Date:
March 14th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 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
075/02:53:16
439 -2
3 8
7 8
7
N/A 5
4 -0
3 186
2
000/00:12:32
877 -6
4 0
0 178
5
Coasting Arc #1 (Orbit 3549)
---------------------------------------
Vector Time (GMT): 2007/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 644443
12 A = 6714010
14 meter
Y = 6094266
54 meter E =
0016591
Z = -2747062
89 I = 51
35504
XDOT = -5485
277660 Wp = 310
83578
YDOT = -1741
788140 meter/sec RA = 242
96048 deg
ZDOT = -5120
062648 TA = 260
74671
MA = 260
93439
Ha = 185
319 n
mi
Hp = 174
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2114314
70 X = 589592
87
Y = 19994312
79 feet Y = 6101166
36 meter
Z = -9012673
53 Z = -2744065
49
XDOT = -17996
317783 XDOT = -5440
520951
YDOT = -5714
528017 feet/sec YDOT = -1802
877367 meter/sec
ZDOT = -16798
105802 ZDOT = -5146
601154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6825410
93 X = -2080385
25
Y = 18917570
99 feet Y = 5766075
64 meter
Z = -9000579
32 Z = -2743376
58
XDOT = -12202
188848 XDOT = -3719
227161
YDOT = -12490
472913 feet/sec YDOT = -3807
096144 meter/sec
ZDOT = -16898
063231 ZDOT = -5150
529673
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 07071
48441143
00020000 00000-0 20000-3 0 9003
2 25544 51
6297 243
6505 0021320 308
7749 51
1512 15
79243643 35505
Satellite: ISS
Catalog Number: 25544
Epoch time: 07071
48441143 = yrday
fracday
Element set: 900
Inclination: 51
6297 deg
RA of node: 243
6505 deg
Eccentricity:
0021320
Arg of perigee: 308
7749 deg
Mean anomaly: 51
1512 deg
Mean motion: 15
79243643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3550
Checksum: 270
Coasting Arc #2 (Orbit 3565)
---------------------------------------
Vector Time (GMT): 2007/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5022680
57 A = 6712351
29 meter
Y = 3004019
37 meter E =
0014520
Z = 3304751
67 I = 51
36406
XDOT = -565
084548 Wp = 347
45001
YDOT = 6092
044882 meter/sec RA = 237
71392 deg
ZDOT = -4668
692834 TA = 153
53871
MA = 153
46449
Ha = 185
521 n
mi
Hp = 173
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16478610
80 X = 4972662
23
Y = 9855706
59 feet Y = 3059906
15 meter
Z = 10842361
11 Z = 3329030
01
XDOT = -1853
951929 XDOT = -610
485305
YDOT = 19987
023892 feet/sec YDOT = 6085
471914 meter/sec
ZDOT = -15317
233708 ZDOT = -4671
548293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10705725
49 X = 3263105
13
Y = 15876751
72 feet Y = 4839233
93 meter
Z = 10934009
21 Z = 3332686
01
XDOT = -8901
860347 XDOT = -2713
287034
YDOT = 16580
756295 feet/sec YDOT = 5053
814519 meter/sec
ZDOT = -15327
128678 ZDOT = -4671
708821
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 07072
49686494
00020000 00000-0 20000-3 0 9016
2 25544 51
6295 238
4083 0021417 312
2159 47
7189 15
79279270 35661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07072
49686494 = yrday
fracday
Element set: 901
Inclination: 51
6295 deg
RA of node: 238
4083 deg
Eccentricity:
0021417
Arg of perigee: 312
2159 deg
Mean anomaly: 47
7189 deg
Mean motion: 15
79279270 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3566
Checksum: 319
Coasting Arc #3 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2007/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1768730
31 A = 6706476
93 meter
Y = -4183956
03 meter E =
0015430
Z = 4938391
71 I = 51
35985
XDOT = 5696
269381 Wp = 321
53861
YDOT = 4778
461808 meter/sec RA = 232
55931 deg
ZDOT = 2023
578578 TA = 108
89863
MA = 108
73129
Ha = 185
718 n
mi
Hp = 173
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5802920
96 X = 1791395
05
Y = -13726889
88 feet Y = -4164050
31 meter
Z = 16202072
53 Z = 4947039
16
XDOT = 18688
547839 XDOT = 5632
582569
YDOT = 15677
368135 feet/sec YDOT = 4841
804615 meter/sec
ZDOT = 6639
037330 ZDOT = 2051
095814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10810326
62 X = 3294987
55
Y = -10207979
03 feet Y = -3111392
01 meter
Z = 16233993
78 Z = 4948121
30
XDOT = 9900
137214 XDOT = 3017
561823
YDOT = 21128
431967 feet/sec YDOT = 6439
946063 meter/sec
ZDOT = 6743
115676 ZDOT = 2055
301658
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 07073
50929628
00020000 00000-0 20000-3 0 9029
2 25544 51
6288 233
1659 0021283 316
6331 43
3159 15
79281514 35826
Satellite: ISS
Catalog Number: 25544
Epoch time: 07073
50929628 = yrday
fracday
Element set: 902
Inclination: 51
6288 deg
RA of node: 233
1659 deg
Eccentricity:
0021283
Arg of perigee: 316
6331 deg
Mean anomaly: 43
3159 deg
Mean motion: 15
79281514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3582
Checksum: 297
Coasting Arc #4 (Orbit 3596)
---------------------------------------
Vector Time (GMT): 2007/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4552136
74 A = 6717028
88 meter
Y = -4916420
41 meter E =
0025397
Z = -21083
17 I = 51
41511
XDOT = 3518
746128 Wp = 349
02170
YDOT = -3288
882561 meter/sec RA = 227
34710 deg
ZDOT = 6036
587297 TA = 10
74766
MA = 10
69349
Ha = 185
836 n
mi
Hp = 173
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14934831
83 X = -4496719
89
Y = -16129988
22 feet Y = -4967015
10 meter
Z = -69170
50 Z = -43062
23
XDOT = 11544
442678 XDOT = 3525
937302
YDOT = -10790
297117 feet/sec YDOT = -3249
493565 meter/sec
ZDOT = 19805
076433 ZDOT = 6053
698598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7422565
73 X = -2262398
04
Y = -20690886
35 feet Y = -6306582
16 meter
Z = -152468
19 Z = -46472
31
XDOT = 13238
232415 XDOT = 4035
013240
YDOT = -4908
158944 feet/sec YDOT = -1496
006846 meter/sec
ZDOT = 19868
932305 ZDOT = 6056
050567
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 07074
45842505
00020000 00000-0 20000-3 0 9033
2 25544 51
6292 228
2516 0021161 320
1425 39
8186 15
79341415 35970
Satellite: ISS
Catalog Number: 25544
Epoch time: 07074
45842505 = yrday
fracday
Element set: 903
Inclination: 51
6292 deg
RA of node: 228
2516 deg
Eccentricity:
0021161
Arg of perigee: 320
1425 deg
Mean anomaly: 39
8186 deg
Mean motion: 15
79341415 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3597
Checksum: 285
Coasting Arc #5 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2007/075/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4207073
16 A = 6721402
18 meter
Y = 5148333
67 meter E =
0005587
Z = -993547
95 I = 51
42951
XDOT = -4320
058077 Wp = 297
84980
YDOT = 2384
178048 meter/sec RA = 223
90125 deg
ZDOT = -5910
728073 TA = 253
04660
MA = 253
10785
Ha = 186
236 n
mi
Hp = 178
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13802733
45 X = 4154017
45
Y = 16890858
49 feet Y = 5195082
81 meter
Z = -3259671
75 Z = -973239
55
XDOT = -14173
418889 XDOT = -4317
684573
YDOT = 7822
106458 feet/sec YDOT = 2335
881715 meter/sec
ZDOT = -19392
152470 ZDOT = -5931
708831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21245706
84 X = -6475691
45
Y = -4993288
83 feet Y = -1521954
44 meter
Z = -3182611
89 Z = -970060
10
XDOT = 6037
076806 XDOT = 1840
101011
YDOT = -13217
053822 feet/sec YDOT = -4028
558005 meter/sec
ZDOT = -19470
680274 ZDOT = -5934
663348
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 07075
15448061
00020000 00000-0 20000-3 0 9041
2 25544 51
6316 224
6532 0015207 313
1832 46
8061 15
77647762 36088
Satellite: ISS
Catalog Number: 25544
Epoch time: 07075
15448061 = yrday
fracday
Element set: 904
Inclination: 51
6316 deg
RA of node: 224
6532 deg
Eccentricity:
0015207
Arg of perigee: 313
1832 deg
Mean anomaly: 46
8061 deg
Mean motion: 15
77647762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3608
Checksum: 281
Coasting Arc #6 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2007/076/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4561601
87 A = 6711630
87 meter
Y = -1228764
36 meter E =
0015430
Z = 4776763
41 I = 51
41855
XDOT = 4224
168807 Wp = 344
40702
YDOT = 5933
275087 meter/sec RA = 218
69252 deg
ZDOT = -2494
852131 TA = 130
15111
MA = 130
01586
Ha = 186
399 n
mi
Hp = 178
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14965885
40 X = 4551798
87
Y = -4031379
15 feet Y = -1177808
41 meter
Z = 15671795
95 Z = 4798899
52
XDOT = 13858
821546 XDOT = 4169
627430
YDOT = 19466
125615 feet/sec YDOT = 5980
206952 meter/sec
ZDOT = -8185
210405 ZDOT = -2474
464474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9141085
67 X = -2786202
91
Y = 12412120
67 feet Y = 3783214
38 meter
Z = 15754832
45 Z = 4802072
93
XDOT = -22090
798724 XDOT = -6733
275451
YDOT = -5924
911900 feet/sec YDOT = -1805
913147 meter/sec
ZDOT = -8107
728706 ZDOT = -2471
235710
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 07076
16794712
00020000 00000-0 20000-3 0 9051
2 25544 51
6315 219
4192 0015293 317
3756 42
6222 15
77695785 36246
Satellite: ISS
Catalog Number: 25544
Epoch time: 07076
16794712 = yrday
fracday
Element set: 905
Inclination: 51
6315 deg
RA of node: 219
4192 deg
Eccentricity:
0015293
Arg of perigee: 317
3756 deg
Mean anomaly: 42
6222 deg
Mean motion: 15
77695785 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3624
Checksum: 309
Coasting Arc #7 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2007/077/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2970240
32 A = 6717075
03 meter
Y = -5068142
16 meter E =
0012993
Z = 3240821
51 I = 51
46093
XDOT = 6056
627194 Wp = 15
00592
YDOT = -519
507859 meter/sec RA = 213
55854 deg
ZDOT = 4746
660754 TA = 23
13292
MA = 23
07448
Ha = 186
685 n
mi
Hp = 177
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9744882
95 X = -2929089
96
Y = -16627762
98 feet Y = -5101126
63 meter
Z = 10632616
50 Z = 3226492
78
XDOT = 19870
824127 XDOT = 6038
928195
YDOT = -1704
422109 feet/sec YDOT = -451
877732 meter/sec
ZDOT = 15573
033970 ZDOT = 4776
040459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18136296
23 X = 5527943
09
Y = 6608927
13 feet Y = 2014400
99 meter
Z = 10578025
35 Z = 3224182
13
XDOT = -13710
617223 XDOT = -4178
996130
YDOT = 12565
478980 feet/sec YDOT = 3829
957993 meter/sec
ZDOT = 15683
404462 ZDOT = 4780
301680
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 07077
18139077
00020000 00000-0 20000-3 0 9062
2 25544 51
6322 214
1841 0015335 321
5610 38
4461 15
77717372 36403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07077
18139077 = yrday
fracday
Element set: 906
Inclination: 51
6322 deg
RA of node: 214
1841 deg
Eccentricity:
0015335
Arg of perigee: 321
5610 deg
Mean anomaly: 38
4461 deg
Mean motion: 15
77717372 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3640
Checksum: 277
Coasting Arc #8 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2007/078/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5863490
04 A = 6716739
74 meter
Y = -221790
46 meter E =
0013627
Z = -3251186
50 I = 51
48619
XDOT = -2412
616104 Wp = 342
81589
YDOT = -5586
323141 meter/sec RA = 208
33111 deg
ZDOT = 4740
017960 TA = 338
91139
MA = 338
96752
Ha = 186
704 n
mi
Hp = 177
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19237172
04 X = -5844780
62
Y = -727659
00 feet Y = -287255
05 meter
Z = -10666622
38 Z = -3279625
61
XDOT = -7915
407165 XDOT = -2372
995680
YDOT = -18327
831829 feet/sec YDOT = -5613
080295 meter/sec
ZDOT = 15551
240026 ZDOT = 4728
394450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15067685
45 X = 4592630
52
Y = -11885715
21 feet Y = -3622766
00 meter
Z = -10773566
63 Z = -3283783
11
XDOT = 17111
826283 XDOT = 5215
684651
YDOT = 7660
075248 feet/sec YDOT = 2334
790936 meter/sec
ZDOT = 15506
739078 ZDOT = 4726
454071
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 07078
13147177
00020000 00000-0 20000-3 0 9079
2 25544 51
6331 209
2770 0015402 325
1447 34
8708 15
77771874 36559
Satellite: ISS
Catalog Number: 25544
Epoch time: 07078
13147177 = yrday
fracday
Element set: 907
Inclination: 51
6331 deg
RA of node: 209
2770 deg
Eccentricity:
0015402
Arg of perigee: 325
1447 deg
Mean anomaly: 34
8708 deg
Mean motion: 15
77771874 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3655
Checksum: 300
Coasting Arc #9 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2007/079/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1057051
74 A = 6711359
85 meter
Y = 4595210
76 meter E =
0017266
Z = -4785315
91 I = 51
49478
XDOT = -7224
705163 Wp = 11
05052
YDOT = -943
928751 meter/sec RA = 203
20165 deg
ZDOT = -2487
124213 TA = 234
48708
MA = 234
64825
Ha = 187
007 n
mi
Hp = 177
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3468017
52 X = 1028835
03
Y = 15076150
80 feet Y = 4606873
03 meter
Z = -15699855
34 Z = -4780249
79
XDOT = -23703
100929 XDOT = -7201
531082
YDOT = -3096
879105 feet/sec YDOT = -1024
590140 meter/sec
ZDOT = -8159
856341 ZDOT = -2522
165368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12641033
73 X = -3852987
08
Y = -8952103
43 feet Y = -2728601
13 meter
Z = -15680147
85 Z = -4779309
06
XDOT = 19134
853419 XDOT = 5832
303322
YDOT = -12408
880926 feet/sec YDOT = -3782
226906 meter/sec
ZDOT = -8291
727969 ZDOT = -2527
318685
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 07079
14486875
00020000 00000-0 20000-3 0 9083
2 25544 51
6337 204
0429 0015515 329
3157 30
7099 15
77823189 36711
Satellite: ISS
Catalog Number: 25544
Epoch time: 07079
14486875 = yrday
fracday
Element set: 908
Inclination: 51
6337 deg
RA of node: 204
0429 deg
Eccentricity:
0015515
Arg of perigee: 329
3157 deg
Mean anomaly: 30
7099 deg
Mean motion: 15
77823189 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3671
Checksum: 316
Coasting Arc #10 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2007/080/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6523106
23 A = 6720929
88 meter
Y = 1336273
08 meter E =
0007322
Z = 938114
12 I = 51
55391
XDOT = -147
255388 Wp = 36
02138
YDOT = 4903
440278 meter/sec RA = 197
99905 deg
ZDOT = -5931
441402 TA = 133
71775
MA = 133
65708
Ha = 187
176 n
mi
Hp = 177
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21401267
16 X = 6503121
82
Y = 4384098
02 feet Y = 1409106
44 meter
Z = 3077802
25 Z = 969754
81
XDOT = -483
121351 XDOT = -173
261461
YDOT = 16087
402486 feet/sec YDOT = 4901
647689 meter/sec
ZDOT = -19460
109588 ZDOT = -5932
220344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18745023
56 X = -5713483
18
Y = 11185303
44 feet Y = 3409280
49 meter
Z = 3196951
19 Z = 974430
72
XDOT = -9757
836681 XDOT = -2974
188620
YDOT = -10763
746716 feet/sec YDOT = -3280
789999 meter/sec
ZDOT = -19462
334651 ZDOT = -5932
119602
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 07080
15824302
00020000 00000-0 20000-3 0 9098
2 25544 51
6335 198
8082 0015442 333
0113 27
0247 15
77812515 36879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07080
15824302 = yrday
fracday
Element set: 909
Inclination: 51
6335 deg
RA of node: 198
8082 deg
Eccentricity:
0015442
Arg of perigee: 333
0113 deg
Mean anomaly: 27
0247 deg
Mean motion: 15
77812515 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3687
Checksum: 279
Coasting Arc #11 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2007/081/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1380565
95 A = 6709042
33 meter
Y = -3956602
63 meter E =
0015600
Z = 5243350
16 I = 51
54245
XDOT = 7421
933471 Wp = 346
44961
YDOT = 2025
540217 meter/sec RA = 192
83297 deg
ZDOT = -411
045532 TA = 107
54238
MA = 107
37187
Ha = 187
246 n
mi
Hp = 176
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4529415
83 X = 1399235
28
Y = -12980979
76 feet Y = -3941059
72 meter
Z = 17202592
38 Z = 5250102
53
XDOT = 24350
175431 XDOT = 7400
728769
YDOT = 6645
473154 feet/sec YDOT = 2108
417847 meter/sec
ZDOT = -1348
574579 ZDOT = -375
041234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5697126
63 X = 1736484
20
Y = 12478361
32 feet Y = 3803404
53 meter
Z = 17227416
38 Z = 5250916
51
XDOT = -21354
203141 XDOT = -6508
761118
YDOT = 11490
395280 feet/sec YDOT = 3502
272481 meter/sec
ZDOT = -1212
913496 ZDOT = -369
696034
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 07081
17159040
00020000 00000-0 20000-3 0 9103
2 25544 51
6337 193
5732 0015668 336
7723 23
2733 15
77905249 37036
Satellite: ISS
Catalog Number: 25544
Epoch time: 07081
17159040 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 193
5732 deg
Eccentricity:
0015668
Arg of perigee: 336
7723 deg
Mean anomaly: 23
2733 deg
Mean motion: 15
77905249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3703
Checksum: 291
Coasting Arc #12 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2007/082/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6142990
27 A = 6719984
12 meter
Y = -2133824
15 meter E =
0022574
Z = 1632501
88 I = 51
60719
XDOT = 2985
903526 Wp = 19
47568
YDOT = -4195
187572 meter/sec RA = 187
68145 deg
ZDOT = 5750
549279 TA = 358
62298
MA = 358
62918
Ha = 187
566 n
mi
Hp = 176
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20154167
55 X = -6126603
40
Y = -7000735
41 feet Y = -2202426
85 meter
Z = 5355977
28 Z = 1602699
00
XDOT = 9796
271412 XDOT = 3004
657588
YDOT = -13763
738754 feet/sec YDOT = -4161
692541 meter/sec
ZDOT = 18866
631494 ZDOT = 5765
100487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19321710
36 X = 5889257
32
Y = -9113908
86 feet Y = -2777919
42 meter
Z = 5243608
71 Z = 1598251
94
XDOT = 2036
348560 XDOT = 620
679041
YDOT = 15206
309172 feet/sec YDOT = 4634
883035 meter/sec
ZDOT = 18920
753194 ZDOT = 5767
045574
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 07082
18491665
00020000 00000-0 20000-3 0 9118
2 25544 51
6333 188
3381 0015825 340
9731 19
0841 15
77905647 37197
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
18491665 = yrday
fracday
Element set: 911
Inclination: 51
6333 deg
RA of node: 188
3381 deg
Eccentricity:
0015825
Arg of perigee: 340
9731 deg
Mean anomaly: 19
0841 deg
Mean motion: 15
77905647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3719
Checksum: 307
Coasting Arc #13 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2007/083/02:59:32
877
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3737167
59 A = 6712209
58 meter
Y = 3363371
39 meter E =
0012777
Z = -4444718
73 I = 51
60992
XDOT = -6391
255035 Wp = 22
62295
YDOT = -2843
262770 meter/sec RA = 182
47452 deg
ZDOT = 3236
958469 TA = 279
70294
MA = 279
84723
Ha = 187
564 n
mi
Hp = 176
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12261048
51 X = -3752907
91
Y = 11034683
05 feet Y = 3321492
27 meter
Z = -14582410
54 Z = -4462912
12
XDOT = -20968
684497 XDOT = -6374
710797
YDOT = -9328
289927 feet/sec YDOT = -2914
640843 meter/sec
ZDOT = 10619
942482 ZDOT = 3205
949973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 704127
49 X = 214618
06
Y = -16419973
07 feet Y = -5004807
79 meter
Z = -14650355
85 Z = -4465428
46
XDOT = 20213
939248 XDOT = 6161
208683
YDOT = -8461
489232 feet/sec YDOT = -2579
061918 meter/sec
ZDOT = 10502
928612 ZDOT = 3201
292641
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 07083
13488632
00020000 00000-0 20000-3 0 9125
2 25544 51
6328 183
4303 0015860 344
2454 15
8215 15
77957210 37348
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
13488632 = yrday
fracday
Element set: 912
Inclination: 51
6328 deg
RA of node: 183
4303 deg
Eccentricity:
0015860
Arg of perigee: 344
2454 deg
Mean anomaly: 15
8215 deg
Mean motion: 15
77957210 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3734
Checksum: 285
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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