Date:
November 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7319 46 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 3449)
---------------------------------------
Vector Time (GMT): 2007/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 996938
64 A = 6719871
87 meter
Y = 5501079
91 meter E =
0011837
Z = 3721366
86 I = 51
88282
XDOT = -6134
738941 Wp = 105
50949
YDOT = -1806
550434 meter/sec RA = 48
24482 deg
ZDOT = 4299
635818 TA = 299
26339
MA = 299
38167
Ha = 186
756 n
mi
Hp = 180
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3270796
05 X = 917272
54
Y = 18048162
43 feet Y = 5511782
42 meter
Z = 12209208
87 Z = 3726017
14
XDOT = -20127
096264 XDOT = -6134
969146
YDOT = -5927
002736 feet/sec YDOT = -1875
154285 meter/sec
ZDOT = 14106
416727 ZDOT = 4269
831906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17230045
42 X = -5251717
84
Y = -6254062
54 feet Y = -1906238
26 meter
Z = 12227481
00 Z = 3726936
21
XDOT = 14782
533553 XDOT = 4505
716227
YDOT = -13276
576893 feet/sec YDOT = -4046
700637 meter/sec
ZDOT = 13992
762316 ZDOT = 4264
993954
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 07318
57630397
00020000 00000-0 20000-3 0 9008
2 25544 51
6423 48
5045 0001908 187
7449 172
3687 15
76199520 34508
Satellite: ISS
Catalog Number: 25544
Epoch time: 07318
57630397 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 48
5045 deg
Eccentricity:
0001908
Arg of perigee: 187
7449 deg
Mean anomaly: 172
3687 deg
Mean motion: 15
76199520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3450
Checksum: 308
Coasting Arc #2 (Orbit 3464)
---------------------------------------
Vector Time (GMT): 2007/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5628635
30 A = 6721513
20 meter
Y = 1835922
83 meter E =
0004177
Z = -3186630
57 I = 51
86767
XDOT = 797
137033 Wp = 100
89696
YDOT = 5938
356154 meter/sec RA = 43
05904 deg
ZDOT = 4833
833965 TA = 222
05125
MA = 222
08332
Ha = 186
668 n
mi
Hp = 180
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18466651
24 X = 5623167
73
Y = 6023368
87 feet Y = 1898835
15 meter
Z = -10454824
71 Z = -3159299
31
XDOT = 2615
278981 XDOT = 707
191911
YDOT = 19482
795781 feet/sec YDOT = 5946
766831 meter/sec
ZDOT = 15859
035317 ZDOT = 4837
488596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14255021
10 X = -4344930
43
Y = 13276350
34 feet Y = 4046631
58 meter
Z = -10350576
57 Z = -3154855
74
XDOT = -17293
385094 XDOT = -5271
023777
YDOT = -6204
490968 feet/sec YDOT = -1891
128847 meter/sec
ZDOT = 15873
559921 ZDOT = 4838
261064
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 07319
52731584
00020000 00000-0 20000-3 0 9015
2 25544 51
6418 43
6056 0001748 192
2604 167
8518 15
76224420 34652
Satellite: ISS
Catalog Number: 25544
Epoch time: 07319
52731584 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 43
6056 deg
Eccentricity:
0001748
Arg of perigee: 192
2604 deg
Mean anomaly: 167
8518 deg
Mean motion: 15
76224420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3465
Checksum: 289
Coasting Arc #3 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2007/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -297215
04 A = 6716398
20 meter
Y = -4857245
39 meter E =
0009934
Z = -4638398
80 I = 51
82808
XDOT = 6727
612654 Wp = 77
99332
YDOT = 2356
441880 meter/sec RA = 37
96797 deg
ZDOT = -2901
883750 TA = 163
36353
MA = 163
33092
Ha = 186
579 n
mi
Hp = 180
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -975114
96 X = -220345
67
Y = -15935844
45 feet Y = -4860138
85 meter
Z = -15217843
83 Z = -4639656
35
XDOT = 22072
219994 XDOT = 6714
859579
YDOT = 7731
108531 feet/sec YDOT = 2431
602776 meter/sec
ZDOT = -9520
615979 ZDOT = -2869
231331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14483488
72 X = 4414567
36
Y = 6705939
18 feet Y = 2043970
26 meter
Z = -15223130
19 Z = -4640010
08
XDOT = -16735
196303 XDOT = -5100
887833
YDOT = 14838
380802 feet/sec YDOT = 4522
738468 meter/sec
ZDOT = -9396
050497 ZDOT = -2863
916191
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 07320
54169877
00020000 00000-0 20000-3 0 9020
2 25544 51
6411 38
3789 0001669 195
0970 165
0145 15
76253398 34818
Satellite: ISS
Catalog Number: 25544
Epoch time: 07320
54169877 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 38
3789 deg
Eccentricity:
0001669
Arg of perigee: 195
0970 deg
Mean anomaly: 165
0145 deg
Mean motion: 15
76253398 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3481
Checksum: 310
Coasting Arc #4 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2007/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6075221
08 A = 6724159
84 meter
Y = -2214384
97 meter E =
0014395
Z = 1817429
72 I = 51
83157
XDOT = 185
455219 Wp = 119
67728
YDOT = -5198
593304 meter/sec RA = 32
78997 deg
ZDOT = -5687
682125 TA = 40
19192
MA = 40
08555
Ha = 186
476 n
mi
Hp = 180
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19931827
70 X = -6058836
84
Y = -7265042
56 feet Y = -2282230
03 meter
Z = 5962695
92 Z = 1787955
55
XDOT = 608
448880 XDOT = 271
203006
YDOT = -17055
752311 feet/sec YDOT = -5196
039662 meter/sec
ZDOT = -18660
374427 ZDOT = -5686
573195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15550582
69 X = 4739817
60
Y = -14476407
24 feet Y = -4412408
93 meter
Z = 5850243
85 Z = 1783154
33
XDOT = 13809
383631 XDOT = 4209
100131
YDOT = 7258
753696 feet/sec YDOT = 2212
468127 meter/sec
ZDOT = -18656
685211 ZDOT = -5686
557652
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 07321
55605100
00020000 00000-0 20000-3 0 9037
2 25544 51
6415 33
1520 0001396 196
8741 163
2377 15
76335070 34972
Satellite: ISS
Catalog Number: 25544
Epoch time: 07321
55605100 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 33
1520 deg
Eccentricity:
0001396
Arg of perigee: 196
8741 deg
Mean anomaly: 163
2377 deg
Mean motion: 15
76335070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3497
Checksum: 271
Coasting Arc #5 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2007/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -692464
39 A = 6713783
86 meter
Y = 4230918
08 meter E =
0004496
Z = 5164966
61 I = 51
77207
XDOT = -7130
977512 Wp = 142
29047
YDOT = -2657
527027 meter/sec RA = 27
67495 deg
ZDOT = 1216
841706 TA = 296
09123
MA = 296
13750
Ha = 186
339 n
mi
Hp = 180
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2271864
79 X = -764814
55
Y = 13880964
83 feet Y = 4222769
81 meter
Z = 16945428
52 Z = 5161427
00
XDOT = -23395
595513 XDOT = -7106
641939
YDOT = -8718
920692 feet/sec YDOT = -2737
133640 meter/sec
ZDOT = 3992
262815 ZDOT = 1182
257882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11428652
95 X = -3483453
42
Y = -8226197
75 feet Y = -2507345
07 meter
Z = 16932385
07 Z = 5160990
97
XDOT = 17522
559898 XDOT = 5340
876257
YDOT = -16370
893774 feet/sec YDOT = -4989
848422 meter/sec
ZDOT = 3860
309600 ZDOT = 1176
622366
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 07322
57037305
00020000 00000-0 20000-3 0 9047
2 25544 51
6416 27
9248 0001427 202
6562 157
4540 15
76378871 35135
Satellite: ISS
Catalog Number: 25544
Epoch time: 07322
57037305 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 27
9248 deg
Eccentricity:
0001427
Arg of perigee: 202
6562 deg
Mean anomaly: 157
4540 deg
Mean motion: 15
76378871 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3513
Checksum: 284
Coasting Arc #6 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2007/323/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6280006
04 A = 6725443
83 meter
Y = 2378497
11 meter E =
0010809
Z = -264150
19 I = 51
78453
XDOT = -1472
701359 Wp = 44
63220
YDOT = 4542
501773 meter/sec RA = 22
51854 deg
ZDOT = 6045
749563 TA = 312
50032
MA = 312
59159
Ha = 186
363 n
mi
Hp = 180
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20603694
34 X = 6254225
79
Y = 7803468
22 feet Y = 2448579
56 meter
Z = -866634
47 Z = -233703
89
XDOT = -4831
697373 XDOT = -1552
756566
YDOT = 14903
221039 feet/sec YDOT = 4525
585418 meter/sec
ZDOT = 19835
136363 ZDOT = 6038
400707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15803702
84 X = -4816968
63
Y = 15356990
91 feet Y = 4680810
83 meter
Z = -750465
90 Z = -228742
01
XDOT = -10282
438036 XDOT = -3134
087113
YDOT = -9642
479392 feet/sec YDOT = -2939
027719 meter/sec
ZDOT = 19807
620440 ZDOT = 6037
362710
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
52127446
00020000 00000-0 20000-3 0 9050
2 25544 51
6412 23
0242 0001053 205
4548 154
6565 15
76359568 35286
Satellite: ISS
Catalog Number: 25544
Epoch time: 07323
52127446 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 23
0242 deg
Eccentricity:
0001053
Arg of perigee: 205
4548 deg
Mean anomaly: 154
6565 deg
Mean motion: 15
76359568 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3528
Checksum: 278
Coasting Arc #7 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2007/324/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1929119
72 A = 6713343
19 meter
Y = -3735250
70 meter E =
0014444
Z = -5246473
94 I = 51
71747
XDOT = 7147
043777 Wp = 99
14871
YDOT = 2774
560822 meter/sec RA = 17
36894 deg
ZDOT = 651
861409 TA = 177
05141
MA = 177
04288
Ha = 186
219 n
mi
Hp = 180
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6329132
94 X = 1996231
52
Y = -12254759
51 feet Y = -3713302
82 meter
Z = -17212841
02 Z = -5236939
12
XDOT = 23448
306354 XDOT = 7112
320328
YDOT = 9102
889837 feet/sec YDOT = 2854
288953 meter/sec
ZDOT = 2138
652916 ZDOT = 686
498302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8563301
70 X = 2610094
36
Y = 10869327
88 feet Y = 3312971
14 meter
Z = -17176918
40 Z = -5235524
73
XDOT = -17085
218997 XDOT = -5207
574750
YDOT = 17052
838078 feet/sec YDOT = 5197
705046 meter/sec
ZDOT = 2270
813249 ZDOT = 692
143878
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
53554028
00020000 00000-0 20000-3 0 9063
2 25544 51
6417 17
7965 0001135 207
1660 152
9445 15
76430100 35446
Satellite: ISS
Catalog Number: 25544
Epoch time: 07324
53554028 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 17
7965 deg
Eccentricity:
0001135
Arg of perigee: 207
1660 deg
Mean anomaly: 152
9445 deg
Mean motion: 15
76430100 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3544
Checksum: 271
Coasting Arc #8 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2007/325/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6096102
29 A = 6724149
12 meter
Y = -2455188
04 meter E =
0009054
Z = -1403036
70 I = 51
72732
XDOT = 2972
816580 Wp = 147
84973
YDOT = -4062
997046 meter/sec RA = 12
23995 deg
ZDOT = -5831
457882 TA = 47
57323
MA = 47
49669
Ha = 186
102 n
mi
Hp = 180
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20000335
59 X = -6061379
03
Y = -8055078
88 feet Y = -2523163
92 meter
Z = -4603138
77 Z = -1432568
17
XDOT = 9753
335237 XDOT = 3046
357677
YDOT = -13330
042801 feet/sec YDOT = -4029
341932 meter/sec
ZDOT = -19132
079665 ZDOT = -5816
837022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15248595
39 X = 4647771
88
Y = -15209469
32 feet Y = -4635846
25 meter
Z = -4715823
13 Z = -1437382
89
XDOT = 7280
652869 XDOT = 2219
142994
YDOT = 13189
840057 feet/sec YDOT = 4020
263249 meter/sec
ZDOT = -19076
823183 ZDOT = -5814
615706
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
54977633
00020000 00000-0 20000-3 0 9077
2 25544 51
6423 12
5690 0000974 204
3171 155
7948 15
76507513 35607
Satellite: ISS
Catalog Number: 25544
Epoch time: 07325
54977633 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 12
5690 deg
Eccentricity:
0000974
Arg of perigee: 204
3171 deg
Mean anomaly: 155
7948 deg
Mean motion: 15
76507513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3560
Checksum: 296
Coasting Arc #9 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2007/326/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3245979
53 A = 6714953
11 meter
Y = 3409920
92 meter E =
0006569
Z = 4784264
00 I = 51
66707
XDOT = -6707
414886 Wp = 63
89427
YDOT = -2839
290491 meter/sec RA = 7
05641 deg
ZDOT = -2521
611651 TA = 50
78417
MA = 50
72587
Ha = 186
092 n
mi
Hp = 179
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10649539
15 X = -3307110
39
Y = 11187404
60 feet Y = 3373280
44 meter
Z = 15696404
21 Z = 4768346
23
XDOT = -22005
954350 XDOT = -6662
917056
YDOT = -9315
257518 feet/sec YDOT = -2914
047648 meter/sec
ZDOT = -8273
004103 ZDOT = -2554
089441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6319422
96 X = -1926160
12
Y = -14160643
44 feet Y = -4316164
12 meter
Z = 15636140
24 Z = 4765895
54
XDOT = 15867
053731 XDOT = 4836
277977
YDOT = -16372
819256 feet/sec YDOT = -4990
435309 meter/sec
ZDOT = -8396
939961 ZDOT = -2559
387300
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
56398248
00020000 00000-0 20000-3 0 9080
2 25544 51
6413 7
3415 0000911 210
6839 149
4272 15
76569507 35763
Satellite: ISS
Catalog Number: 25544
Epoch time: 07326
56398248 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 7
3415 deg
Eccentricity:
0000911
Arg of perigee: 210
6839 deg
Mean anomaly: 149
4272 deg
Mean motion: 15
76569507 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3576
Checksum: 305
Coasting Arc #10 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2007/327/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5484510
34 A = 6721020
22 meter
Y = 2517901
03 meter E =
0012993
Z = 2946040
95 I = 51
65849
XDOT = -4449
401477 Wp = 85
42296
YDOT = 3811
723179 meter/sec RA = 1
94701 deg
ZDOT = 5007
642390 TA = 308
58569
MA = 308
70201
Ha = 186
031 n
mi
Hp = 179
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17993800
32 X = 5441635
35
Y = 8260830
15 feet Y = 2578991
91 meter
Z = 9665488
68 Z = 2972581
71
XDOT = -14597
773876 XDOT = -4516
021092
YDOT = 12505
653475 feet/sec YDOT = 3761
594464 meter/sec
ZDOT = 16429
272932 ZDOT = 4985
865019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14174392
79 X = -4320354
92
Y = 13752683
85 feet Y = 4191818
04 meter
Z = 9766786
18 Z = 2976916
43
XDOT = -5363
403200 XDOT = -1634
765295
YDOT = -17177
987073 feet/sec YDOT = -5235
850460 meter/sec
ZDOT = 16346
732839 ZDOT = 4982
484169
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
57816221
00020000 00000-0 20000-3 0 9099
2 25544 51
6410 2
1131 0000693 201
4679 158
6457 15
76568022 35921
Satellite: ISS
Catalog Number: 25544
Epoch time: 07327
57816221 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 2
1131 deg
Eccentricity:
0000693
Arg of perigee: 201
4679 deg
Mean anomaly: 158
6457 deg
Mean motion: 15
76568022 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3592
Checksum: 282
Coasting Arc #11 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2007/328/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463792
90 A = 6718436
32 meter
Y = -3277077
17 meter E =
0006025
Z = -3810858
88 I = 51
62218
XDOT = 5744
525773 Wp = 110
32045
YDOT = 2980
177743 meter/sec RA = 356
74144 deg
ZDOT = 4169
262847 TA = 203
36346
MA = 203
39085
Ha = 185
947 n
mi
Hp = 179
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14644989
82 X = 4518618
93
Y = -10751565
51 feet Y = -3226853
44 meter
Z = -12502817
86 Z = -3789040
38
XDOT = 18846
869333 XDOT = 5690
519883
YDOT = 9777
486032 feet/sec YDOT = 3044
113757 meter/sec
ZDOT = 13678
683882 ZDOT = 4197
039828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5023264
68 X = 1531091
07
Y = 17518597
14 feet Y = 5339668
41 meter
Z = -12420060
71 Z = -3785634
51
XDOT = -14368
162829 XDOT = -4379
416030
YDOT = 13885
195823 feet/sec YDOT = 4232
207687 meter/sec
ZDOT = 13784
733924 ZDOT = 4201
586900
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
52892655
00020000 00000-0 20000-3 0 9102
2 25544 51
6420 357
2118 0000705 210
7580 149
3544 15
76636329 36076
Satellite: ISS
Catalog Number: 25544
Epoch time: 07328
52892655 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 357
2118 deg
Eccentricity:
0000705
Arg of perigee: 210
7580 deg
Mean anomaly: 149
3544 deg
Mean motion: 15
76636329 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3607
Checksum: 290
Coasting Arc #12 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2007/329/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437378
81 A = 6716642
92 meter
Y = -2744142
60 meter E =
0007969
Z = -4238031
36 I = 51
58718
XDOT = 5713
752432 Wp = 71
91654
YDOT = -3711
488600 meter/sec RA = 351
63394 deg
ZDOT = -3582
373841 TA = 161
66125
MA = 161
63250
Ha = 185
832 n
mi
Hp = 179
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14558329
43 X = -4385775
51
Y = -9003092
52 feet Y = -2793474
68 meter
Z = -13904302
36 Z = -4259463
76
XDOT = 18745
906928 XDOT = 5772
233137
YDOT = -12176
799870 feet/sec YDOT = -3647
266635 meter/sec
ZDOT = -11753
195016 ZDOT = -3554
474295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13258222
03 X = 4041106
08
Y = -10720853
85 feet Y = -3267716
25 meter
Z = -13986175
18 Z = -4262986
19
XDOT = 4543
218420 XDOT = 1384
772974
YDOT = 20800
269745 feet/sec YDOT = 6339
922218 meter/sec
ZDOT = -11647
315716 ZDOT = -3550
101830
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
54304799
00020000 00000-0 20000-3 0 9113
2 25544 51
6413 351
9829 0000709 215
2038 144
9080 15
76679887 36230
Satellite: ISS
Catalog Number: 25544
Epoch time: 07329
54304799 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 351
9829 deg
Eccentricity:
0000709
Arg of perigee: 215
2038 deg
Mean anomaly: 144
9080 deg
Mean motion: 15
76679887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3623
Checksum: 315
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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