Date:
February 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 209)
---------------------------------------
Vector Time (GMT): 2010/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2305786
65 A = 6715711
86 meter
Y = 3514628
02 meter E =
0003858
Z = -5240800
94 I = 51
46811
XDOT = -6718
605560 Wp = 102
21214
YDOT = -3737
203334 meter/sec RA = 206
41813 deg
ZDOT = 449
174782 TA = 172
06685
MA = 172
06075
Ha = 185
355 n
mi
Hp = 183
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7564916
83 X = -2319458
29
Y = 11530931
84 feet Y = 3488766
80 meter
Z = -17194228
82 Z = -5252035
43
XDOT = -22042
669160 XDOT = -6678
498103
YDOT = -12261
165794 feet/sec YDOT = -3812
110501 meter/sec
ZDOT = 1473
670544 ZDOT = 416
634169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13605050
28 X = -4146819
33
Y = 1887901
31 feet Y = 575432
32 meter
Z = -17238628
02 Z = -5254333
82
XDOT = -4995
973931 XDOT = -1522
772854
YDOT = -23710
640272 feet/sec YDOT = -7227
003155 meter/sec
ZDOT = 1344
507486 ZDOT = 409
805882
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 10032
51516884
00016717 00000-0 10270-3 0 9001
2 25544 51
6399 207
3520 0011187 270
2602 89
7280 15
75557979 2108
Satellite: ISS
Catalog Number: 25544
Epoch time: 10032
51516884 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 207
3520 deg
Eccentricity:
0011187
Arg of perigee: 270
2602 deg
Mean anomaly: 89
7280 deg
Mean motion: 15
75557979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 303
Coasting Arc #2 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2010/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5900018
68 A = 6727244
30 meter
Y = 3085696
65 meter E =
0008402
Z = -924946
30 I = 51
53552
XDOT = -2975
401483 Wp = 215
76204
YDOT = 3903
272004 meter/sec RA = 201
27340 deg
ZDOT = -5937
423448 TA = 334
35921
MA = 334
40085
Ha = 185
609 n
mi
Hp = 183
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19357016
68 X = 5869568
50
Y = 10123676
66 feet Y = 3151503
87 meter
Z = -3034600
72 Z = -896358
67
XDOT = -9761
815889 XDOT = -2989
985112
YDOT = 12806
010511 feet/sec YDOT = 3869
917605 meter/sec
ZDOT = -19479
735721 ZDOT = -5951
913161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5367271
19 X = 1635944
26
Y = 21190826
88 feet Y = 6458964
03 meter
Z = -2921126
71 Z = -890359
42
XDOT = -14431
153555 XDOT = -4398
615604
YDOT = 952
453808 feet/sec YDOT = 290
307921 meter/sec
ZDOT = -19537
025738 ZDOT = -5954
885445
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 10033
52999129
00016717 00000-0 10270-3 0 9011
2 25544 51
6404 202
1281 0011264 275
5556 84
4323 15
75613318 2261
Satellite: ISS
Catalog Number: 25544
Epoch time: 10033
52999129 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 202
1281 deg
Eccentricity:
0011264
Arg of perigee: 275
5556 deg
Mean anomaly: 84
4323 deg
Mean motion: 15
75613318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 286
Coasting Arc #3 (Orbit 241)
---------------------------------------
Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2906417
64 A = 6716573
33 meter
Y = -3342884
16 meter E =
0008218
Z = 5055796
17 I = 51
52744
XDOT = 6737
550440 Wp = 303
30295
YDOT = 3326
386363 meter/sec RA = 196
09522 deg
ZDOT = -1671
316605 TA = 162
81181
MA = 162
78397
Ha = 185
865 n
mi
Hp = 183
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9535490
95 X = 2919022
62
Y = -10967467
71 feet Y = -3310312
30 meter
Z = 16587257
78 Z = 5069945
99
XDOT = 22104
824279 XDOT = 6707
972267
YDOT = 10913
341085 feet/sec YDOT = 3401
564234 meter/sec
ZDOT = -5483
322194 ZDOT = -1638
658046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14459504
47 X = 4407256
96
Y = -523263
70 feet Y = -159490
78 meter
Z = 16643226
31 Z = 5072855
38
XDOT = 6989
594372 XDOT = 2130
428365
YDOT = 22604
417616 feet/sec YDOT = 6889
826489 meter/sec
ZDOT = -5353
688104 ZDOT = -1631
804134
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 10034
54480491
00016717 00000-0 10270-3 0 9022
2 25544 51
6402 196
9039 0011096 278
1494 81
8411 15
75548417 2427
Satellite: ISS
Catalog Number: 25544
Epoch time: 10034
54480491 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 196
9039 deg
Eccentricity:
0011096
Arg of perigee: 278
1494 deg
Mean anomaly: 81
8411 deg
Mean motion: 15
75548417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 242
Checksum: 303
Coasting Arc #4 (Orbit 257)
---------------------------------------
Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5812177
31 A = 6725896
52 meter
Y = -2729332
74 meter E =
0007889
Z = 1983953
47 I = 51
58974
XDOT = 3692
900264 Wp = 16
06369
YDOT = -3800
607382 meter/sec RA = 190
97360 deg
ZDOT = 5592
360790 TA = 6
06798
MA = 6
05843
Ha = 186
201 n
mi
Hp = 183
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19068823
19 X = -5790863
00
Y = -8954503
74 feet Y = -2794208
77 meter
Z = 6509033
70 Z = 1955770
09
XDOT = 12115
814516 XDOT = 3707
958572
YDOT = -12469
184325 feet/sec YDOT = -3759
226974 meter/sec
ZDOT = 18347
640387 ZDOT = 5610
337229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6752067
85 X = -2058030
28
Y = -19991412
85 feet Y = -6093382
64 meter
Z = 6397160
84 Z = 1949854
62
XDOT = 15852
787486 XDOT = 4831
929626
YDOT = 537
345348 feet/sec YDOT = 163
782862 meter/sec
ZDOT = 18418
769614 ZDOT = 5614
040978
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 10035
55960188
00016717 00000-0 10270-3 0 9031
2 25544 51
6411 191
6799 0011173 281
8187 78
1724 15
75626802 2586
Satellite: ISS
Catalog Number: 25544
Epoch time: 10035
55960188 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 191
6799 deg
Eccentricity:
0011173
Arg of perigee: 281
8187 deg
Mean anomaly: 78
1724 deg
Mean motion: 15
75626802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 258
Checksum: 321
Coasting Arc #5 (Orbit 272)
---------------------------------------
Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3526371
99 A = 6718071
89 meter
Y = 3340660
95 meter E =
0000697
Z = -4640766
12 I = 51
59404
XDOT = -6528
300907 Wp = 212
40427
YDOT = -2931
728893 meter/sec RA = 185
78357 deg
ZDOT = 2849
466471 TA = 85
76831
MA = 85
76034
Ha = 186
463 n
mi
Hp = 183
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11569461
91 X = -3540922
07
Y = 10960173
73 feet Y = 3301145
69 meter
Z = -15225610
62 Z = -4657932
29
XDOT = -21418
310061 XDOT = -6508
874603
YDOT = -9618
533114 feet/sec YDOT = -3004
623648 meter/sec
ZDOT = 9348
643279 ZDOT = 2817
799555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15865538
08 X = -4835816
01
Y = -434734
51 feet Y = -132507
08 meter
Z = -15293553
65 Z = -4661475
15
XDOT = -8321
201126 XDOT = -2536
302103
YDOT = -20863
033439 feet/sec YDOT = -6359
052592 meter/sec
ZDOT = 9222
937395 ZDOT = 2811
151318
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 10036
51096487
00016717 00000-0 10270-3 0 9041
2 25544 51
6417 186
7834 0011118 285
9045 74
0894 15
75627595 2734
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
51096487 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 186
7834 deg
Eccentricity:
0011118
Arg of perigee: 285
9045 deg
Mean anomaly: 74
0894 deg
Mean motion: 15
75627595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 273
Checksum: 329
Coasting Arc #6 (Orbit 288)
---------------------------------------
Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5526814
58 A = 6723710
61 meter
Y = 2415158
79 meter E =
0006611
Z = -2968790
76 I = 51
64305
XDOT = -4387
525641 Wp = 288
88905
YDOT = 3895
445792 meter/sec RA = 180
67991 deg
ZDOT = -4987
865874 TA = 285
38651
MA = 285
45954
Ha = 186
838 n
mi
Hp = 183
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18132593
78 X = 5513818
72
Y = 7923749
31 feet Y = 2476890
33 meter
Z = -9740127
18 Z = -2941973
39
XDOT = -14394
769162 XDOT = -4406
529322
YDOT = 12780
333962 feet/sec YDOT = 3846
275782 meter/sec
ZDOT = -16364
389352 ZDOT = -5009
226196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7498171
21 X = 2285442
58
Y = 18368907
96 feet Y = 5598843
15 meter
Z = -9633664
23 Z = -2936340
86
XDOT = -17820
126820 XDOT = -5431
574655
YDOT = -1371
907822 feet/sec YDOT = -418
157504 meter/sec
ZDOT = -16448
954481 ZDOT = -5013
641326
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 10037
52573869
00016717 00000-0 10270-3 0 9058
2 25544 51
6415 181
5594 0011157 290
3089 69
6876 15
75656621 2898
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
52573869 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 181
5594 deg
Eccentricity:
0011157
Arg of perigee: 290
3089 deg
Mean anomaly: 69
6876 deg
Mean motion: 15
75656621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 289
Checksum: 340
Coasting Arc #7 (Orbit 304)
---------------------------------------
Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4110414
68 A = 6720428
55 meter
Y = -3501986
59 meter E =
0006819
Z = 4005214
85 I = 51
66249
XDOT = 6075
898545 Wp = 3
63271
YDOT = 2633
954205 meter/sec RA = 175
48291 deg
ZDOT = -3925
425338 TA = 126
94685
MA = 126
88438
Ha = 187
077 n
mi
Hp = 183
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13485612
48 X = 4129812
76
Y = -11489457
31 feet Y = -3455913
20 meter
Z = 13140468
67 Z = 4025229
86
XDOT = 19934
050345 XDOT = 6065
062299
YDOT = 8641
582038 feet/sec YDOT = 2701
838079 meter/sec
ZDOT = -12878
692054 ZDOT = -3895
935353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17638008
99 X = 5376065
14
Y = 825107
00 feet Y = 251492
61 meter
Z = 13219724
93 Z = 4029372
16
XDOT = 8706
299537 XDOT = 2653
680099
YDOT = 18721
060228 feet/sec YDOT = 5706
179158 meter/sec
ZDOT = -12761
606436 ZDOT = -3889
737642
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 10038
54050081
00016717 00000-0 10270-3 0 9068
2 25544 51
6416 176
3354 0011092 293
9261 66
0741 15
75646443 3056
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
54050081 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 176
3354 deg
Eccentricity:
0011092
Arg of perigee: 293
9261 deg
Mean anomaly: 66
0741 deg
Mean motion: 15
75646443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 305
Checksum: 288
Coasting Arc #8 (Orbit 320)
---------------------------------------
Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5036925
84 A = 6720933
29 meter
Y = -2229070
57 meter E =
0003831
Z = 3847099
76 I = 51
69578
XDOT = 4996
378851 Wp = 21
97321
YDOT = -4158
229515 meter/sec RA = 170
38928 deg
ZDOT = 4134
476475 TA = 24
88661
MA = 24
86814
Ha = 187
359 n
mi
Hp = 183
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16525347
24 X = -5030313
73
Y = -7313223
65 feet Y = -2285359
66 meter
Z = 12621718
37 Z = 3822646
86
XDOT = 16392
319065 XDOT = 5022
421462
YDOT = -13642
485286 feet/sec YDOT = -4102
211624 meter/sec
ZDOT = 13564
555363 ZDOT = 4158
811429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7359899
53 X = -2243297
38
Y = -16578418
00 feet Y = -5053101
81 meter
Z = 12524617
82 Z = 3817503
51
XDOT = 20037
783276 XDOT = 6107
516342
YDOT = 1419
444423 feet/sec YDOT = 432
646660 meter/sec
ZDOT = 13660
935306 ZDOT = 4163
853081
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 10039
55524740
00016717 00000-0 10270-3 0 9079
2 25544 51
6428 171
1112 0011214 297
8900 62
1128 15
75719552 3219
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
55524740 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 171
1112 deg
Eccentricity:
0011214
Arg of perigee: 297
8900 deg
Mean anomaly: 62
1128 deg
Mean motion: 15
75719552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 321
Checksum: 282
Coasting Arc #9 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4558707
74 A = 6722925
53 meter
Y = 3785859
46 meter E =
0008447
Z = -3163363
64 I = 51
73244
XDOT = -5444
763291 Wp = 324
10549
YDOT = -2511
153420 meter/sec RA = 165
19586 deg
ZDOT = 4841
348006 TA = 359
03782
MA = 359
03945
Ha = 187
564 n
mi
Hp = 183
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14956390
21 X = -4585336
42
Y = 12420798
75 feet Y = 3734732
53 meter
Z = -10378489
62 Z = -3185573
80
XDOT = -17863
396624 XDOT = -5439
796259
YDOT = -8238
692323 feet/sec YDOT = -2572
012416 meter/sec
ZDOT = 15883
687685 ZDOT = 4814
909979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19387790
36 X = -5909398
50
Y = -499564
78 feet Y = -152267
34 meter
Z = -10466466
27 Z = -3190178
92
XDOT = -8089
274536 XDOT = -2465
610878
YDOT = -16626
542923 feet/sec YDOT = -5067
770283 meter/sec
ZDOT = 15778
686565 ZDOT = 4809
343665
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 10040
50656340
00016717 00000-0 10270-3 0 9089
2 25544 51
6431 166
2144 0011295 302
4814 57
5258 15
75691246 3366
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
50656340 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 166
2144 deg
Eccentricity:
0011295
Arg of perigee: 302
4814 deg
Mean anomaly: 57
5258 deg
Mean motion: 15
75691246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 289
Coasting Arc #10 (Orbit 351)
---------------------------------------
Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428171
90 A = 6718384
07 meter
Y = 2211088
95 meter E =
0010150
Z = -4548448
84 I = 51
74655
XDOT = -5418
539387 Wp = 2
11130
YDOT = 4529
862853 meter/sec RA = 160
10281 deg
ZDOT = -3063
467360 TA = 237
39242
MA = 237
49044
Ha = 187
832 n
mi
Hp = 183
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14528123
02 X = 4425212
90
Y = 7254228
83 feet Y = 2260590
98 meter
Z = -14922732
41 Z = -4526944
52
XDOT = -17777
360194 XDOT = -5453
909057
YDOT = 14861
754767 feet/sec YDOT = 4469
071862 meter/sec
ZDOT = -10050
745932 ZDOT = -3089
875647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6451439
19 X = 1966398
67
Y = 14987039
51 feet Y = 4568049
64 meter
Z = -14837308
24 Z = -4522411
55
XDOT = -22032
335146 XDOT = -6715
455753
YDOT = -601
486063 feet/sec YDOT = -183
332952 meter/sec
ZDOT = -10155
363058 ZDOT = -3095
354660
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 10041
52128705
00016717 00000-0 10270-3 0 9092
2 25544 51
6437 160
9907 0011289 306
1414 53
8705 15
75719331 3520
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
52128705 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 160
9907 deg
Eccentricity:
0011289
Arg of perigee: 306
1414 deg
Mean anomaly: 53
8705 deg
Mean motion: 15
75719331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 352
Checksum: 296
Coasting Arc #11 (Orbit 367)
---------------------------------------
Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4855577
60 A = 6725184
37 meter
Y = -4132051
30 meter E =
0005400
Z = 2140439
31 I = 51
79827
XDOT = 4671
898049 Wp = 61
54953
YDOT = 2618
610995 meter/sec RA = 154
92181 deg
ZDOT = -5530
012313 TA = 94
55981
MA = 94
49812
Ha = 187
975 n
mi
Hp = 182
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15930372
70 X = 4891024
51
Y = -13556598
74 feet Y = -4077555
18 meter
Z = 7022438
67 Z = 2164113
02
XDOT = 15327
749505 XDOT = 4669
132024
YDOT = 8591
243422 feet/sec YDOT = 2670
839532 meter/sec
ZDOT = -18143
085017 ZDOT = -5507
323619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20882015
86 X = 6364838
44
Y = -416507
69 feet Y = -126951
54 meter
Z = 7116229
58 Z = 2169026
78
XDOT = 6463
766805 XDOT = 1970
156122
YDOT = 14904
025796 feet/sec YDOT = 4542
747063 meter/sec
ZDOT = -18052
933420 ZDOT = -5502
534106
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 10042
53599822
00016717 00000-0 10270-3 0 9108
2 25544 51
6441 155
7669 0011203 310
3857 49
6329 15
75738337 3685
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
53599822 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 155
7669 deg
Eccentricity:
0011203
Arg of perigee: 310
3857 deg
Mean anomaly: 49
6329 deg
Mean motion: 15
75738337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 368
Checksum: 317
Coasting Arc #12 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3721481
83 A = 6716074
64 meter
Y = -2424058
90 meter E =
0005949
Z = 5039628
30 I = 51
79581
XDOT = 5641
957302 Wp = 323
42373
YDOT = -4923
577753 meter/sec RA = 149
81834 deg
ZDOT = 1803
795583 TA = 109
26984
MA = 109
20548
Ha = 188
198 n
mi
Hp = 182
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12209586
06 X = -3718579
82
Y = -7952949
15 feet Y = -2465658
46 meter
Z = 16534213
60 Z = 5021556
98
XDOT = 18510
358602 XDOT = 5687
832066
YDOT = -16153
470318 feet/sec YDOT = -4860
229531 meter/sec
ZDOT = 5917
964511 ZDOT = 1831
314800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4718700
99 X = -1438260
06
Y = -13871816
05 feet Y = -4228129
53 meter
Z = 16462387
18 Z = 5017735
61
XDOT = 23499
807293 XDOT = 7162
741263
YDOT = -863
811619 feet/sec YDOT = -263
289781 meter/sec
ZDOT = 6026
995231 ZDOT = 1837
028146
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 10043
55069478
00016717 00000-0 10270-3 0 9111
2 25544 51
6451 150
5425 0011319 314
5954 45
4285 15
75801784 3841
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
55069478 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 150
5425 deg
Eccentricity:
0011319
Arg of perigee: 314
5954 deg
Mean anomaly: 45
4285 deg
Mean motion: 15
75801784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 306
Coasting Arc #13 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4931905
20 A = 6726717
63 meter
Y = 4449580
05 meter E =
0016445
Z = -989155
27 I = 51
85719
XDOT = -3882
790102 Wp = 355
35142
YDOT = -2981
474922 meter/sec RA = 144
65883 deg
ZDOT = 5956
943873 TA = 353
85458
MA = 353
87473
Ha = 188
457 n
mi
Hp = 182
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16180791
35 X = -4976489
66
Y = 14598359
76 feet Y = 4394179
25 meter
Z = -3245260
08 Z = -1013222
13
XDOT = -12738
812672 XDOT = -3878
099008
YDOT = -9781
741869 feet/sec YDOT = -3024
868201 meter/sec
ZDOT = 19543
779110 ZDOT = 5938
093334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21704191
17 X = -6615437
47
Y = 1797279
71 feet Y = 547810
86 meter
Z = -3340613
79 Z = -1018219
08
XDOT = -4150
638308 XDOT = -1265
114556
YDOT = -13991
349278 feet/sec YDOT = -4264
563260 meter/sec
ZDOT = 19468
830042 ZDOT = 5934
099397
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 10044
50196368
00016717 00000-0 10270-3 0 9127
2 25544 51
6453 145
6457 0011459 319
2379 40
7927 15
75762121 3999
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
50196368 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 145
6457 deg
Eccentricity:
0011459
Arg of perigee: 319
2379 deg
Mean anomaly: 40
7927 deg
Mean motion: 15
75762121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 399
Checksum: 320
Coasting Arc #14 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3060438
82 A = 6715041
04 meter
Y = 2832811
07 meter E =
0012847
Z = -5270629
31 I = 51
84184
XDOT = -5619
426774 Wp = 38
74203
YDOT = 5242
879909 meter/sec RA = 139
53925 deg
ZDOT = -435
832363 TA = 227
07488
MA = 227
18275
Ha = 188
637 n
mi
Hp = 181
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10040809
78 X = 3054137
40
Y = 9293999
57 feet Y = 2866999
25 meter
Z = -17292090
90 Z = -5255777
55
XDOT = -18436
439548 XDOT = -5675
518807
YDOT = 17201
049571 feet/sec YDOT = 5179
726499 meter/sec
ZDOT = -1429
896203 ZDOT = -463
267224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2655149
69 X = 809289
63
Y = 13497629
65 feet Y = 4114077
52 meter
Z = -17233016
88 Z = -5252623
55
XDOT = -24054
048680 XDOT = -7331
674038
YDOT = 2728
489581 feet/sec YDOT = 831
643624 meter/sec
ZDOT = -1538
594090 ZDOT = -468
963479
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 10045
51663699
00016717 00000-0 10270-3 0 9136
2 25544 51
6451 140
4223 0011455 322
7341 37
3027 15
75801372 4159
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
51663699 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 140
4223 deg
Eccentricity:
0011455
Arg of perigee: 322
7341 deg
Mean anomaly: 37
3027 deg
Mean motion: 15
75801372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 279
Coasting Arc #15 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 750718
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4841901
35 A = 6726969
70 meter
Y = -4664250
95 meter E =
0002135
Z = -249195
23 I = 51
90369
XDOT = 3136
409846 Wp = 64
17784
YDOT = 3577
048594 meter/sec RA = 134
40539 deg
ZDOT = -6050
594839 TA = 118
51989
MA = 118
49839
Ha = 188
728 n
mi
Hp = 181
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15885503
12 X = 4894908
49
Y = -15302660
59 feet Y = -4609809
57 meter
Z = -817569
66 Z = -225544
85
XDOT = 10290
058549 XDOT = 3125
569505
YDOT = 11735
723732 feet/sec YDOT = 3612
060822 meter/sec
ZDOT = -19851
032936 ZDOT = -6035
385088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21816151
75 X = 6649563
05
Y = -3274231
46 feet Y = -997985
75 meter
Z = -723866
06 Z = -220634
38
XDOT = 1449
713579 XDOT = 441
872699
YDOT = 14002
761921 feet/sec YDOT = 4268
041834 meter/sec
ZDOT = -19790
504518 ZDOT = -6032
145777
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 10046
53129811
00016717 00000-0 10270-3 0 9143
2 25544 51
6443 135
1984 0011367 327
0840 32
9615 15
75821517 4314
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
53129811 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 135
1984 deg
Eccentricity:
0011367
Arg of perigee: 327
0840 deg
Mean anomaly: 32
9615 deg
Mean motion: 15
75821517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 291
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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