Date:
June 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 813)
---------------------------------------
Vector Time (GMT): 2007/151/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5965290
90 A = 6717044
56 meter
Y = -1280961
48 meter E =
0006096
Z = 2800632
46 I = 51
58889
XDOT = 3402
452283 Wp = 122
19944
YDOT = 4658
612422 meter/sec RA = 189
22437 deg
ZDOT = -5111
515599 TA = 25
63287
MA = 25
60266
Ha = 181
839 n
mi
Hp = 181
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19571164
37 X = 5965566
26
Y = -4202629
52 feet Y = -1214253
22 meter
Z = 9188426
69 Z = 2829612
74
XDOT = 11162
901192 XDOT = 3374
937331
YDOT = 15284
161491 feet/sec YDOT = 4696
507631 meter/sec
ZDOT = -16770
064301 ZDOT = -5095
052213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5578192
09 X = 1700232
95
Y = -19171803
16 feet Y = -5843565
60 meter
Z = 9297606
75 Z = 2833910
54
XDOT = 17399
318706 XDOT = 5303
312342
YDOT = -3047
636948 feet/sec YDOT = -928
919742 meter/sec
ZDOT = -16707
378831 ZDOT = -5092
409068
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
52009538
00020000 00000-0 20000-3 0 9005
2 25544 51
6321 190
0406 0008224 262
7780 97
2450 15
78093872 8148
Satellite: ISS
Catalog Number: 25544
Epoch time: 07151
52009538 = yrday
fracday
Element set: 900
Inclination: 51
6321 deg
RA of node: 190
0406 deg
Eccentricity:
0008224
Arg of perigee: 262
7780 deg
Mean anomaly: 97
2450 deg
Mean motion: 15
78093872 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 814
Checksum: 275
Coasting Arc #2 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2007/152/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701061
24 A = 6709545
60 meter
Y = -4114627
44 meter E =
0005120
Z = 5023410
89 I = 51
59141
XDOT = 7440
732594 Wp = 224
01594
YDOT = -889
337396 meter/sec RA = 184
09258 deg
ZDOT = 1788
648184 TA = 208
73563
MA = 208
76384
Ha = 181
407 n
mi
Hp = 180
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5580909
56 X = -1679327
56
Y = -13499433
84 feet Y = -4133529
13 meter
Z = 16481006
85 Z = 5015199
01
XDOT = 24411
852342 XDOT = 7441
435245
YDOT = -2917
773610 feet/sec YDOT = -806
127379 meter/sec
ZDOT = 5868
268320 ZDOT = 1824
797250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14595978
86 X = -4448854
36
Y = -1172861
70 feet Y = -357488
25 meter
Z = 16449518
20 Z = 5013813
15
XDOT = 8538
177622 XDOT = 2602
436539
YDOT = -21924
021595 feet/sec YDOT = -6682
441782 meter/sec
ZDOT = 6004
561083 ZDOT = 1830
190218
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
53329856
00020000 00000-0 20000-3 0 9016
2 25544 51
6314 184
8046 0008060 266
3402 93
6842 15
78103059 8302
Satellite: ISS
Catalog Number: 25544
Epoch time: 07152
53329856 = yrday
fracday
Element set: 901
Inclination: 51
6314 deg
RA of node: 184
8046 deg
Eccentricity:
0008060
Arg of perigee: 266
3402 deg
Mean anomaly: 93
6842 deg
Mean motion: 15
78103059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 830
Checksum: 280
Coasting Arc #3 (Orbit 844)
---------------------------------------
Vector Time (GMT): 2007/153/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6705409
79 A = 6720489
21 meter
Y = 287472
06 meter E =
0008775
Z = -201682
81 I = 51
65770
XDOT = -385
962631 Wp =
49828
YDOT = -4771
809736 meter/sec RA = 178
90708 deg
ZDOT = 6041
206919 TA = 357
30697
MA = 357
31169
Ha = 180
927 n
mi
Hp = 180
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21999375
95 X = -6707146
24
Y = 943149
79 feet Y = 212478
74 meter
Z = -661689
01 Z = -234262
11
XDOT = -1266
281599 XDOT = -361
922191
YDOT = -15655
543753 feet/sec YDOT = -4775
992619 meter/sec
ZDOT = 19820
232673 ZDOT = 6039
389305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8935873
06 X = -2723654
11
Y = 20120498
94 feet Y = 6132728
08 meter
Z = -784602
67 Z = -239146
89
XDOT = -13167
757751 XDOT = -4013
532563
YDOT = -5076
573417 feet/sec YDOT = -1547
339578 meter/sec
ZDOT = 19812
792081 ZDOT = 6038
939026
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
48315890
00020000 00000-0 20000-3 0 9025
2 25544 51
6317 179
8959 0008057 271
2278 88
7964 15
78106288 8457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
48315890 = yrday
fracday
Element set: 902
Inclination: 51
6317 deg
RA of node: 179
8959 deg
Eccentricity:
0008057
Arg of perigee: 271
2278 deg
Mean anomaly: 88
7964 deg
Mean motion: 15
78106288 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 845
Checksum: 334
Coasting Arc #4 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2007/154/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1053178
18 A = 6708899
31 meter
Y = 4199361
33 meter E =
0006166
Z = -5130385
30 I = 51
64828
XDOT = -7579
312316 Wp = 107
52658
YDOT = -245
539640 meter/sec RA = 173
73146 deg
ZDOT = 1354
423793 TA = 175
43228
MA = 175
42665
Ha = 181
452 n
mi
Hp = 180
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3455308
98 X = -1075135
22
Y = 13777432
19 feet Y = 4187462
40 meter
Z = -16831972
77 Z = -5135554
12
XDOT = -24866
510224 XDOT = -7582
582910
YDOT = -805
576246 feet/sec YDOT = -330
314324 meter/sec
ZDOT = 4443
647616 ZDOT = 1317
595377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11001373
02 X = 3353218
50
Y = 8949116
24 feet Y = 2727690
63 meter
Z = -16850970
76 Z = -5136175
89
XDOT = -10758
146091 XDOT = -3279
082929
YDOT = 21333
799373 feet/sec YDOT = 6502
542049 meter/sec
ZDOT = 4304
613961 ZDOT = 1312
046335
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
49632423
00020000 00000-0 20000-3 0 9032
2 25544 51
6323 174
6597 0008103 274
6758 85
3482 15
78137860 8613
Satellite: ISS
Catalog Number: 25544
Epoch time: 07154
49632423 = yrday
fracday
Element set: 903
Inclination: 51
6323 deg
RA of node: 174
6597 deg
Eccentricity:
0008103
Arg of perigee: 274
6758 deg
Mean anomaly: 85
3482 deg
Mean motion: 15
78137860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 861
Checksum: 307
Coasting Arc #5 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2007/155/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6189506
96 A = 6717672
80 meter
Y = 758500
64 meter E =
0004604
Z = -2491184
50 I = 51
70612
XDOT = -2740
545477 Wp = 238
69063
YDOT = 4845
000264 meter/sec RA = 168
59952 deg
ZDOT = -5329
034977 TA = 329
51846
MA = 329
54521
Ha = 181
763 n
mi
Hp = 180
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20306781
37 X = 6192666
99
Y = 2488519
16 feet Y = 827733
33 meter
Z = -8173177
49 Z = -2461108
08
XDOT = -8991
290934 XDOT = -2768
631841
YDOT = 15895
670159 feet/sec YDOT = 4814
197956 meter/sec
ZDOT = -17483
710553 ZDOT = -5342
415804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10683297
46 X = 3256269
07
Y = -17500563
78 feet Y = -5334171
84 meter
Z = -8059550
25 Z = -2456550
92
XDOT = 9517
979219 XDOT = 2901
080066
YDOT = 13892
501808 feet/sec YDOT = 4234
434551 meter/sec
ZDOT = -17533
631048 ZDOT = -5344
250744
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
50947031
00020000 00000-0 20000-3 0 9040
2 25544 51
6317 169
4233 0008027 278
5838 81
4418 15
78179538 8773
Satellite: ISS
Catalog Number: 25544
Epoch time: 07155
50947031 = yrday
fracday
Element set: 904
Inclination: 51
6317 deg
RA of node: 169
4233 deg
Eccentricity:
0008027
Arg of perigee: 278
5838 deg
Mean anomaly: 81
4418 deg
Mean motion: 15
78179538 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 877
Checksum: 315
Coasting Arc #6 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2007/156/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3576505
26 A = 6713707
00 meter
Y = -4209522
34 meter E =
0004981
Z = 3815977
66 I = 51
72088
XDOT = 6289
553660 Wp = 44
48409
YDOT = 1557
643900 meter/sec RA = 163
38894 deg
ZDOT = -4169
815684 TA = 89
12500
MA = 89
06794
Ha = 182
046 n
mi
Hp = 180
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11733941
15 X = 3604773
69
Y = -13810768
82 feet Y = -4169370
47 meter
Z = 12519611
76 Z = 3833420
18
XDOT = 20635
018571 XDOT = 6291
924532
YDOT = 5110
380250 feet/sec YDOT = 1627
991211 meter/sec
ZDOT = -13680
497650 ZDOT = -4139
255115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8029878
35 X = -2447506
92
Y = -16195786
76 feet Y = -4936475
80 meter
Z = 12584948
71 Z = 3835892
37
XDOT = 11747
932410 XDOT = 3580
769798
YDOT = -16382
391305 feet/sec YDOT = -4993
352870 meter/sec
ZDOT = -13564
930456 ZDOT = -4134
590803
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
52259654
00020000 00000-0 20000-3 0 9051
2 25544 51
6310 164
1868 0008026 283
5421 76
4850 15
78241434 8932
Satellite: ISS
Catalog Number: 25544
Epoch time: 07156
52259654 = yrday
fracday
Element set: 905
Inclination: 51
6310 deg
RA of node: 164
1868 deg
Eccentricity:
0008026
Arg of perigee: 283
5421 deg
Mean anomaly: 76
4850 deg
Mean motion: 15
78241434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 893
Checksum: 295
Coasting Arc #7 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2007/157/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526139
95 A = 6711323
86 meter
Y = -2033151
98 meter E =
0001197
Z = 4519224
21 I = 51
73949
XDOT = 5231
580599 Wp = 155
27865
YDOT = -4726
205149 meter/sec RA = 158
27643 deg
ZDOT = 3111
954315 TA = 263
76581
MA = 263
77945
Ha = 182
360 n
mi
Hp = 180
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14849540
53 X = -4525022
03
Y = -6670446
13 feet Y = -2083760
26 meter
Z = 14826851
09 Z = 4497238
73
XDOT = 17163
978343 XDOT = 5268
923654
YDOT = -15505
922406 feet/sec YDOT = -4667
494366 meter/sec
ZDOT = 10209
823868 ZDOT = 3137
459196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11869137
32 X = -3617713
06
Y = 11251193
37 feet Y = 3429363
74 meter
Z = 14743590
00 Z = 4493846
23
XDOT = -6974
039249 XDOT = -2125
687163
YDOT = -20867
366826 feet/sec YDOT = -6360
373409 meter/sec
ZDOT = 10305
544032 ZDOT = 3141
129821
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
53570487
00020000 00000-0 20000-3 0 9064
2 25544 51
6307 158
9500 0008009 287
5931 72
4360 15
78235817 9091
Satellite: ISS
Catalog Number: 25544
Epoch time: 07157
53570487 = yrday
fracday
Element set: 906
Inclination: 51
6307 deg
RA of node: 158
9500 deg
Eccentricity:
0008009
Arg of perigee: 287
5931 deg
Mean anomaly: 72
4360 deg
Mean motion: 15
78235817 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 909
Checksum: 307
Coasting Arc #8 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2007/158/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5270590
30 A = 6719035
90 meter
Y = 3913223
53 meter E =
0009865
Z = -1401450
46 I = 51
79336
XDOT = -3907
512646 Wp = 347
19954
YDOT = -3171
799808 meter/sec RA = 153
08132 deg
ZDOT = 5840
561511 TA = 357
39178
MA = 357
39692
Ha = 182
285 n
mi
Hp = 180
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17291962
92 X = -5307148
84
Y = 12838659
88 feet Y = 3854080
61 meter
Z = -4597934
58 Z = -1427143
20
XDOT = -12819
923379 XDOT = -3900
127011
YDOT = -10406
167350 feet/sec YDOT = -3215
455282 meter/sec
ZDOT = 19161
947216 ZDOT = 5821
596387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5626706
66 X = 1715020
19
Y = 20767433
30 feet Y = 6329913
67 meter
Z = -4694470
97 Z = -1430874
75
XDOT = -12901
758116 XDOT = -3932
455874
YDOT = 7809
660798 feet/sec YDOT = 2380
384611 meter/sec
ZDOT = 19089
943317 ZDOT = 5818
614723
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
48547459
00020000 00000-0 20000-3 0 9073
2 25544 51
6313 154
0416 0007918 290
4985 69
5330 15
78312352 9242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07158
48547459 = yrday
fracday
Element set: 907
Inclination: 51
6313 deg
RA of node: 154
0416 deg
Eccentricity:
0007918
Arg of perigee: 290
4985 deg
Mean anomaly: 69
5330 deg
Mean motion: 15
78312352 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 924
Checksum: 307
Coasting Arc #9 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2007/159/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2180392
62 A = 6707904
15 meter
Y = 3535025
38 meter E =
0008487
Z = -5274021
75 I = 51
77969
XDOT = -6539
317765 Wp = 66
33995
YDOT = 4070
250249 meter/sec RA = 147
93640 deg
ZDOT = 28
053769 TA = 203
90594
MA = 203
94538
Ha = 182
681 n
mi
Hp = 179
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7153519
09 X = 2166321
67
Y = 11597852
28 feet Y = 3559329
69 meter
Z = -17303220
98 Z = -5263463
16
XDOT = -21454
454610 XDOT = -6584
482162
YDOT = 13353
839398 feet/sec YDOT = 3996
871398 meter/sec
ZDOT = 92
039925 ZDOT = -3
823503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13401955
81 X = 4084916
13
Y = -2732008
58 feet Y = -832716
21 meter
Z = -17262913
39 Z = -5261736
00
XDOT = 4800
346382 XDOT = 1463
145577
YDOT = 23794
283734 feet/sec YDOT = 7252
497682 meter/sec
ZDOT = -27
838642 ZDOT = -8
485218
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
49854361
00020000 00000-0 20000-3 0 9089
2 25544 51
6304 148
8044 0008097 295
1208 64
9117 15
78288329 9405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
49854361 = yrday
fracday
Element set: 908
Inclination: 51
6304 deg
RA of node: 148
8044 deg
Eccentricity:
0008097
Arg of perigee: 295
1208 deg
Mean anomaly: 64
9117 deg
Mean motion: 15
78288329 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 940
Checksum: 316
Coasting Arc #10 (Orbit 955)
---------------------------------------
Vector Time (GMT): 2007/160/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5835299
21 A = 6718971
16 meter
Y = -2987770
62 meter E =
0003392
Z = -1462148
46 I = 51
84074
XDOT = 1066
470702 Wp = 213
55969
YDOT = 4933
435714 meter/sec RA = 142
79337 deg
ZDOT = -5821
245882 TA = 342
51254
MA = 342
52422
Ha = 182
770 n
mi
Hp = 179
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19144682
46 X = 5875378
10
Y = -9802397
04 feet Y = -2922292
77 meter
Z = -4797075
00 Z = -1433703
39
XDOT = 3498
919627 XDOT = 1039
503774
YDOT = 16185
812710 feet/sec YDOT = 4945
211477 meter/sec
ZDOT = -19098
575727 ZDOT = -5816
129870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2839571
01 X = -865501
24
Y = -21343813
18 feet Y = -6505594
26 meter
Z = -4690016
83 Z = -1429517
13
XDOT = 14904
560875 XDOT = 4542
910155
YDOT = 2212
040961 feet/sec YDOT = 674
230085 meter/sec
ZDOT = -19078
650266 ZDOT = -5815
172601
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 07160
51159229
00020000 00000-0 20000-3 0 9096
2 25544 51
6299 143
5671 0008085 299
7673 60
2688 15
78336559 9567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07160
51159229 = yrday
fracday
Element set: 909
Inclination: 51
6299 deg
RA of node: 143
5671 deg
Eccentricity:
0008085
Arg of perigee: 299
7673 deg
Mean anomaly: 60
2688 deg
Mean motion: 15
78336559 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 956
Checksum: 335
Coasting Arc #11 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2007/161/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 258808
93 A = 6711008
56 meter
Y = -4997953
60 meter E =
0008079
Z = 4474204
98 I = 51
83590
XDOT = 6526
089898 Wp = 9
88254
YDOT = -2543
093446 meter/sec RA = 137
60104 deg
ZDOT = -3209
634754 TA = 112
15584
MA = 112
07009
Ha = 182
916 n
mi
Hp = 179
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 849110
65 X = 292942
42
Y = -16397485
57 feet Y = -4994869
18 meter
Z = 14679150
21 Z = 4475544
57
XDOT = 21411
056095 XDOT = 6569
634102
YDOT = -8343
482436 feet/sec YDOT = -2469
871171 meter/sec
ZDOT = -10530
297749 ZDOT = -3177
825207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15305005
99 X = -4664965
83
Y = -5935031
25 feet Y = -1808997
52 meter
Z = 14683602
03 Z = 4475561
90
XDOT = -1525
730203 XDOT = -465
042566
YDOT = -21891
805159 feet/sec YDOT = -6672
622212 meter/sec
ZDOT = -10410
469520 ZDOT = -3173
111110
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 07161
52461959
00020000 00000-0 20000-3 0 9106
2 25544 51
6293 138
3298 0008266 303
3344 56
7030 15
78374155 9729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07161
52461959 = yrday
fracday
Element set: 910
Inclination: 51
6293 deg
RA of node: 138
3298 deg
Eccentricity:
0008266
Arg of perigee: 303
3344 deg
Mean anomaly: 56
7030 deg
Mean motion: 15
78374155 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 972
Checksum: 297
Coasting Arc #12 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2007/162/11:35:05
104
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303136
01 A = 6712967
49 meter
Y = 1230076
31 meter E =
0005280
Z = 3921796
43 I = 51
86338
XDOT = 1522
067900 Wp = 56
06479
YDOT = -6376
667967 meter/sec RA = 132
49648 deg
ZDOT = 4057
245691 TA = 351
93566
MA = 351
94414
Ha = 183
097 n
mi
Hp = 179
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17398740
18 X = -5335548
41
Y = 4035683
42 feet Y = 1170591
84 meter
Z = 12866786
19 Z = 3895954
87
XDOT = 4993
661090 XDOT = 1573
549960
YDOT = -20920
826665 feet/sec YDOT = -6359
360120 meter/sec
ZDOT = 13311
173528 ZDOT = 4064
764082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1414477
92 X = -431132
87
Y = 17874578
58 feet Y = 5448171
55 meter
Z = 12769329
66 Z = 3892091
68
XDOT = -17163
864989 XDOT = -5231
546049
YDOT = -10889
584085 feet/sec YDOT = -3319
145229 meter/sec
ZDOT = 13338
804897 ZDOT = 4065
667732
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 07162
53762552
00020000 00000-0 20000-3 0 9112
2 25544 51
6294 133
0927 0008291 306
3712 53
6688 15
78432738 9885
Satellite: ISS
Catalog Number: 25544
Epoch time: 07162
53762552 = yrday
fracday
Element set: 911
Inclination: 51
6294 deg
RA of node: 133
0927 deg
Eccentricity:
0008291
Arg of perigee: 306
3712 deg
Mean anomaly: 53
6688 deg
Mean motion: 15
78432738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 988
Checksum: 309
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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