Date:
February 15th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2111)
---------------------------------------
Vector Time (GMT): 2011/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034833
01 A = 6726916
51 meter
Y = 2330798
98 meter E =
0007362
Z = -4858387
03 I = 51
97137
XDOT = -1233
396464 Wp = 100
91806
YDOT = 7193
761072 meter/sec RA = 84
64500 deg
ZDOT = 2428
594191 TA = 192
70176
MA = 192
72032
Ha = 191
653 n
mi
Hp = 188
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13237641
12 X = 4032070
51
Y = 7646978
30 feet Y = 2375903
48 meter
Z = -15939589
98 Z = -4838792
82
XDOT = -4046
576327 XDOT = -1325
544285
YDOT = 23601
578321 feet/sec YDOT = 7179
453264 meter/sec
ZDOT = 7967
828710 ZDOT = 2422
378610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5404060
79 X = 1647157
73
Y = 14388229
84 feet Y = 4385532
45 meter
Z = -15860545
94 Z = -4834294
40
XDOT = -17144
272523 XDOT = -5225
574265
YDOT = 15188
242138 feet/sec YDOT = 4629
376204 meter/sec
ZDOT = 7942
571391 ZDOT = 2420
895760
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 11042
51171870
00016717 00000-0 10270-3 0 9005
2 25544 51
6441 85
3636 0004739 297
5664 62
5016 15
72289250 21123
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
51171870 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 85
3636 deg
Eccentricity:
0004739
Arg of perigee: 297
5664 deg
Mean anomaly: 62
5016 deg
Mean motion: 15
72289250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2112
Checksum: 292
Coasting Arc #2 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2011/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 87412
04 A = 6735772
89 meter
Y = -6534492
13 meter E =
0003956
Z = -1622544
13 I = 51
99814
XDOT = 4862
120715 Wp = 166
77122
YDOT = 1497
055725 meter/sec RA = 79
58053 deg
ZDOT = -5773
683370 TA = 31
03498
MA = 31
01162
Ha = 191
672 n
mi
Hp = 187
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 286784
90 X = 168357
36
Y = -21438622
48 feet Y = -6533062
03 meter
Z = -5323307
52 Z = -1621922
95
XDOT = 15951
839615 XDOT = 4873
066017
YDOT = 4911
600146 feet/sec YDOT = 1551
488162 meter/sec
ZDOT = -18942
530742 ZDOT = -5750
036993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13622549
47 X = 4152153
08
Y = -16557515
93 feet Y = -5046730
85 meter
Z = -5320638
57 Z = -1621730
63
XDOT = 8285
129637 XDOT = 2525
307513
YDOT = 12866
030834 feet/sec YDOT = 3921
566198 meter/sec
ZDOT = -18847
106910 ZDOT = -5744
598186
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 11043
52864037
00016717 00000-0 10270-3 0 9012
2 25544 51
6446 80
1546 0004643 302
1177 57
9534 15
72335760 21285
Satellite: ISS
Catalog Number: 25544
Epoch time: 11043
52864037 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 80
1546 deg
Eccentricity:
0004643
Arg of perigee: 302
1177 deg
Mean anomaly: 57
9534 deg
Mean motion: 15
72335760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 291
Coasting Arc #3 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2011/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4281486
39 A = 6725282
88 meter
Y = -263807
45 meter E =
0005157
Z = 5180824
90 I = 51
95544
XDOT = -1067
651643 Wp = 356
79067
YDOT = -7518
312196 meter/sec RA = 74
45603 deg
ZDOT = -1260
177440 TA = 105
23587
MA = 105
17885
Ha = 191
888 n
mi
Hp = 187
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14046871
36 X = -4303385
22
Y = -865509
99 feet Y = -311808
16 meter
Z = 16997457
02 Z = 5159972
68
XDOT = -3502
794104 XDOT = -977
379519
YDOT = -24666
378597 feet/sec YDOT = -7529
746559 meter/sec
ZDOT = -4134
440420 ZDOT = -1265
144865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10680369
86 X = -3255376
73
Y = -9319225
44 feet Y = -2840499
92 meter
Z = 16913278
34 Z = 5155167
24
XDOT = 11618
239816 XDOT = 3541
239496
YDOT = -20884
487405 feet/sec YDOT = -6365
591761 meter/sec
ZDOT = -4154
299635 ZDOT = -1266
230529
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 11044
54554478
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 74
9456 0004613 306
8788 53
1951 15
72368467 21440
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
54554478 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 74
9456 deg
Eccentricity:
0004613
Arg of perigee: 306
8788 deg
Mean anomaly: 53
1951 deg
Mean motion: 15
72368467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 325
Coasting Arc #4 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2011/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1935943
03 A = 6736664
82 meter
Y = 6418300
79 meter E =
0013305
Z = 574724
50 I = 51
98503
XDOT = -4708
203026 Wp = 30
68169
YDOT = 875
601773 meter/sec RA = 69
37260 deg
ZDOT = 6031
460070 TA = 335
54239
MA = 335
60545
Ha = 191
964 n
mi
Hp = 187
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6351519
11 X = 1861236
65
Y = 21057417
29 feet Y = 6439531
96 meter
Z = 1885579
08 Z = 583947
74
XDOT = -15446
860323 XDOT = -4746
943243
YDOT = 2872
709229 feet/sec YDOT = 822
735076 meter/sec
ZDOT = 19788
254823 ZDOT = 6008
494122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7473318
39 X = -2277867
44
Y = 20682479
93 feet Y = 6304019
88 meter
Z = 1922644
63 Z = 586022
08
XDOT = -12697
958396 XDOT = -3870
337719
YDOT = -6433
958528 feet/sec YDOT = -1961
070559 meter/sec
ZDOT = 19695
506499 ZDOT = 6003
190381
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 11045
56243307
00016717 00000-0 10270-3 0 9031
2 25544 51
6441 69
7366 0004682 312
0799 47
9965 15
72374052 21606
Satellite: ISS
Catalog Number: 25544
Epoch time: 11045
56243307 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 69
7366 deg
Eccentricity:
0004682
Arg of perigee: 312
0799 deg
Mean anomaly: 47
9965 deg
Mean motion: 15
72374052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2160
Checksum: 311
Coasting Arc #5 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2011/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3772102
72 A = 6724689
43 meter
Y = -1734009
54 meter E =
0012094
Z = -5300115
47 I = 51
93310
XDOT = 3289
287891 Wp = 74
89277
YDOT = 6950
687298 meter/sec RA = 64
26543 deg
ZDOT = 70
185683 TA = 195
75262
MA = 195
79028
Ha = 192
017 n
mi
Hp = 187
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12375665
09 X = 3816958
62
Y = -5689007
67 feet Y = -1691576
76 meter
Z = -17388830
27 Z = -5281682
20
XDOT = 10791
626940 XDOT = 3210
978587
YDOT = 22804
092185 feet/sec YDOT = 6987
032252 meter/sec
ZDOT = 230
267988 ZDOT = 85
974405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13457336
97 X = 4101796
31
Y = 2646982
42 feet Y = 806800
24 meter
Z = -17314354
69 Z = -5277415
31
XDOT = -4324
551397 XDOT = -1318
123266
YDOT = 23838
910408 feet/sec YDOT = 7266
099892 meter/sec
ZDOT = 293
826543 ZDOT = 89
558330
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 11046
51574866
00016717 00000-0 10270-3 0 9045
2 25544 51
6442 64
8528 0004700 314
5338 45
5440 15
72392087 21756
Satellite: ISS
Catalog Number: 25544
Epoch time: 11046
51574866 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 64
8528 deg
Eccentricity:
0004700
Arg of perigee: 314
5338 deg
Mean anomaly: 45
5440 deg
Mean motion: 15
72392087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2175
Checksum: 305
Coasting Arc #6 (Orbit 2190)
---------------------------------------
Vector Time (GMT): 2011/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3734545
99 A = 6736559
94 meter
Y = -5585029
75 meter E =
0008461
Z = 438743
71 I = 51
95778
XDOT = 3728
986253 Wp = 125
21854
YDOT = -2973
979893 meter/sec RA = 59
15948 deg
ZDOT = -6040
220709 TA = 50
03526
MA = 49
96097
Ha = 192
097 n
mi
Hp = 187
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12252447
49 X = -3673946
84
Y = -18323588
43 feet Y = -5626452
87 meter
Z = 1439447
86 Z = 420749
17
XDOT = 12234
206868 XDOT = 3791
306037
YDOT = -9757
151879 feet/sec YDOT = -2931
931765 meter/sec
ZDOT = -19816
997077 ZDOT = -6021
954479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 332479
50 X = 101339
75
Y = -22044711
25 feet Y = -6719227
99 meter
Z = 1366943
92 Z = 416644
51
XDOT = 14102
073025 XDOT = 4298
311858
YDOT = -1027
941076 feet/sec YDOT = -313
316440 meter/sec
ZDOT = -19743
158420 ZDOT = -6017
714686
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 11047
53260229
00016717 00000-0 10270-3 0 9054
2 25544 51
6428 59
6426 0004621 320
2720 39
8103 15
72434038 21913
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
53260229 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 59
6426 deg
Eccentricity:
0004621
Arg of perigee: 320
2720 deg
Mean anomaly: 39
8103 deg
Mean motion: 15
72434038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2191
Checksum: 281
Coasting Arc #7 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2011/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2608563
17 A = 6724855
02 meter
Y = 3359580
51 meter E =
0001814
Z = 5208329
99 I = 51
90128
XDOT = -5127
855477 Wp = 9
71921
YDOT = -5642
174643 meter/sec RA = 54
06850 deg
ZDOT = 1072
865422 TA = 70
09144
MA = 70
07189
Ha = 192
292 n
mi
Hp = 187
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8558278
11 X = -2671237
03
Y = 11022245
77 feet Y = 3330059
80 meter
Z = 17087696
81 Z = 5195505
63
XDOT = -16823
672825 XDOT = -5069
594111
YDOT = -18511
071665 feet/sec YDOT = -5699
191618 meter/sec
ZDOT = 3519
899679 ZDOT = 1048
096928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13318332
78 X = -4059427
83
Y = 4373356
72 feet Y = 1332999
13 meter
Z = 17035820
25 Z = 5192518
01
XDOT = -3438
797419 XDOT = -1048
145453
YDOT = -23772
869046 feet/sec YDOT = -7245
970485 meter/sec
ZDOT = 3420
044086 ZDOT = 1042
429437
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 11048
54943765
00016717 00000-0 10270-3 0 9060
2 25544 51
6421 54
4321 0004706 324
1503 35
9343 15
72456607 22076
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
54943765 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 54
4321 deg
Eccentricity:
0004706
Arg of perigee: 324
1503 deg
Mean anomaly: 35
9343 deg
Mean motion: 15
72456607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2207
Checksum: 290
Coasting Arc #8 (Orbit 2221)
---------------------------------------
Vector Time (GMT): 2011/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5098198
82 A = 6735531
67 meter
Y = 4154738
96 meter E =
0011151
Z = -1423462
40 I = 51
91923
XDOT = -2093
452710 Wp = 14
35930
YDOT = 4562
438023 meter/sec RA = 48
94218 deg
ZDOT = 5839
085076 TA = 330
05108
MA = 330
11483
Ha = 192
255 n
mi
Hp = 186
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16726374
08 X = 5058275
54
Y = 13631033
34 feet Y = 4211526
77 meter
Z = -4670152
24 Z = -1398793
42
XDOT = -6868
283170 XDOT = -2172
679494
YDOT = 14968
628683 feet/sec YDOT = 4538
585226 meter/sec
ZDOT = 19157
103268 ZDOT = 5828
722626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6741694
70 X = 2054868
55
Y = 20519396
00 feet Y = 6254311
90 meter
Z = -4570658
80 Z = -1393136
80
XDOT = -12463
720898 XDOT = -3798
942130
YDOT = 8337
729469 feet/sec YDOT = 2541
339942 meter/sec
ZDOT = 19115
134410 ZDOT = 5826
292968
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 11049
50270407
00016717 00000-0 10270-3 0 9074
2 25544 51
6424 49
5485 0004586 328
0153 32
0730 15
72525296 22221
Satellite: ISS
Catalog Number: 25544
Epoch time: 11049
50270407 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 49
5485 deg
Eccentricity:
0004586
Arg of perigee: 328
0153 deg
Mean anomaly: 32
0730 deg
Mean motion: 15
72525296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2222
Checksum: 289
Coasting Arc #9 (Orbit 2237)
---------------------------------------
Vector Time (GMT): 2011/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 975710
41 A = 6725823
17 meter
Y = -4456145
37 meter E =
0012588
Z = -4953433
77 I = 51
86486
XDOT = 6349
106206 Wp = 52
41511
YDOT = 3772
674388 meter/sec RA = 43
86503 deg
ZDOT = -2139
482520 TA = 196
84664
MA = 196
88849
Ha = 192
358 n
mi
Hp = 186
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3201149
64 X = 1049529
60
Y = -14619899
51 feet Y = -4444822
10 meter
Z = -16251423
15 Z = -4948514
19
XDOT = 20830
400938 XDOT = 6316
840513
YDOT = 12377
540644 feet/sec YDOT = 3843
493331 meter/sec
ZDOT = -7019
299606 ZDOT = -2108
718106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10487870
21 X = 3196702
84
Y = -10707133
37 feet Y = -3263534
25 meter
Z = -16231433
96 Z = -4947341
07
XDOT = 10475
333790 XDOT = 3192
881739
YDOT = 20732
561906 feet/sec YDOT = 6319
284869 meter/sec
ZDOT = -6895
188852 ZDOT = -2101
653562
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 11050
51950435
00016717 00000-0 10270-3 0 9084
2 25544 51
6418 44
3374 0004775 332
0605 28
0303 15
72508604 22383
Satellite: ISS
Catalog Number: 25544
Epoch time: 11050
51950435 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 44
3374 deg
Eccentricity:
0004775
Arg of perigee: 332
0605 deg
Mean anomaly: 28
0303 deg
Mean motion: 15
72508604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2238
Checksum: 281
Coasting Arc #10 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2011/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5859415
95 A = 6734033
70 meter
Y = -2387416
65 meter E =
0011273
Z = 2296244
11 I = 51
87026
XDOT = 67
240332 Wp = 88
47604
YDOT = -5432
064552 meter/sec RA = 38
71952 deg
ZDOT = -5452
973424 TA = 65
82185
MA = 65
70405
Ha = 192
432 n
mi
Hp = 186
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19223805
62 X = -5843438
43
Y = -7832731
80 feet Y = -2452850
64 meter
Z = 7533609
29 Z = 2267818
70
XDOT = 220
604765 XDOT = 154
466722
YDOT = -17821
734094 feet/sec YDOT = -5430
825436 meter/sec
ZDOT = -17890
332755 ZDOT = -5452
434395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12566557
93 X = -3830286
86
Y = -16574167
94 feet Y = -5051806
39 meter
Z = 7418910
82 Z = 2261284
02
XDOT = 8174
572363 XDOT = 2491
609656
YDOT = -14239
564533 feet/sec YDOT = -4340
219270 meter/sec
ZDOT = -17887
999577 ZDOT = -5452
262271
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 11051
53628497
00016717 00000-0 10270-3 0 9098
2 25544 51
6420 39
1269 0004983 335
8589 24
2339 15
72569437 22540
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
53628497 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 39
1269 deg
Eccentricity:
0004983
Arg of perigee: 335
8589 deg
Mean anomaly: 24
2339 deg
Mean motion: 15
72569437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 332
Coasting Arc #11 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2011/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 886841
94 A = 6727206
45 meter
Y = 4878898
88 meter E =
0006113
Z = 4540193
35 I = 51
82325
XDOT = -6858
099596 Wp = 79
72106
YDOT = -1638
978786 meter/sec RA = 33
65279 deg
ZDOT = 3098
409020 TA = 339
48632
MA = 339
51086
Ha = 192
447 n
mi
Hp = 186
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2909586
43 X = 810164
17
Y = 16006886
09 feet Y = 4888387
73 meter
Z = 14895647
48 Z = 4544314
91
XDOT = -22500
326758 XDOT = -6854
313786
YDOT = -5377
226988 feet/sec YDOT = -1715
648785 meter/sec
ZDOT = 10165
383925 ZDOT = 3065
102242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5487366
54 X = -1672549
32
Y = 15299779
61 feet Y = 4663372
83 meter
Z = 14912141
41 Z = 4545220
70
XDOT = -15810
677296 XDOT = -4819
094440
YDOT = -15455
219667 feet/sec YDOT = -4710
750954 meter/sec
ZDOT = 10030
963310 ZDOT = 3057
437617
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 11052
55304741
00016717 00000-0 10270-3 0 9106
2 25544 51
6421 33
9171 0004933 338
1565 21
9386 15
72590990 22702
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
55304741 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 33
9171 deg
Eccentricity:
0004933
Arg of perigee: 338
1565 deg
Mean anomaly: 21
9386 deg
Mean motion: 15
72590990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 292
Coasting Arc #12 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2011/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5959881
43 A = 6732143
99 meter
Y = 469158
37 meter E =
0006747
Z = -3090667
64 I = 51
81372
XDOT = 2106
091991 Wp = 25
71538
YDOT = 5539
214937 meter/sec RA = 28
49383 deg
ZDOT = 4912
053073 TA = 298
53317
MA = 298
60107
Ha = 192
700 n
mi
Hp = 186
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19553416
76 X = 5969205
96
Y = 1539233
50 feet Y = 535857
32 meter
Z = -10139985
68 Z = -3061692
31
XDOT = 6909
750627 XDOT = 2020
133368
YDOT = 18173
277351 feet/sec YDOT = 5562
286211 meter/sec
ZDOT = 16115
659689 ZDOT = 4922
075199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16457900
19 X = 5016367
98
Y = 10779666
21 feet Y = 3285642
26 meter
Z = -10023022
21 Z = -3055017
17
XDOT = -1977
956808 XDOT = -602
881235
YDOT = 18011
135592 feet/sec YDOT = 5489
794128 meter/sec
ZDOT = 16155
947570 ZDOT = 4924
332819
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 11053
50624535
00016717 00000-0 10270-3 0 9119
2 25544 51
6423 29
0325 0004949 344
0507 16
0498 15
72586923 22856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11053
50624535 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 29
0325 deg
Eccentricity:
0004949
Arg of perigee: 344
0507 deg
Mean anomaly: 16
0498 deg
Mean motion: 15
72586923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 299
Coasting Arc #13 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2011/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2746159
50 A = 6728974
76 meter
Y = -4647285
16 meter E =
0009293
Z = -4027794
48 I = 51
77702
XDOT = 6598
176560 Wp = 38
70499
YDOT = -502
479479 meter/sec RA = 23
42962 deg
ZDOT = -3916
634204 TA = 190
86777
MA = 190
88786
Ha = 192
634 n
mi
Hp = 186
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9009709
66 X = -2674422
55
Y = -15246998
57 feet Y = -4677593
44 meter
Z = -13214548
83 Z = -4040960
72
XDOT = 21647
560892 XDOT = 6622
331031
YDOT = -1648
554721 feet/sec YDOT = -428
559774 meter/sec
ZDOT = -12849
849750 ZDOT = -3884
522012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -803228
13 X = -244823
93
Y = -17652111
84 feet Y = -5380363
69 meter
Z = -13267550
89 Z = -4043949
51
XDOT = 18705
679128 XDOT = 5701
490998
YDOT = 8715
028076 feet/sec YDOT = 2656
340558 meter/sec
ZDOT = -12720
193752 ZDOT = -3877
115056
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 11054
52297033
00016717 00000-0 10270-3 0 9122
2 25544 51
6430 23
8218 0004971 347
5941 12
5099 15
72636050 23016
Satellite: ISS
Catalog Number: 25544
Epoch time: 11054
52297033 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 23
8218 deg
Eccentricity:
0004971
Arg of perigee: 347
5941 deg
Mean anomaly: 12
5099 deg
Mean motion: 15
72636050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 282
Coasting Arc #14 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2011/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442638
43 A = 6730010
00 meter
Y = 1303500
02 meter E =
0012496
Z = 3733972
86 I = 51
75203
XDOT = -4117
330468 Wp = 59
83924
YDOT = -4905
111811 meter/sec RA = 18
26254 deg
ZDOT = -4272
332907 TA = 75
19337
MA = 75
05496
Ha = 192
733 n
mi
Hp = 185
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17856425
29 X = -5474948
58
Y = 4276574
86 feet Y = 1242456
57 meter
Z = 12250567
13 Z = 3707454
43
XDOT = -13508
302061 XDOT = -4041
420675
YDOT = -16092
886519 feet/sec YDOT = -4950
729951 meter/sec
ZDOT = -14016
840245 ZDOT = -4292
150092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17934348
44 X = -5466389
40
Y = -4255910
12 feet Y = -1297201
41 meter
Z = 12143466
83 Z = 3701328
69
XDOT = -5048
320702 XDOT = -1538
728150
YDOT = -19106
963013 feet/sec YDOT = -5823
802326 meter/sec
ZDOT = -14096
678655 ZDOT = -4296
667654
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 11055
53967499
00016717 00000-0 10270-3 0 9135
2 25544 51
6430 18
6116 0005071 350
2645 9
8419 15
72672993 23177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
53967499 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 18
6116 deg
Eccentricity:
0005071
Arg of perigee: 350
2645 deg
Mean anomaly: 9
8419 deg
Mean motion: 15
72672993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 316
Coasting Arc #15 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2011/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4374442
10 A = 6730658
95 meter
Y = 3794077
83 meter E =
0012701
Z = 3416031
63 I = 51
72631
XDOT = -5688
051377 Wp = 68
17826
YDOT = 2400
896977 meter/sec RA = 13
19613 deg
ZDOT = 4608
319840 TA = 332
15376
MA = 332
22168
Ha = 192
566 n
mi
Hp = 185
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14351844
17 X = 4315096
74
Y = 12447761
91 feet Y = 3842663
72 meter
Z = 11207452
86 Z = 3437138
06
XDOT = -18661
585883 XDOT = -5736
861867
YDOT = 7876
958586 feet/sec YDOT = 2337
016893 meter/sec
ZDOT = 15119
159580 ZDOT = 4580
569230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7448557
16 X = 2270320
22
Y = 17422024
69 feet Y = 5310233
13 meter
Z = 11292531
13 Z = 3441963
49
XDOT = -19040
900128 XDOT = -5803
666359
YDOT = -1605
479215 feet/sec YDOT = -489
350065 meter/sec
ZDOT = 15007
045838 ZDOT = 4574
147571
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 11056
55635879
00016717 00000-0 10270-3 0 9143
2 25544 51
6437 13
4014 0004905 353
3373 6
7723 15
72724880 23336
Satellite: ISS
Catalog Number: 25544
Epoch time: 11056
55635879 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 13
4014 deg
Eccentricity:
0004905
Arg of perigee: 353
3373 deg
Mean anomaly: 6
7723 deg
Mean motion: 15
72724880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2333
Checksum: 303
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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