Date:
May 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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 1816)
---------------------------------------
Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 159580
32 A = 6722766
01 meter
Y = -4848492
37 meter E =
0011192
Z = -4661693
18 I = 51
86667
XDOT = 6494
943516 Wp = 14
89170
YDOT = 2972
481020 meter/sec RA = 42
91336 deg
ZDOT = -2860
179463 TA = 226
85856
MA = 226
95219
Ha = 190
648 n
mi
Hp = 185
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 523557
47 X = 236431
31
Y = -15907127
19 feet Y = -4846277
63 meter
Z = -15294268
96 Z = -4660731
79
XDOT = 21308
869804 XDOT = 6475
116498
YDOT = 9752
234318 feet/sec YDOT = 3045
000803 meter/sec
ZDOT = -9383
790890 ZDOT = -2828
674197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12039781
72 X = -3669725
47
Y = -10414954
13 feet Y = -3174478
02 meter
Z = -15290449
88 Z = -4660529
12
XDOT = 20199
949649 XDOT = 6156
944653
YDOT = -9715
247099 feet/sec YDOT = -2961
207316 meter/sec
ZDOT = -9258
310962 ZDOT = -2821
933181
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 10134
52079172
00016717 00000-0 10270-3 0 9009
2 25544 51
6472 43
3640 0010257 314
4872 45
5452 15
73992491 18173
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
52079172 = yrday
fracday
Element set: 900
Inclination: 51
6472 deg
RA of node: 43
3640 deg
Eccentricity:
0010257
Arg of perigee: 314
4872 deg
Mean anomaly: 45
5452 deg
Mean motion: 15
73992491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 296
Coasting Arc #2 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5892961
82 A = 6729622
16 meter
Y = -2098704
63 meter E =
0007623
Z = 2481995
02 I = 51
86612
XDOT = -288
321139 Wp = 58
63674
YDOT = -5529
788318 meter/sec RA = 37
75149 deg
ZDOT = -5344
509594 TA = 93
40222
MA = 93
31502
Ha = 190
827 n
mi
Hp = 185
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19333864
25 X = -5881113
03
Y = -6885513
89 feet Y = -2164537
31 meter
Z = 8143028
27 Z = 2453395
02
XDOT = -945
935496 XDOT = -200
501521
YDOT = -18142
350125 feet/sec YDOT = -5532
520775 meter/sec
ZDOT = -17534
480295 ZDOT = -5345
697685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17293585
75 X = -5271084
94
Y = 11134749
15 feet Y = 3393871
54 meter
Z = 8029120
20 Z = 2447275
84
XDOT = -14064
474462 XDOT = -4286
851816
YDOT = -9158
402486 feet/sec YDOT = -2791
481078 meter/sec
ZDOT = -17539
213999 ZDOT = -5345
952427
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 10135
53663536
00016717 00000-0 10270-3 0 9015
2 25544 51
6468 38
1481 0010226 317
9225 42
1152 15
73983237 18335
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
53663536 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 38
1481 deg
Eccentricity:
0010226
Arg of perigee: 317
9225 deg
Mean anomaly: 42
1152 deg
Mean motion: 15
73983237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 294
Coasting Arc #3 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 646617
75 A = 6722575
57 meter
Y = 4783511
13 meter E =
0004512
Z = 4676469
52 I = 51
81877
XDOT = -6934
585139 Wp = 7
55375
YDOT = -1814
113539 meter/sec RA = 32
67267 deg
ZDOT = 2818
562129 TA = 54
72212
MA = 54
67992
Ha = 190
987 n
mi
Hp = 184
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2121449
31 X = 570361
90
Y = 15693934
14 feet Y = 4790314
97 meter
Z = 15342747
77 Z = 4679426
27
XDOT = -22751
263581 XDOT = -6927
476225
YDOT = -5951
816072 feet/sec YDOT = -1891
620843 meter/sec
ZDOT = 9247
251078 ZDOT = 2784
890519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13799739
63 X = 4206160
64
Y = 7746349
25 feet Y = 2361087
25 meter
Z = 15354520
00 Z = 4680057
70
XDOT = -17831
049289 XDOT = -5434
903823
YDOT = 13727
901609 feet/sec YDOT = 4184
264410 meter/sec
ZDOT = 9113
140379 ZDOT = 2777
685187
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 10136
55246048
00016717 00000-0 10270-3 0 9024
2 25544 51
6473 32
9315 0010320 321
9620 38
0814 15
74022411 18493
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
55246048 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 32
9315 deg
Eccentricity:
0010320
Arg of perigee: 321
9620 deg
Mean anomaly: 38
0814 deg
Mean motion: 15
74022411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 271
Coasting Arc #4 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6174079
85 A = 6729486
19 meter
Y = 1051447
92 meter E =
0012514
Z = -2440009
08 I = 51
81636
XDOT = 1202
204302 Wp = 350
83474
YDOT = 5390
408113 meter/sec RA = 27
50714 deg
ZDOT = 5373
180149 TA = 341
65983
MA = 341
70491
Ha = 191
189 n
mi
Hp = 184
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20256167
49 X = 6173716
70
Y = 3449632
29 feet Y = 1120488
46 meter
Z = -8005279
12 Z = -2410015
93
XDOT = 3944
239836 XDOT = 1115
736327
YDOT = 17685
065989 feet/sec YDOT = 5403
367665 meter/sec
ZDOT = 17628
543796 ZDOT = 5378
811212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14647611
92 X = 4464592
11
Y = -14476124
15 feet Y = -4412322
64 meter
Z = -7885814
63 Z = -2403596
30
XDOT = 15548
111441 XDOT = 4739
064367
YDOT = 6132
147550 feet/sec YDOT = 1869
078573 meter/sec
ZDOT = 17650
963910 ZDOT = 5380
013800
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 10137
50478077
00016717 00000-0 10270-3 0 9030
2 25544 51
6475 28
0411 0010440 325
2141 34
8339 15
74060825 18640
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
50478077 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 28
0411 deg
Eccentricity:
0010440
Arg of perigee: 325
2141 deg
Mean anomaly: 34
8339 deg
Mean motion: 15
74060825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 284
Coasting Arc #5 (Orbit 1879)
---------------------------------------
Vector Time (GMT): 2010/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1417970
71 A = 6722262
36 meter
Y = -4596264
28 meter E =
0013676
Z = -4705890
59 I = 51
76503
XDOT = 7159
251211 Wp = 21
64896
YDOT = 613
417431 meter/sec RA = 22
42408 deg
ZDOT = -2746
408765 TA = 221
26443
MA = 221
36787
Ha = 191
226 n
mi
Hp = 184
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4652134
89 X = -1343608
65
Y = -15079607
23 feet Y = -4611704
51 meter
Z = -15439273
59 Z = -4712599
06
XDOT = 23488
356993 XDOT = 7165
201362
YDOT = 2012
524381 feet/sec YDOT = 693
510053 meter/sec
ZDOT = -9010
527445 ZDOT = -2711
614502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14993679
92 X = -4570073
64
Y = -4837449
92 feet Y = -1474454
73 meter
Z = -15465986
00 Z = -4714032
53
XDOT = 14706
091670 XDOT = 4482
416741
YDOT = -17112
762481 feet/sec YDOT = -5215
970004 meter/sec
ZDOT = -8871
934586 ZDOT = -2704
165662
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 10138
52057246
00016717 00000-0 10270-3 0 9045
2 25544 51
6474 22
8246 0010567 328
8487 31
2049 15
74094635 18802
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
52057246 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 22
8246 deg
Eccentricity:
0010567
Arg of perigee: 328
8487 deg
Mean anomaly: 31
2049 deg
Mean motion: 15
74094635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1880
Checksum: 311
Coasting Arc #6 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2010/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6307342
00 A = 6729587
97 meter
Y = -21768
36 meter E =
0010030
Z = 2347833
14 I = 51
76103
XDOT = -2005
466065 Wp = 58
51987
YDOT = -5089
300993 meter/sec RA = 17
25522 deg
ZDOT = -5412
736565 TA = 95
11117
MA = 94
99669
Ha = 191
398 n
mi
Hp = 184
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20693379
25 X = -6318035
15
Y = -71418
50 feet Y = -92360
84 meter
Z = 7702864
63 Z = 2317166
08
XDOT = -6579
613074 XDOT = -1922
113430
YDOT = -16697
181735 feet/sec YDOT = -5111
260697 meter/sec
ZDOT = -17758
322065 ZDOT = -5422
277188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11573017
77 X = -3527455
82
Y = 17209104
70 feet Y = 5245335
11 meter
Z = 7580708
66 Z = 2310600
00
XDOT = -16227
699269 XDOT = -4946
202737
YDOT = -3041
285818 feet/sec YDOT = -926
983917 meter/sec
ZDOT = -17796
315184 ZDOT = -5424
316868
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 10139
53634861
00016717 00000-0 10270-3 0 9052
2 25544 51
6473 17
6078 0010464 333
0369 27
0250 15
74094560 18960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
53634861 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 17
6078 deg
Eccentricity:
0010464
Arg of perigee: 333
0369 deg
Mean anomaly: 27
0250 deg
Mean motion: 15
74094560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 306
Coasting Arc #7 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2010/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2064159
53 A = 6721970
56 meter
Y = 4280986
83 meter E =
0006479
Z = 4749262
43 I = 51
70665
XDOT = -7218
858368 Wp = 19
76646
YDOT = 568
225155 meter/sec RA = 12
16566 deg
ZDOT = 2630
260508 TA = 44
47410
MA = 44
42210
Ha = 191
525 n
mi
Hp = 183
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6772176
94 X = 1993064
27
Y = 14045232
37 feet Y = 4303671
59 meter
Z = 15581569
66 Z = 4759117
78
XDOT = -23683
918529 XDOT = -7237
453180
YDOT = 1864
255757 feet/sec YDOT = 487
395402 meter/sec
ZDOT = 8629
463609 ZDOT = 2595
146141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15427185
62 X = 4702206
18
Y = 1976922
65 feet Y = 602566
02 meter
Z = 15620818
37 Z = 4761225
44
XDOT = -11123
132323 XDOT = -3390
330732
YDOT = 19847
538634 feet/sec YDOT = 6049
529776 meter/sec
ZDOT = 8489
592673 ZDOT = 2587
627847
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 10140
55210643
00016717 00000-0 10270-3 0 9065
2 25544 51
6474 12
3903 0010593 336
7806 23
2878 15
74115187 19121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
55210643 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 12
3903 deg
Eccentricity:
0010593
Arg of perigee: 336
7806 deg
Mean anomaly: 23
2878 deg
Mean motion: 15
74115187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 290
Coasting Arc #8 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2010/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6252367
40 A = 6729637
20 meter
Y = -1018995
89 meter E =
0014575
Z = -2244784
51 I = 51
70229
XDOT = 2724
502309 Wp =
91244
YDOT = 4689
717403 meter/sec RA = 6
99346 deg
ZDOT = 5474
446482 TA = 333
89949
MA = 333
97290
Ha = 191
736 n
mi
Hp = 183
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20513016
41 X = 6274202
10
Y = -3343162
38 feet Y = -948955
97 meter
Z = -7364778
58 Z = -2214357
42
XDOT = 8938
655869 XDOT = 2645
264579
YDOT = 15386
211952 feet/sec YDOT = 4719
741030 meter/sec
ZDOT = 17960
782420 ZDOT = 5487
489986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7974752
48 X = 2430704
56
Y = -19238877
28 feet Y = -5864009
80 meter
Z = -7243580
90 Z = -2207843
46
XDOT = 16329
031419 XDOT = 4977
088776
YDOT = 5
214666 feet/sec YDOT = 1
589430 meter/sec
ZDOT = 18012
728428 ZDOT = 5490
279625
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 10141
50436327
00016717 00000-0 10270-3 0 9071
2 25544 51
6470 7
4993 0010774 339
3463 20
7264 15
74145764 19271
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
50436327 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 7
4993 deg
Eccentricity:
0010774
Arg of perigee: 339
3463 deg
Mean anomaly: 20
7264 deg
Mean motion: 15
74145764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 306
Coasting Arc #9 (Orbit 1942)
---------------------------------------
Vector Time (GMT): 2010/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2648586
02 A = 6721560
64 meter
Y = -3894479
00 meter E =
0016119
Z = -4807902
34 I = 51
64463
XDOT = 7070
152470 Wp = 30
10283
YDOT = -1731
160497 meter/sec RA = 1
89836 deg
ZDOT = -2482
450734 TA = 215
53646
MA = 215
64392
Ha = 191
717 n
mi
Hp = 183
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8689586
69 X = -2581484
29
Y = -12777162
08 feet Y = -3923721
61 meter
Z = -15773957
82 Z = -4820606
51
XDOT = 23196
038287 XDOT = 7101
044544
YDOT = -5679
660424 feet/sec YDOT = -1651
924974 meter/sec
ZDOT = -8144
523405 ZDOT = -2448
028701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15376716
95 X = -4686823
33
Y = 850116
22 feet Y = 259115
42 meter
Z = -15824550
91 Z = -4823323
12
XDOT = 7071
790700 XDOT = 2155
481805
YDOT = -21756
473822 feet/sec YDOT = -6631
373221 meter/sec
ZDOT = -8007
417131 ZDOT = -2440
660742
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 10142
52008846
00016717 00000-0 10270-3 0 9086
2 25544 51
6462 2
2821 0010761 342
9012 17
1787 15
74184057 19437
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
52008846 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 2
2821 deg
Eccentricity:
0010761
Arg of perigee: 342
9012 deg
Mean anomaly: 17
1787 deg
Mean motion: 15
74184057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1943
Checksum: 287
Coasting Arc #10 (Orbit 1958)
---------------------------------------
Vector Time (GMT): 2010/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6080598
26 A = 6729691
25 meter
Y = 1997873
66 meter E =
0012047
Z = 2081332
58 I = 51
64256
XDOT = -3289
010780 Wp = 62
30274
YDOT = -4205
106456 meter/sec RA = 356
72400 deg
ZDOT = -5542
444263 TA = 94
47054
MA = 94
33290
Ha = 191
852 n
mi
Hp = 182
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19949469
35 X = -6112597
79
Y = 6554703
62 feet Y = 1929697
74 meter
Z = 6828518
95 Z = 2051715
03
XDOT = -10790
717781 XDOT = -3214
819520
YDOT = -13796
281022 feet/sec YDOT = -4241
470949 meter/sec
ZDOT = -18183
872254 ZDOT = -5558
242552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4239419
15 X = -1292174
96
Y = 20605095
19 feet Y = 6280433
01 meter
Z = 6710552
54 Z = 2045376
41
XDOT = -15778
395041 XDOT = -4809
254808
YDOT = 2728
665612 feet/sec YDOT = 831
697279 meter/sec
ZDOT = -18246
783697 ZDOT = -5561
619671
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 10143
53579690
00016717 00000-0 10270-3 0 9099
2 25544 51
6467 357
0651 0010847 347
0504 13
0379 15
74234480 19596
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
53579690 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 357
0651 deg
Eccentricity:
0010847
Arg of perigee: 347
0504 deg
Mean anomaly: 13
0379 deg
Mean motion: 15
74234480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1959
Checksum: 319
Coasting Arc #11 (Orbit 1974)
---------------------------------------
Vector Time (GMT): 2010/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3079467
53 A = 6721195
21 meter
Y = 3451115
36 meter E =
0008096
Z = 4870863
30 I = 51
58250
XDOT = -6789
625358 Wp = 27
50428
YDOT = 2835
247817 meter/sec RA = 351
62095 deg
ZDOT = 2289
269179 TA = 40
24298
MA = 40
18308
Ha = 191
971 n
mi
Hp = 182
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10103239
92 X = 3016985
48
Y = 11322556
94 feet Y = 3485202
03 meter
Z = 15980522
64 Z = 4885672
13
XDOT = -22275
673746 XDOT = -6831
946033
YDOT = 9301
994150 feet/sec YDOT = 2759
085361 meter/sec
ZDOT = 7510
725654 ZDOT = 2256
182048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14743997
50 X = 4493970
44
Y = -3316947
74 feet Y = -1011005
67 meter
Z = 16039490
38 Z = 4888836
67
XDOT = -2841
076840 XDOT = -865
960221
YDOT = 22965
215118 feet/sec YDOT = 6999
797568 meter/sec
ZDOT = 7378
940903 ZDOT = 2249
101187
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 10144
55149043
00016717 00000-0 10270-3 0 9109
2 25544 51
6456 351
8469 0010802 351
0402 9
0566 15
74196643 19755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
55149043 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 351
8469 deg
Eccentricity:
0010802
Arg of perigee: 351
0402 deg
Mean anomaly: 9
0566 deg
Mean motion: 15
74196643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1975
Checksum: 298
Coasting Arc #12 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2010/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5729656
20 A = 6729927
03 meter
Y = -2944098
69 meter E =
0016593
Z = -1915237
64 I = 51
58137
XDOT = 3765
015236 Wp = 10
91571
YDOT = 3682
579758 meter/sec RA = 346
44345 deg
ZDOT = 5626
536238 TA = 327
75437
MA = 327
85571
Ha = 192
079 n
mi
Hp = 182
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18798084
65 X = 5771455
85
Y = -9659116
42 feet Y = -2879792
33 meter
Z = -6283588
06 Z = -1887301
23
XDOT = 12352
412193 XDOT = 3696
222922
YDOT = 12081
954587 feet/sec YDOT = 3724
297143 meter/sec
ZDOT = 18459
764560 ZDOT = 5644
660339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 243649
05 X = 74264
23
Y = -21165848
50 feet Y = -6451350
62 meter
Z = -6172316
24 Z = -1881321
99
XDOT = 14855
576070 XDOT = 4527
979586
YDOT = -5209
926499 feet/sec YDOT = -1587
985597 meter/sec
ZDOT = 18531
930251 ZDOT = 5648
532340
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 10145
50368478
00016717 00000-0 10270-3 0 9111
2 25544 51
6445 346
9549 0010775 353
6170 6
4854 15
74248386 19906
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
50368478 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 346
9549 deg
Eccentricity:
0010775
Arg of perigee: 353
6170 deg
Mean anomaly: 6
4854 deg
Mean motion: 15
74248386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1990
Checksum: 331
Coasting Arc #13 (Orbit 2005)
---------------------------------------
Vector Time (GMT): 2010/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3450036
13 A = 6720665
87 meter
Y = -2986486
84 meter E =
0018533
Z = -4948830
15 I = 51
52041
XDOT = 6318
571879 Wp = 40
17751
YDOT = -3865
212192 meter/sec RA = 341
33365 deg
ZDOT = -2062
760817 TA = 209
72814
MA = 209
83358
Ha = 192
088 n
mi
Hp = 182
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11319016
16 X = -3392343
31
Y = -9798185
17 feet Y = -3024743
95 meter
Z = -16236319
37 Z = -4965451
00
XDOT = 20730
222699 XDOT = 6371
344468
YDOT = -12681
142362 feet/sec YDOT = -3794
258814 meter/sec
ZDOT = -6767
587981 ZDOT = -2031
936955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13808794
79 X = -4208920
65
Y = 5593599
56 feet Y = 1704929
15 meter
Z = -16302498
48 Z = -4969001
54
XDOT = -1536
250277 XDOT = -468
249084
YDOT = -23250
428547 feet/sec YDOT = -7086
730621 meter/sec
ZDOT = -6644
809531 ZDOT = -2025
337945
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 10146
51934428
00016717 00000-0 10270-3 0 9128
2 25544 51
6434 341
7370 0010730 357
9682 2
1436 15
74282875 20064
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
51934428 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 341
7370 deg
Eccentricity:
0010730
Arg of perigee: 357
9682 deg
Mean anomaly: 2
1436 deg
Mean motion: 15
74282875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2006
Checksum: 296
Coasting Arc #14 (Orbit 2021)
---------------------------------------
Vector Time (GMT): 2010/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5297341
10 A = 6729971
17 meter
Y = 3797985
70 meter E =
0013621
Z = 1676387
39 I = 51
52475
XDOT = -4082
725364 Wp = 69
38201
YDOT = -3156
028551 meter/sec RA = 336
15501 deg
ZDOT = -5709
021708 TA = 92
06624
MA = 91
91025
Ha = 192
167 n
mi
Hp = 181
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17379728
03 X = -5347560
87
Y = 12460583
02 feet Y = 3738466
63 meter
Z = 5499958
61 Z = 1650531
09
XDOT = -13394
768254 XDOT = -4019
396809
YDOT = -10354
424380 feet/sec YDOT = -3201
329039 meter/sec
ZDOT = -18730
386181 ZDOT = -5728
702571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3626097
19 X = 1105234
42
Y = 21102010
84 feet Y = 6431892
90 meter
Z = 5396960
08 Z = 1644993
43
XDOT = -13570
726687 XDOT = -4136
357494
YDOT = 7178
356881 feet/sec YDOT = 2187
963177 meter/sec
ZDOT = -18808
750383 ZDOT = -5732
907117
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 10147
53498491
00016717 00000-0 10270-3 0 9137
2 25544 51
6441 336
5187 0010968
8547 359
2633 15
74361383 20222
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
53498491 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 336
5187 deg
Eccentricity:
0010968
Arg of perigee:
8547 deg
Mean anomaly: 359
2633 deg
Mean motion: 15
74361383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2022
Checksum: 313
Coasting Arc #15 (Orbit 2037)
---------------------------------------
Vector Time (GMT): 2010/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3674028
36 A = 6720256
76 meter
Y = 2534089
73 meter E =
0009383
Z = 5017474
06 I = 51
46333
XDOT = -5750
573441 Wp = 34
69565
YDOT = 4810
084968 meter/sec RA = 331
03592 deg
ZDOT = 1787
457241 TA = 38
09036
MA = 38
02406
Ha = 192
271 n
mi
Hp = 181
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12053898
81 X = 3621044
38
Y = 8313942
70 feet Y = 2574877
81 meter
Z = 16461529
05 Z = 5035194
43
XDOT = -18866
710765 XDOT = -5812
616527
YDOT = 15781
118661 feet/sec YDOT = 4745
431428 meter/sec
ZDOT = 5864
361027 ZDOT = 1759
370728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12569749
91 X = 3831259
77
Y = -7354687
90 feet Y = -2241708
87 meter
Z = 16532090
36 Z = 5038981
14
XDOT = 5839
381307 XDOT = 1779
843422
YDOT = 22866
730433 feet/sec YDOT = 6969
779436 meter/sec
ZDOT = 5752
469529 ZDOT = 1753
352712
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 10148
55061349
00016717 00000-0 10270-3 0 9149
2 25544 51
6430 331
2997 0010798 5
8778 354
2510 15
74295585 20389
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
55061349 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 331
2997 deg
Eccentricity:
0010798
Arg of perigee: 5
8778 deg
Mean anomaly: 354
2510 deg
Mean motion: 15
74295585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2038
Checksum: 322
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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