Date:
December 6th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 3778)
---------------------------------------
Vector Time (GMT): 2007/339/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2444971
82 A = 6712604
78 meter
Y = -3751987
84 meter E =
0012532
Z = -5011642
92 I = 51
34132
XDOT = 4955
116290 Wp = 103
82699
YDOT = -5611
942327 meter/sec RA = 300
44873 deg
ZDOT = 1784
787892 TA = 183
44477
MA = 183
45340
Ha = 185
166 n
mi
Hp = 179
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8021561
08 X = -2378488
64
Y = -12309671
41 feet Y = -3778956
73 meter
Z = -16442398
05 Z = -5023359
69
XDOT = 16256
943210 XDOT = 5008
831245
YDOT = -18411
884276 feet/sec YDOT = -5556
231231 meter/sec
ZDOT = 5855
603320 ZDOT = 1808
990331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14199169
20 X = 4327906
77
Y = 3574231
60 feet Y = 1089425
79 meter
Z = -16487400
30 Z = -5025359
61
XDOT = 988
832329 XDOT = 301
396094
YDOT = 23493
625354 feet/sec YDOT = 7160
857008 meter/sec
ZDOT = 5947
222248 ZDOT = 1812
713341
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 07339
42944669
00020000 00000-0 20000-3 0 9005
2 25544 51
6370 301
0096 0000830 277
1851 82
9220 15
77016612 37790
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
42944669 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 301
0096 deg
Eccentricity:
0000830
Arg of perigee: 277
1851 deg
Mean anomaly: 82
9220 deg
Mean motion: 15
77016612 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3779
Checksum: 287
Coasting Arc #2 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2007/340/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4339513
47 A = 6720639
82 meter
Y = 4471557
85 meter E =
0004529
Z = -2516050
01 I = 51
35504
XDOT = -2240
072652 Wp = 133
18032
YDOT = -5140
124346 meter/sec RA = 295
30536 deg
ZDOT = -5280
589811 TA = 75
46533
MA = 75
41509
Ha = 185
100 n
mi
Hp = 179
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14237248
90 X = -4376969
79
Y = 14670465
39 feet Y = 4422821
79 meter
Z = -8254757
24 Z = -2537222
34
XDOT = -7349
319725 XDOT = -2156
775795
YDOT = -16863
925021 feet/sec YDOT = -5164
707802 meter/sec
ZDOT = -17324
769721 ZDOT = -5291
270550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8491
00 X = -2588
06
Y = -20410568
97 feet Y = -6221141
42 meter
Z = -8334952
33 Z = -2540493
47
XDOT = 15451
332641 XDOT = 4709
566189
YDOT = 7073
250138 feet/sec YDOT = 2155
926642 meter/sec
ZDOT = -17365
965094 ZDOT = -5293
146161
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 07340
44330772
00020000 00000-0 20000-3 0 9014
2 25544 51
6366 295
7782 0000748 284
2581 75
8501 15
77068864 37950
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
44330772 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 295
7782 deg
Eccentricity:
0000748
Arg of perigee: 284
2581 deg
Mean anomaly: 75
8501 deg
Mean motion: 15
77068864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3795
Checksum: 316
Coasting Arc #3 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2007/341/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1533011
56 A = 6716274
55 meter
Y = 5158708
11 meter E =
0010026
Z = 4011824
92 I = 51
32913
XDOT = -4934
813964 Wp = 74
49466
YDOT = 4483
165687 meter/sec RA = 290
07675 deg
ZDOT = -3868
429221 TA = 55
55321
MA = 55
45851
Ha = 184
968 n
mi
Hp = 179
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5029565
50 X = 1455723
02
Y = 16924895
37 feet Y = 5175418
46 meter
Z = 13162155
25 Z = 4019085
38
XDOT = -16190
334529 XDOT = -4965
786096
YDOT = 14708
548841 feet/sec YDOT = 4427
809121 meter/sec
ZDOT = -12691
696920 ZDOT = -3892
477734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15479926
30 X = -4718281
54
Y = -8448558
55 feet Y = -2575120
65 meter
Z = 13190325
38 Z = 4020411
17
XDOT = 359
354768 XDOT = 109
531333
YDOT = -20670
148604 feet/sec YDOT = -6300
261294 meter/sec
ZDOT = -12782
850574 ZDOT = -3896
212855
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 07341
45714747
00020000 00000-0 20000-3 0 9025
2 25544 51
6364 290
5474 0000937 290
3680 69
7384 15
77112686 38119
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
45714747 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 290
5474 deg
Eccentricity:
0000937
Arg of perigee: 290
3680 deg
Mean anomaly: 69
7384 deg
Mean motion: 15
77112686 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3811
Checksum: 306
Coasting Arc #4 (Orbit 3826)
---------------------------------------
Vector Time (GMT): 2007/342/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247872
83 A = 6715767
71 meter
Y = -3198006
20 meter E =
0009455
Z = 4096131
33 I = 51
31961
XDOT = 1344
573495 Wp = 104
24223
YDOT = 6599
903646 meter/sec RA = 284
94671 deg
ZDOT = 3748
903686 TA = 307
17978
MA = 307
26607
Ha = 184
804 n
mi
Hp = 179
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936590
65 X = 4263419
05
Y = -10492146
31 feet Y = -3150417
75 meter
Z = 13438751
09 Z = 4116805
21
XDOT = 4411
330364 XDOT = 1252
460582
YDOT = 21653
227185 feet/sec YDOT = 6614
423851 meter/sec
ZDOT = 12299
552775 ZDOT = 3755
212973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2068209
83 X = -630390
35
Y = 17260416
15 feet Y = 5260974
84 meter
Z = 13517184
12 Z = 4120037
72
XDOT = -17342
257569 XDOT = -5285
920107
YDOT = -11753
818840 feet/sec YDOT = -3582
563983 meter/sec
ZDOT = 12324
244574 ZDOT = 3756
429746
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 07342
47096665
00020000 00000-0 20000-3 0 9031
2 25544 51
6367 285
3169 0000994 287
0686 73
0370 15
77166717 38271
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
47096665 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 285
3169 deg
Eccentricity:
0000994
Arg of perigee: 287
0686 deg
Mean anomaly: 73
0370 deg
Mean motion: 15
77166717 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3827
Checksum: 324
Coasting Arc #5 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2007/343/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -865296
41 A = 6720725
62 meter
Y = -6224231
33 meter E =
0005469
Z = -2378451
56 I = 51
32991
XDOT = 4818
452455 Wp = 37
48835
YDOT = -2714
698114 meter/sec RA = 279
71740 deg
ZDOT = 5361
913077 TA = 295
55073
MA = 295
60726
Ha = 184
989 n
mi
Hp = 179
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2838899
00 X = -784077
53
Y = -20420706
47 feet Y = -6233453
07 meter
Z = -7803318
77 Z = -2382458
96
XDOT = 15808
571045 XDOT = 4822
402872
YDOT = -8906
489874 feet/sec YDOT = -2660
794224 meter/sec
ZDOT = 17591
578337 ZDOT = 5385
330667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16846586
34 X = 5134839
52
Y = 11874717
74 feet Y = 3619413
97 meter
Z = -7819206
55 Z = -2383294
16
XDOT = -3325
310329 XDOT = -1013
554588
YDOT = 16336
635251 feet/sec YDOT = 4979
406424 meter/sec
ZDOT = 17680
517630 ZDOT = 5389
021774
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 07343
42140561
00020000 00000-0 20000-3 0 9043
2 25544 51
6367 280
4127 0000851 302
7124 57
3958 15
77156040 38427
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
42140561 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 280
4127 deg
Eccentricity:
0000851
Arg of perigee: 302
7124 deg
Mean anomaly: 57
3958 deg
Mean motion: 15
77156040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3842
Checksum: 272
Coasting Arc #6 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2007/344/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183385
25 A = 6711850
45 meter
Y = 1426335
92 meter E =
0013138
Z = -5062829
11 I = 51
29724
XDOT = -660
973061 Wp = 75
06554
YDOT = -7505
656120 meter/sec RA = 274
56829 deg
ZDOT = -1568
435909 TA = 179
79705
MA = 179
79652
Ha = 184
929 n
mi
Hp = 179
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13725017
23 X = -4174429
23
Y = 4679579
79 feet Y = 1379605
87 meter
Z = -16610331
73 Z = -5083130
25
XDOT = -2168
546789 XDOT = -569
375280
YDOT = -24624
856038 feet/sec YDOT = -7512
535080 meter/sec
ZDOT = -5145
787104 ZDOT = -1571
425738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5640248
71 X = 1719147
81
Y = -13262409
03 feet Y = -4042382
27 meter
Z = -16687533
86 Z = -5086360
32
XDOT = 18767
796568 XDOT = 5720
424394
YDOT = 14471
396754 feet/sec YDOT = 4410
881731 meter/sec
ZDOT = -5157
930320 ZDOT = -1572
137161
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 07344
43518638
00020000 00000-0 20000-3 0 9050
2 25544 51
6373 275
1812 0000949 303
8329 56
2745 15
77187876 38583
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
43518638 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 275
1812 deg
Eccentricity:
0000949
Arg of perigee: 303
8329 deg
Mean anomaly: 56
2745 deg
Mean motion: 15
77187876 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3858
Checksum: 325
Coasting Arc #7 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2007/345/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 308621
24 A = 6722969
94 meter
Y = 6703808
39 meter E =
0011803
Z = 293432
06 I = 51
33447
XDOT = -4801
896538 Wp = 132
14021
YDOT = 490
418566 meter/sec RA = 269
36916 deg
ZDOT = -6007
526368 TA = 44
65265
MA = 44
55766
Ha = 184
865 n
mi
Hp = 179
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1012536
86 X = 232209
84
Y = 21994122
00 feet Y = 6706832
28 meter
Z = 962703
60 Z = 294746
89
XDOT = -15754
253734 XDOT = -4777
839894
YDOT = 1608
984798 feet/sec YDOT = 436
856573 meter/sec
ZDOT = -19709
732177 ZDOT = -6030
795642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17259651
83 X = -5260741
88
Y = -13669677
06 feet Y = -4166517
57 meter
Z = 968390
24 Z = 295165
34
XDOT = 8051
669766 XDOT = 2454
148945
YDOT = -11602
567855 feet/sec YDOT = -3536
462682 meter/sec
ZDOT = -19798
344591 ZDOT = -6034
535431
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 07345
44894684
00020000 00000-0 20000-3 0 9061
2 25544 51
6376 269
9503 0001025 309
4079 50
6995 15
77228764 38749
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
44894684 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 269
9503 deg
Eccentricity:
0001025
Arg of perigee: 309
4079 deg
Mean anomaly: 50
6995 deg
Mean motion: 15
77228764 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3874
Checksum: 332
Coasting Arc #8 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2007/346/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228904
77 A = 6711099
30 meter
Y = 587634
99 meter E =
0003281
Z = 5176323
65 I = 51
29644
XDOT = 49
686479 Wp = 40
48186
YDOT = 7654
416846 meter/sec RA = 264
18156 deg
ZDOT = -906
763820 TA = 58
20405
MA = 58
17210
Ha = 184
705 n
mi
Hp = 179
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13874359
48 X = 4196873
72
Y = 1927936
32 feet Y = 634745
06 meter
Z = 16982689
14 Z = 5196790
03
XDOT = 163
013382 XDOT = -31
505158
YDOT = 25112
916161 feet/sec YDOT = 7654
518651 meter/sec
ZDOT = -2974
946915 ZDOT = -906
718410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10335890
17 X = -3150379
33
Y = 9312737
53 feet Y = 2838522
40 meter
Z = 17060738
97 Z = 5200113
24
XDOT = -18669
798464 XDOT = -5690
554572
YDOT = -15256
014101 feet/sec YDOT = -4650
033098 meter/sec
ZDOT = -2973
993138 ZDOT = -906
473108
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 07346
46268749
00020000 00000-0 20000-3 0 9072
2 25544 51
6377 264
7199 0001057 312
7048 47
4028 15
77257794 38906
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
46268749 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 264
7199 deg
Eccentricity:
0001057
Arg of perigee: 312
7048 deg
Mean anomaly: 47
4028 deg
Mean motion: 15
77257794 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3890
Checksum: 330
Coasting Arc #9 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2007/347/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 255271
67 A = 6721326
59 meter
Y = -6449997
95 meter E =
0013772
Z = 1848168
38 I = 51
33526
XDOT = 4941
732335 Wp = 62
38936
YDOT = 1816
370996 meter/sec RA = 259
02283 deg
ZDOT = 5630
811651 TA = 318
25224
MA = 318
35724
Ha = 184
765 n
mi
Hp = 178
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 837505
47 X = 318399
49
Y = -21161410
61 feet Y = -6446790
67 meter
Z = 6063544
56 Z = 1849560
88
XDOT = 16213
032595 XDOT = 4893
700655
YDOT = 5959
222429 feet/sec YDOT = 1871
362863 meter/sec
ZDOT = 18473
791505 ZDOT = 5654
702189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15932754
63 X = 4856303
61
Y = 13949829
62 feet Y = 4251908
07 meter
Z = 6068185
08 Z = 1849582
81
XDOT = -13755
899310 XDOT = -4192
798110
YDOT = 7598
871720 feet/sec YDOT = 2316
136100 meter/sec
ZDOT = 18565
025618 ZDOT = 5658
619808
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 07347
47640760
00020000 00000-0 20000-3 0 9082
2 25544 51
6374 259
4883 0001065 313
6648 46
4428 15
77297509 39068
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
47640760 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 259
4883 deg
Eccentricity:
0001065
Arg of perigee: 313
6648 deg
Mean anomaly: 46
4428 deg
Mean motion: 15
77297509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3906
Checksum: 322
Coasting Arc #10 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2007/348/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4404979
16 A = 6714195
82 meter
Y = -2517253
54 meter E =
0008524
Z = -4406136
70 I = 51
31828
XDOT = 704
110744 Wp = 107
19623
YDOT = -6937
656443 meter/sec RA = 253
79829 deg
ZDOT = 3262
305698 TA = 195
66707
MA = 195
69346
Ha = 184
741 n
mi
Hp = 178
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14452031
36 X = -4355099
28
Y = -8258705
83 feet Y = -2566233
06 meter
Z = -14455829
08 Z = -4427415
22
XDOT = 2310
074618 XDOT = 765
788675
YDOT = -22761
340035 feet/sec YDOT = -6929
438229 meter/sec
ZDOT = 10703
102685 ZDOT = 3265
875207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15359922
36 X = 4681704
34
Y = -6227461
06 feet Y = -1898130
13 meter
Z = -14537191
63 Z = -4430936
01
XDOT = 16084
902884 XDOT = 4902
678399
YDOT = 14678
675578 feet/sec YDOT = 4474
060316 meter/sec
ZDOT = 10715
980448 ZDOT = 3266
230841
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 07348
42675305
00020000 00000-0 20000-3 0 9092
2 25544 51
6374 254
5837 0001146 318
4537 41
6541 15
77315290 39211
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
42675305 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 254
5837 deg
Eccentricity:
0001146
Arg of perigee: 318
4537 deg
Mean anomaly: 41
6541 deg
Mean motion: 15
77315290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3921
Checksum: 295
Coasting Arc #11 (Orbit 3936)
---------------------------------------
Vector Time (GMT): 2007/349/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1055238
40 A = 6716554
14 meter
Y = 5492183
14 meter E =
0005641
Z = -3725860
08 I = 51
33640
XDOT = -5144
306970 Wp = 66
20808
YDOT = -3858
933523 meter/sec RA = 248
66496 deg
ZDOT = -4234
176808 TA = 159
03188
MA = 159
00874
Ha = 184
732 n
mi
Hp = 178
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3462068
25 X = -1098474
87
Y = 18018973
54 feet Y = 5480141
50 meter
Z = -12223950
40 Z = -3731090
87
XDOT = -16877
647540 XDOT = -5080
204608
YDOT = -12660
543053 feet/sec YDOT = -3916
101225 meter/sec
ZDOT = -13891
656194 ZDOT = -4259
012528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12334786
49 X = -3759642
92
Y = -13566459
26 feet Y = -4135056
78 meter
Z = -12243304
82 Z = -3731759
31
XDOT = 19237
644962 XDOT = 5863
634184
YDOT = -4876
803134 feet/sec YDOT = -1486
449595 meter/sec
ZDOT = -13986
728941 ZDOT = -4263
154981
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 07349
44043586
00020000 00000-0 20000-3 0 9107
2 25544 51
6378 249
3517 0001156 325
2578 34
8511 15
77361111 39375
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
44043586 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 249
3517 deg
Eccentricity:
0001156
Arg of perigee: 325
2578 deg
Mean anomaly: 34
8511 deg
Mean motion: 15
77361111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3937
Checksum: 294
Coasting Arc #12 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2007/350/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4542437
44 A = 6719078
66 meter
Y = 4071934
03 meter E =
0012752
Z = 2803729
86 I = 51
35704
XDOT = -1789
680037 Wp = 95
54020
YDOT = 5510
170149 meter/sec RA = 243
43269 deg
ZDOT = -5084
469468 TA = 52
13819
MA = 52
02289
Ha = 184
665 n
mi
Hp = 178
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14903009
96 X = 4482946
81
Y = 13359363
61 feet Y = 4122397
27 meter
Z = 9198588
77 Z = 2825652
91
XDOT = -5871
653666 XDOT = -1826
463111
YDOT = 18077
986054 feet/sec YDOT = 5489
951707 meter/sec
ZDOT = -16681
330277 ZDOT = -5093
252619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19542332
88 X = -5956503
06
Y = 4137274
98 feet Y = 1261041
41 meter
Z = 9282592
24 Z = 2829334
11
XDOT = -10908
372831 XDOT = -3324
872039
YDOT = -13889
191598 feet/sec YDOT = -4233
425599 meter/sec
ZDOT = -16714
217929 ZDOT = -5094
493625
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 07350
45409971
00020000 00000-0 20000-3 0 9115
2 25544 51
6379 244
1199 0001175 327
0225 33
0866 15
77381989 39532
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
45409971 = yrday
fracday
Element set: 911
Inclination: 51
6379 deg
RA of node: 244
1199 deg
Eccentricity:
0001175
Arg of perigee: 327
0225 deg
Mean anomaly: 33
0866 deg
Mean motion: 15
77381989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3953
Checksum: 309
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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