Date:
November 14th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 3417)
---------------------------------------
Vector Time (GMT): 2007/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3585345
05 A = 6714039
04 meter
Y = 2075565
35 meter E =
0002999
Z = 5281504
27 I = 51
89721
XDOT = -3956
720749 Wp = 128
63570
YDOT = -6613
079854 meter/sec RA = 58
58852 deg
ZDOT = -88
958991 TA = 322
19425
MA = 322
21531
Ha = 187
081 n
mi
Hp = 180
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11762943
07 X = -3633945
18
Y = 6809597
60 feet Y = 2035199
76 meter
Z = 17327769
93 Z = 5263968
31
XDOT = -12981
367286 XDOT = -3882
046057
YDOT = -21696
456215 feet/sec YDOT = -6656
908610 meter/sec
ZDOT = -291
860206 ZDOT = -108
000511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2290082
41 X = 698017
12
Y = -13483114
18 feet Y = -4109653
20 meter
Z = 17261234
44 Z = 5261224
26
XDOT = 24014
196939 XDOT = 7319
527227
YDOT = 3619
027780 feet/sec YDOT = 1103
079667 meter/sec
ZDOT = -365
041296 ZDOT = -111
264587
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 07316
54738543
00020000 00000-0 20000-3 0 9005
2 25544 51
6422 58
9536 0002104 181
2448 178
8711 15
76128195 34187
Satellite: ISS
Catalog Number: 25544
Epoch time: 07316
54738543 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 58
9536 deg
Eccentricity:
0002104
Arg of perigee: 181
2448 deg
Mean anomaly: 178
8711 deg
Mean motion: 15
76128195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3418
Checksum: 294
Coasting Arc #2 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2007/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3461345
59 A = 6725857
97 meter
Y = 5706877
95 meter E =
0012434
Z = 786450
27 I = 51
92100
XDOT = -4461
120889 Wp = 60
56573
YDOT = 1870
563858 meter/sec RA = 53
46521 deg
ZDOT = 5996
180707 TA = 307
98353
MA = 308
09576
Ha = 186
964 n
mi
Hp = 180
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11356120
71 X = 3393452
64
Y = 18723352
87 feet Y = 5745204
99 meter
Z = 2580217
42 Z = 803101
57
XDOT = -14636
223390 XDOT = -4510
835325
YDOT = 6137
020530 feet/sec YDOT = 1820
398499 meter/sec
ZDOT = 19672
508881 ZDOT = 5974
387482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21712457
08 X = -6617956
92
Y = -2785740
26 feet Y = -849093
63 meter
Z = 2644201
40 Z = 805952
59
XDOT = 4178
415933 XDOT = 1273
581176
YDOT = -13776
838773 feet/sec YDOT = -4199
180458 meter/sec
ZDOT = 19589
738446 ZDOT = 5970
952278
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 07317
56185685
00020000 00000-0 20000-3 0 9012
2 25544 51
6424 53
7282 0001987 181
3788 178
7371 15
76126555 34343
Satellite: ISS
Catalog Number: 25544
Epoch time: 07317
56185685 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 53
7282 deg
Eccentricity:
0001987
Arg of perigee: 181
3788 deg
Mean anomaly: 178
7371 deg
Mean motion: 15
76126555 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3434
Checksum: 317
Coasting Arc #3 (Orbit 3448)
---------------------------------------
Vector Time (GMT): 2007/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4248732
78 A = 6714881
72 meter
Y = -1212628
26 meter E =
0013881
Z = -5068764
59 I = 51
86598
XDOT = 3891
409504 Wp = 110
71751
YDOT = 6408
482442 meter/sec RA = 48
31009 deg
ZDOT = 1727
695284 TA = 175
87601
MA = 175
86456
Ha = 186
807 n
mi
Hp = 180
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13939412
01 X = 4286600
44
Y = -3978439
18 feet Y = -1164904
28 meter
Z = -16629805
09 Z = -5048031
97
XDOT = 12767
091547 XDOT = 3811
066663
YDOT = 21025
204863 feet/sec YDOT = 6451
548990 meter/sec
ZDOT = 5668
291614 ZDOT = 1746
405636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5393590
16 X = -1643966
28
Y = 13552093
79 feet Y = 4130678
19 meter
Z = -16550998
22 Z = -5044744
26
XDOT = -23443
285818 XDOT = -7145
513517
YDOT = -2315
656844 feet/sec YDOT = -705
812206 meter/sec
ZDOT = 5740
186180 ZDOT = 1749
608748
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 07318
51289969
00020000 00000-0 20000-3 0 9029
2 25544 51
6422 48
8296 0001910 184
6845 175
4302 15
76189889 34490
Satellite: ISS
Catalog Number: 25544
Epoch time: 07318
51289969 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 48
8296 deg
Eccentricity:
0001910
Arg of perigee: 184
6845 deg
Mean anomaly: 175
4302 deg
Mean motion: 15
76189889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3449
Checksum: 331
Coasting Arc #4 (Orbit 3464)
---------------------------------------
Vector Time (GMT): 2007/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3258565
92 A = 6723755
58 meter
Y = -5445212
09 meter E =
0007354
Z = -2214355
50 I = 51
87521
XDOT = 5305
562250 Wp = 148
47288
YDOT = -942
566765 meter/sec RA = 43
20866 deg
ZDOT = -5503
950995 TA = 56
28687
MA = 56
21679
Ha = 186
722 n
mi
Hp = 180
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10690833
07 X = -3186677
43
Y = -17864869
06 feet Y = -5481249
06 meter
Z = -7264945
86 Z = -2230011
77
XDOT = 17406
700294 XDOT = 5342
445495
YDOT = -3092
410646 feet/sec YDOT = -883
030223 meter/sec
ZDOT = -18057
582003 ZDOT = -5478
086637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20693863
14 X = 6307489
49
Y = 2081736
61 feet Y = 634513
32 meter
Z = -7325114
17 Z = -2232694
80
XDOT = -7789
067614 XDOT = -2374
107809
YDOT = 14398
274943 feet/sec YDOT = 4388
594203 meter/sec
ZDOT = -17959
204421 ZDOT = -5473
965507
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 07319
52732236
00020000 00000-0 20000-3 0 9032
2 25544 51
6415 43
6034 0001904 189
4186 170
6943 15
76197515 34650
Satellite: ISS
Catalog Number: 25544
Epoch time: 07319
52732236 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 43
6034 deg
Eccentricity:
0001904
Arg of perigee: 189
4186 deg
Mean anomaly: 170
6943 deg
Mean motion: 15
76197515 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3465
Checksum: 294
Coasting Arc #5 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2007/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5020063
26 A = 6717268
51 meter
Y = 494155
37 meter E =
0008432
Z = 4429732
10 I = 51
83232
XDOT = -3503
833098 Wp = 78
06711
YDOT = -6024
809101 meter/sec RA = 38
02748 deg
ZDOT = -3291
736217 TA = 44
86842
MA = 44
80028
Ha = 186
683 n
mi
Hp = 180
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16470023
82 X = -5046735
02
Y = 1621244
65 feet Y = 437868
70 meter
Z = 14533241
80 Z = 4405279
53
XDOT = -11495
515415 XDOT = -3420
211470
YDOT = -19766
434057 feet/sec YDOT = -6063
523136 meter/sec
ZDOT = -10799
659504 ZDOT = -3308
555437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8306624
61 X = 2531859
18
Y = -14407850
16 feet Y = -4391512
73 meter
Z = 14440189
67 Z = 4401369
81
XDOT = 21679
282618 XDOT = 6607
845342
YDOT = 1587
172837 feet/sec YDOT = 483
770281 meter/sec
ZDOT = -10864
316436 ZDOT = -3311
443650
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 07320
54171931
00020000 00000-0 20000-3 0 9046
2 25544 51
6420 38
3766 0001668 194
8716 165
2399 15
76269527 34811
Satellite: ISS
Catalog Number: 25544
Epoch time: 07320
54171931 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 38
3766 deg
Eccentricity:
0001668
Arg of perigee: 194
8716 deg
Mean anomaly: 165
2399 deg
Mean motion: 15
76269527 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3481
Checksum: 309
Coasting Arc #6 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2007/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2759057
67 A = 6720343
12 meter
Y = 5042443
82 meter E =
0011983
Z = 3473836
46 I = 51
81917
XDOT = -6209
364132 Wp = 99
52131
YDOT = 247
415827 meter/sec RA = 32
93772 deg
ZDOT = 4557
393421 TA = 301
62710
MA = 301
74396
Ha = 186
460 n
mi
Hp = 180
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9052026
46 X = 2685591
73
Y = 16543450
85 feet Y = 5072886
19 meter
Z = 11397101
23 Z = 3487061
99
XDOT = -20371
929568 XDOT = -6233
808578
YDOT = 811
731717 feet/sec YDOT = 177
842252 meter/sec
ZDOT = 14952
078153 ZDOT = 4527
168548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18721994
12 X = -5706463
81
Y = -1987374
65 feet Y = -605751
79 meter
Z = 11447975
54 Z = 3489342
94
XDOT = 10794
689524 XDOT = 3290
221367
YDOT = -15938
724024 feet/sec YDOT = -4858
123083 meter/sec
ZDOT = 14837
020192 ZDOT = 4522
323754
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 07321
55609262
00020000 00000-0 20000-3 0 9052
2 25544 51
6417 33
1499 0001696 197
7607 162
3498 15
76297175 34970
Satellite: ISS
Catalog Number: 25544
Epoch time: 07321
55609262 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 33
1499 deg
Eccentricity:
0001696
Arg of perigee: 197
7607 deg
Mean anomaly: 162
3498 deg
Mean motion: 15
76297175 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3497
Checksum: 324
Coasting Arc #7 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2007/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5789316
63 A = 6720551
41 meter
Y = 5240
96 meter E =
0004626
Z = -3418377
90 I = 51
79431
XDOT = 2716
788825 Wp = 108
38124
YDOT = 5531
811698 meter/sec RA = 27
74548 deg
ZDOT = 4613
237011 TA = 211
29964
MA = 211
32719
Ha = 186
429 n
mi
Hp = 180
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18993820
97 X = 5805433
87
Y = 17194
76 feet Y = 70070
64 meter
Z = -11215150
60 Z = -3390213
82
XDOT = 8913
349164 XDOT = 2632
318733
YDOT = 18148
988510 feet/sec YDOT = 5561
719885 meter/sec
ZDOT = 15135
292032 ZDOT = 4626
230421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10556832
98 X = -3217722
69
Y = 15865455
51 feet Y = 4835790
84 meter
Z = -11107913
06 Z = -3385691
90
XDOT = -18845
572794 XDOT = -5744
130588
YDOT = -1916
501040 feet/sec YDOT = -584
149517 meter/sec
ZDOT = 15185
332768 ZDOT = 4628
489428
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 07322
50704667
00020000 00000-0 20000-3 0 9064
2 25544 51
6411 28
2502 0001555 199
0827 161
0279 15
76331625 35127
Satellite: ISS
Catalog Number: 25544
Epoch time: 07322
50704667 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 28
2502 deg
Eccentricity:
0001555
Arg of perigee: 199
0827 deg
Mean anomaly: 161
0279 deg
Mean motion: 15
76331625 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3512
Checksum: 273
Coasting Arc #8 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2007/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1885379
96 A = 6716690
40 meter
Y = -4627500
01 meter E =
0009033
Z = -4497030
98 I = 51
75518
XDOT = 7011
073467 Wp = 75
86327
YDOT = 219
594357 meter/sec RA = 22
65044 deg
ZDOT = -3168
478162 TA = 162
54106
MA = 162
50999
Ha = 186
368 n
mi
Hp = 180
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6185629
77 X = -1811648
24
Y = -15182086
65 feet Y = -4648171
02 meter
Z = -14754038
64 Z = -4506011
36
XDOT = 23002
209539 XDOT = 7023
489035
YDOT = 720
453926 feet/sec YDOT = 298
065658 meter/sec
ZDOT = -10395
269561 ZDOT = -3134
387555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16077811
76 X = 4900517
02
Y = 3039339
72 feet Y = 926390
75 meter
Z = -14788705
50 Z = -4507597
44
XDOT = -12810
393043 XDOT = -3904
607800
YDOT = 17866
212972 feet/sec YDOT = 5445
621714 meter/sec
ZDOT = -10265
446141 ZDOT = -3128
907984
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 07323
52137421
00020000 00000-0 20000-3 0 9076
2 25544 51
6410 23
0228 0001451 202
9946 157
1154 15
76335492 35286
Satellite: ISS
Catalog Number: 25544
Epoch time: 07323
52137421 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 23
0228 deg
Eccentricity:
0001451
Arg of perigee: 202
9946 deg
Mean anomaly: 157
1154 deg
Mean motion: 15
76335492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3528
Checksum: 264
Coasting Arc #9 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2007/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6389861
23 A = 6723550
02 meter
Y = -321249
23 meter E =
0013997
Z = 2043892
38 I = 51
75233
XDOT = -1535
692596 Wp = 115
90332
YDOT = -5092
665250 meter/sec RA = 17
46347 deg
ZDOT = -5578
133796 TA = 41
29842
MA = 41
19265
Ha = 186
256 n
mi
Hp = 180
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20964111
64 X = -6395723
16
Y = -1053967
28 feet Y = -392737
10 meter
Z = 6705683
68 Z = 2012835
45
XDOT = -5038
361536 XDOT = -1451
533291
YDOT = -16708
219323 feet/sec YDOT = -5109
367546 meter/sec
ZDOT = -18300
963899 ZDOT = -5585
390060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11907285
73 X = 3629340
69
Y = -17331868
82 feet Y = -5282753
62 meter
Z = 6587403
68 Z = 2007840
64
XDOT = 15551
553561 XDOT = 4740
113525
YDOT = 3688
080440 feet/sec YDOT = 1124
126918 meter/sec
ZDOT = -18329
110540 ZDOT = -5586
712893
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 07324
53567655
00020000 00000-0 20000-3 0 9085
2 25544 51
6417 17
7957 0001192 210
0173 150
0923 15
76418815 35441
Satellite: ISS
Catalog Number: 25544
Epoch time: 07324
53567655 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 17
7957 deg
Eccentricity:
0001192
Arg of perigee: 210
0173 deg
Mean anomaly: 150
0923 deg
Mean motion: 15
76418815 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3544
Checksum: 288
Coasting Arc #10 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2007/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 726979
81 A = 6713828
96 meter
Y = 4291480
16 meter E =
0004807
Z = 5109892
30 I = 51
69148
XDOT = -7551
957057 Wp = 139
69316
YDOT = -469
081407 meter/sec RA = 12
34649 deg
ZDOT = 1463
999191 TA = 296
27246
MA = 296
32185
Ha = 186
167 n
mi
Hp = 180
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2385104
36 X = 654114
14
Y = 14079659
31 feet Y = 4299202
07 meter
Z = 16764738
51 Z = 5113247
22
XDOT = -24776
761998 XDOT = -7553
262485
YDOT = -1538
980993 feet/sec YDOT = -553
539020 meter/sec
ZDOT = 4803
146952 ZDOT = 1427
307526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13282097
03 X = -4048383
17
Y = -5202733
70 feet Y = -1585793
23 meter
Z = 16777945
25 Z = 5113917
71
XDOT = 13582
418941 XDOT = 4139
921293
YDOT = -19589
839641 feet/sec YDOT = -5970
983123 meter/sec
ZDOT = 4663
401727 ZDOT = 1421
404847
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 07325
54995636
00020000 00000-0 20000-3 0 9092
2 25544 51
6414 12
5686 0001207 209
7048 150
4048 15
76437307 35600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07325
54995636 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 12
5686 deg
Eccentricity:
0001207
Arg of perigee: 209
7048 deg
Mean anomaly: 150
4048 deg
Mean motion: 15
76437307 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3560
Checksum: 294
Coasting Arc #11 (Orbit 3574)
---------------------------------------
Vector Time (GMT): 2007/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6687631
88 A = 6725202
58 meter
Y = 472034
96 meter E =
0010430
Z = -465375
83 I = 51
70096
XDOT = 74
193514 Wp = 41
80104
YDOT = 4803
418806 meter/sec RA = 7
17988 deg
ZDOT = 6022
957150 TA = 313
13669
MA = 313
22386
Ha = 186
219 n
mi
Hp = 180
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21941049
49 X = 6684117
26
Y = 1548671
14 feet Y = 546800
23 meter
Z = -1526823
58 Z = -432894
74
XDOT = 243
417042 XDOT = -8
783959
YDOT = 15759
248051 feet/sec YDOT = 4803
784158 meter/sec
ZDOT = 19760
358104 ZDOT = 6023
116331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12202780
52 X = -3719407
50
Y = 18310178
92 feet Y = 5580942
53 meter
Z = -1403111
08 Z = -427668
26
XDOT = -12426
477652 XDOT = -3787
590388
YDOT = -6790
427496 feet/sec YDOT = -2069
722301 meter/sec
ZDOT = 19761
442985 ZDOT = 6023
287822
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 07326
50082287
00020000 00000-0 20000-3 0 9100
2 25544 51
6413 7
6678 0000927 216
1684 143
9418 15
76424402 35757
Satellite: ISS
Catalog Number: 25544
Epoch time: 07326
50082287 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 7
6678 deg
Eccentricity:
0000927
Arg of perigee: 216
1684 deg
Mean anomaly: 143
9418 deg
Mean motion: 15
76424402 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3575
Checksum: 289
Coasting Arc #12 (Orbit 3590)
---------------------------------------
Vector Time (GMT): 2007/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 638086
00 A = 6713125
46 meter
Y = -4141745
35 meter E =
0014434
Z = -5256891
45 I = 51
63236
XDOT = 7656
835092 Wp = 96
75071
YDOT = 619
911853 meter/sec RA = 2
02765 deg
ZDOT = 440
347865 TA = 177
43885
MA = 177
43145
Ha = 186
102 n
mi
Hp = 180
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2093458
02 X = 709890
09
Y = -13588403
38 feet Y = -4134207
92 meter
Z = -17247019
21 Z = -5253617
52
XDOT = 25120
850040 XDOT = 7647
194862
YDOT = 2033
831539 feet/sec YDOT = 705
480976 meter/sec
ZDOT = 1444
710842 ZDOT = 477
522676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10872907
67 X = 3314062
26
Y = 8439368
69 feet Y = 2572319
58 meter
Z = -17234960
97 Z = -5253216
10
XDOT = -13213
324931 XDOT = -4027
421439
YDOT = 20267
299368 feet/sec YDOT = 6177
472847 meter/sec
ZDOT = 1586
309587 ZDOT = 483
507162
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 07327
51505718
00020000 00000-0 20000-3 0 9112
2 25544 51
6419 2
4399 0001019 216
2474 143
8622 15
76478043 35911
Satellite: ISS
Catalog Number: 25544
Epoch time: 07327
51505718 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 2
4399 deg
Eccentricity:
0001019
Arg of perigee: 216
2474 deg
Mean anomaly: 143
8622 deg
Mean motion: 15
76478043 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3591
Checksum: 285
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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