Date:
March 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1548)
---------------------------------------
Vector Time (GMT): 2008/086/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4196482
45 A = 6713982
75 meter
Y = -1371849
22 meter E =
0005197
Z = 5056183
55 I = 51
94182
XDOT = 318
346656 Wp = 42
36213
YDOT = -7495
333486 meter/sec RA = 81
82006 deg
ZDOT = -1764
622633 TA = 64
57038
MA = 64
51661
Ha = 186
086 n
mi
Hp = 180
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13767987
03 X = -4205392
49
Y = -4500817
66 feet Y = -1418826
35 meter
Z = 16588528
71 Z = 5035775
32
XDOT = 1044
444409 XDOT = 410
709247
YDOT = -24590
989128 feet/sec YDOT = -7491
257180 meter/sec
ZDOT = -5789
444333 ZDOT = -1762
851519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14483775
65 X = -4414654
82
Y = -1621952
15 feet Y = -494371
02 meter
Z = 16510106
76 Z = 5032280
54
XDOT = -4007
097183 XDOT = -1221
363221
YDOT = -23249
253004 feet/sec YDOT = -7086
372316 meter/sec
ZDOT = -5783
474113 ZDOT = -1762
802910
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 08086
56685484
00020000 00000-0 20000-3 0 9007
2 25544 51
6368 82
3141 0001138 311
7121 48
3946 15
76510337 15490
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
56685484 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 82
3141 deg
Eccentricity:
0001138
Arg of perigee: 311
7121 deg
Mean anomaly: 48
3946 deg
Mean motion: 15
76510337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1549
Checksum: 289
Coasting Arc #2 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2008/087/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -385699
79 A = 6722502
17 meter
Y = 6288408
54 meter E =
0013409
Z = 2326083
65 I = 51
96612
XDOT = -4929
162629 Wp = 69
18679
YDOT = -2325
856878 meter/sec RA = 76
72328 deg
ZDOT = 5450
096937 TA = 316
90004
MA = 317
00495
Ha = 185
876 n
mi
Hp = 180
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1265419
26 X = -467288
83
Y = 20631261
61 feet Y = 6283639
27 meter
Z = 7631508
05 Z = 2324011
64
XDOT = -16171
793401 XDOT = -4929
263881
YDOT = -7630
764034 feet/sec YDOT = -2380
978070 meter/sec
ZDOT = 17880
895464 ZDOT = 5426
150761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3217740
43 X = 980767
28
Y = 20420755
24 feet Y = 6224246
20 meter
Z = 7624241
52 Z = 2323868
81
XDOT = -16055
547953 XDOT = -4893
731016
YDOT = -4136
649484 feet/sec YDOT = -1260
850763 meter/sec
ZDOT = 17788
798998 ZDOT = 5422
025935
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 08087
58105858
00020000 00000-0 20000-3 0 9013
2 25544 51
6371 77
0866 0001071 308
2337 51
8731 15
76578686 15655
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
58105858 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 77
0866 deg
Eccentricity:
0001071
Arg of perigee: 308
2337 deg
Mean anomaly: 51
8731 deg
Mean motion: 15
76578686 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1565
Checksum: 310
Coasting Arc #3 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2008/088/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4435859
80 A = 6716976
72 meter
Y = 2634642
48 meter E =
0007695
Z = -4308694
40 I = 51
93911
XDOT = -631
565140 Wp = 105
50135
YDOT = 6816
231030 meter/sec RA = 71
54483 deg
ZDOT = 3520
886482 TA = 199
99850
MA = 200
02867
Ha = 186
017 n
mi
Hp = 180
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14553345
79 X = 4427000
02
Y = 8643840
16 feet Y = 2684197
23 meter
Z = -14136136
49 Z = -4287166
51
XDOT = -2072
064108 XDOT = -724
842210
YDOT = 22362
962696 feet/sec YDOT = 6808
646995 meter/sec
ZDOT = 11551
464837 ZDOT = 3517
591714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16252972
29 X = 4953905
95
Y = 4969143
34 feet Y = 1514594
89 meter
Z = -14053281
02 Z = -4283440
05
XDOT = 3531
444404 XDOT = 1076
384254
YDOT = 21055
034971 feet/sec YDOT = 6417
574659 meter/sec
ZDOT = 11539
556406 ZDOT = 3517
256792
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 08088
53186242
00020000 00000-0 20000-3 0 9026
2 25544 51
6372 72
1847 0001194 324
5930 35
5155 15
76534866 15805
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
53186242 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 72
1847 deg
Eccentricity:
0001194
Arg of perigee: 324
5930 deg
Mean anomaly: 35
5155 deg
Mean motion: 15
76534866 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1580
Checksum: 293
Coasting Arc #4 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2008/089/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 793988
51 A = 6718712
27 meter
Y = -5524472
01 meter E =
0005766
Z = -3746974
49 I = 51
93568
XDOT = 5249
929964 Wp = 65
05093
YDOT = 3656
555376 meter/sec RA = 66
46111 deg
ZDOT = -4281
415810 TA = 160
01823
MA = 159
99565
Ha = 185
943 n
mi
Hp = 180
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2604949
17 X = 873907
09
Y = -18124908
17 feet Y = -5515146
35 meter
Z = -12293223
38 Z = -3742923
14
XDOT = 17224
179671 XDOT = 5229
449914
YDOT = 11996
572756 feet/sec YDOT = 3715
148554 meter/sec
ZDOT = -14046
639795 ZDOT = -4255
961466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1966234
23 X = -599308
19
Y = -18215362
60 feet Y = -5552042
52 meter
Z = -12278268
84 Z = -3742416
34
XDOT = 18434
940151 XDOT = 5618
969758
YDOT = 7406
253645 feet/sec YDOT = 2257
426111 meter/sec
ZDOT = -13948
612950 ZDOT = -4251
537227
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 08089
54603465
00020000 00000-0 20000-3 0 9030
2 25544 51
6378 66
9560 0001209 329
7398 30
3696 15
76590239 15962
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
54603465 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 66
9560 deg
Eccentricity:
0001209
Arg of perigee: 329
7398 deg
Mean anomaly: 30
3696 deg
Mean motion: 15
76590239 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1596
Checksum: 324
Coasting Arc #5 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2008/090/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4732823
27 A = 6720734
06 meter
Y = -3655548
16 meter E =
0012506
Z = 3055963
57 I = 51
92972
XDOT = 1254
458760 Wp = 90
83643
YDOT = -5774
490619 meter/sec RA = 61
27622 deg
ZDOT = -4947
561920 TA = 53
85272
MA = 53
73707
Ha = 185
954 n
mi
Hp = 180
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15527635
39 X = -4706439
85
Y = -11993268
25 feet Y = -3708325
74 meter
Z = 10026127
21 Z = 3033035
76
XDOT = 4115
678348 XDOT = 1342
971025
YDOT = -18945
179196 feet/sec YDOT = -5759
967710 meter/sec
ZDOT = -16232
158531 ZDOT = -4941
252721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18227869
00 X = -5555854
47
Y = -7379314
92 feet Y = -2249215
19 meter
Z = 9937790
20 Z = 3029038
45
XDOT = -1560
131547 XDOT = -475
528096
YDOT = -18050
675931 feet/sec YDOT = -5501
846024 meter/sec
ZDOT = -16208
565000 ZDOT = -4940
370612
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 08090
56018916
00020000 00000-0 20000-3 0 9046
2 25544 51
6378 61
7278 0001327 331
0624 29
0467 15
76619411 16124
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
56018916 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 61
7278 deg
Eccentricity:
0001327
Arg of perigee: 331
0624 deg
Mean anomaly: 29
0467 deg
Mean motion: 15
76619411 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1612
Checksum: 282
Coasting Arc #6 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2008/091/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1474981
06 A = 6714721
40 meter
Y = 4500325
12 meter E =
0006323
Z = 4756237
73 I = 51
89572
XDOT = -5580
227590 Wp = 113
53274
YDOT = -4618
663003 meter/sec RA = 56
18541 deg
ZDOT = 2634
427589 TA = 310
69594
MA = 310
75086
Ha = 185
835 n
mi
Hp = 179
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4839176
72 X = -1548299
56
Y = 14764846
18 feet Y = 4483421
21 meter
Z = 15604454
50 Z = 4748894
12
XDOT = -18307
833299 XDOT = -5540
963729
YDOT = -15153
093841 feet/sec YDOT = -4680
844693 meter/sec
ZDOT = 8643
135135 ZDOT = 2607
414526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -524097
83 X = -159745
02
Y = 15556583
84 feet Y = 4741646
75 meter
Z = 15576756
24 Z = 4747795
30
XDOT = -20774
323571 XDOT = -6332
013825
YDOT = -9267
131889 feet/sec YDOT = -2824
621800 meter/sec
ZDOT = 8539
023410 ZDOT = 2602
694335
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 08091
57432473
00020000 00000-0 20000-3 0 9057
2 25544 51
6386 56
4998 0001313 326
8551 33
2531 15
76677870 16288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
57432473 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 56
4998 deg
Eccentricity:
0001313
Arg of perigee: 326
8551 deg
Mean anomaly: 33
2531 deg
Mean motion: 15
76677870 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1628
Checksum: 307
Coasting Arc #7 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2008/092/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4953401
69 A = 6723702
02 meter
Y = 4298375
47 meter E =
0009298
Z = -1461971
48 I = 51
90815
XDOT = -2214
335775 Wp = 29
79453
YDOT = 4526
127100 meter/sec RA = 51
01362 deg
ZDOT = 5828
439476 TA = 314
15672
MA = 314
23313
Ha = 185
917 n
mi
Hp = 179
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16251317
87 X = 4912070
37
Y = 14102281
73 feet Y = 4353536
08 meter
Z = -4796494
34 Z = -1438008
62
XDOT = -7264
881153 XDOT = -2293
096338
YDOT = 14849
498360 feet/sec YDOT = 4500
925011 meter/sec
ZDOT = 19122
176757 ZDOT = 5817
490817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19767352
94 X = 6025089
18
Y = 8550385
33 feet Y = 2606157
45 meter
Z = -4704116
20 Z = -1433814
62
XDOT = -1939
745562 XDOT = -591
234447
YDOT = 14938
477086 feet/sec YDOT = 4553
247816 meter/sec
ZDOT = 19080
650347 ZDOT = 5815
782226
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 08092
52506290
00020000 00000-0 20000-3 0 9063
2 25544 51
6383 51
5974 0001331 337
3471 22
7635 15
76664927 16437
Satellite: ISS
Catalog Number: 25544
Epoch time: 08092
52506290 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 51
5974 deg
Eccentricity:
0001331
Arg of perigee: 337
3471 deg
Mean anomaly: 22
7635 deg
Mean motion: 15
76664927 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1643
Checksum: 292
Coasting Arc #8 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2008/093/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2468012
10 A = 6712564
78 meter
Y = -3386068
89 meter E =
0014540
Z = -5256686
97 I = 51
85234
XDOT = 5687
258552 Wp = 79
73542
YDOT = 5143
202432 meter/sec RA = 45
89340 deg
ZDOT = -641
761058 TA = 184
17067
MA = 184
18280
Ha = 185
841 n
mi
Hp = 179
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8097152
55 X = 2531228
08
Y = -11109149
91 feet Y = -3358117
05 meter
Z = -17246348
32 Z = -5244543
69
XDOT = 18658
984752 XDOT = 5632
441311
YDOT = 16874
023726 feet/sec YDOT = 5206
494068 meter/sec
ZDOT = -2105
515282 ZDOT = -614
266029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4246974
32 X = 1294477
77
Y = -13135171
24 feet Y = -4003600
19 meter
Z = -17200119
39 Z = -5242596
39
XDOT = 22101
812031 XDOT = 6736
632307
YDOT = 9768
917499 feet/sec YDOT = 2977
566054 meter/sec
ZDOT = -1999
498489 ZDOT = -609
447139
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 08093
53916478
00020000 00000-0 20000-3 0 9079
2 25544 51
6392 46
3682 0001386 338
4187 21
6919 15
76691824 16597
Satellite: ISS
Catalog Number: 25544
Epoch time: 08093
53916478 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 46
3682 deg
Eccentricity:
0001386
Arg of perigee: 338
4187 deg
Mean anomaly: 21
6919 deg
Mean motion: 15
76691824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1659
Checksum: 328
Coasting Arc #9 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2008/094/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4890225
54 A = 6724382
13 meter
Y = -4594362
94 meter E =
0010195
Z = -367209
92 I = 51
87204
XDOT = 3498
705803 Wp = 134
55078
YDOT = -3249
489822 meter/sec RA = 40
75143 deg
ZDOT = -6046
115985 TA = 49
43258
MA = 49
34388
Ha = 185
828 n
mi
Hp = 179
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16044047
06 X = -4836703
38
Y = -15073369
22 feet Y = -4648749
01 meter
Z = -1204756
94 Z = -390836
16
XDOT = 11478
693579 XDOT = 3564
152909
YDOT = -10661
055848 feet/sec YDOT = -3209
999856 meter/sec
ZDOT = -19836
338534 ZDOT = -6028
960099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20146133
41 X = -6140541
46
Y = -8861341
26 feet Y = -2700936
82 meter
Z = -1295872
13 Z = -394981
82
XDOT = 6725
402321 XDOT = 2049
902628
YDOT = -12447
510106 feet/sec YDOT = -3794
001080 meter/sec
ZDOT = -19770
866725 ZDOT = -6026
160178
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 08094
55324862
00020000 00000-0 20000-3 0 9083
2 25544 51
6400 41
1393 0001371 342
6188 17
4929 15
76719459 16758
Satellite: ISS
Catalog Number: 25544
Epoch time: 08094
55324862 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 41
1393 deg
Eccentricity:
0001371
Arg of perigee: 342
6188 deg
Mean anomaly: 17
4929 deg
Mean motion: 15
76719459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1675
Checksum: 303
Coasting Arc #10 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2008/095/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3665014
34 A = 6712975
92 meter
Y = 2327515
07 meter E =
0005375
Z = 5117956
50 I = 51
81118
XDOT = -5411
095499 Wp = 39
56666
YDOT = -5289
679173 meter/sec RA = 35
59382 deg
ZDOT = -1464
423893 TA = 64
45024
MA = 64
39468
Ha = 185
907 n
mi
Hp = 179
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12024325
27 X = -3715630
74
Y = 7636204
31 feet Y = 2286248
25 meter
Z = 16791195
88 Z = 5100028
67
XDOT = -17752
937990 XDOT = -5344
429397
YDOT = -17354
590464 feet/sec YDOT = -5349
816523 meter/sec
ZDOT = -4804
540333 ZDOT = -1490
548623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8683876
56 X = -2646845
57
Y = 11392231
74 feet Y = 3472352
23 meter
Z = 16722667
78 Z = 5097069
14
XDOT = -21844
408017 XDOT = -6658
175564
YDOT = -9426
985015 feet/sec YDOT = -2873
345033 meter/sec
ZDOT = -4905
307057 ZDOT = -1495
137591
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 08095
56731363
00020000 00000-0 20000-3 0 9094
2 25544 51
6403 35
9109 0001431 345
3661 14
7462 15
76762367 16916
Satellite: ISS
Catalog Number: 25544
Epoch time: 08095
56731363 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 35
9109 deg
Eccentricity:
0001431
Arg of perigee: 345
3661 deg
Mean anomaly: 14
7462 deg
Mean motion: 15
76762367 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1691
Checksum: 292
Coasting Arc #11 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2008/096/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4425087
48 A = 6722226
63 meter
Y = 4568914
46 meter E =
0014349
Z = 2152609
98 I = 51
81844
XDOT = -4921
109726 Wp = 64
84961
YDOT = 2149
984372 meter/sec RA = 30
48124 deg
ZDOT = 5530
394935 TA = 319
21852
MA = 319
32583
Ha = 185
791 n
mi
Hp = 179
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14518003
53 X = 4363211
20
Y = 14989876
85 feet Y = 4618052
54 meter
Z = 7062368
69 Z = 2173956
53
XDOT = -16145
373118 XDOT = -4971
651324
YDOT = 7053
754501 feet/sec YDOT = 2094
671605 meter/sec
ZDOT = 18144
340338 ZDOT = 5506
365031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18957244
70 X = 5778168
18
Y = 8655731
17 feet Y = 2638266
86 meter
Z = 7144723
75 Z = 2177711
80
XDOT = -11911
062058 XDOT = -3630
491715
YDOT = 11125
569502 feet/sec YDOT = 3391
073584 meter/sec
ZDOT = 18052
388345 ZDOT = 5502
367967
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 08096
58136102
00020000 00000-0 20000-3 0 9109
2 25544 51
6406 30
6815 0001446 349
2830 10
8303 15
76776988 17075
Satellite: ISS
Catalog Number: 25544
Epoch time: 08096
58136102 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 30
6815 deg
Eccentricity:
0001446
Arg of perigee: 349
2830 deg
Mean anomaly: 10
8303 deg
Mean motion: 15
76776988 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1707
Checksum: 286
Coasting Arc #12 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2008/097/12:32:04
937
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4898621
96 A = 6716007
16 meter
Y = -1481185
61 meter E =
0008336
Z = -4357025
27 I = 51
77254
XDOT = 4592
331861 Wp = 101
56099
YDOT = 5147
098649 meter/sec RA = 25
29162 deg
ZDOT = 3417
247979 TA = 202
82896
MA = 202
86604
Ha = 185
808 n
mi
Hp = 179
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16071594
37 X = 4935986
67
Y = -4859532
85 feet Y = -1426197
81 meter
Z = -14294702
33 Z = -4333136
57
XDOT = 15066
705580 XDOT = 4517
834280
YDOT = 16886
806591 feet/sec YDOT = 5198
036429 meter/sec
ZDOT = 11211
443500 ZDOT = 3439
376523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13074421
11 X = 3985083
55
Y = -10657281
57 feet Y = -3248339
42 meter
Z = -14203224
36 Z = -4329142
78
XDOT = 19535
653501 XDOT = 5954
467187
YDOT = 8927
787642 feet/sec YDOT = 2721
189673 meter/sec
ZDOT = 11296
848379 ZDOT = 3443
279386
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 08097
53201305
00020000 00000-0 20000-3 0 9114
2 25544 51
6414 25
7793 0001442 352
5374 7
5769 15
76815236 17226
Satellite: ISS
Catalog Number: 25544
Epoch time: 08097
53201305 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 25
7793 deg
Eccentricity:
0001442
Arg of perigee: 352
5374 deg
Mean anomaly: 7
5769 deg
Mean motion: 15
76815236 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1722
Checksum: 282
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data may contain past, current and future orbital data These sources include:
NASA Orbital Flight Dynamics 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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]
If you're still having trouble, please contact the list owner at:
<mailto:list
admin@aus-city
com>
The following physical address is associated with this mailing list:
http://www aus-city com
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list