Date:
September 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 3547)
---------------------------------------
Vector Time (GMT): 2010/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4691242
91 A = 6731181
09 meter
Y = -2053221
65 meter E =
0010460
Z = 4371441
15 I = 51
52220
XDOT = 5160
405227 Wp = 19
13402
YDOT = 4611
561581 meter/sec RA = 199
08765 deg
ZDOT = -3359
936513 TA = 104
83365
MA = 104
71776
Ha = 194
447 n
mi
Hp = 189
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15391216
89 X = 4692618
06
Y = -6736291
52 feet Y = -2000753
70 meter
Z = 14341998
54 Z = 4394234
55
XDOT = 16930
463342 XDOT = 5124
776335
YDOT = 15129
795212 feet/sec YDOT = 4669
069129 meter/sec
ZDOT = -11023
413758 ZDOT = -3334
953774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16691000
69 X = -5087417
01
Y = 1026342
86 feet Y = 312829
30 meter
Z = 14433198
50 Z = 4399238
90
XDOT = -10639
032001 XDOT = -3242
776954
YDOT = -18856
751582 feet/sec YDOT = -5747
537882 meter/sec
ZDOT = -10923
334830 ZDOT = -3329
432456
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 10244
54179406
00016717 00000-0 10270-3 0 9004
2 25544 51
6436 199
9290 0008554 321
0571 38
9974 15
71407948 35483
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54179406 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 199
9290 deg
Eccentricity:
0008554
Arg of perigee: 321
0571 deg
Mean anomaly: 38
9974 deg
Mean motion: 15
71407948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 331
Coasting Arc #2 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2010/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5502597
31 A = 6737416
27 meter
Y = -3179268
36 meter E =
0014189
Z = 2209140
53 I = 51
57243
XDOT = 4186
265025 Wp = 36
26459
YDOT = -3434
646606 meter/sec RA = 194
00898 deg
ZDOT = 5477
717599 TA = 348
51538
MA = 348
54772
Ha = 194
616 n
mi
Hp = 188
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18053140
78 X = -5477368
75
Y = -10430670
48 feet Y = -3240660
67 meter
Z = 7247836
38 Z = 2182470
23
XDOT = 13734
465306 XDOT = 4197
751057
YDOT = -11268
525611 feet/sec YDOT = -3387
769133 meter/sec
ZDOT = 17971
514434 ZDOT = 5498
082269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13645494
55 X = 4159146
74
Y = 15813042
43 feet Y = 4819815
33 meter
Z = 7141013
82 Z = 2176581
01
XDOT = -15427
471259 XDOT = -4702
293240
YDOT = 5150
276593 feet/sec YDOT = 1569
804306 meter/sec
ZDOT = 18052
978711 ZDOT = 5502
547911
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 10245
55929773
00016717 00000-0 10270-3 0 9017
2 25544 51
6437 194
7240 0008494 324
6183 35
4414 15
71441774 35647
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55929773 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 194
7240 deg
Eccentricity:
0008494
Arg of perigee: 324
6183 deg
Mean anomaly: 35
4414 deg
Mean motion: 15
71441774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 318
Coasting Arc #3 (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 = -2422962
53 A = 6728208
21 meter
Y = 3699428
57 meter E =
0009955
Z = -5077327
18 I = 51
57167
XDOT = -7113
978191 Wp = 63
74115
YDOT = -2422
498114 meter/sec RA = 188
85552 deg
ZDOT = 1636
600031 TA = 221
98161
MA = 222
05796
Ha = 194
714 n
mi
Hp = 188
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7949352
15 X = -2439485
58
Y = 12137232
85 feet Y = 3672241
23 meter
Z = -16657897
59 Z = -5089137
94
XDOT = -23339
823460 XDOT = -7094
310894
YDOT = -7947
828458 feet/sec YDOT = -2501
940936 meter/sec
ZDOT = 5369
422675 ZDOT = 1602
088312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11258461
27 X = 3431579
00
Y = -9065109
76 feet Y = -2763045
45 meter
Z = -16705119
20 Z = -5091720
33
XDOT = 19042
220781 XDOT = 5804
068894
YDOT = 14050
540956 feet/sec YDOT = 4282
604883 meter/sec
ZDOT = 5231
203088 ZDOT = 1594
470701
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
51319227
00016717 00000-0 10270-3 0 9022
2 25544 51
6440 189
8442 0008614 328
4187 31
6457 15
71451283 35797
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51319227 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 189
8442 deg
Eccentricity:
0008614
Arg of perigee: 328
4187 deg
Mean anomaly: 31
6457 deg
Mean motion: 15
71451283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 313
Coasting Arc #4 (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 = 6641762
54 A = 6739193
70 meter
Y = 943912
19 meter E =
0003135
Z = -640248
07 I = 51
63975
XDOT = -1237
900025 Wp = 102
65472
YDOT = 4666
956818 meter/sec RA = 183
75658 deg
ZDOT = -5986
438461 TA = 84
30449
MA = 84
26875
Ha = 194
852 n
mi
Hp = 188
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21790559
50 X = 6633824
08
Y = 3096824
78 feet Y = 1018139
98 meter
Z = -2100551
42 Z = -608002
03
XDOT = -4061
351789 XDOT = -1260
914080
YDOT = 15311
538118 feet/sec YDOT = 4652
985204 meter/sec
ZDOT = -19640
546131 ZDOT = -5992
508009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19899058
64 X = -6065233
07
Y = -9432503
64 feet Y = -2875027
11 meter
Z = -1971411
59 Z = -600886
25
XDOT = 7626
403752 XDOT = 2324
527864
YDOT = -11997
335506 feet/sec YDOT = -3656
787862 meter/sec
ZDOT = -19664
764448 ZDOT = -5993
820204
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
53066240
00016717 00000-0 10270-3 0 9030
2 25544 51
6448 184
6392 0008609 332
2908 27
7794 15
71480472 35950
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53066240 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 184
6392 deg
Eccentricity:
0008609
Arg of perigee: 332
2908 deg
Mean anomaly: 27
7794 deg
Mean motion: 15
71480472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 324
Coasting Arc #5 (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 = -309624
70 A = 6727130
74 meter
Y = -4167906
15 meter E =
0007494
Z = 5272135
61 I = 51
63038
XDOT = 7687
097803 Wp = 351
02266
YDOT = -335
963833 meter/sec RA = 178
63633 deg
ZDOT = 193
158268 TA = 97
18566
MA = 97
10045
Ha = 194
877 n
mi
Hp = 188
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1015829
07 X = -288606
12
Y = -13674232
79 feet Y = -4171250
92 meter
Z = 17297032
83 Z = 5270682
62
XDOT = 25220
137149 XDOT = 7689
344975
YDOT = -1102
243548 feet/sec YDOT = -249
989528 meter/sec
ZDOT = 633
721351 ZDOT = 230
507123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2762489
25 X = -842006
72
Y = 13438349
59 feet Y = 4096008
95 meter
Z = 17291133
83 Z = 5270337
59
XDOT = -23532
628429 XDOT = -7172
745145
YDOT = -5814
560805 feet/sec YDOT = -1772
278133 meter/sec
ZDOT = 783
288896 ZDOT = 238
746455
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
54811338
00016717 00000-0 10270-3 0 9049
2 25544 51
6451 179
4344 0008674 335
3906 24
6841 15
71540786 36110
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54811338 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 179
4344 deg
Eccentricity:
0008674
Arg of perigee: 335
3906 deg
Mean anomaly: 24
6841 deg
Mean motion: 15
71540786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 313
Coasting Arc #6 (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 = -6483041
50 A = 6738789
10 meter
Y = 1513796
94 meter E =
0016142
Z = -976666
40 I = 51
69994
XDOT = -1941
305763 Wp = 11
20145
YDOT = -4501
410598 meter/sec RA = 173
51006 deg
ZDOT = 5941
073804 TA = 338
13994
MA = 338
20873
Ha = 195
046 n
mi
Hp = 187
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21269821
20 X = -6494742
83
Y = 4966525
40 feet Y = 1441234
21 meter
Z = -3204286
08 Z = -1008189
05
XDOT = -6369
113395 XDOT = -1919
686117
YDOT = -14768
407475 feet/sec YDOT = -4522
998249 meter/sec
ZDOT = 19491
711957 ZDOT = 5931
695832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21807687
12 X = 6646983
03
Y = 819513
81 feet Y = 249787
81 meter
Z = -3330510
09 Z = -1015139
47
XDOT = 2415
864084 XDOT = 736
355373
YDOT = 14365
528191 feet/sec YDOT = 4378
612993 meter/sec
ZDOT = 19454
060795 ZDOT = 5929
597730
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
50195950
00016717 00000-0 10270-3 0 9052
2 25544 51
6453 174
5541 0008720 339
5979 20
4833 15
71523216 36265
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50195950 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 174
5541 deg
Eccentricity:
0008720
Arg of perigee: 339
5979 deg
Mean anomaly: 20
4833 deg
Mean motion: 15
71523216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 311
Coasting Arc #7 (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 = 2968388
07 A = 6728370
66 meter
Y = 3416057
60 meter E =
0015379
Z = -4991113
83 I = 51
69639
XDOT = -6795
910257 Wp = 41
07653
YDOT = 2992
881517 meter/sec RA = 168
42342 deg
ZDOT = -1985
443952 TA = 209
66236
MA = 209
74966
Ha = 195
161 n
mi
Hp = 187
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9738806
02 X = 2954214
11
Y = 11207538
06 feet Y = 3449172
24 meter
Z = -16375045
39 Z = -4976728
29
XDOT = -22296
293494 XDOT = -6819
227311
YDOT = 9819
165081 feet/sec YDOT = 2916
755038 meter/sec
ZDOT = -6513
923726 ZDOT = -2018
514951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6758001
81 X = -2059838
95
Y = -13291680
51 feet Y = -4051304
22 meter
Z = -16317352
85 Z = -4973529
15
XDOT = 23025
143998 XDOT = 7018
063891
YDOT = -3515
632866 feet/sec YDOT = -1071
564898 meter/sec
ZDOT = -6646
328161 ZDOT = -2025
800823
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
51937678
00016717 00000-0 10270-3 0 9067
2 25544 51
6464 169
3487 0008667 343
8774 16
2111 15
71581818 36421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51937678 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 169
3487 deg
Eccentricity:
0008667
Arg of perigee: 343
8774 deg
Mean anomaly: 16
2111 deg
Mean motion: 15
71581818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 332
Coasting Arc #8 (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 = 5162537
71 A = 6736387
04 meter
Y = -3566694
35 meter E =
0012467
Z = 2448702
58 I = 51
75309
XDOT = 4632
671510 Wp = 67
25306
YDOT = 3013
015823 meter/sec RA = 163
27540 deg
ZDOT = -5352
006182 TA = 85
17222
MA = 85
02989
Ha = 195
226 n
mi
Hp = 187
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16937459
68 X = 5190142
18
Y = -11701753
13 feet Y = -3508809
18 meter
Z = 8033801
12 Z = 2473849
41
XDOT = 15199
053511 XDOT = 4624
633999
YDOT = 9885
222515 feet/sec YDOT = 3064
775674 meter/sec
ZDOT = -17559
075401 ZDOT = -5329
520644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19133074
90 X = -5831761
23
Y = 7490430
86 feet Y = 2283083
33 meter
Z = 8134458
66 Z = 2479383
00
XDOT = -12064
186408 XDOT = -3677
164017
YDOT = -11752
569164 feet/sec YDOT = -3582
183081 meter/sec
ZDOT = -17468
940266 ZDOT = -5324
532993
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
53677601
00016717 00000-0 10270-3 0 9078
2 25544 51
6464 164
1434 0008649 347
2449 12
8493 15
71588382 36588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53677601 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 164
1434 deg
Eccentricity:
0008649
Arg of perigee: 347
2449 deg
Mean anomaly: 12
8493 deg
Mean motion: 15
71588382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 330
Coasting Arc #9 (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 = -4926571
02 A = 6731155
33 meter
Y = -1652436
75 meter E =
0009956
Z = 4268100
41 I = 51
76433
XDOT = 4737
653628 Wp = 55
78967
YDOT = -4918
030257 meter/sec RA = 158
21252 deg
ZDOT = 3564
105701 TA = 358
11773
MA = 358
12147
Ha = 195
445 n
mi
Hp = 187
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16163290
75 X = -4928460
66
Y = -5421380
40 feet Y = -1707538
77 meter
Z = 14002954
11 Z = 4244162
73
XDOT = 15543
483032 XDOT = 4774
982064
YDOT = -16135
269871 feet/sec YDOT = -4864
841906 meter/sec
ZDOT = 11693
260174 ZDOT = 3587
212353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14710693
94 X = 4483819
51
Y = 8770185
94 feet Y = 2673152
67 meter
Z = 13907026
27 Z = 4238861
61
XDOT = -17927
179365 XDOT = -5464
204271
YDOT = 11379
310403 feet/sec YDOT = 3468
413811 meter/sec
ZDOT = 11785
723542 ZDOT = 3592
288536
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
55415655
00016717 00000-0 10270-3 0 9081
2 25544 51
6465 158
9377 0008686 351
1623 8
9385 15
71618074 36741
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55415655 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 158
9377 deg
Eccentricity:
0008686
Arg of perigee: 351
1623 deg
Mean anomaly: 8
9385 deg
Mean motion: 15
71618074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 336
Coasting Arc #10 (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 = -2953412
78 A = 6732817
28 meter
Y = 4777199
74 meter E =
0008883
Z = -3710853
24 I = 51
79856
XDOT = -6346
394798 Wp = 33
96168
YDOT = -582
156488 meter/sec RA = 153
05504 deg
ZDOT = 4313
706946 TA = 281
49194
MA = 281
59167
Ha = 195
364 n
mi
Hp = 186
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9689674
48 X = -2988586
07
Y = 15673227
51 feet Y = 4743975
93 meter
Z = -12174715
36 Z = -3725286
82
XDOT = -20821
505244 XDOT = -6360
368639
YDOT = -1909
962232 feet/sec YDOT = -653
203450 meter/sec
ZDOT = 14152
581844 ZDOT = 4282
842135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12516985
49 X = 3815177
18
Y = -13470556
86 feet Y = -4105825
73 meter
Z = -12232445
31 Z = -3728449
33
XDOT = 19136
668978 XDOT = 5832
856704
YDOT = 5078
537892 feet/sec YDOT = 1547
938349 meter/sec
ZDOT = 14028
919846 ZDOT = 4276
014769
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
50793349
00016717 00000-0 10270-3 0 9097
2 25544 51
6468 154
0575 0008743 354
2940 5
8121 15
71657253 36893
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50793349 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 154
0575 deg
Eccentricity:
0008743
Arg of perigee: 354
2940 deg
Mean anomaly: 5
8121 deg
Mean motion: 15
71657253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 324
Coasting Arc #11 (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 = 5882674
42 A = 6734429
03 meter
Y = -694814
77 meter E =
0008883
Z = -3216104
61 I = 51
83030
XDOT = -1956
655203 Wp = 27
51500
YDOT = 5673
971658 meter/sec RA = 148
00037 deg
ZDOT = -4802
344808 TA = 189
85151
MA = 189
86894
Ha = 195
459 n
mi
Hp = 186
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19300112
92 X = 5905630
12
Y = -2279576
02 feet Y = -628903
03 meter
Z = -10551524
32 Z = -3187470
57
XDOT = -6419
472452 XDOT = -1996
628081
YDOT = 18615
392580 feet/sec YDOT = 5651
867362 meter/sec
ZDOT = -15755
724437 ZDOT = -4811
947760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19456285
33 X = -5930275
77
Y = -1245523
91 feet Y = -379635
69 meter
Z = -10436815
71 Z = -3181141
43
XDOT = 9485
075233 XDOT = 2891
050931
YDOT = -15751
957026 feet/sec YDOT = -4801
196502 meter/sec
ZDOT = -15794
094624 ZDOT = -4814
040041
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
52527763
00016717 00000-0 10270-3 0 9107
2 25544 51
6467 148
8516 0008733 357
2098 2
9014 15
71671831 37050
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52527763 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 148
8516 deg
Eccentricity:
0008733
Arg of perigee: 357
2098 deg
Mean anomaly: 2
9014 deg
Mean motion: 15
71671831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 311
Coasting Arc #12 (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 = 444847
51 A = 6729376
47 meter
Y = -4881804
96 meter E =
0014585
Z = 4609662
36 I = 51
83878
XDOT = 6755
302349 Wp = 31
74637
YDOT = -2197
418433 meter/sec RA = 142
84937 deg
ZDOT = -2962
685698 TA = 87
64853
MA = 87
48155
Ha = 195
490 n
mi
Hp = 186
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1459473
45 X = 477010
61
Y = -16016420
47 feet Y = -4876650
38 meter
Z = 15123564
16 Z = 4611901
77
XDOT = 22163
065451 XDOT = 6793
764514
YDOT = -7209
378061 feet/sec YDOT = -2121
661659 meter/sec
ZDOT = -9720
097434 ZDOT = -2929
774680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3965250
01 X = -1208608
20
Y = 15577662
37 feet Y = 4748071
49 meter
Z = 15132455
44 Z = 4612372
42
XDOT = -21963
101480 XDOT = -6694
353331
YDOT = 3775
736151 feet/sec YDOT = 1150
844379 meter/sec
ZDOT = -9588
266290 ZDOT = -2922
503565
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
54260224
00016717 00000-0 10270-3 0 9117
2 25544 51
6462 143
6453 0008871
9349 359
1828 15
71744652 37212
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54260224 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 143
6453 deg
Eccentricity:
0008871
Arg of perigee:
9349 deg
Mean anomaly: 359
1828 deg
Mean motion: 15
71744652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 303
Coasting Arc #13 (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 = -5651508
01 A = 6737137
81 meter
Y = 3103895
75 meter E =
0019886
Z = 1910168
31 I = 51
88800
XDOT = -914
770085 Wp = 43
75216
YDOT = -5156
961340 meter/sec RA = 137
78579 deg
ZDOT = 5652
553090 TA = 337
41047
MA = 337
49788
Ha = 195
717 n
mi
Hp = 186
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18541692
95 X = -5695075
61
Y = 10183385
01 feet Y = 3040453
65 meter
Z = 6266956
40 Z = 1882607
23
XDOT = -3001
214190 XDOT = -884
495244
YDOT = -16919
164501 feet/sec YDOT = -5167
021430 meter/sec
ZDOT = 18545
121686 ZDOT = 5648
182780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19867810
42 X = 6055708
62
Y = -7357806
31 feet Y = -2242659
36 meter
Z = 6156561
19 Z = 1876519
85
XDOT = 67
533589 XDOT = 20
584238
YDOT = 15742
861436 feet/sec YDOT = 4798
424166 meter/sec
ZDOT = 18527
530552 ZDOT = 5647
191312
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
55991009
00016717 00000-0 10270-3 0 9122
2 25544 51
6463 138
4386 0008902 4
8215 355
3031 15
71725360 37376
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
55991009 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 138
4386 deg
Eccentricity:
0008902
Arg of perigee: 4
8215 deg
Mean anomaly: 355
3031 deg
Mean motion: 15
71725360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 302
Coasting Arc #14 (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 = 1934825
35 A = 6727032
61 meter
Y = 3874909
79 meter E =
0016275
Z = -5158913
17 I = 51
87628
XDOT = -5870
640196 Wp = 67
68708
YDOT = 4765
350511 meter/sec RA = 132
65588 deg
ZDOT = 1387
049210 TA = 215
51788
MA = 215
62634
Ha = 195
660 n
mi
Hp = 186
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6347852
20 X = 1916412
73
Y = 12712958
63 feet Y = 3896443
13 meter
Z = -16925568
16 Z = -5149558
56
XDOT = -19260
630563 XDOT = -5930
228953
YDOT = 15634
352070 feet/sec YDOT = 4699
368335 meter/sec
ZDOT = 4550
686385 ZDOT = 1358
384746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4752037
87 X = -1448421
14
Y = -13438830
22 feet Y = -4096155
45 meter
Z = -16888024
76 Z = -5147469
95
XDOT = 20165
238455 XDOT = 6146
364681
YDOT = -12665
645148 feet/sec YDOT = -3860
488641 meter/sec
ZDOT = 4435
876702 ZDOT = 1352
055219
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
51361686
00016717 00000-0 10270-3 0 9132
2 25544 51
6462 133
5575 0008852 7
5857 352
5438 15
71780871 37522
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51361686 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 133
5575 deg
Eccentricity:
0008852
Arg of perigee: 7
5857 deg
Mean anomaly: 352
5438 deg
Mean motion: 15
71780871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 328
Coasting Arc #15 (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 = 4411952
33 A = 6738450
63 meter
Y = -5067579
26 meter E =
0009063
Z = -519444
54 I = 51
93425
XDOT = 3285
498674 Wp = 89
43691
YDOT = 3468
912285 meter/sec RA = 127
57258 deg
ZDOT = -6026
098000 TA = 96
18150
MA = 96
07825
Ha = 195
712 n
mi
Hp = 185
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14474909
21 X = 4470814
39
Y = -16625916
21 feet Y = -5017913
06 meter
Z = -1704214
37 Z = -497868
24
XDOT = 10779
195125 XDOT = 3275
738140
YDOT = 11380
945818 feet/sec YDOT = 3505
598034 meter/sec
ZDOT = -19770
662731 ZDOT = -6010
160826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16257145
12 X = -4955177
83
Y = 14897529
52 feet Y = 4540767
00 meter
Z = -1617801
01 Z = -493105
75
XDOT = -8465
588610 XDOT = -2580
311408
YDOT = -11344
513343 feet/sec YDOT = -3457
807667 meter/sec
ZDOT = -19706
741662 ZDOT = -6006
614859
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
53088775
00016717 00000-0 10270-3 0 9141
2 25544 51
6464 128
3513 0008682 11
3571 348
7785 15
71758300 37686
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
53088775 = yrday
fracday
Element set: 914
Inclination: 51
6464 deg
RA of node: 128
3513 deg
Eccentricity:
0008682
Arg of perigee: 11
3571 deg
Mean anomaly: 348
7785 deg
Mean motion: 15
71758300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 331
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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