Date:
May 30th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 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 766)
---------------------------------------
Vector Time (GMT): 2007/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843325
38 A = 6710004
14 meter
Y = -2519426
37 meter E =
0002695
Z = 4891783
49 I = 51
48473
XDOT = 5794
357300 Wp = 283
60147
YDOT = 4581
110804 meter/sec RA = 204
66034 deg
ZDOT = -2193
413601 TA = 187
73093
MA = 187
73508
Ha = 182
678 n
mi
Hp = 180
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12609335
25 X = 3847448
55
Y = -8265834
55 feet Y = -2476425
68 meter
Z = 16049158
44 Z = 4910464
39
XDOT = 19010
358595 XDOT = 5753
355380
YDOT = 15029
891090 feet/sec YDOT = 4645
677564 meter/sec
ZDOT = -7196
238850 ZDOT = -2165
363202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2178615
83 X = -664042
10
Y = -14843064
18 feet Y = -4524165
96 meter
Z = 16119302
77 Z = 4913163
48
XDOT = 20606
414639 XDOT = 6280
835182
YDOT = -10722
651873 feet/sec YDOT = -3268
264291 meter/sec
ZDOT = -7089
868353 ZDOT = -2160
991874
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 07148
54380762
00020000 00000-0 20000-3 0 9004
2 25544 51
6339 205
4176 0008415 250
4322 109
5935 15
78093287 7672
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
54380762 = yrday
fracday
Element set: 900
Inclination: 51
6339 deg
RA of node: 205
4176 deg
Eccentricity:
0008415
Arg of perigee: 250
4322 deg
Mean anomaly: 109
5935 deg
Mean motion: 15
78093287 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 767
Checksum: 298
Coasting Arc #2 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2007/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4277201
62 A = 6716406
06 meter
Y = -4138318
38 meter E =
0005403
Z = 3109642
86 I = 51
53209
XDOT = 5589
691180 Wp = 101
93800
YDOT = -2117
065283 meter/sec RA = 199
52659 deg
ZDOT = 4862
833478 TA = 294
32338
MA = 294
37979
Ha = 182
470 n
mi
Hp = 180
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14032813
70 X = -4245714
80
Y = -13577160
03 feet Y = -4185972
82 meter
Z = 10202240
37 Z = 3088939
75
XDOT = 18338
881825 XDOT = 5589
325886
YDOT = -6945
752241 feet/sec YDOT = -2054
560942 meter/sec
ZDOT = 15954
178076 ZDOT = 4889
987506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18146795
49 X = -5531143
26
Y = 7317834
60 feet Y = 2230475
99 meter
Z = 10123633
41 Z = 3085683
46
XDOT = 1644
663629 XDOT = 501
293474
YDOT = -18171
672568 feet/sec YDOT = -5538
725799 meter/sec
ZDOT = 16056
340574 ZDOT = 4893
972607
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 07149
55701272
00020000 00000-0 20000-3 0 9010
2 25544 51
6332 200
1817 0008112 254
1961 105
8310 15
78091389 7838
Satellite: ISS
Catalog Number: 25544
Epoch time: 07149
55701272 = yrday
fracday
Element set: 901
Inclination: 51
6332 deg
RA of node: 200
1817 deg
Eccentricity:
0008112
Arg of perigee: 254
1961 deg
Mean anomaly: 105
8310 deg
Mean motion: 15
78091389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 783
Checksum: 270
Coasting Arc #3 (Orbit 797)
---------------------------------------
Vector Time (GMT): 2007/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5727199
67 A = 6715568
38 meter
Y = 1229423
26 meter E =
0003421
Z = -3283146
96 I = 51
55777
XDOT = -3738
297806 Wp = 245
43371
YDOT = -4814
032378 meter/sec RA = 194
30207 deg
ZDOT = 4713
259692 TA = 75
93988
MA = 75
90185
Ha = 182
095 n
mi
Hp = 180
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18790025
17 X = -5724572
39
Y = 4033540
90 feet Y = 1165393
73 meter
Z = -10771479
54 Z = -3310963
62
XDOT = -12264
756581 XDOT = -3707
085322
YDOT = -15794
069481 feet/sec YDOT = -4855
662359 meter/sec
ZDOT = 15463
450433 ZDOT = 4695
173758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3642466
09 X = -1110223
66
Y = 18809535
14 feet Y = 5733146
31 meter
Z = -10876263
05 Z = -3315084
98
XDOT = -18003
098181 XDOT = -5487
344326
YDOT = 5425
183194 feet/sec YDOT = 1653
595838 meter/sec
ZDOT = 15394
628471 ZDOT = 4692
282758
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 07150
50687128
00020000 00000-0 20000-3 0 9021
2 25544 51
6331 195
2733 0008033 257
8705 102
1561 15
78156883 7981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07150
50687128 = yrday
fracday
Element set: 902
Inclination: 51
6331 deg
RA of node: 195
2733 deg
Eccentricity:
0008033
Arg of perigee: 257
8705 deg
Mean anomaly: 102
1561 deg
Mean motion: 15
78156883 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 798
Checksum: 294
Coasting Arc #4 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2007/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2027592
60 A = 6710260
26 meter
Y = 4204982
91 meter E =
0004258
Z = -4824108
69 I = 51
56807
XDOT = -7281
146903 Wp = 54
03687
YDOT = 754
478645 meter/sec RA = 189
17421 deg
ZDOT = -2401
657850 TA = 192
50721
MA = 192
51778
Ha = 181
818 n
mi
Hp = 180
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6652206
69 X = 2003856
19
Y = 13795875
68 feet Y = 4227524
74 meter
Z = -15827128
24 Z = -4814315
38
XDOT = -23888
277240 XDOT = -7277
375437
YDOT = 2475
323639 feet/sec YDOT = 673
078302 meter/sec
ZDOT = -7879
454887 ZDOT = -2437
020931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15318786
38 X = 4669166
09
Y = -1047539
48 feet Y = -319290
03 meter
Z = -15789663
49 Z = -4812689
43
XDOT = -6764
646150 XDOT = -2061
864146
YDOT = 21903
044338 feet/sec YDOT = 6676
047914 meter/sec
ZDOT = -8012
780990 ZDOT = -2442
295646
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 07151
52003279
00020000 00000-0 20000-3 0 9034
2 25544 51
6334 190
0373 0008048 262
3031 97
7220 15
78153610 8141
Satellite: ISS
Catalog Number: 25544
Epoch time: 07151
52003279 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 190
0373 deg
Eccentricity:
0008048
Arg of perigee: 262
3031 deg
Mean anomaly: 97
7220 deg
Mean motion: 15
78153610 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 814
Checksum: 257
Coasting Arc #5 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2007/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6671172
29 A = 6719964
01 meter
Y = -128505
41 meter E =
0009001
Z = 746263
95 I = 51
62938
XDOT = 762
938631 Wp = 161
57645
YDOT = 4801
054247 meter/sec RA = 183
97680 deg
ZDOT = -5982
378422 TA = 10
27321
MA = 10
25482
Ha = 180
989 n
mi
Hp = 180
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21887048
19 X = 6668488
18
Y = -421605
69 feet Y = -53919
78 meter
Z = 2448372
53 Z = 778666
36
XDOT = 2503
079497 XDOT = 738
257505
YDOT = 15751
490311 feet/sec YDOT = 4809
449037 meter/sec
ZDOT = -19627
225795 ZDOT = -5978
731023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7495943
23 X = 2284763
50
Y = -20552807
57 feet Y = -6264495
75 meter
Z = 2570621
31 Z = 783525
38
XDOT = 14134
931322 XDOT = 4308
327067
YDOT = 2697
831978 feet/sec YDOT = 822
299187 meter/sec
ZDOT = -19612
876400 ZDOT = -5978
004727
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 07152
53317184
00020000 00000-0 20000-3 0 9040
2 25544 51
6326 184
8011 0007946 267
0942 92
9314 15
78208143 8302
Satellite: ISS
Catalog Number: 25544
Epoch time: 07152
53317184 = yrday
fracday
Element set: 904
Inclination: 51
6326 deg
RA of node: 184
8011 deg
Eccentricity:
0007946
Arg of perigee: 267
0942 deg
Mean anomaly: 92
9314 deg
Mean motion: 15
78208143 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 830
Checksum: 284
Coasting Arc #6 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2007/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 762115
12 A = 6708222
14 meter
Y = -4150677
64 meter E =
0005394
Z = 5219110
21 I = 51
61805
XDOT = 7653
550107 Wp = 287
31813
YDOT = 445
105662 meter/sec RA = 178
80891 deg
ZDOT = -762
682213 TA = 169
94228
MA = 169
93148
Ha = 180
731 n
mi
Hp = 180
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2500377
69 X = 783118
27
Y = -13617708
79 feet Y = -4142038
89 meter
Z = 17123064
99 Z = 5222862
75
XDOT = 25110
072530 XDOT = 7651
709042
YDOT = 1460
320413 feet/sec YDOT = 530
681812 meter/sec
ZDOT = -2502
238232 ZDOT = -725
505348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11955149
93 X = -3643929
70
Y = -6949850
39 feet Y = -2118314
40 meter
Z = 17136720
97 Z = 5223272
55
XDOT = 9521
309234 XDOT = 2902
095054
YDOT = -22209
988284 feet/sec YDOT = -6769
604429 meter/sec
ZDOT = -2361
884585 ZDOT = -719
902422
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 07153
54628963
00020000 00000-0 20000-3 0 9053
2 25544 51
6318 179
5647 0007873 271
1442 88
8821 15
78238169 8464
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
54628963 = yrday
fracday
Element set: 905
Inclination: 51
6318 deg
RA of node: 179
5647 deg
Eccentricity:
0007873
Arg of perigee: 271
1442 deg
Mean anomaly: 88
8821 deg
Mean motion: 15
78238169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 846
Checksum: 329
Coasting Arc #7 (Orbit 861)
---------------------------------------
Vector Time (GMT): 2007/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6329879
16 A = 6718360
64 meter
Y = -918595
15 meter E =
0008015
Z = 2038850
56 I = 51
68117
XDOT = 2481
454427 Wp = 42
06497
YDOT = -4708
894507 meter/sec RA = 173
66647 deg
ZDOT = 5575
713669 TA = 340
70890
MA = 340
73922
Ha = 181
438 n
mi
Hp = 180
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20767320
08 X = -6329041
24
Y = -3013763
63 feet Y = -989375
15 meter
Z = 6689142
26 Z = 2008101
76
XDOT = 8141
254681 XDOT = 2506
839660
YDOT = -15449
128960 feet/sec YDOT = -4681
004709 meter/sec
ZDOT = 18293
023847 ZDOT = 5587
829301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9678500
00 X = -2950006
80
Y = 18660965
72 feet Y = 5687862
35 meter
Z = 6572973
07 Z = 2003442
19
XDOT = -10591
808493 XDOT = -3228
383229
YDOT = -11960
611413 feet/sec YDOT = -3645
594359 meter/sec
ZDOT = 18338
179659 ZDOT = 5589
477160
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 07154
55938644
00020000 00000-0 20000-3 0 9066
2 25544 51
6318 174
3282 0007867 276
0847 83
9421 15
78251027 8626
Satellite: ISS
Catalog Number: 25544
Epoch time: 07154
55938644 = yrday
fracday
Element set: 906
Inclination: 51
6318 deg
RA of node: 174
3282 deg
Eccentricity:
0007867
Arg of perigee: 276
0847 deg
Mean anomaly: 83
9421 deg
Mean motion: 15
78251027 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 862
Checksum: 314
Coasting Arc #8 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2007/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3436167
56 A = 6712503
80 meter
Y = 4028685
92 meter E =
0001411
Z = -4126125
30 I = 51
69120
XDOT = -6508
527970 Wp = 196
44433
YDOT = -1700
813932 meter/sec RA = 168
45741 deg
ZDOT = 3757
902926 TA = 111
98969
MA = 111
97470
Ha = 181
622 n
mi
Hp = 180
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11273515
62 X = -3460917
59
Y = 13217473
50 feet Y = 3990123
20 meter
Z = -13537156
49 Z = -4142877
51
XDOT = -21353
438222 XDOT = -6507
280679
YDOT = -5580
098203 feet/sec YDOT = -1773
589703 meter/sec
ZDOT = 12329
077842 ZDOT = 3726
287227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9062670
84 X = 2762302
07
Y = 14763434
43 feet Y = 4499894
81 meter
Z = -13599903
21 Z = -4145250
50
XDOT = -10910
437551 XDOT = -3325
501365
YDOT = 17949
679996 feet/sec YDOT = 5471
062463 meter/sec
ZDOT = 12209
524861 ZDOT = 3721
463178
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 07155
50914331
00020000 00000-0 20000-3 0 9070
2 25544 51
6325 169
4190 0007965 279
7680 80
2585 15
78282087 8778
Satellite: ISS
Catalog Number: 25544
Epoch time: 07155
50914331 = yrday
fracday
Element set: 907
Inclination: 51
6325 deg
RA of node: 169
4190 deg
Eccentricity:
0007965
Arg of perigee: 279
7680 deg
Mean anomaly: 80
2585 deg
Mean motion: 15
78282087 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 877
Checksum: 320
Coasting Arc #9 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2007/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4730479
71 A = 6712002
35 meter
Y = 2105768
74 meter E =
0004824
Z = -4273942
27 I = 51
71680
XDOT = -5186
973905 Wp = 3
12498
YDOT = 4465
338264 meter/sec RA = 163
34354 deg
ZDOT = -3536
428204 TA = 231
06468
MA = 231
10769
Ha = 181
926 n
mi
Hp = 180
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15519946
54 X = 4727343
07
Y = 6908690
11 feet Y = 2158650
84 meter
Z = -14022120
30 Z = -4250968
93
XDOT = -17017
630922 XDOT = -5219
341206
YDOT = 14650
059921 feet/sec YDOT = 4407
154266 meter/sec
ZDOT = -11602
454737 ZDOT = -3561
704254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11212149
81 X = 3417463
26
Y = -12857621
68 feet Y = -3919003
09 meter
Z = -13935130
39 Z = -4247427
74
XDOT = 8044
497214 XDOT = 2451
962751
YDOT = 19708
853076 feet/sec YDOT = 6007
258417 meter/sec
ZDOT = -11697
334864 ZDOT = -3565
347666
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 07156
52219695
00020000 00000-0 20000-3 0 9085
2 25544 51
6317 164
1819 0007933 283
5091 76
5190 15
78329207 8937
Satellite: ISS
Catalog Number: 25544
Epoch time: 07156
52219695 = yrday
fracday
Element set: 908
Inclination: 51
6317 deg
RA of node: 164
1819 deg
Eccentricity:
0007933
Arg of perigee: 283
5091 deg
Mean anomaly: 76
5190 deg
Mean motion: 15
78329207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 893
Checksum: 314
Coasting Arc #10 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2007/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335202
06 A = 6718284
64 meter
Y = -3662323
57 meter E =
0006307
Z = 1792714
62 I = 51
76560
XDOT = 4103
467058 Wp = 121
57840
YDOT = 3185
993149 meter/sec RA = 158
13991 deg
ZDOT = -5692
125931 TA = 38
55187
MA = 38
50685
Ha = 182
091 n
mi
Hp = 180
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17503943
75 X = 5367049
53
Y = -12015497
28 feet Y = -3602484
56 meter
Z = 5881609
63 Z = 1818709
71
XDOT = 13462
818432 XDOT = 4095
187026
YDOT = 10452
733429 feet/sec YDOT = 3231
834998 meter/sec
ZDOT = -18674
953843 ZDOT = -5672
211000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6659332
67 X = -2029764
60
Y = -20130938
31 feet Y = -6135910
00 meter
Z = 5979311
39 Z = 1822494
11
XDOT = 12357
324185 XDOT = 3766
512411
YDOT = -9623
087940 feet/sec YDOT = -2933
117204 meter/sec
ZDOT = -18599
369007 ZDOT = -5669
087673
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 07157
53522834
00020000 00000-0 20000-3 0 9090
2 25544 51
6313 158
9448 0007938 288
4151 71
6151 15
78382783 9097
Satellite: ISS
Catalog Number: 25544
Epoch time: 07157
53522834 = yrday
fracday
Element set: 909
Inclination: 51
6313 deg
RA of node: 158
9448 deg
Eccentricity:
0007938
Arg of perigee: 288
4151 deg
Mean anomaly: 71
6151 deg
Mean motion: 15
78382783 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 909
Checksum: 319
Coasting Arc #11 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2007/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2283856
51 A = 6707680
79 meter
Y = -3488070
99 meter E =
0005350
Z = 5258639
71 I = 51
75559
XDOT = 6703
413866 Wp = 293
01159
YDOT = -3776
933803 meter/sec RA = 152
99963 deg
ZDOT = 408
457382 TA = 153
13196
MA = 153
10424
Ha = 182
296 n
mi
Hp = 179
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7492967
57 X = -2270228
10
Y = -11443802
47 feet Y = -3513534
85 meter
Z = 17252754
96 Z = 5247577
41
XDOT = 21992
827644 XDOT = 6743
165673
YDOT = -12391
515102 feet/sec YDOT = -3701
750260 meter/sec
ZDOT = 1340
083273 ZDOT = 441
118540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13035492
33 X = -3973218
06
Y = 4316886
55 feet Y = 1315787
02 meter
Z = 17210553
80 Z = 5245776
80
XDOT = -5866
903594 XDOT = -1788
232215
YDOT = -23517
300520 feet/sec YDOT = -7168
073199 meter/sec
ZDOT = 1462
949836 ZDOT = 445
907110
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 07158
54823780
00020000 00000-0 20000-3 0 9108
2 25544 51
6308 153
7073 0008007 291
9193 68
1121 15
78391431 9257
Satellite: ISS
Catalog Number: 25544
Epoch time: 07158
54823780 = yrday
fracday
Element set: 910
Inclination: 51
6308 deg
RA of node: 153
7073 deg
Eccentricity:
0008007
Arg of perigee: 291
9193 deg
Mean anomaly: 68
1121 deg
Mean motion: 15
78391431 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 925
Checksum: 287
Coasting Arc #12 (Orbit 940)
---------------------------------------
Vector Time (GMT): 2007/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6020768
17 A = 6718939
92 meter
Y = 2746063
09 meter E =
0011692
Z = 1117875
61 I = 51
81956
XDOT = -1094
184431 Wp = 21
95959
YDOT = -4814
118130 meter/sec RA = 147
84858 deg
ZDOT = 5923
584796 TA = 350
27420
MA = 350
29681
Ha = 182
313 n
mi
Hp = 179
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19753176
42 X = -6056458
02
Y = 9009393
34 feet Y = 2678535
80 meter
Z = 3667570
89 Z = 1088540
31
XDOT = -3589
843934 XDOT = -1069
046673
YDOT = -15794
350821 feet/sec YDOT = -4826
214056 meter/sec
ZDOT = 19434
333321 ZDOT = 5918
329737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3867604
36 X = 1178845
81
Y = 21382158
34 feet Y = 6517281
86 meter
Z = 3557128
65 Z = 1084212
81
XDOT = -14659
658356 XDOT = -4468
263867
YDOT = -583
190496 feet/sec YDOT = -177
756463 meter/sec
ZDOT = 19413
896274 ZDOT = 5917
355584
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 07159
56122189
00020000 00000-0 20000-3 0 9117
2 25544 51
6308 148
4708 0007967 294
4856 65
5478 15
78485568 9410
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
56122189 = yrday
fracday
Element set: 911
Inclination: 51
6308 deg
RA of node: 148
4708 deg
Eccentricity:
0007967
Arg of perigee: 294
4856 deg
Mean anomaly: 65
5478 deg
Mean motion: 15
78485568 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 941
Checksum: 339
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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