Date:
November 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8718 77 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 3527)
---------------------------------------
Vector Time (GMT): 2007/323/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5658645
99 A = 6719897
16 meter
Y = -692047
70 meter E =
0005230
Z = -3563786
44 I = 51
76587
XDOT = 3449
503617 Wp = 112
40954
YDOT = 5238
457642 meter/sec RA = 22
53492 deg
ZDOT = 4463
164454 TA = 205
14838
MA = 205
17386
Ha = 186
342 n
mi
Hp = 180
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18565111
53 X = 5683276
57
Y = -2270497
71 feet Y = -628631
70 meter
Z = -11692212
71 Z = -3536236
40
XDOT = 11317
269086 XDOT = 3368
988355
YDOT = 17186
540821 feet/sec YDOT = 5276
581643 meter/sec
ZDOT = 14642
928000 ZDOT = 4479
727028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6615950
76 X = -2016541
79
Y = 17563827
69 feet Y = 5353454
68 meter
Z = -11587386
09 Z = -3531835
28
XDOT = -19154
496335 XDOT = -5838
290483
YDOT = 2480
161611 feet/sec YDOT = 755
953259 meter/sec
ZDOT = 14706
526749 ZDOT = 4482
549353
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
52130675
00020000 00000-0 20000-3 0 9003
2 25544 51
6406 23
0283 0001500 196
0205 164
0912 15
76407082 35282
Satellite: ISS
Catalog Number: 25544
Epoch time: 07323
52130675 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 23
0283 deg
Eccentricity:
0001500
Arg of perigee: 196
0205 deg
Mean anomaly: 164
0912 deg
Mean motion: 15
76407082 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3528
Checksum: 247
Coasting Arc #2 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2007/324/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2496286
49 A = 6716834
70 meter
Y = -4424573
96 meter E =
0008574
Z = -4402331
92 I = 51
72905
XDOT = 6912
783248 Wp = 76
00659
YDOT = -585
862868 meter/sec RA = 17
43843 deg
ZDOT = -3334
346318 TA = 160
52151
MA = 160
48873
Ha = 186
280 n
mi
Hp = 180
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8189916
30 X = -2425238
46
Y = -14516318
78 feet Y = -4452091
50 meter
Z = -14443346
20 Z = -4414286
70
XDOT = 22679
735066 XDOT = 6935
018719
YDOT = -1922
122269 feet/sec YDOT = -508
435805 meter/sec
ZDOT = -10939
456425 ZDOT = -3300
709213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16610435
62 X = 5062860
78
Y = -749464
24 feet Y = -228436
70 meter
Z = -14489314
04 Z = -4416342
92
XDOT = -8519
617710 XDOT = -2596
779478
YDOT = 19982
937016 feet/sec YDOT = 6090
799202 meter/sec
ZDOT = -10811
445033 ZDOT = -3295
328446
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
53559079
00020000 00000-0 20000-3 0 9019
2 25544 51
6412 17
8005 0001402 200
0042 160
1067 15
76409068 35440
Satellite: ISS
Catalog Number: 25544
Epoch time: 07324
53559079 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 17
8005 deg
Eccentricity:
0001402
Arg of perigee: 200
0042 deg
Mean anomaly: 160
1067 deg
Mean motion: 15
76409068 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3544
Checksum: 251
Coasting Arc #3 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2007/325/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6340822
37 A = 6723111
21 meter
Y = 383889
38 meter E =
0013980
Z = 2179981
26 I = 51
72276
XDOT = -2199
047056 Wp = 113
95803
YDOT = -4924
254240 meter/sec RA = 12
24728 deg
ZDOT = -5507
103735 TA = 41
61832
MA = 41
51201
Ha = 186
179 n
mi
Hp = 180
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20803223
00 X = -6355234
08
Y = 1259479
59 feet Y = 312902
05 meter
Z = 7152169
48 Z = 2149141
65
XDOT = -7214
721313 XDOT = -2117
066564
YDOT = -16155
689764 feet/sec YDOT = -4948
386662 meter/sec
ZDOT = -18067
925641 ZDOT = -5517
588054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7876097
55 X = 2400634
53
Y = -19338890
97 feet Y = -5894493
97 meter
Z = 7034791
23 Z = 2144204
37
XDOT = 16232
628352 XDOT = 4947
705122
YDOT = -2
867639 feet/sec YDOT = -
874056 meter/sec
ZDOT = -18108
340210 ZDOT = -5519
422096
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
54984845
00020000 00000-0 20000-3 0 9025
2 25544 51
6413 12
5732 0001180 206
9938 153
1166 15
76486275 35607
Satellite: ISS
Catalog Number: 25544
Epoch time: 07325
54984845 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 12
5732 deg
Eccentricity:
0001180
Arg of perigee: 206
9938 deg
Mean anomaly: 153
1166 deg
Mean motion: 15
76486275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3560
Checksum: 294
Coasting Arc #4 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2007/326/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1271023
85 A = 6713771
10 meter
Y = 4204200
98 meter E =
0005221
Z = 5075686
80 I = 51
66247
XDOT = -7531
006779 Wp = 137
68383
YDOT = 335
642670 meter/sec RA = 7
12973 deg
ZDOT = 1603
113796 TA = 296
91135
MA = 296
96468
Ha = 186
097 n
mi
Hp = 180
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4170025
75 X = 1199259
79
Y = 13793310
30 feet Y = 4218012
72 meter
Z = 16652515
74 Z = 5081687
58
XDOT = -24708
027489 XDOT = -7541
988153
YDOT = 1101
189863 feet/sec YDOT = 251
365185 meter/sec
ZDOT = 5259
559699 ZDOT = 1566
500299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14237015
24 X = -4339442
25
Y = -2043650
85 feet Y = -622904
78 meter
Z = 16675781
61 Z = 5082778
24
XDOT = 9160
125628 XDOT = 2792
006292
YDOT = -21907
092895 feet/sec YDOT = -6677
281915 meter/sec
ZDOT = 5120
194334 ZDOT = 1560
635233
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
56408298
00020000 00000-0 20000-3 0 9032
2 25544 51
6408 7
3457 0001145 203
5193 156
5920 15
76506212 35760
Satellite: ISS
Catalog Number: 25544
Epoch time: 07326
56408298 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 7
3457 deg
Eccentricity:
0001145
Arg of perigee: 203
5193 deg
Mean anomaly: 156
5920 deg
Mean motion: 15
76506212 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3576
Checksum: 284
Coasting Arc #5 (Orbit 3590)
---------------------------------------
Vector Time (GMT): 2007/327/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6692823
41 A = 6724878
24 meter
Y = -219021
23 meter E =
0010130
Z = -566211
68 I = 51
67149
XDOT = 658
859247 Wp = 41
66853
YDOT = 4775
905782 meter/sec RA = 1
95850 deg
ZDOT = 6009
151908 TA = 312
16586
MA = 312
25185
Ha = 186
093 n
mi
Hp = 180
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21958082
05 X = 6697525
75
Y = -718573
58 feet Y = -144151
94 meter
Z = -1857649
87 Z = -533685
44
XDOT = 2161
611703 XDOT = 576
213019
YDOT = 15668
982226 feet/sec YDOT = 4782
810826 meter/sec
ZDOT = 19715
065315 ZDOT = 6012
152474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8152928
21 X = -2485012
52
Y = 20411961
34 feet Y = 6221565
82 meter
Z = -1733832
25 Z = -528472
07
XDOT = -13687
327494 XDOT = -4171
897420
YDOT = -3811
819864 feet/sec YDOT = -1161
842694 meter/sec
ZDOT = 19726
958493 ZDOT = 6012
776949
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
51490559
00020000 00000-0 20000-3 0 9040
2 25544 51
6412 2
4447 0001000 209
7143 150
3965 15
76523748 35914
Satellite: ISS
Catalog Number: 25544
Epoch time: 07327
51490559 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 2
4447 deg
Eccentricity:
0001000
Arg of perigee: 209
7143 deg
Mean anomaly: 150
3965 deg
Mean motion: 15
76523748 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3591
Checksum: 276
Coasting Arc #6 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2007/328/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 160856
25 A = 6712882
33 meter
Y = -4183787
23 meter E =
0014493
Z = -5259599
31 I = 51
60259
XDOT = 7685
062097 Wp = 96
22285
YDOT = -148
928380 meter/sec RA = 356
80526 deg
ZDOT = 352
787818 TA = 177
13510
MA = 177
12679
Ha = 185
996 n
mi
Hp = 180
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 527743
60 X = 233179
00
Y = -13726336
06 feet Y = -4181583
36 meter
Z = -17255903
24 Z = -5258642
73
XDOT = 25213
458324 XDOT = 7684
442429
YDOT = -488
610169 feet/sec YDOT = -62
993175 meter/sec
ZDOT = 1157
440348 ZDOT = 390
121471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12425893
42 X = 3787412
31
Y = 5865125
15 feet Y = 1787690
14 meter
Z = -17252666
22 Z = -5258612
66
XDOT = -8832
757956 XDOT = -2692
224625
YDOT = 22542
814190 feet/sec YDOT = 6871
049765 meter/sec
ZDOT = 1299
574636 ZDOT = 396
110349
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 07328
52909211
00020000 00000-0 20000-3 0 9053
2 25544 51
6416 357
2163 0001046 213
6707 146
4391 15
76554653 36070
Satellite: ISS
Catalog Number: 25544
Epoch time: 07328
52909211 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 357
2163 deg
Eccentricity:
0001046
Arg of perigee: 213
6707 deg
Mean anomaly: 146
4391 deg
Mean motion: 15
76554653 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3607
Checksum: 285
Coasting Arc #7 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2007/329/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6614172
67 A = 6724131
99 meter
Y = 20107
82 meter E =
0009597
Z = -1185476
39 I = 51
61119
XDOT = 1034
624061 Wp = 147
56599
YDOT = -4863
851019 meter/sec RA = 351
66219 deg
ZDOT = -5884
859382 TA = 45
44157
MA = 45
36325
Ha = 185
911 n
mi
Hp = 179
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21700041
57 X = -6608146
97
Y = 65970
52 feet Y = -53821
73 meter
Z = -3889358
24 Z = -1217594
18
XDOT = 3394
435896 XDOT = 1117
523751
YDOT = -15957
516465 feet/sec YDOT = -4851
816818 meter/sec
ZDOT = -19307
281436 ZDOT = -5879
632459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7945166
37 X = 2421686
71
Y = -20169388
46 feet Y = -6147629
60 meter
Z = -4011653
51 Z = -1222751
99
XDOT = 12064
550061 XDOT = 3677
274859
YDOT = 8569
927628 feet/sec YDOT = 2612
113941 meter/sec
ZDOT = -19287
844834 ZDOT = -5878
935105
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 07329
54325434
00020000 00000-0 20000-3 0 9066
2 25544 51
6406 351
9876 0000971 211
4868 148
6239 15
76601468 36231
Satellite: ISS
Catalog Number: 25544
Epoch time: 07329
54325434 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 351
9876 deg
Eccentricity:
0000971
Arg of perigee: 211
4868 deg
Mean anomaly: 148
6239 deg
Mean motion: 15
76601468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3623
Checksum: 309
Coasting Arc #8 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2007/330/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1613140
65 A = 6714375
03 meter
Y = 4349545
88 meter E =
0006054
Z = 4850584
39 I = 51
54933
XDOT = -7348
278955 Wp = 61
02215
YDOT = -129
129722 meter/sec RA = 346
47180 deg
ZDOT = -2322
937364 TA = 51
63809
MA = 51
58371
Ha = 185
879 n
mi
Hp = 179
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5292456
19 X = -1685221
68
Y = 14270163
63 feet Y = 4331103
00 meter
Z = 15913990
79 Z = 4842573
25
XDOT = -24108
526755 XDOT = -7335
004270
YDOT = -423
653945 feet/sec YDOT = -211
227735 meter/sec
ZDOT = -7621
185578 ZDOT = -2358
603673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11448366
84 X = -3489462
21
Y = -10076676
20 feet Y = -3071370
90 meter
Z = 15883899
37 Z = 4841412
53
XDOT = 8163
765029 XDOT = 2488
315581
YDOT = -21528
695479 feet/sec YDOT = -6561
946382 meter/sec
ZDOT = -7757
017345 ZDOT = -2364
338887
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 07330
55739168
00020000 00000-0 20000-3 0 9073
2 25544 51
6398 346
7588 0000854 217
6909 142
4196 15
76661043 36393
Satellite: ISS
Catalog Number: 25544
Epoch time: 07330
55739168 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 346
7588 deg
Eccentricity:
0000854
Arg of perigee: 217
6909 deg
Mean anomaly: 142
4196 deg
Mean motion: 15
76661043 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3639
Checksum: 328
Coasting Arc #9 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2007/331/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6089191
16 A = 6721001
81 meter
Y = 304974
85 meter E =
0012824
Z = 2815474
13 I = 51
54405
XDOT = -2622
144672 Wp = 82
89614
YDOT = 5155
016305 meter/sec RA = 341
35205 deg
ZDOT = 5094
486274 TA = 309
47357
MA = 309
58694
Ha = 185
717 n
mi
Hp = 179
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19977661
29 X = 6071651
13
Y = 1000573
67 feet Y = 372969
14 meter
Z = 9237119
84 Z = 2845013
16
XDOT = -8602
836850 XDOT = -2704
342294
YDOT = 16912
783154 feet/sec YDOT = 5125
233632 meter/sec
ZDOT = 16714
193811 ZDOT = 5081
548893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7659908
87 X = -2334740
22
Y = 18421249
76 feet Y = 5614796
93 meter
Z = 9349643
56 Z = 2849771
36
XDOT = -11646
973944 XDOT = -3549
997658
YDOT = -13331
426470 feet/sec YDOT = -4063
418788 meter/sec
ZDOT = 16665
417533 ZDOT = 5079
619264
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 07331
57150543
00020000 00000-0 20000-3 0 9081
2 25544 51
6396 341
5303 0000835 224
8703 135
2394 15
76688418 36553
Satellite: ISS
Catalog Number: 25544
Epoch time: 07331
57150543 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 341
5303 deg
Eccentricity:
0000835
Arg of perigee: 224
8703 deg
Mean anomaly: 135
2394 deg
Mean motion: 15
76688418 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3655
Checksum: 296
Coasting Arc #10 (Orbit 3669)
---------------------------------------
Vector Time (GMT): 2007/332/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2894765
55 A = 6717974
16 meter
Y = -4659080
70 meter E =
0006120
Z = -3885366
19 I = 51
50686
XDOT = 6505
640225 Wp = 111
44186
YDOT = 655
779003 meter/sec RA = 336
13801 deg
ZDOT = 4063
531145 TA = 200
95300
MA = 200
97809
Ha = 185
747 n
mi
Hp = 179
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9497262
30 X = 2965523
46
Y = -15285697
83 feet Y = -4626313
66 meter
Z = -12747264
41 Z = -3871132
08
XDOT = 21343
963992 XDOT = 6478
083681
YDOT = 2151
505916 feet/sec YDOT = 728
374150 meter/sec
ZDOT = 13331
795095 ZDOT = 4095
068878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11406400
69 X = 3476670
93
Y = 13968261
10 feet Y = 4257525
98 meter
Z = -12693502
44 Z = -3868979
54
XDOT = -7844
422226 XDOT = -2390
979895
YDOT = 18621
308075 feet/sec YDOT = 5675
774701 meter/sec
ZDOT = 13451
971414 ZDOT = 4100
160887
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 07332
52221469
00020000 00000-0 20000-3 0 9094
2 25544 51
6398 336
6284 0000760 233
1896 126
9199 15
76701123 36707
Satellite: ISS
Catalog Number: 25544
Epoch time: 07332
52221469 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 336
6284 deg
Eccentricity:
0000760
Arg of perigee: 233
1896 deg
Mean anomaly: 126
9199 deg
Mean motion: 15
76701123 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3670
Checksum: 303
Coasting Arc #11 (Orbit 3685)
---------------------------------------
Vector Time (GMT): 2007/333/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5182174
31 A = 6716658
81 meter
Y = -932077
30 meter E =
0007512
Z = -4177818
71 I = 51
47607
XDOT = 3938
248692 Wp = 70
92616
YDOT = -5510
520754 meter/sec RA = 331
02168 deg
ZDOT = -3658
532558 TA = 161
68064
MA = 161
65357
Ha = 185
648 n
mi
Hp = 179
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17001884
23 X = -5151071
36
Y = -3057996
40 feet Y = -989852
96 meter
Z = -13706754
29 Z = -4202918
37
XDOT = 12920
763426 XDOT = 4017
348033
YDOT = -18079
136332 feet/sec YDOT = -5466
038370 meter/sec
ZDOT = -12003
059574 ZDOT = -3639
208917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8067387
38 X = 2458939
67
Y = -15188824
16 feet Y = -4629553
60 meter
Z = -13802441
96 Z = -4206984
31
XDOT = 12156
703615 XDOT = 3705
363262
YDOT = 17289
314001 feet/sec YDOT = 5269
782907 meter/sec
ZDOT = -11929
998441 ZDOT = -3636
263525
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 07333
53628117
00020000 00000-0 20000-3 0 9109
2 25544 51
6388 331
3986 0000754 233
8223 126
2872 15
76746728 36869
Satellite: ISS
Catalog Number: 25544
Epoch time: 07333
53628117 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 331
3986 deg
Eccentricity:
0000754
Arg of perigee: 233
8223 deg
Mean anomaly: 126
2872 deg
Mean motion: 15
76746728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3686
Checksum: 310
Coasting Arc #12 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2007/334/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3874120
41 A = 6721718
35 meter
Y = 4935811
51 meter E =
0013365
Z = 2392771
69 I = 51
46866
XDOT = -5310
468090 Wp = 107
67440
YDOT = -1557
287583 meter/sec RA = 325
80670 deg
ZDOT = -5365
262269 TA = 45
22939
MA = 45
12074
Ha = 185
544 n
mi
Hp = 179
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12710368
79 X = -3940649
18
Y = 16193607
31 feet Y = 4892116
71 meter
Z = 7850300
82 Z = 2373789
94
XDOT = -17422
795572 XDOT = -5266
595977
YDOT = -5109
211230 feet/sec YDOT = -1616
426489 meter/sec
ZDOT = -17602
566499 ZDOT = -5390
954219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11831661
76 X = -3606290
50
Y = -16879588
20 feet Y = -5144898
48 meter
Z = 7778489
42 Z = 2370883
57
XDOT = 8653
206081 XDOT = 2637
497214
YDOT = -14253
528422 feet/sec YDOT = -4344
475463 meter/sec
ZDOT = -17700
574068 ZDOT = -5395
134976
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 07334
55032208
00020000 00000-0 20000-3 0 9113
2 25544 51
6386 326
1694 0000724 252
7563 107
3523 15
76819250 37022
Satellite: ISS
Catalog Number: 25544
Epoch time: 07334
55032208 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 326
1694 deg
Eccentricity:
0000724
Arg of perigee: 252
7563 deg
Mean anomaly: 107
3523 deg
Mean motion: 15
76819250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3702
Checksum: 277
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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