Date:
November 24th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
329/05:06:49
510 -2
5 3
3 3
3
N/A 0
6 0
1 190
2
000/00:07:39
021 2
0 0
1 189
6
Coasting Arc #1 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2010/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494349
14 A = 6724916
38 meter
Y = -1183405
07 meter E =
0007727
Z = 4863461
54 I = 51
84463
XDOT = 4164
702813 Wp = 180
83446
YDOT = -6020
289654 meter/sec RA = 139
44976 deg
ZDOT = 2376
214047 TA = 246
00665
MA = 246
08756
Ha = 191
119 n
mi
Hp = 187
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14745239
97 X = -4504408
45
Y = -3882562
58 feet Y = -1233720
35 meter
Z = 15956238
64 Z = 4841602
89
XDOT = 13663
723140 XDOT = 4220
169776
YDOT = -19751
606477 feet/sec YDOT = -5973
407562 meter/sec
ZDOT = 7795
977846 ZDOT = 2396
580773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10669723
69 X = 3252131
78
Y = -11020346
56 feet Y = -3359001
63 meter
Z = 15868424
73 Z = 4836695
86
XDOT = 9713
874468 XDOT = 2960
788938
YDOT = 20784
010656 feet/sec YDOT = 6334
966448 meter/sec
ZDOT = 7877
851805 ZDOT = 2401
169230
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 10326
55179053
00016717 00000-0 10270-3 0 9004
2 25544 51
6391 140
1510 0007307 235
6466 124
4006 15
72982782 8385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55179053 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 140
1510 deg
Eccentricity:
0007307
Arg of perigee: 235
6466 deg
Mean anomaly: 124
4006 deg
Mean motion: 15
72982782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 293
Coasting Arc #2 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2010/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2886283
49 A = 6732476
46 meter
Y = 5605918
82 meter E =
0002134
Z = -2358031
76 I = 51
89384
XDOT = -5436
581603 Wp = 271
17136
YDOT = -516
846596 meter/sec RA = 134
29786 deg
ZDOT = 5421
606246 TA = 62
39511
MA = 62
37344
Ha = 190
866 n
mi
Hp = 187
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9469434
03 X = -2937300
28
Y = 18392122
11 feet Y = 5573357
68 meter
Z = -7736324
68 Z = -2372176
89
XDOT = -17836
553816 XDOT = -5456
735778
YDOT = -1695
690931 feet/sec YDOT = -577
755034 meter/sec
ZDOT = 17787
422066 ZDOT = 5395
145780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11687845
80 X = -3562455
40
Y = -17042626
74 feet Y = -5194592
63 meter
Z = -7793214
38 Z = -2375371
74
XDOT = 8789
424395 XDOT = 2679
016556
YDOT = -14119
154950 feet/sec YDOT = -4303
518429 meter/sec
ZDOT = 17681
100670 ZDOT = 5389
199484
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 10327
50472725
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 135
2637 0007301 237
9655 122
0799 15
73033075 8538
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
50472725 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 135
2637 deg
Eccentricity:
0007301
Arg of perigee: 237
9655 deg
Mean anomaly: 122
0799 deg
Mean motion: 15
73033075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 305
Coasting Arc #3 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2010/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4899061
76 A = 6725704
37 meter
Y = -293511
34 meter E =
0003412
Z = -4601720
35 I = 51
89250
XDOT = -2411
566665 Wp = 86
62549
YDOT = 6666
887035 meter/sec RA = 129
23121 deg
ZDOT = -2994
323014 TA = 153
74856
MA = 153
73127
Ha = 190
673 n
mi
Hp = 187
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16073037
28 X = 4924334
41
Y = -962963
72 feet Y = -238585
25 meter
Z = -15097507
71 Z = -4577858
99
XDOT = -7911
964124 XDOT = -2471
391702
YDOT = 21872
988961 feet/sec YDOT = 6639
585292 meter/sec
ZDOT = -9823
894403 ZDOT = -3006
183135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6593694
30 X = -2009758
02
Y = 14787814
57 feet Y = 4507325
88 meter
Z = -15001609
96 Z = -4572490
72
XDOT = -14713
515042 XDOT = -4484
679385
YDOT = -16569
221199 feet/sec YDOT = -5050
298621 meter/sec
ZDOT = -9871
625981 ZDOT = -3008
871599
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 10328
52117269
00016717 00000-0 10270-3 0 9026
2 25544 51
6404 130
0519 0007123 242
1841 117
8600 15
73083659 8699
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52117269 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 130
0519 deg
Eccentricity:
0007123
Arg of perigee: 242
1841 deg
Mean anomaly: 117
8600 deg
Mean motion: 15
73083659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 289
Coasting Arc #4 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2010/329/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2223537
25 A = 6734512
11 meter
Y = 5984817
62 meter E =
0005753
Z = -2131340
10 I = 51
93332
XDOT = -5335
919705 Wp = 315
83404
YDOT = -4
959399 meter/sec RA = 125
53717 deg
ZDOT = 5547
930655 TA = 20
45007
MA = 20
42704
Ha = 190
200 n
mi
Hp = 189
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7295069
72 X = -2279941
55
Y = 19635228
42 feet Y = 5959637
55 meter
Z = -6992585
61 Z = -2142278
53
XDOT = -17506
298245 XDOT = -5362
418833
YDOT = -16
270995 feet/sec YDOT = -64
777629 meter/sec
ZDOT = 18201
872229 ZDOT = 5521
944076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18007602
84 X = 5488717
35
Y = -10670932
09 feet Y = -3252500
10 meter
Z = -7036614
16 Z = -2144760
00
XDOT = 12886
340255 XDOT = 3927
756510
YDOT = 9801
904213 feet/sec YDOT = 2987
620404 meter/sec
ZDOT = 18097
427074 ZDOT = 5516
095772
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 10329
21996601
00016717 00000-0 10270-3 0 9039
2 25544 51
6439 126
4725 0008237 265
8305 94
1916 15
72478090 8805
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
21996601 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 126
4725 deg
Eccentricity:
0008237
Arg of perigee: 265
8305 deg
Mean anomaly: 94
1916 deg
Mean motion: 15
72478090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 318
Coasting Arc #5 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2010/330/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4782923
64 A = 6727196
82 meter
Y = -972102
97 meter E =
0004027
Z = -4632811
14 I = 51
92636
XDOT = -1430
905615 Wp = 23
98476
YDOT = 6967
312018 meter/sec RA = 120
47506 deg
ZDOT = -2936
511405 TA = 217
00480
MA = 217
03258
Ha = 189
390 n
mi
Hp = 189
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15692006
70 X = 4815943
95
Y = -3189314
21 feet Y = -918432
39 meter
Z = -15199511
62 Z = -4609495
38
XDOT = -4694
572229 XDOT = -1494
443885
YDOT = 22858
635231 feet/sec YDOT = 6950
955780 meter/sec
ZDOT = -9634
223770 ZDOT = -2943
616498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14389119
52 X = -4385803
63
Y = -7225277
11 feet Y = -2202264
46 meter
Z = -15105779
13 Z = -4604241
48
XDOT = 17223
892509 XDOT = 5249
842437
YDOT = -14080
625279 feet/sec YDOT = -4291
774585 meter/sec
ZDOT = -9662
864402 ZDOT = -2945
241070
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 10330
23677950
00016717 00000-0 10270-3 0 9047
2 25544 51
6445 121
2632 0008267 270
8205 89
2010 15
72518309 8965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
23677950 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 121
2632 deg
Eccentricity:
0008267
Arg of perigee: 270
8205 deg
Mean anomaly: 89
2010 deg
Mean motion: 15
72518309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 296
Coasting Arc #6 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2010/331/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 278198
40 A = 6732543
57 meter
Y = -6030227
78 meter E =
0005102
Z = 2975452
58 I = 51
95872
XDOT = 5396
622986 Wp = 100
98088
YDOT = -2228
933820 meter/sec RA = 115
32656 deg
ZDOT = -5015
597420 TA = 44
86904
MA = 44
82781
Ha = 190
112 n
mi
Hp = 189
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 912724
40 X = 331154
54
Y = -19784211
89 feet Y = -6026820
92 meter
Z = 9761983
53 Z = 2976932
28
XDOT = 17705
455991 XDOT = 5445
511287
YDOT = -7312
775000 feet/sec YDOT = -2168
311831 meter/sec
ZDOT = -16455
372112 ZDOT = -4989
261843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12616460
38 X = -3845497
12
Y = 15262877
17 feet Y = 4652124
96 meter
Z = 9768005
74 Z = 2977288
15
XDOT = -17497
592462 XDOT = -5333
266182
YDOT = -3987
144405 feet/sec YDOT = -1215
281615 meter/sec
ZDOT = -16349
475100 ZDOT = -4983
320010
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 10331
25357333
00016717 00000-0 10270-3 0 9051
2 25544 51
6443 116
0534 0008198 274
7189 85
3037 15
72520407 9120
Satellite: ISS
Catalog Number: 25544
Epoch time: 10331
25357333 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 116
0534 deg
Eccentricity:
0008198
Arg of perigee: 274
7189 deg
Mean anomaly: 85
3037 deg
Mean motion: 15
72520407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 295
Coasting Arc #7 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2010/332/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4487253
38 A = 6729084
72 meter
Y = 2878084
52 meter E =
0002430
Z = 4105239
48 I = 51
95962
XDOT = -746
143422 Wp = 117
28169
YDOT = -6633
562399 meter/sec RA = 110
27319 deg
ZDOT = 3832
244045 TA = 293
49586
MA = 293
52139
Ha = 190
732 n
mi
Hp = 189
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14721959
90 X = -4539045
82
Y = 9442534
53 feet Y = 2827615
57 meter
Z = 13468633
46 Z = 4083314
56
XDOT = -2447
977107 XDOT = -690
526736
YDOT = -21763
656166 feet/sec YDOT = -6641
595445 meter/sec
ZDOT = 12572
979151 ZDOT = 3828
754015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17523184
54 X = 5341066
65
Y = 1096894
03 feet Y = 334333
30 meter
Z = 13380451
26 Z = 4078361
54
XDOT = -10710
552964 XDOT = -3264
576543
YDOT = 17789
544535 feet/sec YDOT = 5422
253174 meter/sec
ZDOT = 12559
034169 ZDOT = 3827
993615
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 10332
27034466
00016717 00000-0 10270-3 0 9064
2 25544 51
6447 110
8428 0008272 279
7080 80
3148 15
72550550 9283
Satellite: ISS
Catalog Number: 25544
Epoch time: 10332
27034466 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 110
8428 deg
Eccentricity:
0008272
Arg of perigee: 279
7080 deg
Mean anomaly: 80
3148 deg
Mean motion: 15
72550550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 301
Coasting Arc #8 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2010/333/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1528709
62 A = 6730278
43 meter
Y = 5413130
41 meter E =
0002744
Z = -3692652
58 I = 51
97339
XDOT = -4682
659542 Wp = 288
25891
YDOT = 4290
626301 meter/sec RA = 105
12026 deg
ZDOT = 4349
370771 TA = 27
57943
MA = 27
56488
Ha = 190
944 n
mi
Hp = 189
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5015451
52 X = 1486003
81
Y = 17759614
21 feet Y = 5429986
71 meter
Z = -12115001
92 Z = -3685329
57
XDOT = -15363
056239 XDOT = -4751
418792
YDOT = 14076
857944 feet/sec YDOT = 4237
877375 meter/sec
ZDOT = 14269
589144 ZDOT = 4326
455288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6059283
07 X = 1846869
48
Y = -17451487
82 feet Y = -5319213
49 meter
Z = -12085635
43 Z = -3683701
68
XDOT = 19462
011358 XDOT = 5932
021062
YDOT = -3064
943399 feet/sec YDOT = -934
194748 meter/sec
ZDOT = 14177
397340 ZDOT = 4321
270709
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 10333
22354763
00016717 00000-0 10270-3 0 9076
2 25544 51
6444 105
9581 0008496 283
6049 76
4167 15
72596776 9436
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
22354763 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 105
9581 deg
Eccentricity:
0008496
Arg of perigee: 283
6049 deg
Mean anomaly: 76
4167 deg
Mean motion: 15
72596776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 336
Coasting Arc #9 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2010/334/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3566270
94 A = 6730944
21 meter
Y = -4525845
18 meter E =
0004234
Z = -3479140
78 I = 51
98213
XDOT = 2637
217510 Wp = 311
58507
YDOT = 5598
755470 meter/sec RA = 100
07036 deg
ZDOT = -4573
582801 TA = 269
41780
MA = 269
46631
Ha = 191
067 n
mi
Hp = 189
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11700363
98 X = 3633516
03
Y = -14848573
44 feet Y = -4485588
89 meter
Z = -11414503
86 Z = -3461652
37
XDOT = 8652
288419 XDOT = 2596
633162
YDOT = 18368
620310 feet/sec YDOT = 5628
019660 meter/sec
ZDOT = -15005
192917 ZDOT = -4560
869389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18074280
49 X = -5509040
69
Y = 5683386
64 feet Y = 1732296
25 meter
Z = -11344119
61 Z = -3457687
66
XDOT = 3490
399445 XDOT = 1063
873751
YDOT = -18790
100514 feet/sec YDOT = -5727
222637 meter/sec
ZDOT = -14954
162961 ZDOT = -4558
028871
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 10334
24027780
00016717 00000-0 10270-3 0 9086
2 25544 51
6440 100
7477 0008588 287
1789 72
8433 15
72610989 9597
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
24027780 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 100
7477 deg
Eccentricity:
0008588
Arg of perigee: 287
1789 deg
Mean anomaly: 72
8433 deg
Mean motion: 15
72610989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 337
Coasting Arc #10 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2010/335/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2983159
03 A = 6728019
72 meter
Y = -4262471
82 meter E =
0006409
Z = 4268552
49 I = 51
97773
XDOT = 3329
885633 Wp = 13
85164
YDOT = -5934
974305 meter/sec RA = 94
91848 deg
ZDOT = -3592
181996 TA = 112
52184
MA = 112
45399
Ha = 191
191 n
mi
Hp = 188
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9787267
17 X = -2956009
83
Y = -13984487
61 feet Y = -4295679
70 meter
Z = 14004437
30 Z = 4254125
76
XDOT = 10924
821630 XDOT = 3413
454653
YDOT = -19471
700475 feet/sec YDOT = -5897
270095 meter/sec
ZDOT = -11785
374003 ZDOT = -3575
802368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 613612
38 X = 187029
05
Y = 17105532
81 feet Y = 5213766
40 meter
Z = 13946504
35 Z = 4250894
53
XDOT = -18607
980408 XDOT = -5671
712428
YDOT = 10241
891318 feet/sec YDOT = 3121
728474 meter/sec
ZDOT = -11719
413126 ZDOT = -3572
077121
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 10335
25698534
00016717 00000-0 10270-3 0 9090
2 25544 51
6444 95
5367 0008638 292
4594 67
5653 15
72706649 9751
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
25698534 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 95
5367 deg
Eccentricity:
0008638
Arg of perigee: 292
4594 deg
Mean anomaly: 67
5653 deg
Mean motion: 15
72706649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 355
Coasting Arc #11 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2010/336/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2165910
83 A = 6732546
82 meter
Y = 5725661
03 meter E =
0008345
Z = 2788977
51 I = 51
99354
XDOT = -4041
537100 Wp = 41
92880
YDOT = -4043
338872 meter/sec RA = 89
86401 deg
ZDOT = 5159
433464 TA = 349
81844
MA = 349
83534
Ha = 191
467 n
mi
Hp = 188
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7106006
65 X = -2243323
91
Y = 18784977
15 feet Y = 5701007
49 meter
Z = 9150188
66 Z = 2778267
62
XDOT = -13259
636154 XDOT = -4021
087515
YDOT = -13265
547479 feet/sec YDOT = -4088
419783 meter/sec
ZDOT = 16927
275145 ZDOT = 5139
848626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16064184
61 X = 4896363
47
Y = -12087221
22 feet Y = -3684185
03 meter
Z = 9107014
08 Z = 2775817
89
XDOT = 3363
001002 XDOT = 1025
042705
YDOT = 17170
740108 feet/sec YDOT = 5233
641585 meter/sec
ZDOT = 16848
604998 ZDOT = 5135
454803
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 10336
27367386
00016717 00000-0 10270-3 0 9103
2 25544 51
6436 90
3250 0008652 296
3847 63
6427 15
72695397 9917
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
27367386 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 90
3250 deg
Eccentricity:
0008652
Arg of perigee: 296
3847 deg
Mean anomaly: 63
6427 deg
Mean motion: 15
72695397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 334
Coasting Arc #12 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2010/337/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953005
67 A = 6726226
90 meter
Y = 2726740
12 meter E =
0003043
Z = -4711884
83 I = 51
97091
XDOT = -1531
655526 Wp = 77
25053
YDOT = 7013
068026 meter/sec RA = 84
71762 deg
ZDOT = 2775
598063 TA = 219
98614
MA = 220
00856
Ha = 191
619 n
mi
Hp = 188
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12969178
70 X = 3945110
97
Y = 8945997
76 feet Y = 2770901
31 meter
Z = -15458939
73 Z = -4692699
60
XDOT = -5025
116556 XDOT = -1623
446791
YDOT = 23008
753366 feet/sec YDOT = 6995
426638 meter/sec
ZDOT = 9106
292858 ZDOT = 2767
934802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6540347
43 X = -1993497
90
Y = -14416369
77 feet Y = -4394109
51 meter
Z = -15381853
84 Z = -4688389
05
XDOT = 15209
758343 XDOT = 4635
934343
YDOT = -16575
838661 feet/sec YDOT = -5052
315624 meter/sec
ZDOT = 9075
325235 ZDOT = 2766
159132
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 10337
22679889
00016717 00000-0 10270-3 0 9114
2 25544 51
6431 85
4391 0008623 299
9538 60
0768 15
72736839 10061
Satellite: ISS
Catalog Number: 25544
Epoch time: 10337
22679889 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 85
4391 deg
Eccentricity:
0008623
Arg of perigee: 299
9538 deg
Mean anomaly: 60
0768 deg
Mean motion: 15
72736839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 339
Coasting Arc #13 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2010/338/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 474303
17 A = 6733904
77 meter
Y = -6390823
31 meter E =
0002956
Z = -2065415
39 I = 51
99288
XDOT = 4831
090743 Wp = 266
46169
YDOT = 2165
338999 meter/sec RA = 79
65622 deg
ZDOT = -5583
955461 TA = 296
45055
MA = 296
48088
Ha = 191
688 n
mi
Hp = 188
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1556112
76 X = 555764
93
Y = -20967268
08 feet Y = -6385063
64 meter
Z = -6776297
22 Z = -2062914
06
XDOT = 15850
035247 XDOT = 4833
644881
YDOT = 7104
130574 feet/sec YDOT = 2219
378104 meter/sec
ZDOT = -18320
063848 ZDOT = -5560
479056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11928228
07 X = -3635723
92
Y = 17317722
23 feet Y = 5278441
74 meter
Z = -6766084
04 Z = -2062302
41
XDOT = -8955
625189 XDOT = -2729
674558
YDOT = -13297
880204 feet/sec YDOT = -4053
193886 meter/sec
ZDOT = -18225
709991 ZDOT = -5555
196405
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 10338
24344571
00016717 00000-0 10270-3 0 9125
2 25544 51
6430 80
2291 0008665 303
8059 56
2278 15
72744242 10229
Satellite: ISS
Catalog Number: 25544
Epoch time: 10338
24344571 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 80
2291 deg
Eccentricity:
0008665
Arg of perigee: 303
8059 deg
Mean anomaly: 56
2278 deg
Mean motion: 15
72744242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 288
Coasting Arc #14 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2010/339/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4361087
42 A = 6724817
45 meter
Y = -1037776
37 meter E =
0008824
Z = 5016964
56 I = 51
95629
XDOT = -478
480275 Wp = 346
27630
YDOT = -7429
966834 meter/sec RA = 74
51871 deg
ZDOT = -1945
157194 TA = 122
48769
MA = 122
40237
Ha = 191
865 n
mi
Hp = 187
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14308029
60 X = -4373530
61
Y = -3404778
11 feet Y = -1086614
93 meter
Z = 16459857
48 Z = 4995747
66
XDOT = -1569
817175 XDOT = -385
912052
YDOT = -24376
531608 feet/sec YDOT = -7434
799647 meter/sec
ZDOT = -6381
749325 ZDOT = -1947
257852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10911018
31 X = 3325678
38
Y = 10003131
28 feet Y = 3048954
42 meter
Z = 16374558
84 Z = 4990965
53
XDOT = -9833
175489 XDOT = -2997
151889
YDOT = 21227
193641 feet/sec YDOT = 6470
048622 meter/sec
ZDOT = -6390
001738 ZDOT = -1947
672530
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 10339
26007086
00016717 00000-0 10270-3 0 9136
2 25544 51
6433 75
0173 0008674 307
8602 52
1775 15
72787977 10387
Satellite: ISS
Catalog Number: 25544
Epoch time: 10339
26007086 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 75
0173 deg
Eccentricity:
0008674
Arg of perigee: 307
8602 deg
Mean anomaly: 52
1775 deg
Mean motion: 15
72787977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 317
Coasting Arc #15 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2010/340/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1310710
84 A = 6734746
33 meter
Y = 6460644
11 meter E =
0013964
Z = 1331892
00 I = 51
97997
XDOT = -4980
605671 Wp = 23
68049
YDOT = -202
242470 meter/sec RA = 69
44297 deg
ZDOT = 5873
822579 TA = 350
87879
MA = 350
90413
Ha = 191
953 n
mi
Hp = 187
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4300232
42 X = 1231899
13
Y = 21196338
93 feet Y = 6474860
41 meter
Z = 4369724
39 Z = 1338069
01
XDOT = -16340
569788 XDOT = -5006
508303
YDOT = -663
525165 feet/sec YDOT = -258
084282 meter/sec
ZDOT = 19271
071453 ZDOT = 5849
563545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6261680
55 X = 1908560
23
Y = -20696666
42 feet Y = -6308343
92 meter
Z = 4394386
19 Z = 1339408
91
XDOT = 12674
531250 XDOT = 3863
197125
YDOT = 7911
561655 feet/sec YDOT = 2411
443992 meter/sec
ZDOT = 19173
509539 ZDOT = 5844
085708
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 10340
27667540
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 69
8052 0008629 311
9958 48
0469 15
72826150 10543
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
27667540 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 69
8052 deg
Eccentricity:
0008629
Arg of perigee: 311
9958 deg
Mean anomaly: 48
0469 deg
Mean motion: 15
72826150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 314
Coasting Arc #16 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2010/341/05:10:39
021
Vector Time (MET): N/A
Weight (LBS) : 829629
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207926
09 A = 6723763
93 meter
Y = -663126
70 meter E =
0009247
Z = -5208650
70 I = 51
93081
XDOT = 2496
992451 Wp = 64
24038
YDOT = 7192
612776 meter/sec RA = 64
31618 deg
ZDOT = 1106
981729 TA = 216
25878
MA = 216
32149
Ha = 192
123 n
mi
Hp = 187
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13805531
80 X = 4240331
42
Y = -2175612
53 feet Y = -615889
19 meter
Z = -17088749
01 Z = -5188129
83
XDOT = 8192
232452 XDOT = 2411
000174
YDOT = 23597
810946 feet/sec YDOT = 7220
054678 meter/sec
ZDOT = 3631
829821 ZDOT = 1118
904381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13360197
57 X = -4072188
22
Y = -4432374
38 feet Y = -1350987
71 meter
Z = -17006190
62 Z = -5183486
90
XDOT = 3217
042991 XDOT = 980
554704
YDOT = -23745
930256 feet/sec YDOT = -7237
759542 meter/sec
ZDOT = 3679
572926 ZDOT = 1121
533828
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 10341
22972363
00016717 00000-0 10270-3 0 9156
2 25544 51
6417 64
9190 0008512 316
2485 43
8002 15
72859241 10697
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
22972363 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 64
9190 deg
Eccentricity:
0008512
Arg of perigee: 316
2485 deg
Mean anomaly: 43
8002 deg
Mean motion: 15
72859241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 297
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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