -4699
221211 feet/sec YDOT = -1432
322625 meter/sec
ZDOT = -18771
543444 ZDOT = -5721
566442
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 07070
53527189
00020000 00000-0 20000-3 0 9069
2 25544 51
6308 248
5582 0021162 305
1566 54
7617 15
79197116 35350
Satellite: ISS
Catalog Number: 25544
Epoch time: 07070
53527189 = yrday
fracday
Element set: 906
Inclination: 51
6308 deg
RA of node: 248
5582 deg
Eccentricity:
0021162
Arg of perigee: 305
1566 deg
Mean anomaly: 54
7617 deg
Mean motion: 15
79197116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3535
Checksum: 301
Coasting Arc #8 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2007/071/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4838537
08 A = 6709908
42 meter
Y = 2149145
78 meter E =
0017131
Z = 4138447
62 I = 51
34189
XDOT = 167
339725 Wp = 337
55028
YDOT = 6751
069525 meter/sec RA = 242
65359 deg
ZDOT = -3690
966777 TA = 150
38982
MA = 150
29272
Ha = 185
295 n
mi
Hp = 174
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15874465
48 X = 4794041
77
Y = 7051003
21 feet Y = 2203004
25 meter
Z = 13577584
04 Z = 4161844
91
XDOT = 549
014845 XDOT = 109
765741
YDOT = 22149
178230 feet/sec YDOT = 6752
618875 meter/sec
ZDOT = -12109
471052 ZDOT = -3690
293738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14587839
91 X = 4446373
60
Y = 9300918
35 feet Y = 2834919
91 meter
Z = 13665794
29 Z = 4165334
10
XDOT = -1974
394098 XDOT = -601
795321
YDOT = 20934
752087 feet/sec YDOT = 6380
912436 meter/sec
ZDOT = -12106
020936 ZDOT = -3689
915181
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 07071
54776957
00020000 00000-0 20000-3 0 9071
2 25544 51
6302 243
3167 0021066 308
4775 51
4500 15
79181875 35515
Satellite: ISS
Catalog Number: 25544
Epoch time: 07071
54776957 = yrday
fracday
Element set: 907
Inclination: 51
6302 deg
RA of node: 243
3167 deg
Eccentricity:
0021066
Arg of perigee: 308
4775 deg
Mean anomaly: 51
4500 deg
Mean motion: 15
79181875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3551
Checksum: 298
Coasting Arc #9 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2007/072/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1010041
27 A = 6708766
20 meter
Y = -4962888
63 meter E =
0012866
Z = 4399576
60 I = 51
35304
XDOT = 5683
597313 Wp = 327
44025
YDOT = 4047
374858 meter/sec RA = 237
50588 deg
ZDOT = 3275
890676 TA = 89
66659
MA = 89
51917
Ha = 185
415 n
mi
Hp = 174
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3313783
68 X = 1044089
87
Y = -16282443
00 feet Y = -4951403
38 meter
Z = 14434306
42 Z = 4404566
04
XDOT = 18646
972811 XDOT = 5622
003102
YDOT = 13278
788903 feet/sec YDOT = 4110
587650 meter/sec
ZDOT = 10747
672823 ZDOT = 3303
351582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5326677
90 X = 1623571
42
Y = -15722711
54 feet Y = -4792282
48 meter
Z = 14452375
53 Z = 4405084
06
XDOT = 15552
425403 XDOT = 4740
379263
YDOT = 15198
110587 feet/sec YDOT = 4632
384107 meter/sec
ZDOT = 10851
424483 ZDOT = 3307
514182
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 07072
56024195
00020000 00000-0 20000-3 0 9085
2 25544 51
6302 238
0749 0021080 312
3824 47
5557 15
79255693 35672
Satellite: ISS
Catalog Number: 25544
Epoch time: 07072
56024195 = yrday
fracday
Element set: 908
Inclination: 51
6302 deg
RA of node: 238
0749 deg
Eccentricity:
0021080
Arg of perigee: 312
3824 deg
Mean anomaly: 47
5557 deg
Mean motion: 15
79255693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3567
Checksum: 299
Coasting Arc #10 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2007/073/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4771259
96 A = 6716520
75 meter
Y = -4534943
28 meter E =
0024118
Z = -1251283
11 I = 51
39698
XDOT = 2569
478238 Wp = 338
32401
YDOT = -4323
853191 meter/sec RA = 232
27447 deg
ZDOT = 5859
406063 TA = 7
85073
MA = 7
81305
Ha = 185
611 n
mi
Hp = 173
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15653740
04 X = -4714116
57
Y = -14878422
85 feet Y = -4587978
70 meter
Z = -4105259
54 Z = -1274322
62
XDOT = 8430
046712 XDOT = 2589
173774
YDOT = -14185
870050 feet/sec YDOT = -4295
009635 meter/sec
ZDOT = 19223
773174 ZDOT = 5871
936278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13846311
80 X = -4220355
84
Y = -16551827
44 feet Y = -5044997
00 meter
Z = -4192476
32 Z = -1277866
78
XDOT = 8667
995137 XDOT = 2642
004918
YDOT = -12143
247595 feet/sec YDOT = -3701
261867 meter/sec
ZDOT = 19270
267511 ZDOT = 5873
577537
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 07073
50941446
00020000 00000-0 20000-3 0 9098
2 25544 51
6311 233
1616 0020972 316
3604 43
5903 15
79267459 35821
Satellite: ISS
Catalog Number: 25544
Epoch time: 07073
50941446 = yrday
fracday
Element set: 909
Inclination: 51
6311 deg
RA of node: 233
1616 deg
Eccentricity:
0020972
Arg of perigee: 316
3604 deg
Mean anomaly: 43
5903 deg
Mean motion: 15
79267459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3582
Checksum: 291
Coasting Arc #11 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2007/074/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3474903
89 A = 6705037
98 meter
Y = 2382640
71 meter E =
0015133
Z = -5216116
26 I = 51
37761
XDOT = -4894
517308 Wp = 6
35471
YDOT = -5930
205459 meter/sec RA = 227
08891 deg
ZDOT = 566
829758 TA = 268
95813
MA = 269
13152
Ha = 185
776 n
mi
Hp = 173
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11400603
33 X = -3475950
22
Y = 7817062
70 feet Y = 2343776
36 meter
Z = -17113242
31 Z = -5232999
62
XDOT = -16058
127651 XDOT = -4830
594632
YDOT = -19456
054654 feet/sec YDOT = -5984
581259 meter/sec
ZDOT = 1859
677683 ZDOT = 543
208144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12003869
05 X = -3658779
29
Y = 6694982
73 feet Y = 2040630
74 meter
Z = -17176368
13 Z = -5235357
00
XDOT = -13636
553812 XDOT = -4156
421602
YDOT = -20034
421714 feet/sec YDOT = -6106
491738 meter/sec
ZDOT = 1770
063912 ZDOT = 539
515480
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 07074
52184075
00020000 00000-0 20000-3 0 9100
2 25544 51
6313 227
9216 0020909 320
5081 39
4561 15
79328983 35987
Satellite: ISS
Catalog Number: 25544
Epoch time: 07074
52184075 = yrday
fracday
Element set: 910
Inclination: 51
6313 deg
RA of node: 227
9216 deg
Eccentricity:
0020909
Arg of perigee: 320
5081 deg
Mean anomaly: 39
4561 deg
Mean motion: 15
79328983 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3598
Checksum: 299
Coasting Arc #12 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2007/075/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3361846
35 A = 6714847
89 meter
Y = 5383967
55 meter E =
0014970
Z = -2207417
49 I = 51
43154
XDOT = -5321
205776 Wp = 327
44694
YDOT = 1072
359284 meter/sec RA = 221
91907 deg
ZDOT = -5458
973984 TA = 237
39488
MA = 237
53948
Ha = 186
095 n
mi
Hp = 173
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11029679
62 X = 3312115
21
Y = 17663935
52 feet Y = 5421283
40 meter
Z = -7242183
37 Z = -2191207
11
XDOT = -17458
024199 XDOT = -5306
283410
YDOT = 3518
239120 feet/sec YDOT = 1012
937684 meter/sec
ZDOT = -17910
019631 ZDOT = -5484
787682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9640992
78 X = 2938574
60
Y = 18482681
10 feet Y = 5633521
20 meter
Z = -7180489
41 Z = -2188613
17
XDOT = -16233
829336 XDOT = -4948
071182
YDOT = 1434
264744 feet/sec YDOT = 437
163894 meter/sec
ZDOT = -18006
900061 ZDOT = -5488
503139
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 07075
53424174
00020000 00000-0 20000-3 0 9110
2 25544 51
6312 222
6789 0021080 324
5413 35
4350 15
79368996 36146
Satellite: ISS
Catalog Number: 25544
Epoch time: 07075
53424174 = yrday
fracday
Element set: 911
Inclination: 51
6312 deg
RA of node: 222
6789 deg
Eccentricity:
0021080
Arg of perigee: 324
5413 deg
Mean anomaly: 35
4350 deg
Mean motion: 15
79368996 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3614
Checksum: 288
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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