Date:
January 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 554)
---------------------------------------
Vector Time (GMT): 2008/023/13:37:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231129
59 A = 6711604
48 meter
Y = -1296797
32 meter E =
0009485
Z = -5053575
02 I = 51
85613
XDOT = 4040
404571 Wp = 81
41941
YDOT = 6311
880907 meter/sec RA = 46
70270 deg
ZDOT = 1767
343535 TA = 205
52586
MA = 205
57273
Ha = 184
768 n
mi
Hp = 179
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13881658
77 X = 4269864
69
Y = -4254584
38 feet Y = -1249265
47 meter
Z = -16579970
53 Z = -5032926
85
XDOT = 13255
920507 XDOT = 3960
938698
YDOT = 20708
270693 feet/sec YDOT = 6356
618560 meter/sec
ZDOT = 5798
371179 ZDOT = 1786
778655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13961650
11 X = 4255510
96
Y = 4299152
25 feet Y = 1310381
61 meter
Z = -16501120
49 Z = -5029541
52
XDOT = -324
333089 XDOT = -98
856726
YDOT = 23543
460570 feet/sec YDOT = 7176
046782 meter/sec
ZDOT = 5873
324771 ZDOT = 1790
189390
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 08023
58065239
00020000 00000-0 20000-3 0 9000
2 25544 51
6372 47
2194 0005784 320
8473 39
2273 15
77356894 5550
Satellite: ISS
Catalog Number: 25544
Epoch time: 08023
58065239 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 47
2194 deg
Eccentricity:
0005784
Arg of perigee: 320
8473 deg
Mean anomaly: 39
2273 deg
Mean motion: 15
77356894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 555
Checksum: 302
Coasting Arc #2 (Orbit 570)
---------------------------------------
Vector Time (GMT): 2008/024/13:37:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3019120
16 A = 6719481
06 meter
Y = -5411460
98 meter E =
0001913
Z = -2601851
60 I = 51
86183
XDOT = 5582
711875 Wp = 24
19944
YDOT = -579
655177 meter/sec RA = 41
59309 deg
ZDOT = -5272
085552 TA = 185
28663
MA = 185
28865
Ha = 184
786 n
mi
Hp = 179
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9905249
85 X = -2945745
04
Y = -17754137
07 feet Y = -5444812
12 meter
Z = -8536258
53 Z = -2616340
07
XDOT = 18315
983843 XDOT = 5614
388823
YDOT = -1901
755831 feet/sec YDOT = -517
048762 meter/sec
ZDOT = -17296
868610 ZDOT = -5244
888636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1424747
57 X = 434263
06
Y = -20256730
69 feet Y = -6174251
51 meter
Z = -8592207
14 Z = -2618904
74
XDOT = 14992
520846 XDOT = 4569
720354
YDOT = 8347
612033 feet/sec YDOT = 2544
352148 meter/sec
ZDOT = -17192
899133 ZDOT = -5240
395656
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 08024
59429294
00020000 00000-0 20000-3 0 9018
2 25544 51
6366 41
9863 0005734 325
8140 34
2655 15
77415522 5719
Satellite: ISS
Catalog Number: 25544
Epoch time: 08024
59429294 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 41
9863 deg
Eccentricity:
0005734
Arg of perigee: 325
8140 deg
Mean anomaly: 34
2655 deg
Mean motion: 15
77415522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 571
Checksum: 289
Coasting Arc #3 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2008/025/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5889901
83 A = 6718939
79 meter
Y = -1605633
22 meter E =
0010687
Z = 2801192
95 I = 51
83757
XDOT = -902
744315 Wp = 75
07162
YDOT = -5675
151020 meter/sec RA = 36
38525 deg
ZDOT = -5132
258113 TA = 72
89521
MA = 72
77820
Ha = 184
870 n
mi
Hp = 179
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19323824
89 X = -5885116
97
Y = -5267825
54 feet Y = -1671470
77 meter
Z = 9190265
59 Z = 2772592
15
XDOT = -2961
759564 XDOT = -814
285891
YDOT = -18619
261878 feet/sec YDOT = -5684
751303 meter/sec
ZDOT = -16838
117170 ZDOT = -5136
428803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13876442
70 X = -4229539
74
Y = -14512276
86 feet Y = -4423341
99 meter
Z = 9080712
21 Z = 2767801
08
XDOT = 6096
645991 XDOT = 1858
257698
YDOT = -16415
106170 feet/sec YDOT = -5003
324361 meter/sec
ZDOT = -16854
628316 ZDOT = -5137
290711
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 08025
60790534
00020000 00000-0 20000-3 0 9020
2 25544 51
6365 36
7536 0005946 329
4423 30
6394 15
77484445 5873
Satellite: ISS
Catalog Number: 25544
Epoch time: 08025
60790534 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 36
7536 deg
Eccentricity:
0005946
Arg of perigee: 329
4423 deg
Mean anomaly: 30
6394 deg
Mean motion: 15
77484445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 587
Checksum: 305
Coasting Arc #4 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2008/026/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -134628
86 A = 6711391
33 meter
Y = 4500408
18 meter E =
0002875
Z = 4974665
95 I = 51
78832
XDOT = -7036
457840 Wp = 46
74251
YDOT = -2426
427325 meter/sec RA = 31
27518 deg
ZDOT = 2005
889854 TA = 23
92411
MA = 23
91076
Ha = 184
954 n
mi
Hp = 179
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -441695
74 X = -209108
60
Y = 14765118
69 feet Y = 4498486
18 meter
Z = 16321082
51 Z = 4973831
08
XDOT = -23085
491602 XDOT = -7018
546230
YDOT = -7960
719570 feet/sec YDOT = -2505
012875 meter/sec
ZDOT = 6581
003457 ZDOT = 1971
750980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7864202
33 X = -2397008
87
Y = 12507913
88 feet Y = 3812412
15 meter
Z = 16318332
37 Z = 4973827
71
XDOT = -15103
911260 XDOT = -4603
672152
YDOT = -17906
395338 feet/sec YDOT = -5457
869299 meter/sec
ZDOT = 6450
189198 ZDOT = 1966
017667
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 08026
62149186
00020000 00000-0 20000-3 0 9035
2 25544 51
6366 31
5211 0005913 332
9498 27
1358 15
77509036 6036
Satellite: ISS
Catalog Number: 25544
Epoch time: 08026
62149186 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 31
5211 deg
Eccentricity:
0005913
Arg of perigee: 332
9498 deg
Mean anomaly: 27
1358 deg
Mean motion: 15
77509036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 603
Checksum: 283
Coasting Arc #5 (Orbit 617)
---------------------------------------
Vector Time (GMT): 2008/027/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6196732
53 A = 6721911
19 meter
Y = 2511744
31 meter E =
0014557
Z = -598243
58 I = 51
79871
XDOT = -1303
816039 Wp = 19
84288
YDOT = 4637
347962 meter/sec RA = 26
10192 deg
ZDOT = 6020
691802 TA = 333
64572
MA = 333
71970
Ha = 184
988 n
mi
Hp = 178
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20330487
31 X = 6171091
38
Y = 8240630
92 feet Y = 2580896
33 meter
Z = -1962741
41 Z = -568202
65
XDOT = -4277
611675 XDOT = -1384
821577
YDOT = 15214
396202 feet/sec YDOT = 4622
314958 meter/sec
ZDOT = 19752
925858 ZDOT = 6014
161270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13765364
93 X = 4195683
23
Y = 17093571
40 feet Y = 5210120
56 meter
Z = -1847596
15 Z = -563147
31
XDOT = -9988
494412 XDOT = -3044
493097
YDOT = 10155
034163 feet/sec YDOT = 3095
254413 meter/sec
ZDOT = 19728
403502 ZDOT = 6013
217387
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 08027
57170366
00020000 00000-0 20000-3 0 9045
2 25544 51
6367 26
6156 0005723 337
8050 22
2867 15
77565518 6181
Satellite: ISS
Catalog Number: 25544
Epoch time: 08027
57170366 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 26
6156 deg
Eccentricity:
0005723
Arg of perigee: 337
8050 deg
Mean anomaly: 22
2867 deg
Mean motion: 15
77565518 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 618
Checksum: 298
Coasting Arc #6 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2008/028/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2196809
45 A = 6710096
17 meter
Y = -3584980
53 meter E =
0013489
Z = -5240010
12 I = 51
73288
XDOT = 6945
014031 Wp = 71
85806
YDOT = 3246
547838 meter/sec RA = 20
94747 deg
ZDOT = 696
043093 TA = 204
72272
MA = 204
78743
Ha = 185
087 n
mi
Hp = 178
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7207380
09 X = 2262188
63
Y = -11761747
13 feet Y = -3560048
90 meter
Z = -17191634
24 Z = -5229179
44
XDOT = 22785
479104 XDOT = 6904
813266
YDOT = 10651
403669 feet/sec YDOT = 3323
986150 meter/sec
ZDOT = 2283
605947 ZDOT = 729
683891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11985471
64 X = 3653171
76
Y = -6931381
31 feet Y = -2112685
02 meter
Z = -17150560
74 Z = -5227490
91
XDOT = 14559
856907 XDOT = 4437
844385
YDOT = 19252
143709 feet/sec YDOT = 5868
053403 meter/sec
ZDOT = 2412
587546 ZDOT = 735
356684
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 08028
58523575
00020000 00000-0 20000-3 0 9052
2 25544 51
6374 21
3824 0005885 341
3631 18
7318 15
77578888 6340
Satellite: ISS
Catalog Number: 25544
Epoch time: 08028
58523575 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 21
3824 deg
Eccentricity:
0005885
Arg of perigee: 341
3631 deg
Mean anomaly: 18
7318 deg
Mean motion: 15
77578888 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 634
Checksum: 314
Coasting Arc #7 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2008/029/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5692034
67 A = 6720364
37 meter
Y = -3087611
35 meter E =
0002988
Z = -1800099
75 I = 51
74126
XDOT = 3746
897690 Wp = 88
94840
YDOT = -3597
906461 meter/sec RA = 15
81448 deg
ZDOT = -5684
671680 TA = 110
99469
MA = 110
96272
Ha = 185
112 n
mi
Hp = 178
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18674654
43 X = -5648341
03
Y = -10129958
50 feet Y = -3151018
56 meter
Z = -5905839
08 Z = -1827645
28
XDOT = 12292
971424 XDOT = 3814
466314
YDOT = -11804
155056 feet/sec YDOT = -3555
628530 meter/sec
ZDOT = -18650
497638 ZDOT = -5666
305481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11970359
32 X = -3648565
52
Y = -17515998
51 feet Y = -5338876
35 meter
Z = -6011489
53 Z = -1832302
01
XDOT = 15139
821363 XDOT = 4614
617551
YDOT = -3978
502639 feet/sec YDOT = -1212
647604 meter/sec
ZDOT = -18580
603104 ZDOT = -5663
367826
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 08029
59873904
00020000 00000-0 20000-3 0 9069
2 25544 51
6381 16
1494 0005958 345
2479 14
8511 15
77641947 6504
Satellite: ISS
Catalog Number: 25544
Epoch time: 08029
59873904 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 16
1494 deg
Eccentricity:
0005958
Arg of perigee: 345
2479 deg
Mean anomaly: 14
8511 deg
Mean motion: 15
77641947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 650
Checksum: 315
Coasting Arc #8 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2008/030/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4273517
62 A = 6713356
16 meter
Y = 2732706
07 meter E =
0011880
Z = 4396199
83 I = 51
68950
XDOT = -5843
302230 Wp = 39
75517
YDOT = -3767
456755 meter/sec RA = 10
61589 deg
ZDOT = -3324
469565 TA = 83
66385
MA = 83
52856
Ha = 185
204 n
mi
Hp = 178
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14020727
11 X = -4325113
24
Y = 8965571
09 feet Y = 2684628
46 meter
Z = 14423227
79 Z = 4375314
14
XDOT = -19170
939074 XDOT = -5784
590185
YDOT = -12360
422424 feet/sec YDOT = -3832
471441 meter/sec
ZDOT = -10907
052380 ZDOT = -3352
713570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16609888
71 X = -5062694
08
Y = 1834164
16 feet Y = 559053
23 meter
Z = 14343611
56 Z = 4371932
80
XDOT = -11573
371020 XDOT = -3527
563487
YDOT = -18304
735313 feet/sec YDOT = -5579
283324 meter/sec
ZDOT = -11015
437517 ZDOT = -3357
505355
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 08030
61221354
00020000 00000-0 20000-3 0 9071
2 25544 51
6382 10
9167 0005943 348
6334 11
4696 15
77687375 6664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08030
61221354 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 10
9167 deg
Eccentricity:
0005943
Arg of perigee: 348
6334 deg
Mean anomaly: 11
4696 deg
Mean motion: 15
77687375 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 666
Checksum: 297
Coasting Arc #9 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2008/031/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4274913
40 A = 6714991
87 meter
Y = 3461742
88 meter E =
0011051
Z = 3839294
17 I = 51
66754
XDOT = -5917
098822 Wp = 68
83472
YDOT = 2714
513779 meter/sec RA = 5
50559 deg
ZDOT = 4135
332701 TA = 338
02026
MA = 338
06762
Ha = 185
026 n
mi
Hp = 178
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14025306
42 X = 4217235
58
Y = 11357424
13 feet Y = 3509224
64 meter
Z = 12596109
50 Z = 3859921
57
XDOT = -19413
053877 XDOT = -5967
101603
YDOT = 8905
885102 feet/sec YDOT = 2648
065561 meter/sec
ZDOT = 13567
364504 ZDOT = 4106
466524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7801458
65 X = 2377884
60
Y = 16212200
26 feet Y = 4941478
64 meter
Z = 12675333
65 Z = 3863441
70
XDOT = -20244
581297 XDOT = -6170
548379
YDOT = -793
699359 feet/sec YDOT = -241
919565 meter/sec
ZDOT = 13457
221368 ZDOT = 4101
761073
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 08031
62565784
00020000 00000-0 20000-3 0 9082
2 25544 51
6388 5
6836 0005803 352
0136 8
0936 15
77752619 6829
Satellite: ISS
Catalog Number: 25544
Epoch time: 08031
62565784 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 5
6836 deg
Eccentricity:
0005803
Arg of perigee: 352
0136 deg
Mean anomaly: 8
0936 deg
Mean motion: 15
77752619 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 682
Checksum: 303
Coasting Arc #10 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2008/032/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5855290
70 A = 6718645
29 meter
Y = -2020438
81 meter E =
0009843
Z = -2591718
64 I = 51
65013
XDOT = 3766
899460 Wp = 20
99335
YDOT = 4183
918828 meter/sec RA =
29424 deg
ZDOT = 5263
769086 TA = 309
52213
MA = 309
60910
Ha = 185
305 n
mi
Hp = 177
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19210271
33 X = 5890038
29
Y = -6628736
24 feet Y = -1954767
13 meter
Z = -8503013
91 Z = -2563189
82
XDOT = 12358
594029 XDOT = 3694
264218
YDOT = 13726
767809 feet/sec YDOT = 4225
635906 meter/sec
ZDOT = 17269
583615 ZDOT = 5281
892309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20283827
71 X = 6182510
69
Y = 1838880
16 feet Y = 560490
67 meter
Z = -8394091
22 Z = -2558519
00
XDOT = 5698
328897 XDOT = 1736
850648
YDOT = 16064
696361 feet/sec YDOT = 4896
519451 meter/sec
ZDOT = 17339
299460 ZDOT = 5285
018475
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 08032
57573667
00020000 00000-0 20000-3 0 9097
2 25544 51
6385
7771 0005958 355
8515 4
2599 15
77755158 6973
Satellite: ISS
Catalog Number: 25544
Epoch time: 08032
57573667 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node:
7771 deg
Eccentricity:
0005958
Arg of perigee: 355
8515 deg
Mean anomaly: 4
2599 deg
Mean motion: 15
77755158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 697
Checksum: 332
Coasting Arc #11 (Orbit 712)
---------------------------------------
Vector Time (GMT): 2008/033/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2130120
15 A = 6710047
25 meter
Y = -3856973
78 meter E =
0016082
Z = -5074348
36 I = 51
59346
XDOT = 7282
246423 Wp = 56
64559
YDOT = -1897
044861 meter/sec RA = 355
16398 deg
ZDOT = -1609
997112 TA = 197
84157
MA = 197
89810
Ha = 185
218 n
mi
Hp = 177
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6988583
17 X = -2062182
75
Y = -12654113
46 feet Y = -3880413
71 meter
Z = -16648124
54 Z = -5084531
60
XDOT = 23891
884589 XDOT = 7310
739172
YDOT = -6223
900463 feet/sec YDOT = -1815
451193 meter/sec
ZDOT = -5282
142756 ZDOT = -1574
551555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1354655
75 X = -412899
07
Y = -14346467
21 feet Y = -4372803
21 meter
Z = -16687441
97 Z = -5086332
31
XDOT = 23393
474128 XDOT = 7130
330914
YDOT = 3796
800709 feet/sec YDOT = 1157
264856 meter/sec
ZDOT = -5146
748782 ZDOT = -1568
729029
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 08033
58912413
00020000 00000-0 20000-3 0 9107
2 25544 51
6392 355
5430 0005894
1143
0023 15
77823337 7130
Satellite: ISS
Catalog Number: 25544
Epoch time: 08033
58912413 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 355
5430 deg
Eccentricity:
0005894
Arg of perigee:
1143 deg
Mean anomaly:
0023 deg
Mean motion: 15
77823337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 713
Checksum: 249
Coasting Arc #12 (Orbit 728)
---------------------------------------
Vector Time (GMT): 2008/034/13:41:41
655
Vector Time (MET): N/A
Weight (LBS) : 539961
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6598906
31 A = 6721222
96 meter
Y = 1260364
45 meter E =
0009770
Z = 117611
45 I = 51
60305
XDOT = -1008
566484 Wp = 106
42759
YDOT = -4679
138028 meter/sec RA = 349
98191 deg
ZDOT = -6035
610908 TA = 72
29267
MA = 72
18604
Ha = 185
253 n
mi
Hp = 177
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21649955
07 X = -6613080
78
Y = 4135053
97 feet Y = 1186492
46 meter
Z = 385864
35 Z = 85520
36
XDOT = -3308
945156 XDOT = -926
849438
YDOT = -15351
502718 feet/sec YDOT = -4689
958986 meter/sec
ZDOT = -19801
873059 ZDOT = -6040
312319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21608952
63 X = -6586408
76
Y = -4353388
39 feet Y = -1326912
78 meter
Z = 263235
56 Z = 80234
20
XDOT = 2523
904681 XDOT = 769
286147
YDOT = -13845
475034 feet/sec YDOT = -4220
100790 meter/sec
ZDOT = -19820
303685 ZDOT = -6041
228563
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 08034
60248161
00020000 00000-0 20000-3 0 9114
2 25544 51
6398 350
3091 0005828 4
0230 356
0981 15
77855750 7297
Satellite: ISS
Catalog Number: 25544
Epoch time: 08034
60248161 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 350
3091 deg
Eccentricity:
0005828
Arg of perigee: 4
0230 deg
Mean anomaly: 356
0981 deg
Mean motion: 15
77855750 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 729
Checksum: 283
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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