Date:
August 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6200 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
232/21:38:12
000 0
0 0
0 0
0
011/23:01:30
047 0
0 0
0 184
5
000/00:00:00
000 0
0 0
0 184
1
Coasting Arc #1 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2007/222/21:38:12
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5891054
40 A = 6723233
12 meter
Y = -2032766
64 meter E =
0007351
Z = 2520683
42 I = 51
63732
XDOT = 3714
188068 Wp = 108
76985
YDOT = -4172
226946 meter/sec RA = 180
36500 deg
ZDOT = 5300
874906 TA = 279
79912
MA = 279
88212
Ha = 186
775 n
mi
Hp = 182
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19327606
29 X = -5880130
60
Y = -6669181
90 feet Y = -2098582
91 meter
Z = 8269958
72 Z = 2492091
66
XDOT = 12185
656390 XDOT = 3734
816390
YDOT = -13688
408617 feet/sec YDOT = -4130
578016 meter/sec
ZDOT = 17391
321870 ZDOT = 5318
967687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2212476
09 X = 674362
71
Y = -20369690
92 feet Y = -6208681
79 meter
Z = 8161324
06 Z = 2487571
57
XDOT = 14540
470022 XDOT = 4431
935263
YDOT = 8594
416688 feet/sec YDOT = 2619
578206 meter/sec
ZDOT = 17459
373039 ZDOT = 5321
616902
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 07222
95996563
00020000 00000-0 20000-3 0 9004
2 25544 51
6284 181
0347 0008680 228
2286 131
8137 15
76200412 19422
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
95996563 = yrday
fracday
Element set: 900
Inclination: 51
6284 deg
RA of node: 181
0347 deg
Eccentricity:
0008680
Arg of perigee: 228
2286 deg
Mean anomaly: 131
8137 deg
Mean motion: 15
76200412 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1942
Checksum: 288
Coasting Arc #2 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2007/223/21:38:17
978
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3772249
10 A = 6718149
64 meter
Y = 3651931
99 meter E =
0008374
Z = -4197606
29 I = 51
65031
XDOT = -6354
037121 Wp = 172
86374
YDOT = -2360
138909 meter/sec RA = 175
16497 deg
ZDOT = 3649
447987 TA = 134
36272
MA = 134
29409
Ha = 186
578 n
mi
Hp = 182
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12376145
34 X = -3792414
49
Y = 11981404
16 feet Y = 3609636
15 meter
Z = -13771674
16 Z = -4215980
11
XDOT = -20846
578482 XDOT = -6344
901368
YDOT = -7743
237890 feet/sec YDOT = -2431
142534 meter/sec
ZDOT = 11973
254550 ZDOT = 3618
602855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14570400
74 X = -4441058
14
Y = -9083832
85 feet Y = -2768752
25 meter
Z = -13840860
94 Z = -4218694
42
XDOT = 1866
037952 XDOT = 568
768368
YDOT = -21094
633428 feet/sec YDOT = -6429
644269 meter/sec
ZDOT = 11856
021223 ZDOT = 3613
715269
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 07223
91097835
00020000 00000-0 20000-3 0 9016
2 25544 51
6293 176
1333 0008600 230
9580 129
0820 15
76207676 19574
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
91097835 = yrday
fracday
Element set: 901
Inclination: 51
6293 deg
RA of node: 176
1333 deg
Eccentricity:
0008600
Arg of perigee: 230
9580 deg
Mean anomaly: 129
0820 deg
Mean motion: 15
76207676 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1957
Checksum: 292
Coasting Arc #3 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2007/224/21:38:31
303
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5090900
30 A = 6719579
28 meter
Y = 2165215
16 meter E =
0003454
Z = -3810535
82 I = 51
68453
XDOT = -4916
086351 Wp = 196
76988
YDOT = 4211
894470 meter/sec RA = 170
06540 deg
ZDOT = -4176
960171 TA = 29
53049
MA = 29
51098
Ha = 186
419 n
mi
Hp = 182
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16702428
81 X = 5084820
62
Y = 7103724
29 feet Y = 2222110
68 meter
Z = -12501757
94 Z = -3785819
49
XDOT = -16128
892228 XDOT = -4942
528593
YDOT = 13818
551412 feet/sec YDOT = 4156
772391 meter/sec
ZDOT = -13703
937570 ZDOT = -4200
905940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2568431
00 X = -782857
77
Y = 18032701
49 feet Y = 5496367
41 meter
Z = -12407772
47 Z = -3781889
05
XDOT = -16155
685619 XDOT = -4924
252977
YDOT = -11787
196282 feet/sec YDOT = -3592
737427 meter/sec
ZDOT = -13794
179743 ZDOT = -4204
465986
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 07224
92538195
00020000 00000-0 20000-3 0 9028
2 25544 51
6300 170
9062 0008474 235
2909 124
7457 15
76236439 19731
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
92538195 = yrday
fracday
Element set: 902
Inclination: 51
6300 deg
RA of node: 170
9062 deg
Eccentricity:
0008474
Arg of perigee: 235
2909 deg
Mean anomaly: 124
7457 deg
Mean motion: 15
76236439 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1973
Checksum: 301
Coasting Arc #4 (Orbit 1988)
---------------------------------------
Vector Time (GMT): 2007/225/21:43:20
313
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5908522
14 A = 6724782
03 meter
Y = -2822003
29 meter E =
0012080
Z = 1496712
00 I = 51
73039
XDOT = 3308
635601 Wp = 155
80670
YDOT = 3846
920593 meter/sec RA = 164
85884 deg
ZDOT = -5802
552040 TA = 7
70460
MA = 7
68606
Ha = 186
120 n
mi
Hp = 182
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19384915
16 X = 5932368
48
Y = -9258540
99 feet Y = -2755797
58 meter
Z = 4910472
46 Z = 1525472
81
XDOT = 10855
103679 XDOT = 3293
559982
YDOT = 12621
130554 feet/sec YDOT = 3883
835491 meter/sec
ZDOT = -19037
244225 ZDOT = -5786
515556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14524936
00 X = 4427200
49
Y = 15793751
24 feet Y = 4813935
38 meter
Z = 5019154
58 Z = 1529838
32
XDOT = -7702
840644 XDOT = -2347
825828
YDOT = 13120
163541 feet/sec YDOT = 3999
025847 meter/sec
ZDOT = -18975
941953 ZDOT = -5783
867107
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 07225
93977581
00020000 00000-0 20000-3 0 9037
2 25544 51
6298 165
6779 0008640 239
4460 120
5852 15
76244493 19895
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
93977581 = yrday
fracday
Element set: 903
Inclination: 51
6298 deg
RA of node: 165
6779 deg
Eccentricity:
0008640
Arg of perigee: 239
4460 deg
Mean anomaly: 120
5852 deg
Mean motion: 15
76244493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1989
Checksum: 334
Coasting Arc #5 (Orbit 2004)
---------------------------------------
Vector Time (GMT): 2007/226/21:47:49
394
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -389472
03 A = 6714116
97 meter
Y = -4232135
35 meter E =
0004966
Z = 5201317
86 I = 51
72248
XDOT = 7397
449449 Wp = 245
17058
YDOT = -1899
428042 meter/sec RA = 159
70239 deg
ZDOT = -994
365953 TA = 214
27946
MA = 214
31152
Ha = 186
079 n
mi
Hp = 183
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1277795
39 X = -367385
32
Y = -13884958
49 feet Y = -4236367
21 meter
Z = 17064691
14 Z = 5199479
44
XDOT = 24269
847272 XDOT = 7422
969704
YDOT = -6231
719297 feet/sec YDOT = -1816
562890 meter/sec
ZDOT = -3262
355488 ZDOT = -958
367838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12665964
74 X = 3860586
05
Y = -5852763
27 feet Y = -1783922
24 meter
Z = 17057169
07 Z = 5199025
13
XDOT = 13428
016183 XDOT = 4092
859332
YDOT = 19975
535752 feet/sec YDOT = 6088
543297 meter/sec
ZDOT = -3126
106171 ZDOT = -952
837161
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 07226
95416304
00020000 00000-0 20000-3 0 9042
2 25544 51
6306 160
4502 0008453 242
1166 117
9142 15
76207743 20057
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
95416304 = yrday
fracday
Element set: 904
Inclination: 51
6306 deg
RA of node: 160
4502 deg
Eccentricity:
0008453
Arg of perigee: 242
1166 deg
Mean anomaly: 117
9142 deg
Mean motion: 15
76207743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2005
Checksum: 261
Coasting Arc #6 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2007/227/21:52:33
518
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5942311
31 A = 6721462
41 meter
Y = 87964
05 meter E =
0005695
Z = 3138450
15 I = 51
77581
XDOT = 2493
162307 Wp = 115
99273
YDOT = -5426
471443 meter/sec RA = 154
57394 deg
ZDOT = 4863
387507 TA = 280
47897
MA = 280
54313
Ha = 185
782 n
mi
Hp = 183
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19495772
01 X = -5958099
11
Y = 288595
98 feet Y = 21425
50 meter
Z = 10296752
46 Z = 3109544
45
XDOT = 8179
666362 XDOT = 2530
031488
YDOT = -17803
383999 feet/sec YDOT = -5398
385357 meter/sec
ZDOT = 15955
995757 ZDOT = 4875
588668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7379207
30 X = -2249182
39
Y = -18109685
28 feet Y = -5519832
07 meter
Z = 10187154
84 Z = 3105044
80
XDOT = 18205
907053 XDOT = 5549
160470
YDOT = 1600
088932 feet/sec YDOT = 487
707106 meter/sec
ZDOT = 16001
554384 ZDOT = 4877
273776
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 07227
96853559
00020000 00000-0 20000-3 0 9052
2 25544 51
6318 155
2226 0008680 246
0677 113
9578 15
76293574 20211
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
96853559 = yrday
fracday
Element set: 905
Inclination: 51
6318 deg
RA of node: 155
2226 deg
Eccentricity:
0008680
Arg of perigee: 246
0677 deg
Mean anomaly: 113
9578 deg
Mean motion: 15
76293574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2021
Checksum: 315
Coasting Arc #7 (Orbit 2035)
---------------------------------------
Vector Time (GMT): 2007/228/21:57:24
709
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4275698
05 A = 6723328
21 meter
Y = 4643437
08 meter E =
0004160
Z = -2309689
51 I = 51
80836
XDOT = -5081
162149 Wp = 286
49730
YDOT = -1967
808456 meter/sec RA = 149
36878 deg
ZDOT = 5443
254934 TA = 47
57619
MA = 47
54101
Ha = 185
548 n
mi
Hp = 183
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14027880
74 X = -4316083
92
Y = 15234373
63 feet Y = 4595398
01 meter
Z = -7577721
48 Z = -2330558
75
XDOT = -16670
479492 XDOT = -5085
222283
YDOT = -6456
064489 feet/sec YDOT = -2024
651578 meter/sec
ZDOT = 17858
447947 ZDOT = 5418
561018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19550538
37 X = -5959004
10
Y = -6741486
17 feet Y = -2054804
98 meter
Z = -7656255
90 Z = -2333626
80
XDOT = -1266
374243 XDOT = -385
990869
YDOT = -16527
912414 feet/sec YDOT = -5037
707704 meter/sec
ZDOT = 17764
549393 ZDOT = 5414
634655
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 07228
91950449
00020000 00000-0 20000-3 0 9065
2 25544 51
6323 150
3220 0008568 250
2343 109
7898 15
76276752 20362
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
91950449 = yrday
fracday
Element set: 906
Inclination: 51
6323 deg
RA of node: 150
3220 deg
Eccentricity:
0008568
Arg of perigee: 250
2343 deg
Mean anomaly: 109
7898 deg
Mean motion: 15
76276752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2036
Checksum: 299
Coasting Arc #8 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2007/229/22:02:40
860
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2109241
58 A = 6713531
31 meter
Y = 3592362
81 meter E =
0007407
Z = -5270687
54 I = 51
79989
XDOT = -6397
315085 Wp = 113
68143
YDOT = 4271
208821 meter/sec RA = 144
22744 deg
ZDOT = 348
513286 TA = 159
63513
MA = 159
60557
Ha = 185
295 n
mi
Hp = 183
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6920083
91 X = 2094518
38
Y = 11785967
24 feet Y = 3615867
26 meter
Z = -17292281
97 Z = -5260476
64
XDOT = -20988
566551 XDOT = -6446
293919
YDOT = 14013
152301 feet/sec YDOT = 4199
396580 meter/sec
ZDOT = 1143
416293 ZDOT = 317
316359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7550609
61 X = -2301425
81
Y = 11451578
55 feet Y = 3490441
14 meter
Z = -17253093
75 Z = -5258742
97
XDOT = -20926
109731 XDOT = -6378
278246
YDOT = -12239
833798 feet/sec YDOT = -3730
701342 meter/sec
ZDOT = 1025
661369 ZDOT = 312
621585
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 07229
93386076
00020000 00000-0 20000-3 0 9078
2 25544 51
6323 145
0953 0008523 254
4037 105
6187 15
76318606 20522
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
93386076 = yrday
fracday
Element set: 907
Inclination: 51
6323 deg
RA of node: 145
0953 deg
Eccentricity:
0008523
Arg of perigee: 254
4037 deg
Mean anomaly: 105
6187 deg
Mean motion: 15
76318606 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2052
Checksum: 292
Coasting Arc #9 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2007/230/22:07:36
963
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5750635
22 A = 6722412
40 meter
Y = -2132995
70 meter E =
0006215
Z = -2741677
49 I = 51
85264
XDOT = -358
874981 Wp = 224
97398
YDOT = 5693
223703 meter/sec RA = 139
09533 deg
ZDOT = -5179
222564 TA = 346
28553
MA = 346
30241
Ha = 185
207 n
mi
Hp = 183
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18866913
46 X = 5787377
83
Y = -6998017
38 feet Y = -2068483
36 meter
Z = -8995004
89 Z = -2713651
77
XDOT = -1177
411354 XDOT = -397
351122
YDOT = 18678
555455 feet/sec YDOT = 5688
995525 meter/sec
ZDOT = -16992
200013 ZDOT = -5181
059327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15072907
59 X = 4594222
23
Y = 13402838
21 feet Y = 4085185
09 meter
Z = -8888991
43 Z = -2709364
59
XDOT = -16015
295406 XDOT = -4881
462040
YDOT = 6731
118155 feet/sec YDOT = 2051
644814 meter/sec
ZDOT = -16998
433341 ZDOT = -5181
122482
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
94820756
00020000 00000-0 20000-3 0 9080
2 25544 51
6326 139
8668 0008603 258
1938 101
8261 15
76309228 20687
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
94820756 = yrday
fracday
Element set: 908
Inclination: 51
6326 deg
RA of node: 139
8668 deg
Eccentricity:
0008603
Arg of perigee: 258
1938 deg
Mean anomaly: 101
8261 deg
Mean motion: 15
76309228 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2068
Checksum: 309
Coasting Arc #10 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2007/231/22:12:25
605
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2435246
43 A = 6722313
57 meter
Y = -5631001
73 meter E =
0006135
Z = 2738493
48 I = 51
87370
XDOT = 5700
405492 Wp = 127
21091
YDOT = -57
498119 meter/sec RA = 133
89458 deg
ZDOT = -5183
138451 TA = 21
58063
MA = 21
55479
Ha = 184
878 n
mi
Hp = 183
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7989653
64 X = 2484729
04
Y = -18474415
11 feet Y = -5603492
85 meter
Z = 8984558
65 Z = 2750443
89
XDOT = 18702
117757 XDOT = 5725
803494
YDOT = -188
642123 feet/sec YDOT = 6
389213 meter/sec
ZDOT = -17005
047411 ZDOT = -5155
384228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19958525
27 X = 6083358
50
Y = -2447921
82 feet Y = -746126
57 meter
Z = 9029165
02 Z = 2752089
50
XDOT = 9453
170337 XDOT = 2881
326319
YDOT = 14687
846749 feet/sec YDOT = 4476
855689 meter/sec
ZDOT = -16899
789493 ZDOT = -5151
055838
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
96254491
00020000 00000-0 20000-3 0 9091
2 25544 51
6328 134
6396 0008554 262
0575 97
9618 15
76309005 20848
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
96254491 = yrday
fracday
Element set: 909
Inclination: 51
6328 deg
RA of node: 134
6396 deg
Eccentricity:
0008554
Arg of perigee: 262
0575 deg
Mean anomaly: 97
9618 deg
Mean motion: 15
76309005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2084
Checksum: 311
Coasting Arc #11 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2007/232/21:38:12
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1375162
94 A = 6715087
66 meter
Y = 4402776
08 meter E =
0005263
Z = -4884520
73 I = 51
86852
XDOT = -5880
563656 Wp = 141
10807
YDOT = 4402
875688 meter/sec RA = 128
88430 deg
ZDOT = 2310
374270 TA = 151
32723
MA = 151
29829
Ha = 184
514 n
mi
Hp = 184
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4511689
43 X = 1349556
32
Y = 14444803
40 feet Y = 4418010
99 meter
Z = -16025330
48 Z = -4877902
17
XDOT = -19293
187849 XDOT = -5940
583573
YDOT = 14445
130210 feet/sec YDOT = 4336
780206 meter/sec
ZDOT = 7579
968078 ZDOT = 2281
660966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11558281
07 X = -3522964
07
Y = 9809976
80 feet Y = 2990080
93 meter
Z = -15999668
66 Z = -4876699
01
XDOT = -20062
327203 XDOT = -6114
997331
YDOT = -11437
535870 feet/sec YDOT = -3486
160933 meter/sec
ZDOT = 7471
614377 ZDOT = 2277
348062
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
91347653
00020000 00000-0 20000-3 0 9102
2 25544 51
6328 129
7382 0008533 266
3305 93
6883 15
76363934 20997
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
91347653 = yrday
fracday
Element set: 910
Inclination: 51
6328 deg
RA of node: 129
7382 deg
Eccentricity:
0008533
Arg of perigee: 266
3305 deg
Mean anomaly: 93
6883 deg
Mean motion: 15
76363934 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2099
Checksum: 311
Coasting Arc #12 (Orbit 2114)
---------------------------------------
Vector Time (GMT): 2007/233/21:42:50
750
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5047355
69 A = 6718587
84 meter
Y = -1885103
32 meter E =
0002928
Z = -4013763
48 I = 51
89769
XDOT = -681
179692 Wp = 320
03492
YDOT = 6581
102720 meter/sec RA = 123
77571 deg
ZDOT = -3943
696311 TA = 269
35743
MA = 269
39097
Ha = 184
466 n
mi
Hp = 184
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16559565
91 X = 5087558
14
Y = -6184722
19 feet Y = -1828435
91 meter
Z = -13168515
34 Z = -3989145
97
XDOT = -2234
841508 XDOT = -735
562230
YDOT = 21591
544356 feet/sec YDOT = 6573
181570 meter/sec
ZDOT = -12938
636190 ZDOT = -3947
137142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12591783
55 X = 3837975
63
Y = 12504460
70 feet Y = 3811359
62 meter
Z = -13075368
36 Z = -3985372
28
XDOT = -19595
097001 XDOT = -5972
585566
YDOT = 6176
743595 feet/sec YDOT = 1882
671448 meter/sec
ZDOT = -12950
862132 ZDOT = -3947
422778
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
92779492
00020000 00000-0 20000-3 0 9115
2 25544 51
6333 124
5101 0008630 270
2620 89
7556 15
76344234 21151
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
92779492 = yrday
fracday
Element set: 911
Inclination: 51
6333 deg
RA of node: 124
5101 deg
Eccentricity:
0008630
Arg of perigee: 270
2620 deg
Mean anomaly: 89
7556 deg
Mean motion: 15
76344234 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2115
Checksum: 278
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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