Date:
September 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2423)
---------------------------------------
Vector Time (GMT): 2007/253/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6016489
02 A = 6720723
69 meter
Y = -16119
77 meter E =
0013569
Z = 2993875
01 I = 51
76790
XDOT = -2474
530098 Wp = 58
38210
YDOT = -5330
383062 meter/sec RA = 23
23451 deg
ZDOT = -4978
087770 TA = 87
06629
MA = 86
91101
Ha = 187
564 n
mi
Hp = 179
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19739137
19 X = -6030405
17
Y = -52886
39 feet Y = -83477
18 meter
Z = 9822424
57 Z = 2964613
39
XDOT = -8118
537066 XDOT = -2390
558631
YDOT = -17488
133406 feet/sec YDOT = -5357
585450 meter/sec
ZDOT = -16332
308957 ZDOT = -4989
904630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18685226
81 X = 5695257
13
Y = 6532119
01 feet Y = 1990989
88 meter
Z = 9711337
63 Z = 2960015
71
XDOT = 2333
437775 XDOT = 711
231834
YDOT = 17789
700804 feet/sec YDOT = 5422
300805 meter/sec
ZDOT = -16377
798245 ZDOT = -4991
952905
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 07253
51691485
00020000 00000-0 20000-3 0 9005
2 25544 51
6343 23
5691 0008856 349
5619 10
5360 15
76688168 24247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07253
51691485 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 23
5691 deg
Eccentricity:
0008856
Arg of perigee: 349
5619 deg
Mean anomaly: 10
5360 deg
Mean motion: 15
76688168 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2424
Checksum: 304
Coasting Arc #2 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2007/254/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1481310
51 A = 6714257
40 meter
Y = 4460958
39 meter E =
0007252
Z = 4788145
28 I = 51
72133
XDOT = -7279
756814 Wp = 43
08348
YDOT = -288
099689 meter/sec RA = 18
12967 deg
ZDOT = 2523
524514 TA = 22
29079
MA = 22
25928
Ha = 187
547 n
mi
Hp = 179
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4859942
62 X = 1408057
49
Y = 14635690
24 feet Y = 4477114
01 meter
Z = 15709138
05 Z = 4795163
19
XDOT = -23883
716582 XDOT = -7288
252957
YDOT = -945
208952 feet/sec YDOT = -369
553364 meter/sec
ZDOT = 8279
279900 ZDOT = 2488
139027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19549
33 X = 5958
64
Y = -15393757
21 feet Y = -4692017
20 meter
Z = 15736306
63 Z = 4796426
26
XDOT = 21325
134605 XDOT = 6499
901028
YDOT = 8343
300687 feet/sec YDOT = 2543
038050 meter/sec
ZDOT = 8144
917957 ZDOT = 2482
570993
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 07254
53099360
00020000 00000-0 20000-3 0 9013
2 25544 51
6357 18
3397 0008960 352
7432 7
3601 15
76766136 24404
Satellite: ISS
Catalog Number: 25544
Epoch time: 07254
53099360 = yrday
fracday
Element set: 901
Inclination: 51
6357 deg
RA of node: 18
3397 deg
Eccentricity:
0008960
Arg of perigee: 352
7432 deg
Mean anomaly: 7
3601 deg
Mean motion: 15
76766136 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2440
Checksum: 289
Coasting Arc #3 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2007/255/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6566009
40 A = 6723613
11 meter
Y = 429752
44 meter E =
0016981
Z = -1333700
12 I = 51
72554
XDOT = 859
533538 Wp = 16
72301
YDOT = 4940
079468 meter/sec RA = 12
94738 deg
ZDOT = 5857
708249 TA = 328
61959
MA = 328
72080
Ha = 187
809 n
mi
Hp = 178
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21542025
58 X = 6567194
71
Y = 1409948
96 feet Y = 503183
80 meter
Z = -4375656
56 Z = -1301799
61
XDOT = 2819
991924 XDOT = 775
773265
YDOT = 16207
609803 feet/sec YDOT = 4949
223381 meter/sec
ZDOT = 19218
202917 ZDOT = 5861
680028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20192330
74 X = -6154622
41
Y = -7704679
90 feet Y = -2348386
43 meter
Z = -4254512
79 Z = -1296775
50
XDOT = 1624
403586 XDOT = 495
118213
YDOT = -14814
268759 feet/sec YDOT = -4515
389118 meter/sec
ZDOT = 19233
863754 ZDOT = 5862
481672
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 07255
48167654
00020000 00000-0 20000-3 0 9021
2 25544 51
6365 13
4378 0009095 357
2379 2
8734 15
76755223 24556
Satellite: ISS
Catalog Number: 25544
Epoch time: 07255
48167654 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 13
4378 deg
Eccentricity:
0009095
Arg of perigee: 357
2379 deg
Mean anomaly: 2
8734 deg
Mean motion: 15
76755223 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2455
Checksum: 309
Coasting Arc #4 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2007/256/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 53978
90 A = 6712169
18 meter
Y = -4189622
61 meter E =
0018148
Z = -5257343
24 I = 51
65922
XDOT = 7649
847113 Wp = 56
04630
YDOT = 684
062603 meter/sec RA = 7
81184 deg
ZDOT = -457
771507 TA = 209
55188
MA = 209
65457
Ha = 187
810 n
mi
Hp = 178
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 177096
13 X = 126363
22
Y = -13745480
99 feet Y = -4188614
65 meter
Z = -17248501
46 Z = -5256904
88
XDOT = 25097
923600 XDOT = 7643
853051
YDOT = 2244
299879 feet/sec YDOT = 769
573969 meter/sec
ZDOT = -1501
875023 ZDOT = -420
622994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4088557
69 X = -1246192
38
Y = 13126067
79 feet Y = 4000825
46 meter
Z = -17247331
78 Z = -5256986
73
XDOT = -22532
362100 XDOT = -6867
863968
YDOT = -8844
533213 feet/sec YDOT = -2695
813723 meter/sec
ZDOT = -1360
786576 ZDOT = -414
767748
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 07256
49571733
00020000 00000-0 20000-3 0 9031
2 25544 51
6367 8
2093 0009178 1
0975 359
0208 15
76808956 24715
Satellite: ISS
Catalog Number: 25544
Epoch time: 07256
49571733 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 8
2093 deg
Eccentricity:
0009178
Arg of perigee: 1
0975 deg
Mean anomaly: 359
0208 deg
Mean motion: 15
76808956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2471
Checksum: 308
Coasting Arc #5 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2007/257/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6658473
31 A = 6723950
39 meter
Y = -756547
73 meter E =
0007903
Z = -565329
55 I = 51
67059
XDOT = 1038
290584 Wp = 83
40157
YDOT = -4704
008285 meter/sec RA = 2
65809 deg
ZDOT = -6004
529558 TA = 102
75005
MA = 102
66170
Ha = 187
889 n
mi
Hp = 178
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21845384
88 X = -6646772
31
Y = -2482111
98 feet Y = -830941
16 meter
Z = -1854755
73 Z = -597648
21
XDOT = 3406
465172 XDOT = 1119
983509
YDOT = -15433
098049 feet/sec YDOT = -4691
941155 meter/sec
ZDOT = -19699
900126 ZDOT = -5999
286761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20423774
22 X = 6225166
38
Y = 8110531
57 feet Y = 2472090
02 meter
Z = -1977514
46 Z = -602746
41
XDOT = -6842
485643 XDOT = -2085
589624
YDOT = 12485
056049 feet/sec YDOT = 3805
445084 meter/sec
ZDOT = -19680
552952 ZDOT = -5998
632540
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 07257
50973767
00020000 00000-0 20000-3 0 9048
2 25544 51
6369 2
9791 0009197 4
9382 355
1872 15
76837428 24875
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
50973767 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 2
9791 deg
Eccentricity:
0009197
Arg of perigee: 4
9382 deg
Mean anomaly: 355
1872 deg
Mean motion: 15
76837428 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2487
Checksum: 335
Coasting Arc #6 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2007/258/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1748773
80 A = 6712975
58 meter
Y = 4073904
44 meter E =
0013648
Z = 5038998
91 I = 51
60533
XDOT = -7438
943408 Wp = 24
83871
YDOT = -1041
557819 meter/sec RA = 357
48071 deg
ZDOT = -1725
730512 TA = 81
83891
MA = 81
68413
Ha = 188
060 n
mi
Hp = 178
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5737446
84 X = -1818677
65
Y = 13365828
23 feet Y = 4053958
07 meter
Z = 16532148
64 Z = 5030333
26
XDOT = -24405
982309 XDOT = -7418
360291
YDOT = -3417
184445 feet/sec YDOT = -1124
629290 meter/sec
ZDOT = -5661
845511 ZDOT = -1761
819249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8928347
96 X = 2721360
46
Y = -11529049
30 feet Y = -3514054
23 meter
Z = 16499734
06 Z = 5029118
94
XDOT = 21952
086367 XDOT = 6690
995925
YDOT = 8635
819953 feet/sec YDOT = 2632
197922 meter/sec
ZDOT = -5798
942997 ZDOT = -1767
517825
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 07258
52373747
00020000 00000-0 20000-3 0 9054
2 25544 51
6375 357
7496 0009365 9
0287 351
1044 15
76869412 25036
Satellite: ISS
Catalog Number: 25544
Epoch time: 07258
52373747 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 357
7496 deg
Eccentricity:
0009365
Arg of perigee: 9
0287 deg
Mean anomaly: 351
1044 deg
Mean motion: 15
76869412 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2503
Checksum: 312
Coasting Arc #7 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2007/259/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6173382
76 A = 6721366
49 meter
Y = 1084280
50 meter E =
0020138
Z = 2392272
41 I = 51
60534
XDOT = -2917
003014 Wp = 49
99017
YDOT = 4695
022785 meter/sec RA = 352
35681 deg
ZDOT = 5382
548896 TA = 337
07273
MA = 337
16251
Ha = 187
995 n
mi
Hp = 177
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20253880
43 X = 6149177
98
Y = 3557350
71 feet Y = 1153179
50 meter
Z = 7848662
76 Z = 2422204
24
XDOT = -9570
219861 XDOT = -2995
434436
YDOT = 15403
618060 feet/sec YDOT = 4661
964860 meter/sec
ZDOT = 17659
281154 ZDOT = 5368
187247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18862895
55 X = -5749410
56
Y = -8078822
51 feet Y = -2462425
10 meter
Z = 7962394
22 Z = 2426937
76
XDOT = 12342
582334 XDOT = 3762
019095
YDOT = -11412
565042 feet/sec YDOT = -3478
549825 meter/sec
ZDOT = 17605
317612 ZDOT = 5366
100808
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 07259
53771588
00020000 00000-0 20000-3 0 9062
2 25544 51
6375 352
5199 0009371 13
1312 347
0095 15
76902880 25195
Satellite: ISS
Catalog Number: 25544
Epoch time: 07259
53771588 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 352
5199 deg
Eccentricity:
0009371
Arg of perigee: 13
1312 deg
Mean anomaly: 347
0095 deg
Mean motion: 15
76902880 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2519
Checksum: 309
Coasting Arc #8 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2007/260/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3270616
76 A = 6716326
92 meter
Y = -4136216
04 meter E =
0011904
Z = -4164119
74 I = 51
55985
XDOT = 6587
450606 Wp = 57
37894
YDOT = 1504
327036 meter/sec RA = 347
14930 deg
ZDOT = 3693
654970 TA = 250
31870
MA = 250
44718
Ha = 188
140 n
mi
Hp = 177
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10730369
93 X = 3336854
25
Y = -13570262
61 feet Y = -4099271
88 meter
Z = -13661810
16 Z = -4148069
92
XDOT = 21612
370754 XDOT = 6552
196073
YDOT = 4935
456154 feet/sec YDOT = 1577
794575 meter/sec
ZDOT = 12118
290585 ZDOT = 3725
571534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13433779
73 X = -4094616
06
Y = 10976072
22 feet Y = 3345506
81 meter
Z = -13601372
13 Z = -4145698
23
XDOT = -19211
326129 XDOT = -5855
612204
YDOT = -8402
806900 feet/sec YDOT = -2561
175543 meter/sec
ZDOT = 12239
603086 ZDOT = 3730
631021
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 07260
48830236
00020000 00000-0 20000-3 0 9075
2 25544 51
6374 347
6178 0009415 16
2429 343
9036 15
76937765 25345
Satellite: ISS
Catalog Number: 25544
Epoch time: 07260
48830236 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 347
6178 deg
Eccentricity:
0009415
Arg of perigee: 16
2429 deg
Mean anomaly: 343
9036 deg
Mean motion: 15
76937765 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2534
Checksum: 312
Coasting Arc #9 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2007/261/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5193987
33 A = 6716897
85 meter
Y = -1619852
07 meter E =
0014885
Z = -3955837
03 I = 51
53375
XDOT = 4522
433763 Wp = 41
51589
YDOT = -4786
560718 meter/sec RA = 342
03599 deg
ZDOT = -3975
472119 TA = 187
16735
MA = 187
18865
Ha = 188
199 n
mi
Hp = 177
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17040640
83 X = -5156270
93
Y = -5314475
29 feet Y = -1677723
30 meter
Z = -12978467
94 Z = -3980978
06
XDOT = 14837
381112 XDOT = 4594
934010
YDOT = -15703
939363 feet/sec YDOT = -4735
582949 meter/sec
ZDOT = -13042
887529 ZDOT = -3953
325789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15607466
28 X = 4757155
72
Y = 8517228
91 feet Y = 2596051
37 meter
Z = -13074078
39 Z = -3984979
09
XDOT = -17062
355185 XDOT = -5200
605860
YDOT = 11361
037742 feet/sec YDOT = 3462
844304 meter/sec
ZDOT = -12959
382826 ZDOT = -3950
019885
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 07261
50224082
00020000 00000-0 20000-3 0 9086
2 25544 51
6370 342
3876 0009448 20
0376 340
1158 15
76946027 25501
Satellite: ISS
Catalog Number: 25544
Epoch time: 07261
50224082 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 342
3876 deg
Eccentricity:
0009448
Arg of perigee: 20
0376 deg
Mean anomaly: 340
1158 deg
Mean motion: 15
76946027 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2550
Checksum: 279
Coasting Arc #10 (Orbit 2565)
---------------------------------------
Vector Time (GMT): 2007/262/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511735
96 A = 6720699
33 meter
Y = 4217785
66 meter E =
0018323
Z = 2643766
25 I = 51
51933
XDOT = -5200
609830 Wp = 71
15771
YDOT = -2276
559808 meter/sec RA = 336
82108 deg
ZDOT = -5208
018262 TA = 78
66375
MA = 78
45794
Ha = 188
324 n
mi
Hp = 177
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14802283
33 X = -4571407
58
Y = 13837879
47 feet Y = 4166999
23 meter
Z = 8673773
77 Z = 2621703
15
XDOT = -17062
368209 XDOT = -5149
466672
YDOT = -7469
028242 feet/sec YDOT = -2334
429978 meter/sec
ZDOT = -17086
674089 ZDOT = -5233
158803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17075227
89 X = 5204529
46
Y = -10975812
42 feet Y = -3345427
63 meter
Z = 8590517
20 Z = 2618389
64
XDOT = 14566
740862 XDOT = 4439
942615
YDOT = 9122
286286 feet/sec YDOT = 2780
472860 meter/sec
ZDOT = -17182
360842 ZDOT = -5237
183585
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 07262
51615832
00020000 00000-0 20000-3 0 9096
2 25544 51
6367 337
1573 0009648 24
3167 335
8451 15
76989451 25662
Satellite: ISS
Catalog Number: 25544
Epoch time: 07262
51615832 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 337
1573 deg
Eccentricity:
0009648
Arg of perigee: 24
3167 deg
Mean anomaly: 335
8451 deg
Mean motion: 15
76989451 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2566
Checksum: 320
Coasting Arc #11 (Orbit 2581)
---------------------------------------
Vector Time (GMT): 2007/263/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3817019
04 A = 6712693
67 meter
Y = 2423446
75 meter E =
0010581
Z = 4952164
00 I = 51
46722
XDOT = -5659
080528 Wp = 59
87878
YDOT = 4849
198165 meter/sec RA = 331
69058 deg
ZDOT = 1990
918079 TA = 10
86750
MA = 10
84466
Ha = 188
176 n
mi
Hp = 176
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12523028
33 X = 3765579
19
Y = 7950940
78 feet Y = 2465843
16 meter
Z = 16247257
21 Z = 4970582
22
XDOT = -18566
537165 XDOT = -5722
555950
YDOT = 15909
442798 feet/sec YDOT = 4785
560207 meter/sec
ZDOT = 6531
883460 ZDOT = 1963
272004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10990157
22 X = -3349799
92
Y = -9847556
87 feet Y = -3001535
33 meter
Z = 16317448
71 Z = 4973558
37
XDOT = 20202
404499 XDOT = 6157
692891
YDOT = -11907
322947 feet/sec YDOT = -3629
352034 meter/sec
ZDOT = 6427
507193 ZDOT = 1959
104193
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 07263
53005313
00020000 00000-0 20000-3 0 9108
2 25544 51
6370 331
9263 0009607 27
4219 332
7451 15
77044653 25822
Satellite: ISS
Catalog Number: 25544
Epoch time: 07263
53005313 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 331
9263 deg
Eccentricity:
0009607
Arg of perigee: 27
4219 deg
Mean anomaly: 332
7451 deg
Mean motion: 15
77044653 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2582
Checksum: 272
Coasting Arc #12 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2007/264/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5208123
99 A = 6723405
32 meter
Y = -4168294
72 meter E =
0020463
Z = -754927
10 I = 51
47752
XDOT = 3539
327479 Wp = 34
89437
YDOT = 3358
093715 meter/sec RA = 326
49702 deg
ZDOT = 5971
547861 TA = 316
84172
MA = 317
00193
Ha = 188
503 n
mi
Hp = 176
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17087020
96 X = 5258014
71
Y = -13675507
61 feet Y = -4109775
58 meter
Z = -2476794
96 Z = -729504
83
XDOT = 11611
966794 XDOT = 3472
505006
YDOT = 11017
367832 feet/sec YDOT = 3397
298867 meter/sec
ZDOT = 19591
692458 ZDOT = 5988
579602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18890672
06 X = -5757876
84
Y = 11072249
03 feet Y = 3374821
50 meter
Z = -2380780
83 Z = -725662
00
XDOT = -8989
068689 XDOT = -2739
868137
YDOT = -11180
199739 feet/sec YDOT = -3407
724880 meter/sec
ZDOT = 19656
734056 ZDOT = 5991
372540
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 07264
48056244
00020000 00000-0 20000-3 0 9113
2 25544 51
6365 327
0234 0009917 30
5116 329
6624 15
77006577 25971
Satellite: ISS
Catalog Number: 25544
Epoch time: 07264
48056244 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 327
0234 deg
Eccentricity:
0009917
Arg of perigee: 30
5116 deg
Mean anomaly: 329
6624 deg
Mean motion: 15
77006577 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2597
Checksum: 296
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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