Date:
September 4th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 3578)
---------------------------------------
Vector Time (GMT): 2010/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2412178
69 A = 6728243
65 meter
Y = 3703164
02 meter E =
0009910
Z = -5079835
80 I = 51
57106
XDOT = -7118
735458 Wp = 64
42788
YDOT = -2415
220978 meter/sec RA = 188
85700 deg
ZDOT = 1626
337450 TA = 221
19453
MA = 221
26936
Ha = 194
687 n
mi
Hp = 188
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7913972
07 X = -2428732
12
Y = 12149488
26 feet Y = 3676097
10 meter
Z = -16666127
96 Z = -5091594
24
XDOT = -23355
431294 XDOT = -7099
099329
YDOT = -7923
953339 feet/sec YDOT = -2494
717173 meter/sec
ZDOT = 5335
752789 ZDOT = 1591
802544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11228658
28 X = 3422495
04
Y = -9087850
28 feet Y = -2769976
77 meter
Z = -16713140
06 Z = -5094165
09
XDOT = 19062
676079 XDOT = 5810
303669
YDOT = 14034
871434 feet/sec YDOT = 4277
828813 meter/sec
ZDOT = 5197
440502 ZDOT = 1584
179865
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 10246
51321039
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 189
8456 0008498 327
8779 32
1864 15
71435228 35794
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51321039 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 189
8456 deg
Eccentricity:
0008498
Arg of perigee: 327
8779 deg
Mean anomaly: 32
1864 deg
Mean motion: 15
71435228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 332
Coasting Arc #2 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2010/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6644970
72 A = 6739270
33 meter
Y = 931698
27 meter E =
0003196
Z = -624373
43 I = 51
63922
XDOT = -1215
059472 Wp = 105
13680
YDOT = 4670
266058 meter/sec RA = 183
75792 deg
ZDOT = -5988
631873 TA = 81
64911
MA = 81
61288
Ha = 194
839 n
mi
Hp = 188
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21801085
03 X = 6637091
49
Y = 3056752
86 feet Y = 1005962
26 meter
Z = -2048469
25 Z = -592111
66
XDOT = -3986
415591 XDOT = -1238
101574
YDOT = 15322
395205 feet/sec YDOT = 4656
549704 meter/sec
ZDOT = -19647
742367 ZDOT = -5994
590531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19920715
22 X = -6071834
00
Y = -9397275
85 feet Y = -2864289
68 meter
Z = -1919266
66 Z = -584992
48
XDOT = 7560
602875 XDOT = 2304
471756
YDOT = -12028
391921 feet/sec YDOT = -3666
253857 meter/sec
ZDOT = -19671
516588 ZDOT = -5995
878256
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 10247
53069351
00016717 00000-0 10270-3 0 9014
2 25544 51
6442 184
6406 0008500 331
7975 28
2726 15
71456516 35951
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53069351 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 184
6406 deg
Eccentricity:
0008500
Arg of perigee: 331
7975 deg
Mean anomaly: 28
2726 deg
Mean motion: 15
71456516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 309
Coasting Arc #3 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2010/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -341744
14 A = 6727225
23 meter
Y = -4166575
94 meter E =
0007320
Z = 5271308
84 I = 51
62983
XDOT = 7685
259167 Wp = 350
71117
YDOT = -358
511398 meter/sec RA = 178
63822 deg
ZDOT = 222
000812 TA = 97
22211
MA = 97
13889
Ha = 194
880 n
mi
Hp = 188
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1121207
80 X = -320734
02
Y = -13669868
56 feet Y = -4170279
93 meter
Z = 17294320
35 Z = 5269699
80
XDOT = 25214
104878 XDOT = 7687
618497
YDOT = -1176
218496 feet/sec YDOT = -272
557025 meter/sec
ZDOT = 728
349121 ZDOT = 259
341009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2660135
07 X = -810809
17
Y = 13463718
15 feet Y = 4103741
29 meter
Z = 17287796
42 Z = 5269320
35
XDOT = -23545
201780 XDOT = -7176
577503
YDOT = -5749
173405 feet/sec YDOT = -1752
348054 meter/sec
ZDOT = 877
881552 ZDOT = 267
578297
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 10248
54816256
00016717 00000-0 10270-3 0 9021
2 25544 51
6446 179
4358 0008573 334
9290 25
1455 15
71509450 36118
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54816256 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 179
4358 deg
Eccentricity:
0008573
Arg of perigee: 334
9290 deg
Mean anomaly: 25
1455 deg
Mean motion: 15
71509450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 313
Coasting Arc #4 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2010/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6471227
90 A = 6738868
87 meter
Y = 1541161
83 meter E =
0015950
Z = -1012982
24 I = 51
69928
XDOT = -1993
068550 Wp = 10
93744
YDOT = -4489
193334 meter/sec RA = 173
51158 deg
ZDOT = 5932
921539 TA = 338
00297
MA = 338
07135
Ha = 195
064 n
mi
Hp = 187
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21231062
65 X = -6483059
68
Y = 5056305
20 feet Y = 1468730
47 meter
Z = -3323432
53 Z = -1044447
81
XDOT = -6538
938813 XDOT = -1971
542072
YDOT = -14728
324586 feet/sec YDOT = -4511
360348 meter/sec
ZDOT = 19464
965680 ZDOT = 5923
291880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21793322
03 X = 6642604
56
Y = 722504
36 feet Y = 220219
33 meter
Z = -3449427
40 Z = -1051385
47
XDOT = 2583
016419 XDOT = 787
303404
YDOT = 14372
703922 feet/sec YDOT = 4380
800155 meter/sec
ZDOT = 19426
306711 ZDOT = 5921
138285
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 10249
50203035
00016717 00000-0 10270-3 0 9034
2 25544 51
6447 174
5557 0008626 339
1935 20
8874 15
71483811 36263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50203035 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 174
5557 deg
Eccentricity:
0008626
Arg of perigee: 339
1935 deg
Mean anomaly: 20
8874 deg
Mean motion: 15
71483811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 311
Coasting Arc #5 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2010/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3025918
33 A = 6728580
63 meter
Y = 3390660
81 meter E =
0015234
Z = -4974051
97 I = 51
69610
XDOT = -6762
843939 Wp = 40
74406
YDOT = 3030
304647 meter/sec RA = 168
42593 deg
ZDOT = -2040
640185 TA = 209
43915
MA = 209
52503
Ha = 195
196 n
mi
Hp = 187
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9927553
58 X = 3011941
19
Y = 11124215
24 feet Y = 3424419
89 meter
Z = -16319068
13 Z = -4959386
46
XDOT = -22187
808199 XDOT = -6786
313793
YDOT = 9941
944380 feet/sec YDOT = 2954
547077 meter/sec
ZDOT = -6695
013731 ZDOT = -2073
550925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6961169
00 X = -2121764
31
Y = -13257552
99 feet Y = -4040902
15 meter
Z = -16260254
75 Z = -4956125
65
XDOT = 22951
848283 XDOT = 6995
723357
YDOT = -3646
875589 feet/sec YDOT = -1111
567679 meter/sec
ZDOT = -6826
775460 ZDOT = -2080
801160
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 10250
51947577
00016717 00000-0 10270-3 0 9044
2 25544 51
6459 169
3504 0008580 343
5311 16
5571 15
71534605 36428
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51947577 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 169
3504 deg
Eccentricity:
0008580
Arg of perigee: 343
5311 deg
Mean anomaly: 16
5571 deg
Mean motion: 15
71534605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 306
Coasting Arc #6 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2010/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5109752
63 A = 6736414
76 meter
Y = -3600494
76 meter E =
0012499
Z = 2509224
36 I = 51
75210
XDOT = 4708
553402 Wp = 66
63976
YDOT = 2960
178167 meter/sec RA = 163
27749 deg
ZDOT = -5315
154969 TA = 85
04307
MA = 84
90038
Ha = 195
276 n
mi
Hp = 187
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16764280
28 X = 5137444
98
Y = -11812646
86 feet Y = -3543199
36 meter
Z = 8232363
39 Z = 2534114
97
XDOT = 15448
009849 XDOT = 4700
922076
YDOT = 9711
870627 feet/sec YDOT = 3012
788850 meter/sec
ZDOT = -17438
172471 ZDOT = -5292
299807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18988998
40 X = -5787846
71
Y = 7638543
30 feet Y = 2328228
00 meter
Z = 8331993
89 Z = 2539591
74
XDOT = -12334
910380 XDOT = -3759
680684
YDOT = -11651
656600 feet/sec YDOT = -3551
424932 meter/sec
ZDOT = -17346
557822 ZDOT = -5287
230824
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 10251
53690841
00016717 00000-0 10270-3 0 9057
2 25544 51
6458 164
1453 0008570 346
9373 13
1565 15
71532889 36582
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53690841 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 164
1453 deg
Eccentricity:
0008570
Arg of perigee: 346
9373 deg
Mean anomaly: 13
1565 deg
Mean motion: 15
71532889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 323
Coasting Arc #7 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2010/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4995197
48 A = 6731532
79 meter
Y = -1580648
63 meter E =
0010182
Z = 4215567
43 I = 51
76445
XDOT = 4642
903746 Wp = 56
22065
YDOT = -4948
695891 meter/sec RA = 158
21560 deg
ZDOT = 3645
313324 TA = 356
72756
MA = 356
73421
Ha = 195
515 n
mi
Hp = 187
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16388443
17 X = -4997629
57
Y = -5185855
07 feet Y = -1636521
11 meter
Z = 13830601
81 Z = 4191295
03
XDOT = 15232
623840 XDOT = 4680
187642
YDOT = -16235
878908 feet/sec YDOT = -4896
567332 meter/sec
ZDOT = 11959
689382 ZDOT = 3667
959576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14980006
70 X = 4565906
04
Y = 8588051
51 feet Y = 2617638
10 meter
Z = 13733334
60 Z = 4185920
39
XDOT = -17656
773088 XDOT = -5381
784437
YDOT = 11524
767536 feet/sec YDOT = 3512
749145 meter/sec
ZDOT = 12050
307764 ZDOT = 3672
933806
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 10252
55432765
00016717 00000-0 10270-3 0 9060
2 25544 51
6460 158
9398 0008617 350
9089 9
1916 15
71554027 36746
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55432765 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 158
9398 deg
Eccentricity:
0008617
Arg of perigee: 350
9089 deg
Mean anomaly: 9
1916 deg
Mean motion: 15
71554027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 330
Coasting Arc #8 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2836936
95 A = 6732770
61 meter
Y = 4786884
75 meter E =
0008732
Z = -3789047
72 I = 51
79718
XDOT = -6415
453952 Wp = 36
43293
YDOT = -468
173026 meter/sec RA = 153
05835 deg
ZDOT = 4223
740992 TA = 277
82175
MA = 277
92087
Ha = 195
450 n
mi
Hp = 186
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9307535
94 X = -2871847
34
Y = 15705002
45 feet Y = 4754964
90 meter
Z = -12431258
93 Z = -3802914
82
XDOT = -21048
077271 XDOT = -6430
260204
YDOT = -1536
000740 feet/sec YDOT = -539
996910 meter/sec
ZDOT = 13857
417954 ZDOT = 4192
538659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12147113
43 X = 3702440
17
Y = -13577297
35 feet Y = -4138360
23 meter
Z = -12486719
25 Z = -3805952
03
XDOT = 19422
980185 XDOT = 5920
124360
YDOT = 4783
187228 feet/sec YDOT = 1457
915467 meter/sec
ZDOT = 13732
406020 ZDOT = 4185
637355
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 10253
50814568
00016717 00000-0 10270-3 0 9072
2 25544 51
6462 154
0598 0008680 354
0627 6
0431 15
71585218 36890
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50814568 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 154
0598 deg
Eccentricity:
0008680
Arg of perigee: 354
0627 deg
Mean anomaly: 6
0431 deg
Mean motion: 15
71585218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 316
Coasting Arc #9 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2010/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5924899
51 A = 6734956
54 meter
Y = -821755
49 meter E =
0008358
Z = -3107258
12 I = 51
83077
XDOT = -1784
259139 Wp = 27
97906
YDOT = 5651
701999 meter/sec RA = 148
00377 deg
ZDOT = -4894
959236 TA = 187
91930
MA = 187
93250
Ha = 195
558 n
mi
Hp = 186
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19438646
68 X = 5948742
78
Y = -2696048
21 feet Y = -755366
59 meter
Z = -10194416
41 Z = -3078416
79
XDOT = -5853
868566 XDOT = -1823
545899
YDOT = 18542
329394 feet/sec YDOT = 5631
529370 meter/sec
ZDOT = -16059
577545 ZDOT = -4903
723014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19665492
51 X = -5994042
12
Y = -860451
39 feet Y = -262265
58 meter
Z = -10078879
61 Z = -3072042
50
XDOT = 8941
878392 XDOT = 2725
484534
YDOT = -15767
040662 feet/sec YDOT = -4805
793994 meter/sec
ZDOT = -16094
586012 ZDOT = -4905
629816
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 10254
52553890
00016717 00000-0 10270-3 0 9084
2 25544 51
6462 148
8542 0008668 357
0094 3
1015 15
71590288 37055
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52553890 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 148
8542 deg
Eccentricity:
0008668
Arg of perigee: 357
0094 deg
Mean anomaly: 3
1015 deg
Mean motion: 15
71590288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 313
Coasting Arc #10 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2010/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 261959
44 A = 6729310
87 meter
Y = -4820174
04 meter E =
0014307
Z = 4687802
36 I = 51
83722
XDOT = 6767
797613 Wp = 29
94008
YDOT = -2368
515349 meter/sec RA = 142
85462 deg
ZDOT = -2797
795368 TA = 87
67861
MA = 87
51480
Ha = 195
601 n
mi
Hp = 186
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 859446
97 X = 293067
37
Y = -15814219
28 feet Y = -4817070
52 meter
Z = 15379929
02 Z = 4689150
73
XDOT = 22204
060409 XDOT = 6807
371073
YDOT = -7770
719649 feet/sec YDOT = -2292
612626 meter/sec
ZDOT = -9179
118663 ZDOT = -2764
820941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3338777
68 X = -1017659
44
Y = 15476337
07 feet Y = 4717187
54 meter
Z = 15385251
10 Z = 4689424
54
XDOT = -22099
379697 XDOT = -6735
890932
YDOT = 4277
684900 feet/sec YDOT = 1303
838358 meter/sec
ZDOT = -9047
036322 ZDOT = -2757
536671
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 10255
54291781
00016717 00000-0 10270-3 0 9096
2 25544 51
6458 143
6481 0008818
7257 359
3917 15
71658650 37218
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54291781 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 143
6481 deg
Eccentricity:
0008818
Arg of perigee:
7257 deg
Mean anomaly: 359
3917 deg
Mean motion: 15
71658650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 328
Coasting Arc #11 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5618744
69 A = 6737690
36 meter
Y = 3267260
24 meter E =
0020055
Z = 1727385
71 I = 51
88845
XDOT = -1152
020585 Wp = 42
19852
YDOT = -5022
652023 meter/sec RA = 137
78936 deg
ZDOT = 5729
250648 TA = 336
85462
MA = 336
94482
Ha = 195
834 n
mi
Hp = 186
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18434201
74 X = -5663253
57
Y = 10719357
74 feet Y = 3204179
25 meter
Z = 5667275
95 Z = 1699981
50
XDOT = -3779
595096 XDOT = -1123
602568
YDOT = -16478
517135 feet/sec YDOT = -5035
375570 meter/sec
ZDOT = 18796
754096 ZDOT = 5723
723255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19836318
91 X = 6046110
01
Y = -7904236
50 feet Y = -2409211
29 meter
Z = 5557511
85 Z = 1693929
61
XDOT = 863
593801 XDOT = 263
223390
YDOT = 15423
260079 feet/sec YDOT = 4701
009672 meter/sec
ZDOT = 18774
528354 ZDOT = 5722
476242
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 10256
56028550
00016717 00000-0 10270-3 0 9103
2 25544 51
6458 138
4418 0008853 4
6678 355
4565 15
71631193 37375
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
56028550 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 138
4418 deg
Eccentricity:
0008853
Arg of perigee: 4
6678 deg
Mean anomaly: 355
4565 deg
Mean motion: 15
71631193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 322
Coasting Arc #12 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2010/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2153804
44 A = 6727124
12 meter
Y = 3692389
17 meter E =
0016775
Z = -5206521
52 I = 51
87506
XDOT = -5770
758476 Wp = 67
01305
YDOT = 4950
085406 meter/sec RA = 132
66362 deg
ZDOT = 1132
590320 TA = 213
72866
MA = 213
83551
Ha = 195
806 n
mi
Hp = 186
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7066287
54 X = 2137647
80
Y = 12114137
70 feet Y = 3716383
88 meter
Z = -17081763
52 Z = -5196097
62
XDOT = -18932
934634 XDOT = -5831
184279
YDOT = 16240
437683 feet/sec YDOT = 4885
215483 meter/sec
ZDOT = 3715
847507 ZDOT = 1104
409047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5542711
07 X = -1689418
33
Y = -12937939
73 feet Y = -3943484
03 meter
Z = -17039937
39 Z = -5193772
92
XDOT = 19950
194002 XDOT = 6080
819132
YDOT = -13251
937659 feet/sec YDOT = -4039
190598 meter/sec
ZDOT = 3602
976838 ZDOT = 1098
187340
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 10257
51405340
00016717 00000-0 10270-3 0 9116
2 25544 51
6458 133
5611 0008815 7
5497 352
5797 15
71677439 37520
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51405340 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 133
5611 deg
Eccentricity:
0008815
Arg of perigee: 7
5497 deg
Mean anomaly: 352
5797 deg
Mean motion: 15
71677439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 320
Coasting Arc #13 (Orbit 3767)
---------------------------------------
Vector Time (GMT): 2010/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4263806
64 A = 6738856
89 meter
Y = -5212452
84 meter E =
0009781
Z = -256117
41 I = 51
93403
XDOT = 3532
037955 Wp = 90
70106
YDOT = 3176
676584 meter/sec RA = 127
57651 deg
ZDOT = -6048
054943 TA = 92
06581
MA = 91
95379
Ha = 195
879 n
mi
Hp = 186
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13988866
91 X = 4323020
52
Y = -17101223
22 feet Y = -5164441
31 meter
Z = -840280
22 Z = -235259
95
XDOT = 11588
051032 XDOT = 3525
633594
YDOT = 10422
167271 feet/sec YDOT = 3216
138048 meter/sec
ZDOT = -19842
699945 ZDOT = -6030
911925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15822358
56 X = -4822654
89
Y = 15424869
63 feet Y = 4701500
26 meter
Z = -756749
84 Z = -230657
35
XDOT = -9338
776532 XDOT = -2846
459087
YDOT = -10514
194588 feet/sec YDOT = -3204
726510 meter/sec
ZDOT = -19773
949574 ZDOT = -6027
099830
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 10258
53139485
00016717 00000-0 10270-3 0 9124
2 25544 51
6459 128
3554 0008650 11
4718 348
6642 15
71644975 37687
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
53139485 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 128
3554 deg
Eccentricity:
0008650
Arg of perigee: 11
4718 deg
Mean anomaly: 348
6642 deg
Mean motion: 15
71644975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 335
Coasting Arc #14 (Orbit 3783)
---------------------------------------
Vector Time (GMT): 2010/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3822440
54 A = 6726766
33 meter
Y = -1684175
67 meter E =
0008815
Z = 5267972
31 I = 51
91134
XDOT = 3738
053904 Wp = 33
71769
YDOT = -6709
650822 meter/sec RA = 122
48069 deg
ZDOT = 573
969600 TA = 50
88837
MA = 50
81002
Ha = 196
050 n
mi
Hp = 185
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12540815
43 X = -3828914
44
Y = -5525510
72 feet Y = -1726956
57 meter
Z = 17283373
71 Z = 5249387
29
XDOT = 12263
956377 XDOT = 3810
016405
YDOT = -22013
290097 feet/sec YDOT = -6667
447284 meter/sec
ZDOT = 1883
102361 ZDOT = 592
303932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12061165
47 X = 3676243
24
Y = 6700884
41 feet Y = 2042429
57 meter
Z = 17208857
11 Z = 5245259
65
XDOT = -13799
452528 XDOT = -4206
073130
YDOT = 19870
382710 feet/sec YDOT = 6056
492650 meter/sec
ZDOT = 1956
513515 ZDOT = 596
345319
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 10259
54872080
00016717 00000-0 10270-3 0 9132
2 25544 51
6458 123
1488 0008837 15
0041 345
1381 15
71700532 37843
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
54872080 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 123
1488 deg
Eccentricity:
0008837
Arg of perigee: 15
0041 deg
Mean anomaly: 345
1381 deg
Mean motion: 15
71700532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3784
Checksum: 299
Coasting Arc #15 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2010/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2134642
04 A = 6737994
49 meter
Y = 6257180
48 meter E =
0017694
Z = -1253409
05 I = 51
96387
XDOT = -4929
165015 Wp = 27
73611
YDOT = -510
302259 meter/sec RA = 117
36634 deg
ZDOT = 5895
545223 TA = 318
58414
MA = 318
71814
Ha = 196
008 n
mi
Hp = 185
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7003418
78 X = -2198363
54
Y = 20528807
34 feet Y = 6232953
30 meter
Z = -4112234
41 Z = -1263934
07
XDOT = -16171
801229 XDOT = -4951
731675
YDOT = -1674
220009 feet/sec YDOT = -565
549107 meter/sec
ZDOT = 19342
339970 ZDOT = 5871
544706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8555816
25 X = 2607812
79
Y = -19923092
50 feet Y = -6072558
59 meter
Z = -4154355
64 Z = -1266247
60
XDOT = 14653
731237 XDOT = 4466
457281
YDOT = 2312
466105 feet/sec YDOT = 704
839669 meter/sec
ZDOT = 19246
121965 ZDOT = 5866
217975
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 10260
50245200
00016717 00000-0 10270-3 0 9149
2 25544 51
6451 118
2675 0008915 17
4602 342
6865 15
71713637 37990
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
50245200 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 118
2675 deg
Eccentricity:
0008915
Arg of perigee: 17
4602 deg
Mean anomaly: 342
6865 deg
Mean motion: 15
71713637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 303
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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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
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