Date:
September 14th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4800 7 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 2454)
---------------------------------------
Vector Time (GMT): 2007/255/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6580155
83 A = 6724358
09 meter
Y = 1301056
72 meter E =
0019336
Z = -261654
51 I = 51
72769
XDOT = -702
257521 Wp = 22
97388
YDOT = 4734
505308 meter/sec RA = 12
94817 deg
ZDOT = 6047
744447 TA = 334
18019
MA = 334
27657
Ha = 187
812 n
mi
Hp = 178
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21588437
77 X = 6566389
24
Y = 4268558
78 feet Y = 1374562
74 meter
Z = -858446
54 Z = -229721
66
XDOT = -2303
994491 XDOT = -784
526119
YDOT = 15533
153896 feet/sec YDOT = 4726
192746 meter/sec
ZDOT = 19841
681257 ZDOT = 6044
132686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19510546
27 X = -5946814
50
Y = -10188889
62 feet Y = -3105573
56 meter
Z = -737076
98 Z = -224661
06
XDOT = 5957
938051 XDOT = 1815
979518
YDOT = -12797
203698 feet/sec YDOT = -3900
587687 meter/sec
ZDOT = 19828
530994 ZDOT = 6043
736247
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
48168286
00020000 00000-0 20000-3 0 9001
2 25544 51
6362 13
4392 0009160 357
2628 2
8485 15
76745246 24556
Satellite: ISS
Catalog Number: 25544
Epoch time: 07255
48168286 = yrday
fracday
Element set: 900
Inclination: 51
6362 deg
RA of node: 13
4392 deg
Eccentricity:
0009160
Arg of perigee: 357
2628 deg
Mean anomaly: 2
8485 deg
Mean motion: 15
76745246 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2455
Checksum: 299
Coasting Arc #2 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2007/256/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1410631
15 A = 6712341
15 meter
Y = -3981009
68 meter E =
0016672
Z = -5228814
66 I = 51
65930
XDOT = 7477
963330 Wp = 62
48797
YDOT = 1642
823128 meter/sec RA = 7
79215 deg
ZDOT = 776
063394 TA = 214
84464
MA = 214
95390
Ha = 187
845 n
mi
Hp = 178
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4628054
95 X = 1480443
31
Y = -13061055
39 feet Y = -3964845
26 meter
Z = -17154903
73 Z = -5221791
91
XDOT = 24534
000425 XDOT = 7455
267263
YDOT = 5389
839660 feet/sec YDOT = 1726
319098 meter/sec
ZDOT = 2546
139744 ZDOT = 812
336252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8024522
13 X = -2445874
35
Y = 11336441
09 feet Y = 3455347
24 meter
Z = -17128716
55 Z = -5220832
80
XDOT = -21379
590367 XDOT = -6516
499144
YDOT = -11125
034294 feet/sec YDOT = -3390
910453 meter/sec
ZDOT = 2684
017475 ZDOT = 818
088526
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
49573221
00020000 00000-0 20000-3 0 9013
2 25544 51
6364 8
2109 0009211 1
2859 358
8328 15
76803588 24717
Satellite: ISS
Catalog Number: 25544
Epoch time: 07256
49573221 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 8
2109 deg
Eccentricity:
0009211
Arg of perigee: 1
2859 deg
Mean anomaly: 358
8328 deg
Mean motion: 15
76803588 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2471
Checksum: 292
Coasting Arc #3 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2007/257/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6337897
53 A = 6722983
68 meter
Y = -1571155
65 meter E =
0006311
Z = -1613134
61 I = 51
66689
XDOT = 2558
281371 Wp = 61
59853
YDOT = -4431
735781 meter/sec RA = 2
65853 deg
ZDOT = -5748
929887 TA = 136
20463
MA = 136
15456
Ha = 187
941 n
mi
Hp = 178
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20793627
08 X = -6312021
21
Y = -5154710
13 feet Y = -1641885
02 meter
Z = -5292436
38 Z = -1643861
42
XDOT = 8393
311585 XDOT = 2635
575067
YDOT = -14539
815556 feet/sec YDOT = -4402
695835 meter/sec
ZDOT = -18861
318528 ZDOT = -5736
313617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18825556
38 X = 5738029
59
Y = 10163380
44 feet Y = 3097798
36 meter
Z = -5409248
70 Z = -1648739
00
XDOT = -11111
336199 XDOT = -3386
735273
YDOT = 10592
067399 feet/sec YDOT = 3228
462143 meter/sec
ZDOT = -18813
952354 ZDOT = -5734
492677
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
50976505
00020000 00000-0 20000-3 0 9029
2 25544 51
6366 2
9806 0009252 4
9679 355
1582 15
76816363 24873
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
50976505 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 2
9806 deg
Eccentricity:
0009252
Arg of perigee: 4
9679 deg
Mean anomaly: 355
1582 deg
Mean motion: 15
76816363 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2487
Checksum: 314
Coasting Arc #4 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2007/258/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3015958
37 A = 6714856
32 meter
Y = 3808547
49 meter E =
0015634
Z = 4633930
59 I = 51
61068
XDOT = -6884
782641 Wp = 34
28203
YDOT = -1958
474285 meter/sec RA = 357
46458 deg
ZDOT = -2853
915427 TA = 84
00419
MA = 83
82604
Ha = 188
154 n
mi
Hp = 178
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9894876
56 X = -3080833
02
Y = 12495234
54 feet Y = 3774458
84 meter
Z = 15203184
34 Z = 4619121
12
XDOT = -22587
869558 XDOT = -6848
507034
YDOT = -6425
440569 feet/sec YDOT = -2035
261134 meter/sec
ZDOT = -9363
239591 ZDOT = -2887
273858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12610292
87 X = 3843617
27
Y = -9834249
96 feet Y = -2997479
39 meter
Z = 15147419
71 Z = 4616933
53
XDOT = 19708
076421 XDOT = 6007
021693
YDOT = 10565
994923 feet/sec YDOT = 3220
515253 meter/sec
ZDOT = -9490
081264 ZDOT = -2892
576769
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
52378166
00020000 00000-0 20000-3 0 9032
2 25544 51
6370 357
7514 0009374 9
4071 350
7268 15
76821747 25039
Satellite: ISS
Catalog Number: 25544
Epoch time: 07258
52378166 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 357
7514 deg
Eccentricity:
0009374
Arg of perigee: 9
4071 deg
Mean anomaly: 350
7268 deg
Mean motion: 15
76821747 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2503
Checksum: 303
Coasting Arc #5 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2007/259/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5543647
91 A = 6719210
74 meter
Y = 1876985
75 meter E =
0017503
Z = 3277642
49 I = 51
59749
XDOT = -4272
327922 Wp = 57
11488
YDOT = 4352
430214 meter/sec RA = 352
35215 deg
ZDOT = 4724
759726 TA = 341
45700
MA = 341
52070
Ha = 188
008 n
mi
Hp = 177
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18187821
23 X = 5506324
76
Y = 6158089
72 feet Y = 1938769
38 meter
Z = 10753420
23 Z = 3304483
14
XDOT = -14016
823891 XDOT = -4343
632232
YDOT = 14279
626686 feet/sec YDOT = 4304
256108 meter/sec
ZDOT = 15501
180204 ZDOT = 4703
831152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16373242
37 X = -4990564
27
Y = -9921177
57 feet Y = -3023974
92 meter
Z = 10855511
34 Z = 3308759
86
XDOT = 16127
085899 XDOT = 4915
535782
YDOT = -9709
199440 feet/sec YDOT = -2959
363989 meter/sec
ZDOT = 15422
252259 ZDOT = 4700
702488
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
53777916
00020000 00000-0 20000-3 0 9041
2 25544 51
6372 352
5215 0009370 12
8949 347
2454 15
76880604 25192
Satellite: ISS
Catalog Number: 25544
Epoch time: 07259
53777916 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 352
5215 deg
Eccentricity:
0009370
Arg of perigee: 12
8949 deg
Mean anomaly: 347
2454 deg
Mean motion: 15
76880604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2519
Checksum: 315
Coasting Arc #6 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2007/260/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4336324
21 A = 6718885
98 meter
Y = -3797695
74 meter E =
0011716
Z = -3449613
29 I = 51
56751
XDOT = 5722
623844 Wp = 39
63777
YDOT = 2406
443535 meter/sec RA = 347
14014 deg
ZDOT = 4561
675160 TA = 279
40085
MA = 279
53328
Ha = 188
268 n
mi
Hp = 177
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14226785
45 X = 4395226
12
Y = -12459631
69 feet Y = -3748875
23 meter
Z = -11317628
89 Z = -3428404
03
XDOT = 18775
012613 XDOT = 5673
129250
YDOT = 7895
155956 feet/sec YDOT = 2470
160487 meter/sec
ZDOT = 14966
125852 ZDOT = 4589
355739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16481502
87 X = -5023562
07
Y = 9370681
55 feet Y = 2856183
74 meter
Z = -11237569
15 Z = -3425211
08
XDOT = -16065
164385 XDOT = -4896
662105
YDOT = -10250
603194 feet/sec YDOT = -3124
383854 meter/sec
ZDOT = 15071
465166 ZDOT = 4593
782583
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
48838871
00020000 00000-0 20000-3 0 9056
2 25544 51
6371 347
6195 0009501 15
6057 344
5399 15
76872763 25342
Satellite: ISS
Catalog Number: 25544
Epoch time: 07260
48838871 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 347
6195 deg
Eccentricity:
0009501
Arg of perigee: 15
6057 deg
Mean anomaly: 344
5399 deg
Mean motion: 15
76872763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2534
Checksum: 320
Coasting Arc #7 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2007/261/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4331249
53 A = 6714843
52 meter
Y = -2398882
96 meter E =
0017988
Z = -4553252
95 I = 51
52592
XDOT = 5585
673102 Wp = 45
60375
YDOT = -4337
831832 meter/sec RA = 342
02448 deg
ZDOT = -3022
908514 TA = 194
23640
MA = 194
28716
Ha = 188
280 n
mi
Hp = 177
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14210136
24 X = -4281983
84
Y = -7870350
93 feet Y = -2447041
99 meter
Z = -14938493
94 Z = -4574174
71
XDOT = 18325
699152 XDOT = 5648
449142
YDOT = -14231
731732 feet/sec YDOT = -4275
018689 meter/sec
ZDOT = -9917
678852 ZDOT = -2995
620535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12458989
32 X = 3797499
94
Y = 10308096
56 feet Y = 3141907
83 meter
Z = -15018179
90 Z = -4577541
23
XDOT = -19911
249015 XDOT = -6068
948700
YDOT = 9742
800716 feet/sec YDOT = 2969
605658 meter/sec
ZDOT = -9814
607091 ZDOT = -2991
492241
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
50235513
00020000 00000-0 20000-3 0 9065
2 25544 51
6367 342
3896 0009483 19
7470 340
4060 15
76894179 25503
Satellite: ISS
Catalog Number: 25544
Epoch time: 07261
50235513 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 342
3896 deg
Eccentricity:
0009483
Arg of perigee: 19
7470 deg
Mean anomaly: 340
4060 deg
Mean motion: 15
76894179 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2550
Checksum: 300
Coasting Arc #8 (Orbit 2565)
---------------------------------------
Vector Time (GMT): 2007/262/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5294629
58 A = 6722589
56 meter
Y = 3761288
15 meter E =
0016916
Z = 1728306
74 I = 51
52464
XDOT = -4117
645121 Wp = 80
43410
YDOT = -3157
808863 meter/sec RA = 336
81975 deg
ZDOT = -5692
081857 TA = 80
38907
MA = 80
19799
Ha = 188
402 n
mi
Hp = 177
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17370831
97 X = -5344691
23
Y = 12340184
22 feet Y = 3701800
69 meter
Z = 5670297
71 Z = 1702463
66
XDOT = -13509
334388 XDOT = -4054
376682
YDOT = -10360
265300 feet/sec YDOT = -3203
500911 meter/sec
ZDOT = -18674
809243 ZDOT = -5711
931868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19199365
27 X = 5851966
53
Y = -9300982
27 feet Y = -2834939
40 meter
Z = 5572641
04 Z = 1698540
99
XDOT = 10833
650283 XDOT = 3302
096606
YDOT = 11028
968687 feet/sec YDOT = 3361
629656 meter/sec
ZDOT = -18750
516814 ZDOT = -5715
157525
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
51630473
00020000 00000-0 20000-3 0 9072
2 25544 51
6362 337
1595 0009663 24
2732 335
8886 15
76932939 25666
Satellite: ISS
Catalog Number: 25544
Epoch time: 07262
51630473 = yrday
fracday
Element set: 907
Inclination: 51
6362 deg
RA of node: 337
1595 deg
Eccentricity:
0009663
Arg of perigee: 24
2732 deg
Mean anomaly: 335
8886 deg
Mean motion: 15
76932939 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2566
Checksum: 320
Coasting Arc #9 (Orbit 2581)
---------------------------------------
Vector Time (GMT): 2007/263/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2824309
17 A = 6711817
17 meter
Y = 3173119
65 meter E =
0009988
Z = 5189414
63 I = 51
46334
XDOT = -6380
930838 Wp = 45
86199
YDOT = 4240
734387 meter/sec RA = 331
67432 deg
ZDOT = 885
554575 TA = 35
73057
MA = 35
66377
Ha = 188
292 n
mi
Hp = 176
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9266106
19 X = 2763407
62
Y = 10410497
53 feet Y = 3204362
12 meter
Z = 17025638
56 Z = 5202987
27
XDOT = -20934
812460 XDOT = -6432
178999
YDOT = 13913
170560 feet/sec YDOT = 4169
092664 meter/sec
ZDOT = 2905
362779 ZDOT = 854
431434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7529238
51 X = -2294911
90
Y = -11652479
76 feet Y = -3551675
83 meter
Z = 17077524
24 Z = 5205229
39
XDOT = 21928
870473 XDOT = 6683
919720
YDOT = -10111
569864 feet/sec YDOT = -3082
006495 meter/sec
ZDOT = 2787
718005 ZDOT = 849
696448
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
53023536
00020000 00000-0 20000-3 0 9082
2 25544 51
6366 331
9287 0009638 27
1954 332
9714 15
76990595 25828
Satellite: ISS
Catalog Number: 25544
Epoch time: 07263
53023536 = yrday
fracday
Element set: 908
Inclination: 51
6366 deg
RA of node: 331
9287 deg
Eccentricity:
0009638
Arg of perigee: 27
1954 deg
Mean anomaly: 332
9714 deg
Mean motion: 15
76990595 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2582
Checksum: 322
Coasting Arc #10 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2007/264/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5686174
35 A = 6723777
87 meter
Y = -3559478
37 meter E =
0022464
Z = 213904
64 I = 51
47790
XDOT = 2378
358968 Wp = 39
92648
YDOT = 4181
585080 meter/sec RA = 326
49940 deg
ZDOT = 6029
232150 TA = 322
40813
MA = 322
56495
Ha = 188
589 n
mi
Hp = 176
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18655427
66 X = 5724515
25
Y = -11678078
64 feet Y = -3495677
98 meter
Z = 701786
87 Z = 241621
23
XDOT = 7803
014987 XDOT = 2302
134158
YDOT = 13719
111155 feet/sec YDOT = 4207
755055 meter/sec
ZDOT = 19780
945373 ZDOT = 6040
601062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20019415
11 X = -6101917
73
Y = 9136052
35 feet Y = 2784668
76 meter
Z = 806580
87 Z = 245845
85
XDOT = -5163
397200 XDOT = -1573
803467
YDOT = -13147
975733 feet/sec YDOT = -4007
503003 meter/sec
ZDOT = 19824
587538 ZDOT = 6042
534281
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
54415307
00020000 00000-0 20000-3 0 9096
2 25544 51
6361 326
6988 0009955 31
0720 329
1032 15
76952765 25984
Satellite: ISS
Catalog Number: 25544
Epoch time: 07264
54415307 = yrday
fracday
Element set: 909
Inclination: 51
6361 deg
RA of node: 326
6988 deg
Eccentricity:
0009955
Arg of perigee: 31
0720 deg
Mean anomaly: 329
1032 deg
Mean motion: 15
76952765 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2598
Checksum: 312
Coasting Arc #11 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2007/265/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1330513
49 A = 6712250
76 meter
Y = -4160055
89 meter E =
0020143
Z = -5112310
69 I = 51
41522
XDOT = 6538
492934 Wp = 73
75020
YDOT = -3802
336454 meter/sec RA = 321
31293 deg
ZDOT = 1402
508768 TA = 209
68029
MA = 209
79473
Ha = 188
571 n
mi
Hp = 176
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4365201
74 X = -1259061
61
Y = -13648477
33 feet Y = -4174535
04 meter
Z = -16772672
87 Z = -5118600
67
XDOT = 21451
748470 XDOT = 6573
712153
YDOT = -12474
857133 feet/sec YDOT = -3729
022381 meter/sec
ZDOT = 4601
406719 ZDOT = 1434
358325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2689442
05 X = 819741
94
Y = 14045812
98 feet Y = 4281163
79 meter
Z = -16797038
86 Z = -5119737
44
XDOT = -21682
084662 XDOT = -6608
699405
YDOT = 9758
757024 feet/sec YDOT = 2974
469141 meter/sec
ZDOT = 4721
859680 ZDOT = 1439
222830
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 07265
49468156
00020000 00000-0 20000-3 0 9103
2 25544 51
6354 321
7954 0009931 34
5544 325
6265 15
76998891 26138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07265
49468156 = yrday
fracday
Element set: 910
Inclination: 51
6354 deg
RA of node: 321
7954 deg
Eccentricity:
0009931
Arg of perigee: 34
5544 deg
Mean anomaly: 325
6265 deg
Mean motion: 15
76998891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2613
Checksum: 323
Coasting Arc #12 (Orbit 2628)
---------------------------------------
Vector Time (GMT): 2007/266/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623533
83 A = 6721328
77 meter
Y = 2957126
92 meter E =
0010996
Z = -2208065
76 I = 51
42473
XDOT = -689
942820 Wp = 71
59213
YDOT = -5376
414870 meter/sec RA = 316
17032 deg
ZDOT = -5461
939962 TA = 133
23580
MA = 133
14395
Ha = 188
635 n
mi
Hp = 176
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18449914
15 X = -5645456
56
Y = 9701859
99 feet Y = 2894118
71 meter
Z = -7244310
23 Z = -2235438
19
XDOT = -2263
591928 XDOT = -603
238627
YDOT = -17639
156398 feet/sec YDOT = -5383
645666 meter/sec
ZDOT = -17919
750531 ZDOT = -5465
080841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19261002
19 X = 5870753
47
Y = -7875793
54 feet Y = -2400541
87 meter
Z = -7347865
04 Z = -2239629
26
XDOT = -127
809493 XDOT = -38
956333
YDOT = 16360
991934 feet/sec YDOT = 4986
830341 meter/sec
ZDOT = -17932
313111 ZDOT = -5465
769036
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 07266
50856365
00020000 00000-0 20000-3 0 9110
2 25544 51
6354 316
5644 0010059 39
1485 321
0405 15
77046594 26292
Satellite: ISS
Catalog Number: 25544
Epoch time: 07266
50856365 = yrday
fracday
Element set: 911
Inclination: 51
6354 deg
RA of node: 316
5644 deg
Eccentricity:
0010059
Arg of perigee: 39
1485 deg
Mean anomaly: 321
0405 deg
Mean motion: 15
77046594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2629
Checksum: 294
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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