Date:
February 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 269)
---------------------------------------
Vector Time (GMT): 2010/036/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4330545
80 A = 6721403
75 meter
Y = -3522716
55 meter E =
0002507
Z = 3740767
10 I = 51
60193
XDOT = 5842
586361 Wp = 21
74449
YDOT = -2671
214797 meter/sec RA = 187
04855 deg
ZDOT = 4249
618198 TA = 23
51496
MA = 23
50350
Ha = 186
773 n
mi
Hp = 183
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14207827
42 X = -4309004
03
Y = -11557468
99 feet Y = -3571022
87 meter
Z = 12272857
94 Z = 3719781
88
XDOT = 19168
590422 XDOT = 5851
378525
YDOT = -8763
828074 feet/sec YDOT = -2605
830423 meter/sec
ZDOT = 13942
316924 ZDOT = 4278
022425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18034577
00 X = 5496939
07
Y = -3497257
78 feet Y = -1065964
17 meter
Z = 12189491
85 Z = 3715357
12
XDOT = -5824
649255 XDOT = -1775
353093
YDOT = 18935
036979 feet/sec YDOT = 5771
399271 meter/sec
ZDOT = 14054
852690 ZDOT = 4283
919100
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
32061981
00016717 00000-0 10270-3 0 9007
2 25544 51
6453 187
7709 0011359 288
7645 71
2286 15
75672958 2704
Satellite: ISS
Catalog Number: 25544
Epoch time: 10036
32061981 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 187
7709 deg
Eccentricity:
0011359
Arg of perigee: 288
7645 deg
Mean anomaly: 71
2286 deg
Mean motion: 15
75672958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 325
Coasting Arc #2 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2010/037/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5346416
07 A = 6722511
67 meter
Y = 2417711
38 meter E =
0007599
Z = -3270452
90 I = 51
63605
XDOT = -4662
500442 Wp = 308
26713
YDOT = -3900
834532 meter/sec RA = 181
84707 deg
ZDOT = 4735
582407 TA = 13
34960
MA = 13
32950
Ha = 186
839 n
mi
Hp = 183
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17540735
13 X = -5357166
95
Y = 7932123
95 feet Y = 2357864
57 meter
Z = -10729832
33 Z = -3296451
46
XDOT = -15296
917461 XDOT = -4641
538366
YDOT = -12798
013557 feet/sec YDOT = -3952
856302 meter/sec
ZDOT = 15536
687686 ZDOT = 4712
983110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4852510
87 X = 1479045
31
Y = -18569538
77 feet Y = -5659995
42 meter
Z = -10832850
46 Z = -3301852
82
XDOT = 18279
176283 XDOT = 5571
492931
YDOT = -4239
831764 feet/sec YDOT = -1292
300722 meter/sec
ZDOT = 15446
897275 ZDOT = 4708
214289
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
27192728
00016717 00000-0 10270-3 0 9017
2 25544 51
6447 182
8734 0011579 292
1418 67
8516 15
75725879 2856
Satellite: ISS
Catalog Number: 25544
Epoch time: 10037
27192728 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 182
8734 deg
Eccentricity:
0011579
Arg of perigee: 292
1418 deg
Mean anomaly: 67
8516 deg
Mean motion: 15
75725879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 337
Coasting Arc #3 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2010/038/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3750048
01 A = 6718544
68 meter
Y = 3331318
29 meter E =
0008614
Z = -4473065
58 I = 51
65202
XDOT = -6384
055017 Wp = 350
81107
YDOT = 2890
617217 meter/sec RA = 176
74776 deg
ZDOT = -3190
166649 TA = 247
25378
MA = 247
34484
Ha = 187
197 n
mi
Hp = 183
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12303307
13 X = 3734246
89
Y = 10929521
96 feet Y = 3373165
38 meter
Z = -14675412
00 Z = -4454886
40
XDOT = -20945
062391 XDOT = -6400
406943
YDOT = 9483
652286 feet/sec YDOT = 2819
135631 meter/sec
ZDOT = -10466
426013 ZDOT = -3221
219468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16243567
31 X = -4951039
32
Y = 3014553
23 feet Y = 918835
82 meter
Z = -14603168
29 Z = -4451045
69
XDOT = 5630
805517 XDOT = 1716
269522
YDOT = -21103
735304 feet/sec YDOT = -6432
418521 meter/sec
ZDOT = -10589
487367 ZDOT = -3227
675750
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
28663428
00016717 00000-0 10270-3 0 9020
2 25544 51
6438 177
6493 0011631 296
0890 63
9077 15
75759377 3014
Satellite: ISS
Catalog Number: 25544
Epoch time: 10038
28663428 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 177
6493 deg
Eccentricity:
0011631
Arg of perigee: 296
0890 deg
Mean anomaly: 63
9077 deg
Mean motion: 15
75759377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 328
Coasting Arc #4 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2010/039/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5758242
73 A = 6724721
18 meter
Y = -2648559
80 meter E =
0003759
Z = 2247256
86 I = 51
70428
XDOT = 3878
923657 Wp = 63
90639
YDOT = 3787
861681 meter/sec RA = 171
55798 deg
ZDOT = -5466
196669 TA = 90
89238
MA = 90
84931
Ha = 187
368 n
mi
Hp = 182
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18891872
46 X = 5776514
88
Y = -8689500
65 feet Y = -2584065
65 meter
Z = 7372889
96 Z = 2275274
09
XDOT = 12726
127485 XDOT = 3862
832077
YDOT = 12427
367719 feet/sec YDOT = 3831
148380 meter/sec
ZDOT = -17933
716107 ZDOT = -5447
392158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4433208
91 X = -1351242
08
Y = 20275777
43 feet Y = 6180056
96 meter
Z = 7483934
89 Z = 2281103
35
XDOT = -16172
117809 XDOT = -4929
261508
YDOT = 3066
239824 feet/sec YDOT = 934
589898 meter/sec
ZDOT = -17858
964965 ZDOT = -5443
412521
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
30131838
00016717 00000-0 10270-3 0 9030
2 25544 51
6442 172
4250 0011614 300
7934 59
2087 15
75824778 3170
Satellite: ISS
Catalog Number: 25544
Epoch time: 10039
30131838 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 172
4250 deg
Eccentricity:
0011614
Arg of perigee: 300
7934 deg
Mean anomaly: 59
2087 deg
Mean motion: 15
75824778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 317
Checksum: 294
Coasting Arc #5 (Orbit 332)
---------------------------------------
Vector Time (GMT): 2010/040/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2986860
06 A = 6716225
60 meter
Y = -3344111
27 meter E =
0005763
Z = 5003421
94 I = 51
70400
XDOT = 6749
752248 Wp = 305
04170
YDOT = -3178
249371 meter/sec RA = 166
44829 deg
ZDOT = 1909
913679 TA = 126
56366
MA = 126
51060
Ha = 187
685 n
mi
Hp = 182
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9799409
65 X = -2973548
75
Y = -10971493
66 feet Y = -3377437
89 meter
Z = 16415426
30 Z = 4988944
31
XDOT = 22144
856458 XDOT = 6775
512554
YDOT = -10427
327334 feet/sec YDOT = -3102
625691 meter/sec
ZDOT = 6266
120993 ZDOT = 1942
765606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14694971
94 X = 4479027
45
Y = -1531937
18 feet Y = -466934
45 meter
Z = 16357851
07 Z = 4985873
00
XDOT = -4711
649703 XDOT = -1436
110830
YDOT = 22934
996880 feet/sec YDOT = 6990
587049 meter/sec
ZDOT = 6396
342471 ZDOT = 1949
605185
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
31598121
00016717 00000-0 10270-3 0 9046
2 25544 51
6434 167
1994 0011555 304
7583 55
2492 15
75799262 3338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10040
31598121 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 167
1994 deg
Eccentricity:
0011555
Arg of perigee: 304
7583 deg
Mean anomaly: 55
2492 deg
Mean motion: 15
75799262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 333
Checksum: 308
Coasting Arc #6 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2010/041/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963515
75 A = 6726389
05 meter
Y = 2902063
31 meter E =
0015157
Z = -1059140
46 I = 51
76724
XDOT = -2966
267704 Wp = 347
62633
YDOT = -3929
890192 meter/sec RA = 161
27874 deg
ZDOT = 5932
650966 TA =
79212
MA =
78972
Ha = 187
765 n
mi
Hp = 182
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19565340
39 X = -5990378
95
Y = 9521205
08 feet Y = 2835225
58 meter
Z = -3474870
27 Z = -1088175
56
XDOT = -9731
849422 XDOT = -2950
921455
YDOT = -12893
340525 feet/sec YDOT = -3962
975143 meter/sec
ZDOT = 19464
077972 ZDOT = 5918
278388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3453244
20 X = 1052548
83
Y = -21464338
16 feet Y = -6542330
27 meter
Z = -3589972
97 Z = -1094223
76
XDOT = 14644
744919 XDOT = 4463
718251
YDOT = -890
313317 feet/sec YDOT = -271
367499 meter/sec
ZDOT = 19406
888506 ZDOT = 5915
219617
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
26720385
00016717 00000-0 10270-3 0 9051
2 25544 51
6426 162
3006 0011716 308
0457 51
9649 15
75852919 3488
Satellite: ISS
Catalog Number: 25544
Epoch time: 10041
26720385 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 162
3006 deg
Eccentricity:
0011716
Arg of perigee: 308
0457 deg
Mean anomaly: 51
9649 deg
Mean motion: 15
75852919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 303
Coasting Arc #7 (Orbit 363)
---------------------------------------
Vector Time (GMT): 2010/042/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2174841
42 A = 6714751
75 meter
Y = 3571327
89 meter E =
0010842
Z = -5259942
75 I = 51
75591
XDOT = -6864
387913 Wp = 35
81943
YDOT = 3452
941744 meter/sec RA = 156
15214 deg
ZDOT = -485
683562 TA = 229
52632
MA = 229
62088
Ha = 187
953 n
mi
Hp = 182
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7135306
49 X = 2160295
63
Y = 11716955
00 feet Y = 3595567
01 meter
Z = -17257030
01 Z = -5249412
96
XDOT = -22520
957721 XDOT = -6900
129855
YDOT = 11328
549029 feet/sec YDOT = 3375
980254 meter/sec
ZDOT = -1593
450006 ZDOT = -519
116498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13758827
61 X = -4193690
65
Y = -582908
50 feet Y = -177670
51 meter
Z = -17215097
98 Z = -5247161
86
XDOT = 3209
216987 XDOT = 978
169338
YDOT = -23987
006002 feet/sec YDOT = -7311
239429 meter/sec
ZDOT = -1725
997247 ZDOT = -526
083961
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
28182081
00016717 00000-0 10270-3 0 9060
2 25544 51
6418 157
0753 0011591 312
1251 47
8927 15
75909554 3647
Satellite: ISS
Catalog Number: 25544
Epoch time: 10042
28182081 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 157
0753 deg
Eccentricity:
0011591
Arg of perigee: 312
1251 deg
Mean anomaly: 47
8927 deg
Mean motion: 15
75909554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 301
Coasting Arc #8 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2010/043/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5968311
73 A = 6726565
13 meter
Y = -3093320
60 meter E =
0000125
Z = -237457
31 I = 51
82429
XDOT = 2001
219184 Wp = 146
42575
YDOT = 4325
140940 meter/sec RA = 151
01124 deg
ZDOT = -6045
424367 TA = 36
14806
MA = 36
14722
Ha = 188
087 n
mi
Hp = 181
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19581075
22 X = 6003611
70
Y = -10148689
62 feet Y = -3026382
02 meter
Z = -779059
42 Z = -208378
42
XDOT = 6565
679738 XDOT = 1982
072608
YDOT = 14190
094948 feet/sec YDOT = 4347
412695 meter/sec
ZDOT = -19834
069445 ZDOT = -6035
749265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2209648
75 X = -673500
94
Y = 21947624
19 feet Y = 6689635
85 meter
Z = -663766
59 Z = -202316
06
XDOT = -13934
012099 XDOT = -4247
086888
YDOT = -2001
343799 feet/sec YDOT = -610
009590 meter/sec
ZDOT = -19795
493755 ZDOT = -6033
666496
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
29641409
00016717 00000-0 10270-3 0 9077
2 25544 51
6426 151
8508 0011732 316
5032 43
5206 15
75965495 3805
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
29641409 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 151
8508 deg
Eccentricity:
0011732
Arg of perigee: 316
5032 deg
Mean anomaly: 43
5206 deg
Mean motion: 15
75965495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 296
Coasting Arc #9 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2010/044/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1336521
70 A = 6714896
74 meter
Y = -4037507
09 meter E =
0011643
Z = 5201678
19 I = 51
81008
XDOT = 6736
998541 Wp = 338
06570
YDOT = -3580
796442 meter/sec RA = 145
86188 deg
ZDOT = -1038
541632 TA = 121
87231
MA = 121
75895
Ha = 188
255 n
mi
Hp = 181
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4384913
71 X = -1316542
27
Y = -13246414
35 feet Y = -4052341
05 meter
Z = 17065873
34 Z = 5195234
19
XDOT = 22103
013585 XDOT = 6781
583826
YDOT = -11748
019823 feet/sec YDOT = -3505
210062 meter/sec
ZDOT = -3407
288819 ZDOT = -1005
705948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13601206
80 X = 4145647
83
Y = 3252710
15 feet Y = 991426
05 meter
Z = 17040130
41 Z = 5193831
75
XDOT = -1590
975526 XDOT = -484
929340
YDOT = 23989
922830 feet/sec YDOT = 7312
128479 meter/sec
ZDOT = -3277
093856 ZDOT = -998
858207
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
31098621
00016717 00000-0 10270-3 0 9084
2 25544 51
6421 146
6247 0011544 319
9936 40
0376 15
75944202 3963
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
31098621 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 146
6247 deg
Eccentricity:
0011544
Arg of perigee: 319
9936 deg
Mean anomaly: 40
0376 deg
Mean motion: 15
75944202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 396
Checksum: 301
Coasting Arc #10 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2010/045/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5742694
72 A = 6725470
26 meter
Y = 3107596
68 meter E =
0016857
Z = 1563346
76 I = 51
87009
XDOT = -1109
529311 Wp = 19
95626
YDOT = -4966
489810 meter/sec RA = 140
74817 deg
ZDOT = 5793
977785 TA = 357
26174
MA = 357
27095
Ha = 188
412 n
mi
Hp = 181
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18840861
93 X = -5784611
84
Y = 10195527
15 feet Y = 3043144
15 meter
Z = 5129090
41 Z = 1535347
63
XDOT = -3640
188027 XDOT = -1082
055950
YDOT = -16294
257906 feet/sec YDOT = -4978
743383 meter/sec
ZDOT = 19009
113467 ZDOT = 5788
654778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1043348
16 X = 318012
52
Y = -21423464
87 feet Y = -6529872
09 meter
Z = 5018067
20 Z = 1529506
88
XDOT = 14321
187701 XDOT = 4365
098011
YDOT = 5147
101547 feet/sec YDOT = 1568
836551 meter/sec
ZDOT = 18987
780225 ZDOT = 5787
475413
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
32553366
00016717 00000-0 10270-3 0 9099
2 25544 51
6417 141
3986 0011527 324
0787 35
9601 15
76002870 4122
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
32553366 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 141
3986 deg
Eccentricity:
0011527
Arg of perigee: 324
0787 deg
Mean anomaly: 35
9601 deg
Mean motion: 15
76002870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 412
Checksum: 295
Coasting Arc #11 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2010/046/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 641118
16 A = 6716306
48 meter
Y = 4652360
48 meter E =
0008008
Z = -4803546
41 I = 51
86257
XDOT = -6388
250588 Wp = 41
37204
YDOT = 3481
644693 meter/sec RA = 135
57910 deg
ZDOT = 2527
700712 TA = 253
24567
MA = 253
33355
Ha = 188
472 n
mi
Hp = 181
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2103406
03 X = 612381
14
Y = 15263649
86 feet Y = 4659368
90 meter
Z = -15759666
71 Z = -4800502
00
XDOT = -20958
827387 XDOT = -6438
986962
YDOT = 11422
718809 feet/sec YDOT = 3409
923943 meter/sec
ZDOT = 8292
981339 ZDOT = 2496
543977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14297849
25 X = -4357984
45
Y = -5775949
16 feet Y = -1760509
30 meter
Z = -15747391
44 Z = -4799804
91
XDOT = 266
843841 XDOT = 81
334003
YDOT = -22859
507690 feet/sec YDOT = -6967
577944 meter/sec
ZDOT = 8169
430928 ZDOT = 2490
042547
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
27665131
00016717 00000-0 10270-3 0 9100
2 25544 51
6418 136
4996 0011381 328
1232 31
9242 15
76047062 4272
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
27665131 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 136
4996 deg
Eccentricity:
0011381
Arg of perigee: 328
1232 deg
Mean anomaly: 31
9242 deg
Mean motion: 15
76047062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 286
Coasting Arc #12 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2010/047/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5378611
86 A = 6722784
63 meter
Y = -2882823
33 meter E =
0008008
Z = -2830304
67 I = 51
90562
XDOT = 376
943338 Wp = 351
68396
YDOT = 5735
818421 meter/sec RA = 130
48881 deg
ZDOT = -5116
376797 TA = 220
63442
MA = 220
69421
Ha = 188
597 n
mi
Hp = 180
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17646364
36 X = 5424197
16
Y = -9458081
80 feet Y = -2822421
81 meter
Z = -9285776
49 Z = -2804065
04
XDOT = 1236
690741 XDOT = 337
630269
YDOT = 18818
301905 feet/sec YDOT = 5739
813473 meter/sec
ZDOT = -16786
013115 ZDOT = -5114
641519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -378670
15 X = -115418
66
Y = 20065587
94 feet Y = 6115991
20 meter
Z = -9181716
67 Z = -2798587
24
XDOT = -15614
960066 XDOT = -4759
439828
YDOT = -7986
944491 feet/sec YDOT = -2434
420681 meter/sec
ZDOT = -16778
892857 ZDOT = -5114
206543
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 10047
29115389
00016717 00000-0 10270-3 0 9119
2 25544 51
6419 131
2743 0011515 332
7517 27
3042 15
76103919 4431
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
29115389 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 131
2743 deg
Eccentricity:
0011515
Arg of perigee: 332
7517 deg
Mean anomaly: 27
3042 deg
Mean motion: 15
76103919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 443
Checksum: 284
Coasting Arc #13 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2010/048/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -72420
17 A = 6719123
09 meter
Y = -5373308
23 meter E =
0014028
Z = 4037608
27 I = 51
91119
XDOT = 5900
514168 Wp = 24
91111
YDOT = -3030
048357 meter/sec RA = 125
30665 deg
ZDOT = -3909
252119 TA = 105
34061
MA = 105
18554
Ha = 188
702 n
mi
Hp = 180
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -237598
98 X = -31943
13
Y = -17628964
00 feet Y = -5373891
47 meter
Z = 13246746
30 Z = 4037355
15
XDOT = 19358
642283 XDOT = 5952
948272
YDOT = -9941
103535 feet/sec YDOT = -2963
772406 meter/sec
ZDOT = -12825
630313 ZDOT = -3880
460362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15683387
36 X = 4780296
47
Y = 8056080
54 feet Y = 2455493
35 meter
Z = 13245529
05 Z = 4037237
25
XDOT = 160
400439 XDOT = 48
890054
YDOT = 20681
022248 feet/sec YDOT = 6303
575581 meter/sec
ZDOT = -12711
437250 ZDOT = -3874
446074
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 10048
30563436
00016717 00000-0 10270-3 0 9123
2 25544 51
6411 126
0477 0011376 336
0558 24
0076 15
76095839 4595
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
30563436 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 126
0477 deg
Eccentricity:
0011376
Arg of perigee: 336
0558 deg
Mean anomaly: 24
0076 deg
Mean motion: 15
76095839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 302
Coasting Arc #14 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4918357
95 A = 6719360
61 meter
Y = 2327713
82 meter E =
0011211
Z = 3929538
06 I = 51
92943
XDOT = 139
181291 Wp = 39
42495
YDOT = -6554
280478 meter/sec RA = 120
22597 deg
ZDOT = 4058
929898 TA = 8
62022
MA = 8
60098
Ha = 188
859 n
mi
Hp = 180
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16136344
99 X = -4963110
04
Y = 7636856
37 feet Y = 2272463
86 meter
Z = 12892185
24 Z = 3905536
16
XDOT = 456
631532 XDOT = 192
744796
YDOT = -21503
544876 feet/sec YDOT = -6552
424315 meter/sec
ZDOT = 13316
699142 ZDOT = 4059
736566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 626422
27 X = 190933
51
Y = -17909680
49 feet Y = -5458870
61 meter
Z = 12796975
62 Z = 3900518
17
XDOT = 17641
470831 XDOT = 5377
120309
YDOT = 10129
088767 feet/sec YDOT = 3087
346256 meter/sec
ZDOT = 13319
650120 ZDOT = 4059
829357
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 10049
32009019
00016717 00000-0 10270-3 0 9139
2 25544 51
6415 120
8212 0011336 339
9015 20
1702 15
76169660 4759
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32009019 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 120
8212 deg
Eccentricity:
0011336
Arg of perigee: 339
9015 deg
Mean anomaly: 20
1702 deg
Mean motion: 15
76169660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 272
Coasting Arc #15 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2010/050/06:21:43
892
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -252209
25 A = 6722117
79 meter
Y = 6020417
53 meter E =
0012581
Z = -2964822
13 I = 51
95416
XDOT = -5392
851238 Wp = 5
47194
YDOT = 2243
938288 meter/sec RA = 115
04569 deg
ZDOT = 5029
312248 TA = 320
43070
MA = 320
52247
Ha = 188
907 n
mi
Hp = 179
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -827458
15 X = -305109
46
Y = 19752026
02 feet Y = 6017301
24 meter
Z = -9727106
72 Z = -2966176
17
XDOT = -17693
081489 XDOT = -5441
973778
YDOT = 7362
002257 feet/sec YDOT = 2183
357838 meter/sec
ZDOT = 16500
368269 ZDOT = 5002
994618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17375469
38 X = -5296043
07
Y = -9424436
27 feet Y = -2872568
17 meter
Z = -9732260
21 Z = -2966392
91
XDOT = 575
163954 XDOT = 175
309973
YDOT = -17944
556527 feet/sec YDOT = -5469
500830 meter/sec
ZDOT = 16395
953327 ZDOT = 4997
486574
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 10050
27112312
00016717 00000-0 10270-3 0 9147
2 25544 51
6425 115
9221 0011322 344
2397 15
8413 15
76185467 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
27112312 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 115
9221 deg
Eccentricity:
0011322
Arg of perigee: 344
2397 deg
Mean anomaly: 15
8413 deg
Mean motion: 15
76185467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 273
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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