Date:
July 8th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6260737
17 A = 6731051
78 meter
Y = 2186426
59 meter E =
0018001
Z = 1085435
56 I = 51
50400
XDOT = -686
069538 Wp = 146
50947
YDOT = 4910
269103 meter/sec RA = 206
73044 deg
ZDOT = -5902
151140 TA = 21
57988
MA = 21
50410
Ha = 190
880 n
mi
Hp = 183
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20540476
27 X = 6230550
07
Y = 7173315
60 feet Y = 2256268
82 meter
Z = 3561140
30 Z = 1115777
02
XDOT = -2250
884312 XDOT = -712
254732
YDOT = 16109
806768 feet/sec YDOT = 4902
451828 meter/sec
ZDOT = -19364
012927 ZDOT = -5905
546666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2057771
29 X = 627208
69
Y = -21639550
76 feet Y = -6595735
07 meter
Z = 3680320
97 Z = 1121761
83
XDOT = 14575
374701 XDOT = 4442
574209
YDOT = -1926
543976 feet/sec YDOT = -587
210604 meter/sec
ZDOT = -19377
062186 ZDOT = -5906
128554
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 09187
53393670
00010596 00000-0 82463-4 0 9001
2 25544 51
6368 207
5647 0007615 192
2231 167
8748 15
74205203 9000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53393670 = yrday
fracday
Element set: 900
Inclination: 51
6368 deg
RA of node: 207
5647 deg
Eccentricity:
0007615
Arg of perigee: 192
2231 deg
Mean anomaly: 167
8748 deg
Mean motion: 15
74205203 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 311
Coasting Arc #2 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 312529
67 A = 6719947
04 meter
Y = -4292869
83 meter E =
0009603
Z = 5161158
13 I = 51
49314
XDOT = 7365
546929 Wp = 173
13486
YDOT = 1931
703710 meter/sec RA = 201
60355 deg
ZDOT = 1151
104438 TA = 265
79854
MA = 265
90829
Ha = 190
763 n
mi
Hp = 183
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1025359
81 X = 335438
42
Y = -14084218
61 feet Y = -4289247
82 meter
Z = 16932933
51 Z = 5162731
22
XDOT = 24165
180213 XDOT = 7337
807087
YDOT = 6337
610598 feet/sec YDOT = 2013
914245 meter/sec
ZDOT = 3776
589363 ZDOT = 1186
818762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13852366
00 X = -4222201
16
Y = 2706967
80 feet Y = 825083
78 meter
Z = 16938863
47 Z = 5162965
59
XDOT = 147
779902 XDOT = 45
043314
YDOT = -23950
631235 feet/sec YDOT = -7300
152401 meter/sec
ZDOT = 3916
858817 ZDOT = 1193
858567
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 09188
54962998
00010596 00000-0 82463-4 0 9019
2 25544 51
6361 202
3462 0007542 196
3449 163
7473 15
74219562 9166
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
54962998 = yrday
fracday
Element set: 901
Inclination: 51
6361 deg
RA of node: 202
3462 deg
Eccentricity:
0007542
Arg of perigee: 196
3449 deg
Mean anomaly: 163
7473 deg
Mean motion: 15
74219562 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 916
Checksum: 335
Coasting Arc #3 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6563344
72 A = 6730968
13 meter
Y = -1182570
35 meter E =
0003676
Z = -911210
01 I = 51
55986
XDOT = 60
682980 Wp = 80
65005
YDOT = -4895
444824 meter/sec RA = 196
43982 deg
ZDOT = 5937
121526 TA = 269
39719
MA = 269
43931
Ha = 190
561 n
mi
Hp = 183
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21533283
20 X = -6545206
79
Y = -3879823
99 feet Y = -1255863
94 meter
Z = -2989534
14 Z = -943050
37
XDOT = 199
091142 XDOT = 86
579174
YDOT = -16061
170684 feet/sec YDOT = -4894
622467 meter/sec
ZDOT = 19478
745165 ZDOT = 5937
478372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2128091
83 X = 648642
39
Y = 21758751
88 feet Y = 6632067
57 meter
Z = -3114574
68 Z = -949322
36
XDOT = -13890
099821 XDOT = -4233
702425
YDOT = 4137
459400 feet/sec YDOT = 1261
097625 meter/sec
ZDOT = 19479
863239 ZDOT = 5937
462315
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 09189
50183316
00010596 00000-0 82463-4 0 9026
2 25544 51
6368 197
4548 0007646 199
8184 160
2683 15
74284009 9311
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50183316 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 197
4548 deg
Eccentricity:
0007646
Arg of perigee: 199
8184 deg
Mean anomaly: 160
2683 deg
Mean motion: 15
74284009 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 337
Coasting Arc #4 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187088
80 A = 6719723
18 meter
Y = 4254091
17 meter E =
0012333
Z = -5207320
88 I = 51
54957
XDOT = -7599
339784 Wp = 113
92989
YDOT = -778
683118 meter/sec RA = 191
31269 deg
ZDOT = -915
787050 TA = 147
36611
MA = 147
28984
Ha = 190
395 n
mi
Hp = 184
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 613808
41 X = 164800
72
Y = 13956992
02 feet Y = 4256059
49 meter
Z = -17084386
09 Z = -5206465
50
XDOT = -24932
217138 XDOT = -7585
618967
YDOT = -2554
734638 feet/sec YDOT = -863
586522 meter/sec
ZDOT = -3004
550688 ZDOT = -952
670812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13155405
21 X = 4009767
51
Y = -4715182
79 feet Y = -1437187
72 meter
Z = -17080778
67 Z = -5206221
34
XDOT = 4408
803023 XDOT = 1343
803161
YDOT = 23630
594395 feet/sec YDOT = 7202
605172 meter/sec
ZDOT = -3149
380442 ZDOT = -959
931159
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 09190
51750705
00010596 00000-0 82463-4 0 9032
2 25544 51
6360 192
2358 0007488 204
9277 155
1525 15
74238333 9474
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
51750705 = yrday
fracday
Element set: 903
Inclination: 51
6360 deg
RA of node: 192
2358 deg
Eccentricity:
0007488
Arg of perigee: 204
9277 deg
Mean anomaly: 155
1525 deg
Mean motion: 15
74238333 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 947
Checksum: 316
Coasting Arc #5 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6682757
85 A = 6731174
63 meter
Y = 167948
77 meter E =
0016241
Z = 693926
18 I = 51
61777
XDOT = 504
491900 Wp = 154
22936
YDOT = 4825
315437 meter/sec RA = 186
15598 deg
ZDOT = -5988
484841 TA = 18
20184
MA = 18
14378
Ha = 190
150 n
mi
Hp = 184
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21925058
56 X = 6677012
23
Y = 551013
04 feet Y = 242647
06 meter
Z = 2276660
68 Z = 726376
55
XDOT = 1655
157152 XDOT = 479
587402
YDOT = 15831
087392 feet/sec YDOT = 4830
818516 meter/sec
ZDOT = -19647
259977 ZDOT = -5986
093903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6166010
19 X = -1879399
91
Y = -21033206
66 feet Y = -6410921
39 meter
Z = 2404064
90 Z = 732758
98
XDOT = 13000
607480 XDOT = 3962
585160
YDOT = -6069
180030 feet/sec YDOT = -1849
886073 meter/sec
ZDOT = -19637
585848 ZDOT = -5985
536167
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 09191
53317084
00010596 00000-0 82463-4 0 9045
2 25544 51
6357 187
0171 0007334 208
8616 151
2143 15
74272086 9639
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
53317084 = yrday
fracday
Element set: 904
Inclination: 51
6357 deg
RA of node: 187
0171 deg
Eccentricity:
0007334
Arg of perigee: 208
8616 deg
Mean anomaly: 151
2143 deg
Mean motion: 15
74272086 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 963
Checksum: 304
Coasting Arc #6 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2009/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -683616
60 A = 6719499
80 meter
Y = -4160324
79 meter E =
0007698
Z = 5234144
92 I = 51
60779
XDOT = 7660
094136 Wp = 190
47964
YDOT = -398
465829 meter/sec RA = 181
02932 deg
ZDOT = 676
462325 TA = 253
04264
MA = 253
12704
Ha = 190
039 n
mi
Hp = 184
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2242836
62 X = -662470
50
Y = -13649359
56 feet Y = -4167851
76 meter
Z = 17172391
46 Z = 5230874
84
XDOT = 25131
542441 XDOT = 7660
694450
YDOT = -1307
302589 feet/sec YDOT = -312
802894 meter/sec
ZDOT = 2219
364584 ZDOT = 713
675948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12169955
66 X = -3709402
49
Y = 6608851
05 feet Y = 2014377
80 meter
Z = 17159301
50 Z = 5230155
10
XDOT = -8836
089359 XDOT = -2693
240037
YDOT = -22475
093578 feet/sec YDOT = -6850
408523 meter/sec
ZDOT = 2365
447499 ZDOT = 720
988398
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 09192
54882444
00010596 00000-0 82463-4 0 9055
2 25544 51
6353 181
7985 0007362 213
7123 146
3573 15
74270696 9792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
54882444 = yrday
fracday
Element set: 905
Inclination: 51
6353 deg
RA of node: 181
7985 deg
Eccentricity:
0007362
Arg of perigee: 213
7123 deg
Mean anomaly: 146
3573 deg
Mean motion: 15
74270696 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 979
Checksum: 337
Coasting Arc #7 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6658110
15 A = 6731098
70 meter
Y = 855932
82 meter E =
0003801
Z = -475134
03 I = 51
67755
XDOT = -1029
845072 Wp = 51
60324
YDOT = -4691
674682 meter/sec RA = 175
88150 deg
ZDOT = 6014
155556 TA = 303
23355
MA = 303
26998
Ha = 189
826 n
mi
Hp = 184
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21844193
41 X = -6664878
40
Y = 2808178
53 feet Y = 781440
14 meter
Z = -1558838
69 Z = -507495
14
XDOT = -3378
756799 XDOT = -1006
520786
YDOT = -15392
633471 feet/sec YDOT = -4703
061211 meter/sec
ZDOT = 19731
481484 ZDOT = 6009
208800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10021525
81 X = 3054561
07
Y = 19601315
11 feet Y = 5974480
84 meter
Z = -1685851
95 Z = -513847
68
XDOT = -11876
923435 XDOT = -3620
086263
YDOT = 7758
600995 feet/sec YDOT = 2364
821583 meter/sec
ZDOT = 19711
772852 ZDOT = 6008
148365
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 09193
50098962
00010596 00000-0 82463-4 0 9067
2 25544 51
6354 176
9067 0007417 215
9640 144
1025 15
74335922 9948
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
50098962 = yrday
fracday
Element set: 906
Inclination: 51
6354 deg
RA of node: 176
9067 deg
Eccentricity:
0007417
Arg of perigee: 215
9640 deg
Mean anomaly: 144
1025 deg
Mean motion: 15
74335922 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 994
Checksum: 325
Coasting Arc #8 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1100602
06 A = 6719301
01 meter
Y = 4038357
41 meter E =
0011093
Z = -5264734
67 I = 51
66722
XDOT = -7527
961666 Wp = 114
72849
YDOT = 1542
520908 meter/sec RA = 170
75372 deg
ZDOT = -395
731492 TA = 151
54257
MA = 151
48196
Ha = 189
624 n
mi
Hp = 184
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3610899
15 X = 1080937
61
Y = 13249204
10 feet Y = 4050555
54 meter
Z = -17272751
53 Z = -5259435
35
XDOT = -24698
036962 XDOT = -7542
728524
YDOT = 5060
764133 feet/sec YDOT = 1458
256305 meter/sec
ZDOT = -1298
331668 ZDOT = -432
337805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11076606
70 X = 3376149
72
Y = -8161843
90 feet Y = -2487730
02 meter
Z = -17251696
60 Z = -5258317
12
XDOT = 12879
679439 XDOT = 3925
726293
YDOT = 20491
086668 feet/sec YDOT = 6245
683217 meter/sec
ZDOT = -1441
982448 ZDOT = -439
516250
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 09194
51662286
00010596 00000-0 82463-4 0 9076
2 25544 51
6356 171
6874 0007280 221
5484 138
5126 15
74302391 10108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51662286 = yrday
fracday
Element set: 907
Inclination: 51
6356 deg
RA of node: 171
6874 deg
Eccentricity:
0007280
Arg of perigee: 221
5484 deg
Mean anomaly: 138
5126 deg
Mean motion: 15
74302391 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 304
Coasting Arc #9 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6462885
64 A = 6731192
65 meter
Y = -1835252
99 meter E =
0014174
Z = 218133
79 I = 51
73726
XDOT = 1495
658718 Wp = 163
22815
YDOT = 4538
541844 meter/sec RA = 165
61451 deg
ZDOT = -6045
197334 TA = 14
40318
MA = 14
36282
Ha = 189
354 n
mi
Hp = 184
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21203693
03 X = 6481867
76
Y = -6021171
21 feet Y = -1762875
10 meter
Z = 715662
03 Z = 249576
33
XDOT = 4907
016792 XDOT = 1474
163202
YDOT = 14890
229146 feet/sec YDOT = 4555
147592 meter/sec
ZDOT = -19833
324585 ZDOT = -6037
983202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13439456
13 X = -4096346
23
Y = -17465403
64 feet Y = -5323455
03 meter
Z = 839027
79 Z = 255735
67
XDOT = 10700
233855 XDOT = 3261
431279
YDOT = -9196
371199 feet/sec YDOT = -2803
053941 meter/sec
ZDOT = -19804
719588 ZDOT = -6036
478530
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 09195
53224486
00010596 00000-0 82463-4 0 9086
2 25544 51
6359 166
4690 0007223 226
6083 133
4480 15
74337370 10266
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
53224486 = yrday
fracday
Element set: 908
Inclination: 51
6359 deg
RA of node: 166
4690 deg
Eccentricity:
0007223
Arg of perigee: 226
6083 deg
Mean anomaly: 133
4480 deg
Mean motion: 15
74337370 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 312
Coasting Arc #10 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1502933
83 A = 6719130
68 meter
Y = -3883853
05 meter E =
0005871
Z = 5275775
12 I = 51
72514
XDOT = 7228
763905 Wp = 213
74803
YDOT = -2649
083566 meter/sec RA = 160
48692 deg
ZDOT = 104
389451 TA = 235
23478
MA = 235
29006
Ha = 189
224 n
mi
Hp = 185
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4930885
26 X = -1485020
99
Y = -12742300
04 feet Y = -3900560
17 meter
Z = 17308973
48 Z = 5268516
94
XDOT = 23716
417012 XDOT = 7257
342045
YDOT = -8691
219048 feet/sec YDOT = -2568
087519 meter/sec
ZDOT = 342
485076 ZDOT = 139
575924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9812063
22 X = -2990716
87
Y = 9560191
87 feet Y = 2913946
48 meter
Z = 17280235
81 Z = 5267015
87
XDOT = -16474
647530 XDOT = -5021
472567
YDOT = -17805
341566 feet/sec YDOT = -5427
068109 meter/sec
ZDOT = 480
517363 ZDOT = 146
461692
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 09196
54785648
00010596 00000-0 82463-4 0 9091
2 25544 51
6358 161
2508 0007261 230
8693 129
1825 15
74341687 10421
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196
54785648 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 161
2508 deg
Eccentricity:
0007261
Arg of perigee: 230
8693 deg
Mean anomaly: 129
1825 deg
Mean motion: 15
74341687 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 332
Coasting Arc #11 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2009/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6130509
38 A = 6731089
57 meter
Y = 2771819
37 meter E =
0005188
Z = 46912
72 I = 51
79331
XDOT = -1921
309534 Wp = 33
92975
YDOT = -4357
133599 meter/sec RA = 155
35614 deg
ZDOT = 6049
224996 TA = 326
57866
MA = 326
61140
Ha = 188
980 n
mi
Hp = 185
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20113219
73 X = -6161276
59
Y = 9093895
56 feet Y = 2703092
39 meter
Z = 153913
14 Z = 17056
28
XDOT = -6303
508970 XDOT = -1901
830623
YDOT = -14295
057739 feet/sec YDOT = -4378
510689 meter/sec
ZDOT = 19846
538702 ZDOT = 6039
937997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16409856
70 X = 5001724
32
Y = 14764128
22 feet Y = 4500106
28 meter
Z = 36807
27 Z = 11218
85
XDOT = -9433
885818 XDOT = -2875
448397
YDOT = 10425
289543 feet/sec YDOT = 3177
628253 meter/sec
ZDOT = 19809
805970 ZDOT = 6038
028860
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 09197
56345553
00010596 00000-0 82463-4 0 9103
2 25544 51
6356 156
0318 0007289 234
0808 125
9680 15
74381654 10582
Satellite: ISS
Catalog Number: 25544
Epoch time: 09197
56345553 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 156
0318 deg
Eccentricity:
0007289
Arg of perigee: 234
0808 deg
Mean anomaly: 125
9680 deg
Mean motion: 15
74381654 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1058
Checksum: 325
Coasting Arc #12 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2009/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1846114
03 A = 6719041
00 meter
Y = 3733917
82 meter E =
0009707
Z = -5279746
03 I = 51
77991
XDOT = -6762
504293 Wp = 115
50400
YDOT = 3665
618803 meter/sec RA = 150
22584 deg
ZDOT = 224
031645 TA = 156
64170
MA = 156
59757
Ha = 188
761 n
mi
Hp = 185
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6056804
56 X = 1829871
60
Y = 12250386
55 feet Y = 3754472
15 meter
Z = -17322001
41 Z = -5270816
47
XDOT = -22186
693875 XDOT = -6804
079568
YDOT = 12026
308409 feet/sec YDOT = 3589
764028 meter/sec
ZDOT = 735
011959 ZDOT = 191
078930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8560286
04 X = 2609175
18
Y = -10709796
76 feet Y = -3264346
05 meter
Z = -17286709
96 Z = -5268989
20
XDOT = 19412
139210 XDOT = 5916
820031
YDOT = 14518
200118 feet/sec YDOT = 4425
147396 meter/sec
ZDOT = 605
778177 ZDOT = 184
641188
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 09198
51557084
00010596 00000-0 82463-4 0 9114
2 25544 51
6363 151
1389 0007284 239
1257 120
9191 15
74375356 10734
Satellite: ISS
Catalog Number: 25544
Epoch time: 09198
51557084 = yrday
fracday
Element set: 911
Inclination: 51
6363 deg
RA of node: 151
1389 deg
Eccentricity:
0007284
Arg of perigee: 239
1257 deg
Mean anomaly: 120
9191 deg
Mean motion: 15
74375356 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1073
Checksum: 318
Coasting Arc #13 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2009/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5657903
36 A = 6731014
59 meter
Y = -3615085
58 meter E =
0011914
Z = -345781
44 I = 51
84642
XDOT = 2305
021440 Wp = 173
80692
YDOT = 4182
853303 meter/sec RA = 145
10493 deg
ZDOT = -6045
517324 TA = 9
94319
MA = 9
91963
Ha = 188
556 n
mi
Hp = 185
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18562675
06 X = 5699587
09
Y = -11860516
98 feet Y = -3551582
46 meter
Z = -1134453
53 Z = -318194
77
XDOT = 7562
406298 XDOT = 2287
444720
YDOT = 13723
271993 feet/sec YDOT = 4208
532195 meter/sec
ZDOT = -19834
374424 ZDOT = -6034
361502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18732639
57 X = -5709708
54
Y = -11600289
80 feet Y = -3535768
33 meter
Z = -1026277
13 Z = -312809
27
XDOT = 8198
033484 XDOT = 2498
760606
YDOT = -11497
560078 feet/sec YDOT = -3504
456312 meter/sec
ZDOT = -19790
311230 ZDOT = -6032
086863
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 09199
53114917
00010596 00000-0 82463-4 0 9122
2 25544 51
6370 145
9203 0007287 243
2066 116
8353 15
74394323 10891
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199
53114917 = yrday
fracday
Element set: 912
Inclination: 51
6370 deg
RA of node: 145
9203 deg
Eccentricity:
0007287
Arg of perigee: 243
2066 deg
Mean anomaly: 116
8353 deg
Mean motion: 15
74394323 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1089
Checksum: 313
Coasting Arc #14 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2009/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2177472
02 A = 6718970
55 meter
Y = -3571979
86 meter E =
0004540
Z = 5261228
82 I = 51
83045
XDOT = 6156
920767 Wp = 247
95840
YDOT = -4587
590796 meter/sec RA = 139
97314 deg
ZDOT = -568
514017 TA = 207
41897
MA = 207
44294
Ha = 188
311 n
mi
Hp = 185
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7143937
08 X = -2162925
61
Y = -11719094
02 feet Y = -3596249
29 meter
Z = 17261249
40 Z = 5250685
39
XDOT = 20199
871283 XDOT = 6210
524111
YDOT = -15051
150907 feet/sec YDOT = -4518
440686 meter/sec
ZDOT = -1865
203468 ZDOT = -538
474579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7224514
08 X = -2202031
89
Y = 11730928
47 feet Y = 3575587
00 meter
Z = 17219623
86 Z = 5248541
35
XDOT = -21661
899149 XDOT = -6602
546861
YDOT = -10785
438885 feet/sec YDOT = -3287
401772 meter/sec
ZDOT = -1747
423913 ZDOT = -532
614809
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 09200
54671557
00010596 00000-0 82463-4 0 9135
2 25544 51
6375 140
7021 0007316 247
6889 112
3500 15
74427985 11056
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200
54671557 = yrday
fracday
Element set: 913
Inclination: 51
6375 deg
RA of node: 140
7021 deg
Eccentricity:
0007316
Arg of perigee: 247
6889 deg
Mean anomaly: 112
3500 deg
Mean motion: 15
74427985 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1105
Checksum: 301
Coasting Arc #15 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5072953
57 A = 6730769
58 meter
Y = 4368141
04 meter E =
0006889
Z = 656161
50 I = 51
89245
XDOT = -2667
515995 Wp = 30
69639
YDOT = -4004
302791 meter/sec RA = 134
86045 deg
ZDOT = 6012
106141 TA = 336
42505
MA = 336
45660
Ha = 188
013 n
mi
Hp = 185
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16643548
47 X = -5124609
31
Y = 14331171
39 feet Y = 4311123
36 meter
Z = 2152760
81 Z = 631392
79
XDOT = -8751
692898 XDOT = -2651
746250
YDOT = -13137
476349 feet/sec YDOT = -4034
045479 meter/sec
ZDOT = 19724
757682 ZDOT = 5999
185077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20421967
36 X = 6224615
65
Y = 8108147
78 feet Y = 2471363
44 meter
Z = 2055662
20 Z = 626565
84
XDOT = -6934
540808 XDOT = -2113
648038
YDOT = 12459
176708 feet/sec YDOT = 3797
557061 meter/sec
ZDOT = 19673
760225 ZDOT = 5996
562117
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 09201
56227128
00010596 00000-0 82463-4 0 9140
2 25544 51
6376 135
4826 0007317 251
6777 108
3590 15
74434787 11213
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
56227128 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 135
4826 deg
Eccentricity:
0007317
Arg of perigee: 251
6777 deg
Mean anomaly: 108
3590 deg
Mean motion: 15
74434787 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1121
Checksum: 313
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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