Date:
August 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11500 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
240/18:18:54
000 0
0 0
0 0
0
019/19:42:12
047 0
0 0
0 185
7
000/00:00:00
000 0
0 0
0 182
8
Coasting Arc #1 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2007/230/18:18:54
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5795532
88 A = 6723592
54 meter
Y = 2399613
30 meter E =
0005618
Z = 2412758
75 I = 51
84914
XDOT = -32
605357 Wp = 67
10055
YDOT = -5504
451249 meter/sec RA = 139
92126 deg
ZDOT = 5388
407809 TA = 320
06246
MA = 320
10377
Ha = 185
255 n
mi
Hp = 184
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19014215
49 X = -5833655
69
Y = 7872747
03 feet Y = 2334591
18 meter
Z = 7915875
15 Z = 2384511
57
XDOT = -106
972955 XDOT = 2
772827
YDOT = -18059
223259 feet/sec YDOT = -5504
618139 meter/sec
ZDOT = 17678
503312 ZDOT = 5388
335257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2454103
49 X = 748010
74
Y = -20473827
50 feet Y = -6240422
62 meter
Z = 7809057
51 Z = 2380200
73
XDOT = 14359
959847 XDOT = 4376
915761
YDOT = 8473
572144 feet/sec YDOT = 2582
744790 meter/sec
ZDOT = 17677
518983 ZDOT = 5388
107786
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 07230
82179889
00020000 00000-0 20000-3 0 9003
2 25544 51
6301 140
5304 0008406 258
7593 101
2626 15
76153621 20661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
82179889 = yrday
fracday
Element set: 900
Inclination: 51
6301 deg
RA of node: 140
5304 deg
Eccentricity:
0008406
Arg of perigee: 258
7593 deg
Mean anomaly: 101
2626 deg
Mean motion: 15
76153621 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2066
Checksum: 276
Coasting Arc #2 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2007/231/18:23:59
499
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2206049
31 A = 6722013
86 meter
Y = 5588022
92 meter E =
0003939
Z = -3011773
71 I = 51
86591
XDOT = -5866
098771 Wp = 273
49440
YDOT = 369
934202 meter/sec RA = 134
71971 deg
ZDOT = 4977
827175 TA = 51
77204
MA = 51
73658
Ha = 184
987 n
mi
Hp = 184
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7237694
60 X = -2253740
83
Y = 18333408
52 feet Y = 5563087
07 meter
Z = -9881147
35 Z = -3022606
35
XDOT = -19245
730877 XDOT = -5893
980798
YDOT = 1213
694889 feet/sec YDOT = 304
180125 meter/sec
ZDOT = 16331
453986 ZDOT = 4949
261995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13070027
33 X = -3983744
33
Y = -14726609
36 feet Y = -4488670
53 meter
Z = -9921518
34 Z = -3024078
79
XDOT = 6629
209380 XDOT = 2020
583019
YDOT = -16824
967591 feet/sec YDOT = -5128
250122 meter/sec
ZDOT = 16223
161465 ZDOT = 4944
819615
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 07231
77283524
00020000 00000-0 20000-3 0 9011
2 25544 51
6304 135
6292 0008313 261
7696 98
2526 15
76171884 20812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
77283524 = yrday
fracday
Element set: 901
Inclination: 51
6304 deg
RA of node: 135
6292 deg
Eccentricity:
0008313
Arg of perigee: 261
7696 deg
Mean anomaly: 98
2526 deg
Mean motion: 15
76171884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2081
Checksum: 295
Coasting Arc #3 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2007/232/18:28:33
846
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3803332
81 A = 6714079
80 meter
Y = 1838320
20 meter E =
0006460
Z = -5224206
90 I = 51
85925
XDOT = -4303
066092 Wp = 79
66841
YDOT = 6320
574204 meter/sec RA = 129
60013 deg
ZDOT = -908
417153 TA = 181
70352
MA = 181
70572
Ha = 184
642 n
mi
Hp = 184
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12478126
01 X = 3807871
98
Y = 6031234
25 feet Y = 1880876
84 meter
Z = -17139786
40 Z = -5205719
22
XDOT = -14117
670906 XDOT = -4369
010958
YDOT = 20736
792008 feet/sec YDOT = 6272
086221 meter/sec
ZDOT = -2980
371237 ZDOT = -929
481296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10762690
46 X = -3280468
05
Y = 8868526
54 feet Y = 2703126
89 meter
Z = -17069429
52 Z = -5202762
12
XDOT = -12230
829563 XDOT = -3727
956851
YDOT = -20732
946298 feet/sec YDOT = -6319
402032 meter/sec
ZDOT = -3059
466744 ZDOT = -932
525464
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 07232
78725664
00020000 00000-0 20000-3 0 9020
2 25544 51
6308 130
4025 0008175 265
5441 94
4789 15
76215694 20973
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
78725664 = yrday
fracday
Element set: 902
Inclination: 51
6308 deg
RA of node: 130
4025 deg
Eccentricity:
0008175
Arg of perigee: 265
5441 deg
Mean anomaly: 94
4789 deg
Mean motion: 15
76215694 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2097
Checksum: 305
Coasting Arc #4 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2007/233/18:33:17
606
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4679058
31 A = 6724618
81 meter
Y = -4531610
78 meter E =
0007160
Z = -1651618
31 I = 51
91259
XDOT = 2361
014463 Wp = 209
07634
YDOT = 4538
861592 meter/sec RA = 124
45471 deg
ZDOT = -5760
433552 TA = 349
11990
MA = 349
13538
Ha = 183
679 n
mi
Hp = 183
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15351241
19 X = 4737406
94
Y = -14867489
42 feet Y = -4478960
56 meter
Z = -5418695
24 Z = -1628746
06
XDOT = 7746
110442 XDOT = 2338
067827
YDOT = 14891
278189 feet/sec YDOT = 4565
135847 meter/sec
ZDOT = -18899
060210 ZDOT = -5749
019228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7774845
77 X = 2369772
99
Y = 19929407
77 feet Y = 6074483
49 meter
Z = -5332502
68 Z = -1625346
82
XDOT = -15315
149747 XDOT = -4668
057643
YDOT = 925
883306 feet/sec YDOT = 282
209232 meter/sec
ZDOT = -18855
191218 ZDOT = -5747
062283
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 07233
80165950
00020000 00000-0 20000-3 0 9031
2 25544 51
6308 125
1740 0008275 270
4290 89
5926 15
76254461 21138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
80165950 = yrday
fracday
Element set: 903
Inclination: 51
6308 deg
RA of node: 125
1740 deg
Eccentricity:
0008275
Arg of perigee: 270
4290 deg
Mean anomaly: 89
5926 deg
Mean motion: 15
76254461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2113
Checksum: 281
Coasting Arc #5 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2007/234/18:38:17
623
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -131405
47 A = 6719990
21 meter
Y = -5633407
80 meter E =
0003861
Z = 3659611
66 I = 51
91242
XDOT = 5597
832685 Wp = 68
00698
YDOT = -2975
977205 meter/sec RA = 119
26143 deg
ZDOT = -4374
987266 TA = 68
20312
MA = 68
16205
Ha = 184
095 n
mi
Hp = 183
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -431120
31 X = -86179
73
Y = -18482309
06 feet Y = -5634624
65 meter
Z = 12006599
92 Z = 3659082
74
XDOT = 18365
592798 XDOT = 5651
947234
YDOT = -9763
704741 feet/sec YDOT = -2913
076199 meter/sec
ZDOT = -14353
632761 ZDOT = -4347
661923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17489053
37 X = 5330663
47
Y = 5998307
39 feet Y = 1828284
09 meter
Z = 12003890
01 Z = 3658785
68
XDOT = 3131
589337 XDOT = 954
508430
YDOT = 19420
592529 feet/sec YDOT = 5919
396603 meter/sec
ZDOT = -14250
340020 ZDOT = -4343
503638
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 07234
81604675
00020000 00000-0 20000-3 0 9046
2 25544 51
6310 119
9462 0008286 272
8539 87
1676 15
76235054 21297
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
81604675 = yrday
fracday
Element set: 904
Inclination: 51
6310 deg
RA of node: 119
9462 deg
Eccentricity:
0008286
Arg of perigee: 272
8539 deg
Mean anomaly: 87
1676 deg
Mean motion: 15
76235054 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2129
Checksum: 305
Coasting Arc #6 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2007/235/18:43:08
433
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4401413
15 A = 6714514
81 meter
Y = 95380
10 meter E =
0004575
Z = 5073842
52 I = 51
90880
XDOT = 1805
989527 Wp = 244
26606
YDOT = -7290
329711 meter/sec RA = 114
15076 deg
ZDOT = 1702
927550 TA = 189
41234
MA = 189
42092
Ha = 184
780 n
mi
Hp = 183
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14440331
87 X = -4426800
15
Y = 312926
85 feet Y = 46018
70 meter
Z = 16646464
98 Z = 5052399
01
XDOT = 5925
162491 XDOT = 1879
104419
YDOT = -23918
404565 feet/sec YDOT = -7269
725438 meter/sec
ZDOT = 5587
032644 ZDOT = 1711
878020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4260383
57 X = 1298564
91
Y = -13898629
08 feet Y = -4236302
14 meter
Z = 16565118
34 Z = 5049048
07
XDOT = 19850
380870 XDOT = 6050
396089
YDOT = 12786
102619 feet/sec YDOT = 3897
204078 meter/sec
ZDOT = 5620
085454 ZDOT = 1713
002046
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 07235
83041427
00020000 00000-0 20000-3 0 9050
2 25544 51
6323 114
7185 0008432 277
1939 82
8266 15
76304789 21458
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
83041427 = yrday
fracday
Element set: 905
Inclination: 51
6323 deg
RA of node: 114
7185 deg
Eccentricity:
0008432
Arg of perigee: 277
1939 deg
Mean anomaly: 82
8266 deg
Mean motion: 15
76304789 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2145
Checksum: 300
Coasting Arc #7 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2007/236/18:47:24
472
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2770375
74 A = 6725306
64 meter
Y = 6065106
22 meter E =
0009973
Z = 824485
26 I = 51
95717
XDOT = -4044
195169 Wp = 16
09244
YDOT = -2663
262751 meter/sec RA = 108
99728 deg
ZDOT = 5994
807011 TA = 352
87190
MA = 352
88607
Ha = 184
981 n
mi
Hp = 183
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9089159
24 X = -2841995
90
Y = 19898642
45 feet Y = 6033725
81 meter
Z = 2705004
14 Z = 810853
39
XDOT = -13268
356855 XDOT = -4043
234876
YDOT = -8737
738685 feet/sec YDOT = -2708
482237 meter/sec
ZDOT = 19668
002006 ZDOT = 5975
162748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16563603
93 X = -5048586
48
Y = -14299964
32 feet Y = -4358629
13 meter
Z = 2654030
82 Z = 808948
59
XDOT = 11084
228644 XDOT = 3378
472891
YDOT = -9197
581909 feet/sec YDOT = -2803
422966 meter/sec
ZDOT = 19593
132391 ZDOT = 5971
986753
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 07236
84476580
00020000 00000-0 20000-3 0 9065
2 25544 51
6335 109
4912 0008299 280
9288 79
0942 15
76320219 21613
Satellite: ISS
Catalog Number: 25544
Epoch time: 07236
84476580 = yrday
fracday
Element set: 906
Inclination: 51
6335 deg
RA of node: 109
4912 deg
Eccentricity:
0008299
Arg of perigee: 280
9288 deg
Mean anomaly: 79
0942 deg
Mean motion: 15
76320219 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2161
Checksum: 310
Coasting Arc #8 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2007/237/18:51:52
301
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2366224
41 A = 6717444
37 meter
Y = 4562332
48 meter E =
0000946
Z = -4326181
20 I = 51
93907
XDOT = -4157
585968 Wp = 173
41841
YDOT = 5465
523211 meter/sec RA = 103
81791 deg
ZDOT = 3489
011837 TA = 131
70606
MA = 131
69796
Ha = 185
282 n
mi
Hp = 183
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7763203
45 X = 2336047
31
Y = 14968282
41 feet Y = 4588624
40 meter
Z = -14193507
89 Z = -4314759
38
XDOT = -13640
373912 XDOT = -4235
341952
YDOT = 17931
506599 feet/sec YDOT = 5418
595831 meter/sec
ZDOT = 11446
889230 ZDOT = 3468
626014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16429065
48 X = -5007579
16
Y = 3955646
94 feet Y = 1205681
19 meter
Z = -14149598
47 Z = -4312797
61
XDOT = -13759
477752 XDOT = -4193
888819
YDOT = -16465
611408 feet/sec YDOT = -5018
718357 meter/sec
ZDOT = 11370
207536 ZDOT = 3465
639257
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 07237
79570447
00020000 00000-0 20000-3 0 9078
2 25544 51
6335 104
5911 0008444 284
9887 75
0342 15
76328126 21760
Satellite: ISS
Catalog Number: 25544
Epoch time: 07237
79570447 = yrday
fracday
Element set: 907
Inclination: 51
6335 deg
RA of node: 104
5911 deg
Eccentricity:
0008444
Arg of perigee: 284
9887 deg
Mean anomaly: 75
0342 deg
Mean motion: 15
76328126 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2176
Checksum: 310
Coasting Arc #9 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2007/238/18:56:50
671
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4116575
03 A = 6715834
23 meter
Y = -2415383
82 meter E =
0006896
Z = -4729569
91 I = 51
93986
XDOT = 1057
757111 Wp = 21
99956
YDOT = 7127
687033 meter/sec RA = 98
71352 deg
ZDOT = -2714
447039 TA = 221
37649
MA = 221
42875
Ha = 185
418 n
mi
Hp = 183
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13505823
59 X = 4166253
21
Y = -7924487
60 feet Y = -2369072
12 meter
Z = -15516961
65 Z = -4709451
35
XDOT = 3470
331728 XDOT = 991
161678
YDOT = 23384
799977 feet/sec YDOT = 7139
143160 meter/sec
ZDOT = -8905
666138 ZDOT = -2709
470197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4955660
39 X = 1510485
29
Y = 14933203
45 feet Y = 4551640
41 meter
Z = -15440911
19 Z = -4706389
73
XDOT = -22519
652765 XDOT = -6863
990163
YDOT = -1731
745907 feet/sec YDOT = -527
836152 meter/sec
ZDOT = -8885
892423 ZDOT = -2708
420011
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 07238
81002154
00020000 00000-0 20000-3 0 9088
2 25544 51
6339 99
3632 0008498 288
9626 71
0617 15
76353492 21922
Satellite: ISS
Catalog Number: 25544
Epoch time: 07238
81002154 = yrday
fracday
Element set: 908
Inclination: 51
6339 deg
RA of node: 99
3632 deg
Eccentricity:
0008498
Arg of perigee: 288
9626 deg
Mean anomaly: 71
0617 deg
Mean motion: 15
76353492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2192
Checksum: 312
Coasting Arc #10 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2007/239/19:01:22
527
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 419106
00 A = 6725380
24 meter
Y = -6708707
81 meter E =
0005423
Z = -4462
88 I = 51
97545
XDOT = 4735
414341 Wp = 170
13868
YDOT = 299
147209 meter/sec RA = 93
54499 deg
ZDOT = -6067
770106 TA = 9
90961
MA = 9
89893
Ha = 185
510 n
mi
Hp = 183
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1375019
70 X = 494114
30
Y = -22010196
24 feet Y = -6703601
74 meter
Z = -14641
99 Z = -2244
61
XDOT = 15536
136288 XDOT = 4761
192875
YDOT = 981
454097 feet/sec YDOT = 352
245332 meter/sec
ZDOT = -19907
382239 ZDOT = -6044
703279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21458395
78 X = 6540519
03
Y = 5086927
61 feet Y = 1550495
54 meter
Z = -7059
61 Z = -2151
77
XDOT = -3249
441181 XDOT = -990
429672
YDOT = 13689
963752 feet/sec YDOT = 4172
700952 meter/sec
ZDOT = -19819
801386 ZDOT = -6041
075463
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 07239
82432101
00020000 00000-0 20000-3 0 9090
2 25544 51
6339 94
1352 0008454 293
0851 66
9422 15
76391579 22086
Satellite: ISS
Catalog Number: 25544
Epoch time: 07239
82432101 = yrday
fracday
Element set: 909
Inclination: 51
6339 deg
RA of node: 94
1352 deg
Eccentricity:
0008454
Arg of perigee: 293
0851 deg
Mean anomaly: 66
9422 deg
Mean motion: 15
76391579 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2208
Checksum: 298
Coasting Arc #11 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2007/240/18:18:54
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3917905
78 A = 6714748
99 meter
Y = 2346609
10 meter E =
0004575
Z = -4926295
89 I = 51
94023
XDOT = -1546
661244 Wp = 85
37533
YDOT = 7214
135752 meter/sec RA = 88
54662 deg
ZDOT = 2208
445091 TA = 205
97120
MA = 205
99417
Ha = 185
741 n
mi
Hp = 182
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12854021
60 X = 3915305
17
Y = 7698848
77 feet Y = 2390406
60 meter
Z = -16162388
10 Z = -4907269
40
XDOT = -5074
347915 XDOT = -1637
943902
YDOT = 23668
424383 feet/sec YDOT = 7196
329813 meter/sec
ZDOT = 7245
554760 ZDOT = 2200
709515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11565528
31 X = -3525173
03
Y = 9647544
37 feet Y = 2940571
52 meter
Z = -16089884
25 Z = -4904196
72
XDOT = -19916
777966 XDOT = -6070
633924
YDOT = -11851
455020 feet/sec YDOT = -3612
323490 meter/sec
ZDOT = 7217
096489 ZDOT = 2199
771010
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 07240
77521071
00020000 00000-0 20000-3 0 9103
2 25544 51
6336 89
2335 0008421 297
2505 62
7802 15
76440538 22238
Satellite: ISS
Catalog Number: 25544
Epoch time: 07240
77521071 = yrday
fracday
Element set: 910
Inclination: 51
6336 deg
RA of node: 89
2335 deg
Eccentricity:
0008421
Arg of perigee: 297
2505 deg
Mean anomaly: 62
7802 deg
Mean motion: 15
76440538 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2223
Checksum: 273
Coasting Arc #12 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2007/241/18:23:26
840
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2558154
84 A = 6718515
70 meter
Y = -4800300
40 meter E =
0006451
Z = -3947724
99 I = 51
95115
XDOT = 3794
665197 Wp = 352
91510
YDOT = 5347
353108 meter/sec RA = 83
44108 deg
ZDOT = -4036
272929 TA = 235
32005
MA = 235
38086
Ha = 185
855 n
mi
Hp = 182
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8392896
46 X = 2630819
55
Y = -15749017
07 feet Y = -4771287
60 meter
Z = -12951853
66 Z = -3935120
83
XDOT = 12449
688967 XDOT = 3754
195583
YDOT = 17543
809408 feet/sec YDOT = 5389
560699 meter/sec
ZDOT = -13242
365253 ZDOT = -4017
937203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12519424
02 X = 3815920
44
Y = 12765488
23 feet Y = 3890920
81 meter
Z = -12904615
28 Z = -3933326
74
XDOT = -19543
429688 XDOT = -5956
837369
YDOT = 5827
889000 feet/sec YDOT = 1776
340567 meter/sec
ZDOT = -13172
109702 ZDOT = -4014
859037
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 07241
78947564
00020000 00000-0 20000-3 0 9115
2 25544 51
6339 84
0047 0008521 300
9111 59
1215 15
76434981 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 07241
78947564 = yrday
fracday
Element set: 911
Inclination: 51
6339 deg
RA of node: 84
0047 deg
Eccentricity:
0008521
Arg of perigee: 300
9111 deg
Mean anomaly: 59
1215 deg
Mean motion: 15
76434981 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2239
Checksum: 287
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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