Date:
December 27th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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) : 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 1768)
---------------------------------------
Vector Time (GMT): 2008/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2186597
35 A = 6732575
48 meter
Y = 5114955
86 meter E =
0013807
Z = -3807222
80 I = 51
82271
XDOT = -6421
624539 Wp = 106
86839
YDOT = 378
093693 meter/sec RA = 145
70360 deg
ZDOT = 4204
685921 TA = 207
20239
MA = 207
27478
Ha = 196
415 n
mi
Hp = 184
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7173875
82 X = -2225136
26
Y = 16781351
24 feet Y = 5090288
88 meter
Z = -12490888
44 Z = -3817938
52
XDOT = -21068
321979 XDOT = -6445
800833
YDOT = 1240
464871 feet/sec YDOT = 306
147856 meter/sec
ZDOT = 13794
901314 ZDOT = 4173
430887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16482709
47 X = -5023929
84
Y = -7769581
42 feet Y = -2368168
42 meter
Z = -12532135
92 Z = -3819795
03
XDOT = -957
555170 XDOT = -291
862816
YDOT = -19978
157310 feet/sec YDOT = -6089
342348 meter/sec
ZDOT = 13673
438875 ZDOT = 4167
664169
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 08354
50819197
00010596 00000-0 82463-4 0 9000
2 25544 51
6389 146
6585 0007537 107
9744 252
2240 15
71643793 17699
Satellite: ISS
Catalog Number: 25544
Epoch time: 08354
50819197 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 146
6585 deg
Eccentricity:
0007537
Arg of perigee: 107
9744 deg
Mean anomaly: 252
2240 deg
Mean motion: 15
71643793 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1769
Checksum: 339
Coasting Arc #2 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2008/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5764751
47 A = 6734696
83 meter
Y = -1559845
43 meter E =
0011986
Z = -3118058
89 I = 51
85334
XDOT = -1057
193918 Wp = 109
07783
YDOT = 5837
532401 meter/sec RA = 140
64992 deg
ZDOT = -4893
918360 TA = 106
97349
MA = 106
84209
Ha = 196
392 n
mi
Hp = 184
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18913226
61 X = 5796912
53
Y = -5117603
12 feet Y = -1495200
55 meter
Z = -10229851
99 Z = -3089975
56
XDOT = -3468
483983 XDOT = -1098
617669
YDOT = 19152
009188 feet/sec YDOT = 5825
479055 meter/sec
ZDOT = -16056
162598 ZDOT = -4899
154357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4681236
14 X = 1426840
77
Y = 19084162
13 feet Y = 5816852
62 meter
Z = -10120803
25 Z = -3084820
83
XDOT = -17677
728458 XDOT = -5388
171634
YDOT = -4155
773165 feet/sec YDOT = -1266
679661 meter/sec
ZDOT = -16076
059128 ZDOT = -4899
982822
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 08355
52554367
00010596 00000-0 82463-4 0 9019
2 25544 51
6387 141
4517 0007477 110
9350 249
2613 15
71666491 17853
Satellite: ISS
Catalog Number: 25544
Epoch time: 08355
52554367 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 141
4517 deg
Eccentricity:
0007477
Arg of perigee: 110
9350 deg
Mean anomaly: 249
2613 deg
Mean motion: 15
71666491 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1785
Checksum: 322
Coasting Arc #3 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2008/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -344193
52 A = 6729394
34 meter
Y = -4813078
65 meter E =
0013887
Z = 4678752
66 I = 51
85712
XDOT = 6416
825190 Wp = 88
59348
YDOT = -3204
246231 meter/sec RA = 135
50164 deg
ZDOT = -2816
707687 TA = 29
14138
MA = 29
06396
Ha = 196
431 n
mi
Hp = 184
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1129243
83 X = -313076
04
Y = -15790940
44 feet Y = -4816754
10 meter
Z = 15350238
39 Z = 4677155
66
XDOT = 21052
576084 XDOT = 6465
861858
YDOT = -10512
618867 feet/sec YDOT = -3132
215118 meter/sec
ZDOT = -9241
166952 ZDOT = -2785
415680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15797496
85 X = 4815077
04
Y = -1126965
62 feet Y = -343499
12 meter
Z = 15343658
36 Z = 4676747
07
XDOT = 10309
317606 XDOT = 3142
280006
YDOT = 20013
378138 feet/sec YDOT = 6100
077656 meter/sec
ZDOT = -9119
760683 ZDOT = -2779
703056
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 08356
54288810
00010596 00000-0 82463-4 0 9020
2 25544 51
6385 136
2448 0007571 115
2270 244
9677 15
71636893 18014
Satellite: ISS
Catalog Number: 25544
Epoch time: 08356
54288810 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 136
2448 deg
Eccentricity:
0007571
Arg of perigee: 115
2270 deg
Mean anomaly: 244
9677 deg
Mean motion: 15
71636893 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1801
Checksum: 324
Coasting Arc #4 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2008/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5166063
10 A = 6737418
94 meter
Y = 3944188
31 meter E =
0019445
Z = 1752213
10 I = 51
90608
XDOT = -1749
591864 Wp = 83
27633
YDOT = -4853
026912 meter/sec RA = 130
43822 deg
ZDOT = 5714
080742 TA = 296
03755
MA = 296
23763
Ha = 196
251 n
mi
Hp = 184
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16949025
93 X = -5218295
72
Y = 12940250
37 feet Y = 3886126
15 meter
Z = 5748730
63 Z = 1726989
70
XDOT = -5740
130787 XDOT = -1722
952726
YDOT = -15922
004304 feet/sec YDOT = -4872
443583 meter/sec
ZDOT = 18746
984062 ZDOT = 5705
645280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13134184
39 X = -4003299
40
Y = -16832329
32 feet Y = -5130493
98 meter
Z = 5650960
41 Z = 1722412
73
XDOT = 14626
261861 XDOT = 4458
084615
YDOT = -5072
336121 feet/sec YDOT = -1546
048050 meter/sec
ZDOT = 18713
819519 ZDOT = 5703
972189
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 08357
56022014
00010596 00000-0 82463-4 0 9036
2 25544 51
6398 131
0385 0007506 119
4198 240
7714 15
71710656 18177
Satellite: ISS
Catalog Number: 25544
Epoch time: 08357
56022014 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 131
0385 deg
Eccentricity:
0007506
Arg of perigee: 119
4198 deg
Mean anomaly: 240
7714 deg
Mean motion: 15
71710656 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1817
Checksum: 303
Coasting Arc #5 (Orbit 1831)
---------------------------------------
Vector Time (GMT): 2008/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2558983
50 A = 6727079
93 meter
Y = 3443697
28 meter E =
0021402
Z = -5199918
72 I = 51
88973
XDOT = -5115
819531 Wp = 106
93662
YDOT = 5604
376332 meter/sec RA = 125
31350 deg
ZDOT = 1191
890701 TA = 174
44910
MA = 174
42534
Ha = 196
180 n
mi
Hp = 184
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8395615
14 X = 2545545
81
Y = 11298219
41 feet Y = 3472238
88 meter
Z = -17060100
80 Z = -5187519
24
XDOT = -16784
184812 XDOT = -5183
898406
YDOT = 18387
061456 feet/sec YDOT = 5546
787466 meter/sec
ZDOT = 3910
402561 ZDOT = 1166
873218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11049913
50 X = -3368013
63
Y = 8814020
29 feet Y = 2686513
38 meter
Z = -17011631
69 Z = -5185145
34
XDOT = -18218
576130 XDOT = -5553
022004
YDOT = -15466
665354 feet/sec YDOT = -4714
239600 meter/sec
ZDOT = 3813
540792 ZDOT = 1162
367233
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 08358
51396373
00010596 00000-0 82463-4 0 9045
2 25544 51
6401 126
1582 0007466 121
7517 238
4374 15
71714750 18324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08358
51396373 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 126
1582 deg
Eccentricity:
0007466
Arg of perigee: 121
7517 deg
Mean anomaly: 238
4374 deg
Mean motion: 15
71714750 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1832
Checksum: 309
Coasting Arc #6 (Orbit 1847)
---------------------------------------
Vector Time (GMT): 2008/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598372
94 A = 6738643
04 meter
Y = -5678898
56 meter E =
0018896
Z = -319665
80 I = 51
94495
XDOT = 3865
941679 Wp = 132
81047
YDOT = 2777
005932 meter/sec RA = 120
22677 deg
ZDOT = -6052
799049 TA = 50
64753
MA = 50
48025
Ha = 196
133 n
mi
Hp = 184
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11805685
50 X = 3663160
76
Y = -18631556
94 feet Y = -5638297
17 meter
Z = -1048772
32 Z = -302028
28
XDOT = 12683
535691 XDOT = 3864
005012
YDOT = 9110
911851 feet/sec YDOT = 2820
227216 meter/sec
ZDOT = -19858
264596 ZDOT = -6034
022461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19153587
54 X = 5838013
48
Y = 10944750
45 feet Y = 3335959
94 meter
Z = -980596
51 Z = -298885
82
XDOT = -7716
161690 XDOT = -2351
886083
YDOT = 11805
220392 feet/sec YDOT = 3598
231176 meter/sec
ZDOT = -19785
044917 ZDOT = -6030
481691
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 08359
53128039
00010596 00000-0 82463-4 0 9051
2 25544 51
6403 120
9505 0007375 125
4436 234
7416 15
71717604 18487
Satellite: ISS
Catalog Number: 25544
Epoch time: 08359
53128039 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 120
9505 deg
Eccentricity:
0007375
Arg of perigee: 125
4436 deg
Mean anomaly: 234
7416 deg
Mean motion: 15
71717604 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1848
Checksum: 308
Coasting Arc #7 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2008/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3979530
97 A = 6726579
11 meter
Y = -1243417
47 meter E =
0009921
Z = 5272064
85 I = 51
91977
XDOT = 2901
864427 Wp = 124
52557
YDOT = -7118
454962 meter/sec RA = 115
13110 deg
ZDOT = 505
362674 TA = 320
65797
MA = 320
73001
Ha = 196
092 n
mi
Hp = 185
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13056203
97 X = -3990941
92
Y = -4079453
66 feet Y = -1287983
55 meter
Z = 17296800
70 Z = 5252704
31
XDOT = 9520
552582 XDOT = 2978
793516
YDOT = -23354
511030 feet/sec YDOT = -7085
574583 meter/sec
ZDOT = 1658
014021 ZDOT = 519
645690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3241928
07 X = 988139
67
Y = -13386503
88 feet Y = -4080206
38 meter
Z = 17221415
01 Z = 5249087
30
XDOT = 22931
375280 XDOT = 6989
483185
YDOT = 7783
466938 feet/sec YDOT = 2372
400723 meter/sec
ZDOT = 1713
056000 ZDOT = 522
139469
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 08360
54858740
00010596 00000-0 82463-4 0 9064
2 25544 51
6416 115
7443 0007238 129
0487 231
1320 15
71757423 18644
Satellite: ISS
Catalog Number: 25544
Epoch time: 08360
54858740 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 115
7443 deg
Eccentricity:
0007238
Arg of perigee: 129
0487 deg
Mean anomaly: 231
1320 deg
Mean motion: 15
71757423 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1864
Checksum: 308
Coasting Arc #8 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2008/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1379466
38 A = 6738031
38 meter
Y = 6488385
44 meter E =
0011396
Z = -1182791
49 I = 51
97007
XDOT = -4925
144568 Wp = 77
18969
YDOT = 20
696842 meter/sec RA = 110
01927 deg
ZDOT = 5907
567977 TA = 269
93360
MA = 270
06419
Ha = 195
977 n
mi
Hp = 185
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4525808
33 X = -1446172
26
Y = 21287353
82 feet Y = 6472586
68 meter
Z = -3880549
50 Z = -1189653
88
XDOT = -16158
610786 XDOT = -4953
707822
YDOT = 67
903026 feet/sec YDOT = -34
539660 meter/sec
ZDOT = 19381
784701 ZDOT = 5883
572265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21579879
55 X = -6577547
29
Y = -2781880
10 feet Y = -847917
05 meter
Z = -3906786
35 Z = -1190788
48
XDOT = -1575
440034 XDOT = -480
194122
YDOT = -14638
419860 feet/sec YDOT = -4461
790373 meter/sec
ZDOT = 19288
451468 ZDOT = 5879
120007
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 08361
50230651
00010596 00000-0 82463-4 0 9077
2 25544 51
6423 110
8638 0007249 131
4040 228
7746 15
71726177 18790
Satellite: ISS
Catalog Number: 25544
Epoch time: 08361
50230651 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 110
8638 deg
Eccentricity:
0007249
Arg of perigee: 131
4040 deg
Mean anomaly: 228
7746 deg
Mean motion: 15
71726177 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1879
Checksum: 307
Coasting Arc #9 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2008/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4368013
65 A = 6728060
93 meter
Y = -1284662
16 meter E =
0017278
Z = -4967590
45 I = 51
94586
XDOT = -244
049110 Wp = 95
91603
YDOT = 7379
733867 meter/sec RA = 104
95191 deg
ZDOT = -2131
103138 TA = 153
50868
MA = 153
42027
Ha = 195
908 n
mi
Hp = 185
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14330753
46 X = 4406185
84
Y = -4214770
88 feet Y = -1235602
26 meter
Z = -16297868
92 Z = -4946278
23
XDOT = -800
686058 XDOT = -316
199908
YDOT = 24211
725287 feet/sec YDOT = 7376
601703 meter/sec
ZDOT = -6991
808194 ZDOT = -2132
462765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5598776
61 X = 1706507
11
Y = 13945648
23 feet Y = 4250633
58 meter
Z = -16215052
13 Z = -4942347
89
XDOT = -23153
780307 XDOT = -7057
272238
YDOT = 1191
275441 feet/sec YDOT = 363
100754 meter/sec
ZDOT = -6996
585569 ZDOT = -2132
559281
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 08362
51959734
00010596 00000-0 82463-4 0 9080
2 25544 51
6427 105
6575 0007197 136
0768 224
0967 15
71737077 18959
Satellite: ISS
Catalog Number: 25544
Epoch time: 08362
51959734 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 105
6575 deg
Eccentricity:
0007197
Arg of perigee: 136
0768 deg
Mean anomaly: 224
0967 deg
Mean motion: 15
71737077 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1895
Checksum: 349
Coasting Arc #10 (Orbit 1910)
---------------------------------------
Vector Time (GMT): 2008/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -936768
99 A = 6735846
28 meter
Y = -6162099
70 meter E =
0020280
Z = 2524455
47 I = 51
97848
XDOT = 4736
370748 Wp = 115
99644
YDOT = -2914
786677 meter/sec RA = 99
81842 deg
ZDOT = -5333
162756 TA = 35
54466
MA = 35
40972
Ha = 195
909 n
mi
Hp = 185
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3073389
08 X = -880057
00
Y = -20216862
55 feet Y = -6172258
50 meter
Z = 8282334
22 Z = 2520041
48
XDOT = 15539
274106 XDOT = 4794
519658
YDOT = -9562
948414 feet/sec YDOT = -2861
495879 meter/sec
ZDOT = -17497
253137 ZDOT = -5310
012881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19726837
88 X = 6012740
19
Y = -5413897
00 feet Y = -1650155
81 meter
Z = 8264738
24 Z = 2519092
22
XDOT = 10895
182683 XDOT = 3320
851682
YDOT = 13004
218994 feet/sec YDOT = 3963
685950 meter/sec
ZDOT = -17407
389827 ZDOT = -5305
772419
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 08363
53688020
00010596 00000-0 82463-4 0 9091
2 25544 51
6426 100
4516 0007328 138
7563 221
4153 15
71746732 19119
Satellite: ISS
Catalog Number: 25544
Epoch time: 08363
53688020 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 100
4516 deg
Eccentricity:
0007328
Arg of perigee: 138
7563 deg
Mean anomaly: 221
4153 deg
Mean motion: 15
71746732 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1911
Checksum: 300
Coasting Arc #11 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2008/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3650022
32 A = 6730652
90 meter
Y = 3717568
36 meter E =
0016421
Z = 4254793
43 I = 51
96584
XDOT = -2296
749306 Wp = 121
62509
YDOT = -6404
033182 meter/sec RA = 94
76924 deg
ZDOT = 3606
596539 TA = 291
79991
MA = 291
97453
Ha = 195
753 n
mi
Hp = 185
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11975138
84 X = -3711990
27
Y = 12196746
59 feet Y = 3676404
61 meter
Z = 13959296
04 Z = 4236911
84
XDOT = -7535
266753 XDOT = -2242
487643
YDOT = -21010
607553 feet/sec YDOT = -6429
413880 meter/sec
ZDOT = 11832
665809 ZDOT = 3595
569954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13676264
20 X = -4168525
33
Y = -10346732
62 feet Y = -3153684
10 meter
Z = 13889976
43 Z = 4233664
81
XDOT = 19073
694835 XDOT = 5813
662186
YDOT = -9302
833027 feet/sec YDOT = -2835
503507 meter/sec
ZDOT = 11789
325866 ZDOT = 3593
386524
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 08364
55415182
00010596 00000-0 82463-4 0 9103
2 25544 51
6431 95
2447 0007195 142
5714 217
5951 15
71804392 19278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08364
55415182 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 95
2447 deg
Eccentricity:
0007195
Arg of perigee: 142
5714 deg
Mean anomaly: 217
5951 deg
Mean motion: 15
71804392 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1927
Checksum: 311
Coasting Arc #12 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2008/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2930081
09 A = 6732554
44 meter
Y = 4807446
68 meter E =
0011925
Z = -3706340
77 I = 51
97318
XDOT = -3355
579862 Wp = 125
93810
YDOT = 5385
761276 meter/sec RA = 89
62443 deg
ZDOT = 4335
855371 TA = 189
79169
MA = 189
81495
Ha = 195
603 n
mi
Hp = 185
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9613126
93 X = 2894110
16
Y = 15772462
85 feet Y = 4840011
87 meter
Z = -12159910
68 Z = -3692193
41
XDOT = -11009
120281 XDOT = -3436
617459
YDOT = 17669
820458 feet/sec YDOT = 5347
783604 meter/sec
ZDOT = 14225
247280 ZDOT = 4319
357995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14159133
73 X = -4315703
96
Y = 11918279
57 feet Y = 3632691
61 meter
Z = -12104534
91 Z = -3689462
24
XDOT = -18252
233447 XDOT = -5563
280755
YDOT = -7310
754401 feet/sec YDOT = -2228
317941 meter/sec
ZDOT = 14161
421398 ZDOT = 4316
401242
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 08365
50783866
00010596 00000-0 82463-4 0 9117
2 25544 51
6429 90
3645 0007101 145
6591 214
5031 15
71799401 19422
Satellite: ISS
Catalog Number: 25544
Epoch time: 08365
50783866 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 90
3645 deg
Eccentricity:
0007101
Arg of perigee: 145
6591 deg
Mean anomaly: 214
5031 deg
Mean motion: 15
71799401 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1942
Checksum: 309
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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