Date:
February 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7857 65 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
There are no maneuvers
Coasting Arc #1 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2007/038/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4543176
55 A = 6710408
08 meter
Y = -371598
28 meter E =
0027900
Z = -4943242
84 I = 51
87461
XDOT = 2908
444488 Wp = 153
52058
YDOT = 6790
210936 meter/sec RA = 53
65379 deg
ZDOT = 2142
792899 TA = 137
32935
MA = 137
11232
Ha = 190
275 n
mi
Hp = 173
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14905434
87 X = 4571007
13
Y = -1219154
46 feet Y = -320638
42 meter
Z = -16217988
30 Z = -4921104
86
XDOT = 9542
140708 XDOT = 2821
890100
YDOT = 22277
594933 feet/sec YDOT = 6822
250870 meter/sec
ZDOT = 7030
160430 ZDOT = 2156
711530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11160564
14 X = 3401739
95
Y = 10089003
70 feet Y = 3075128
33 meter
Z = -16134908
84 Z = -4917920
21
XDOT = -8983
513137 XDOT = -2738
174804
YDOT = 21370
184167 feet/sec YDOT = 6513
632134 meter/sec
ZDOT = 7083
270548 ZDOT = 2158
980863
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 07038
50315087
00020000 00000-0 20000-3 0 9006
2 25544 51
6337 54
1905 0021565 179
4805 180
6386 15
77960804 30297
Satellite: ISS
Catalog Number: 25544
Epoch time: 07038
50315087 = yrday
fracday
Element set: 900
Inclination: 51
6337 deg
RA of node: 54
1905 deg
Eccentricity:
0021565
Arg of perigee: 179
4805 deg
Mean anomaly: 180
6386 deg
Mean motion: 15
77960804 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3029
Checksum: 295
Coasting Arc #2 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2007/039/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1815347
59 A = 6716675
10 meter
Y = -5683322
19 meter E =
0022975
Z = -3060732
99 I = 51
87744
XDOT = 5868
546133 Wp = 171
77623
YDOT = 776
712869 meter/sec RA = 48
54617 deg
ZDOT = -4949
709942 TA = 43
68949
MA = 43
50786
Ha = 190
028 n
mi
Hp = 173
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5955864
81 X = -1736792
68
Y = -18646070
18 feet Y = -5703183
22 meter
Z = -10041774
90 Z = -3069360
98
XDOT = 19253
760278 XDOT = 5883
469119
YDOT = 2548
270566 feet/sec YDOT = 842
421635 meter/sec
ZDOT = -16239
205846 ZDOT = -4921
164701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9246766
94 X = 2818414
56
Y = -17233098
08 feet Y = -5252648
30 meter
Z = -10074876
35 Z = -3070822
31
XDOT = 10408
928093 XDOT = 3172
641283
YDOT = 14965
020326 feet/sec YDOT = 4561
338195 meter/sec
ZDOT = -16131
925571 ZDOT = -4917
010914
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 07039
51640394
00020000 00000-0 20000-3 0 9011
2 25544 51
6328 48
9548 0021587 183
2389 176
8640 15
78002796 30451
Satellite: ISS
Catalog Number: 25544
Epoch time: 07039
51640394 = yrday
fracday
Element set: 901
Inclination: 51
6328 deg
RA of node: 48
9548 deg
Eccentricity:
0021587
Arg of perigee: 183
2389 deg
Mean anomaly: 176
8640 deg
Mean motion: 15
78002796 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3045
Checksum: 314
Coasting Arc #3 (Orbit 3060)
---------------------------------------
Vector Time (GMT): 2007/040/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5557309
44 A = 6715643
94 meter
Y = -1580998
76 meter E =
0023509
Z = 3392873
56 I = 51
85401
XDOT = -1107
085775 Wp = 154
47981
YDOT = -6065
402740 meter/sec RA = 43
34532 deg
ZDOT = -4648
662310 TA = 345
43852
MA = 345
50614
Ha = 189
801 n
mi
Hp = 173
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18232642
51 X = -5555699
22
Y = -5187003
81 feet Y = -1643134
72 meter
Z = 11131474
95 Z = 3365880
38
XDOT = -3632
171177 XDOT = -1016
597210
YDOT = -19899
615288 feet/sec YDOT = -6077
276802 meter/sec
ZDOT = -15251
516765 ZDOT = -4653
820728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9329087
78 X = -2843505
96
Y = -16569637
84 feet Y = -5050425
61 meter
Z = 11029923
80 Z = 3361920
77
XDOT = 10293
439030 XDOT = 3137
440216
YDOT = -15941
502100 feet/sec YDOT = -4858
969840 meter/sec
ZDOT = -15271
632073 ZDOT = -4654
793456
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 07040
52963286
00020000 00000-0 20000-3 0 9023
2 25544 51
6324 43
7195 0021386 187
0610 173
0257 15
78076556 30610
Satellite: ISS
Catalog Number: 25544
Epoch time: 07040
52963286 = yrday
fracday
Element set: 902
Inclination: 51
6324 deg
RA of node: 43
7195 deg
Eccentricity:
0021386
Arg of perigee: 187
0610 deg
Mean anomaly: 173
0257 deg
Mean motion: 15
78076556 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3061
Checksum: 285
Coasting Arc #4 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2007/041/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -62705
59 A = 6710665
39 meter
Y = 4727295
00 meter E =
0024737
Z = 4770317
92 I = 51
81508
XDOT = -6727
389311 Wp = 174
20498
YDOT = -2717
992850 meter/sec RA = 38
23822 deg
ZDOT = 2579
756088 TA = 250
43453
MA = 250
70179
Ha = 189
502 n
mi
Hp = 173
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -205727
00 X = -138735
28
Y = 15509498
05 feet Y = 4726168
57 meter
Z = 15650649
33 Z = 4769828
74
XDOT = -22071
487241 XDOT = -6709
028175
YDOT = -8917
299378 feet/sec YDOT = -2793
119674 meter/sec
ZDOT = 8463
766692 ZDOT = 2547
119350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10946717
18 X = -3336559
40
Y = 10990708
39 feet Y = 3349967
92 meter
Z = 15649389
45 Z = 4769933
90
XDOT = -8989
011746 XDOT = -2739
850780
YDOT = -20947
568880 feet/sec YDOT = -6384
818995 meter/sec
ZDOT = 8340
885126 ZDOT = 2542
301786
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 07041
54283921
00020000 00000-0 20000-3 0 9038
2 25544 51
6318 38
4837 0021369 191
0430 169
0269 15
78082596 30779
Satellite: ISS
Catalog Number: 25544
Epoch time: 07041
54283921 = yrday
fracday
Element set: 903
Inclination: 51
6318 deg
RA of node: 38
4837 deg
Eccentricity:
0021369
Arg of perigee: 191
0430 deg
Mean anomaly: 169
0269 deg
Mean motion: 15
78082596 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3077
Checksum: 299
Coasting Arc #5 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2007/042/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5949692
35 A = 6719960
05 meter
Y = 3002933
88 meter E =
0012969
Z = -926372
30 I = 51
82405
XDOT = -1423
204581 Wp = 174
95545
YDOT = 4658
196846 meter/sec RA = 33
05527 deg
ZDOT = 5953
028907 TA = 174
95807
MA = 174
94500
Ha = 189
249 n
mi
Hp = 173
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19519988
01 X = 5920171
01
Y = 9852145
28 feet Y = 3069301
64 meter
Z = -3039279
21 Z = -897540
67
XDOT = -4669
306369 XDOT = -1504
105770
YDOT = 15282
798052 feet/sec YDOT = 4641
829192 meter/sec
ZDOT = 19530
934734 ZDOT = 5945
918759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7634068
85 X = 2326864
19
Y = 20505223
72 feet Y = 6249992
19 meter
Z = -2930650
04 Z = -893262
13
XDOT = -12396
545579 XDOT = -3778
467092
YDOT = 7405
986220 feet/sec YDOT = 2257
344600 meter/sec
ZDOT = 19504
800114 ZDOT = 5945
063075
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 07042
49269724
00020000 00000-0 20000-3 0 9049
2 25544 51
6319 33
5756 0021518 194
2333 165
8228 15
78173602 30924
Satellite: ISS
Catalog Number: 25544
Epoch time: 07042
49269724 = yrday
fracday
Element set: 904
Inclination: 51
6319 deg
RA of node: 33
5756 deg
Eccentricity:
0021518
Arg of perigee: 194
2333 deg
Mean anomaly: 165
8228 deg
Mean motion: 15
78173602 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3092
Checksum: 295
Coasting Arc #6 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2007/043/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2484066
30 A = 6708433
37 meter
Y = -3367820
90 meter E =
0022851
Z = -5251787
73 I = 51
75958
XDOT = 6576
459970 Wp = 158
92870
YDOT = 3968
696325 meter/sec RA = 27
90176 deg
ZDOT = 545
437345 TA = 116
36284
MA = 116
12804
Ha = 189
048 n
mi
Hp = 174
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8149823
82 X = 2547052
93
Y = -11049281
15 feet Y = -3339690
23 meter
Z = -17230274
72 Z = -5239567
53
XDOT = 21576
312239 XDOT = 6528
943078
YDOT = 13020
657235 feet/sec YDOT = 4041
972259 meter/sec
ZDOT = 1789
492603 ZDOT = 577
270041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13512981
70 X = 4118756
82
Y = -2733292
88 feet Y = -833107
67 meter
Z = -17184791
08 Z = -5237924
32
XDOT = 7185
241461 XDOT = 2190
061597
YDOT = 23099
865251 feet/sec YDOT = 7040
838928 meter/sec
ZDOT = 1909
510997 ZDOT = 582
018952
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 07043
50585624
00020000 00000-0 20000-3 0 9053
2 25544 51
6315 28
3386 0021294 198
6025 161
4364 15
78144106 31086
Satellite: ISS
Catalog Number: 25544
Epoch time: 07043
50585624 = yrday
fracday
Element set: 905
Inclination: 51
6315 deg
RA of node: 28
3386 deg
Eccentricity:
0021294
Arg of perigee: 198
6025 deg
Mean anomaly: 161
4364 deg
Mean motion: 15
78144106 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3108
Checksum: 281
Coasting Arc #7 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2007/044/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5230857
17 A = 6718740
10 meter
Y = -3765321
88 meter E =
0025461
Z = -1837907
33 I = 51
76918
XDOT = 4214
956513 Wp = 187
79363
YDOT = -3088
197817 meter/sec RA = 22
76516 deg
ZDOT = -5685
017640 TA = 12
63898
MA = 12
57526
Ha = 188
633 n
mi
Hp = 174
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17161604
87 X = -5179436
00
Y = -12353418
26 feet Y = -3823528
63 meter
Z = -6029879
70 Z = -1863193
61
XDOT = 13828
597484 XDOT = 4276
792113
YDOT = -10131
882602 feet/sec YDOT = -3040
717760 meter/sec
ZDOT = -18651
632678 ZDOT = -5664
391800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4876861
55 X = -1486467
40
Y = -20547118
17 feet Y = -6262761
62 meter
Z = -6125294
29 Z = -1866989
70
XDOT = 15667
295455 XDOT = 4775
391655
YDOT = 1803
550569 feet/sec YDOT = 549
722213 meter/sec
ZDOT = -18574
545301 ZDOT = -5661
521408
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 07044
51899065
00020000 00000-0 20000-3 0 9063
2 25544 51
6317 23
1023 0021194 202
5287 157
4950 15
78197501 31244
Satellite: ISS
Catalog Number: 25544
Epoch time: 07044
51899065 = yrday
fracday
Element set: 906
Inclination: 51
6317 deg
RA of node: 23
1023 deg
Eccentricity:
0021194
Arg of perigee: 202
5287 deg
Mean anomaly: 157
4950 deg
Mean motion: 15
78197501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3124
Checksum: 279
Coasting Arc #8 (Orbit 3139)
---------------------------------------
Vector Time (GMT): 2007/045/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4742435
75 A = 6712201
37 meter
Y = 2041244
25 meter E =
0015920
Z = 4279266
42 I = 51
72003
XDOT = -5131
221709 Wp = 179
75599
YDOT = -4548
259900 meter/sec RA = 17
56283 deg
ZDOT = -3532
627557 TA = 305
86240
MA = 306
01015
Ha = 188
459 n
mi
Hp = 174
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15559172
41 X = -4785696
12
Y = 6696995
56 feet Y = 1987969
59 meter
Z = 14039587
99 Z = 4256123
30
XDOT = -16834
716893 XDOT = -5062
820648
YDOT = -14922
112533 feet/sec YDOT = -4605
257456 meter/sec
ZDOT = -11589
985424 ZDOT = -3557
388459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16295158
58 X = -4966764
34
Y = -4881756
19 feet Y = -1487959
29 meter
Z = 13952916
89 Z = 4252849
07
XDOT = -3664
583715 XDOT = -1116
965116
YDOT = -21014
288788 feet/sec YDOT = -6405
155222 meter/sec
ZDOT = -11683
527347 ZDOT = -3561
139135
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 07045
53209986
00020000 00000-0 20000-3 0 9074
2 25544 51
6313 17
8662 0021167 206
8013 153
2061 15
78243214 31401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07045
53209986 = yrday
fracday
Element set: 907
Inclination: 51
6313 deg
RA of node: 17
8662 deg
Eccentricity:
0021167
Arg of perigee: 206
8013 deg
Mean anomaly: 153
2061 deg
Mean motion: 15
78243214 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3140
Checksum: 267
Coasting Arc #9 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2007/046/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3412514
92 A = 6712501
67 meter
Y = 4078739
72 meter E =
0020998
Z = 4110819
84 I = 51
69486
XDOT = -6507
133395 Wp = 181
61898
YDOT = 1618
023870 meter/sec RA = 12
45002 deg
ZDOT = 3776
225771 TA = 229
58321
MA = 229
76659
Ha = 188
066 n
mi
Hp = 174
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11195915
11 X = 3346683
25
Y = 13381692
01 feet Y = 4116532
16 meter
Z = 13486941
75 Z = 4127237
56
XDOT = -21348
862845 XDOT = -6543
086404
YDOT = 5308
477265 feet/sec YDOT = 1545
056331 meter/sec
ZDOT = 12389
192162 ZDOT = 3744
527819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 258855
43 X = 78899
13
Y = 17397434
09 feet Y = 5302737
91 meter
Z = 13549098
68 Z = 4129765
28
XDOT = -18736
716810 XDOT = -5710
951284
YDOT = -9328
573112 feet/sec YDOT = -2843
349085 meter/sec
ZDOT = 12270
336599 ZDOT = 3739
998596
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 07046
54518308
00020000 00000-0 20000-3 0 9088
2 25544 51
6320 12
6297 0021304 210
8053 149
1863 15
78315522 31561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07046
54518308 = yrday
fracday
Element set: 908
Inclination: 51
6320 deg
RA of node: 12
6297 deg
Eccentricity:
0021304
Arg of perigee: 210
8053 deg
Mean anomaly: 149
1863 deg
Mean motion: 15
78315522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3156
Checksum: 271
Coasting Arc #10 (Orbit 3170)
---------------------------------------
Vector Time (GMT): 2007/047/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6352737
77 A = 6718155
06 meter
Y = -821158
38 meter E =
0014409
Z = -2044162
36 I = 51
68540
XDOT = 2412
380270 Wp = 211
08835
YDOT = 4738
386799 meter/sec RA = 7
24007 deg
ZDOT = 5564
120968 TA = 126
11444
MA = 125
98097
Ha = 187
801 n
mi
Hp = 175
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20842315
51 X = 6371377
77
Y = -2694089
17 feet Y = -750014
29 meter
Z = -6706569
43 Z = -2013256
52
XDOT = 7914
633431 XDOT = 2332
187072
YDOT = 15545
888449 feet/sec YDOT = 4764
914980 meter/sec
ZDOT = 18254
990054 ZDOT = 5575
645153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18132247
85 X = 5526709
14
Y = 10696916
46 feet Y = 3260420
14 meter
Z = -6590589
65 Z = -2008811
73
XDOT = -2601
446568 XDOT = -792
920914
YDOT = 15744
652338 feet/sec YDOT = 4798
970033 meter/sec
ZDOT = 18298
853978 ZDOT = 5577
490692
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 07047
49492816
00020000 00000-0 20000-3 0 9099
2 25544 51
6319 7
7196 0021095 214
1312 145
8498 15
78315939 31710
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
49492816 = yrday
fracday
Element set: 909
Inclination: 51
6319 deg
RA of node: 7
7196 deg
Eccentricity:
0021095
Arg of perigee: 214
1312 deg
Mean anomaly: 145
8498 deg
Mean motion: 15
78315939 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3171
Checksum: 311
Coasting Arc #11 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2007/048/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -650710
41 A = 6707870
29 meter
Y = -4161096
34 meter E =
0015286
Z = -5220834
23 I = 51
62345
XDOT = 7667
948489 Wp = 173
15237
YDOT = -299
477578 meter/sec RA = 2
09670 deg
ZDOT = -732
162703 TA = 89
97643
MA = 89
80127
Ha = 187
487 n
mi
Hp = 175
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2134876
68 X = -578771
04
Y = -13651890
89 feet Y = -4167970
87 meter
Z = -17128721
24 Z = -5223820
43
XDOT = 25157
311315 XDOT = 7674
283995
YDOT = -982
537985 feet/sec YDOT = -213
694894 meter/sec
ZDOT = -2402
108607 ZDOT = -694
897641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6566720
89 X = 2001536
53
Y = -12141170
29 feet Y = -3700628
70 meter
Z = -17140451
43 Z = -5224409
60
XDOT = 19831
716425 XDOT = 6044
707166
YDOT = 13849
845601 feet/sec YDOT = 4221
432939 meter/sec
ZDOT = -2262
179638 ZDOT = -689
512354
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 07048
50796364
00020000 00000-0 20000-3 0 9109
2 25544 51
6329 2
4824 0021099 218
3548 141
6118 15
78351333 31870
Satellite: ISS
Catalog Number: 25544
Epoch time: 07048
50796364 = yrday
fracday
Element set: 910
Inclination: 51
6329 deg
RA of node: 2
4824 deg
Eccentricity:
0021099
Arg of perigee: 218
3548 deg
Mean anomaly: 141
6118 deg
Mean motion: 15
78351333 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3187
Checksum: 291
Coasting Arc #12 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2007/049/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6646860
05 A = 6719411
28 meter
Y = -289574
67 meter E =
0024866
Z = -815020
58 I = 51
63484
XDOT = 944
975740 Wp = 197
74234
YDOT = -4791
402762 meter/sec RA = 356
92972 deg
ZDOT = -5980
176363 TA = 351
17899
MA = 351
22260
Ha = 187
128 n
mi
Hp = 175
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21807283
63 X = -6639168
87
Y = -950048
12 feet Y = -363860
61 meter
Z = -2673952
05 Z = -847291
39
XDOT = 3100
314107 XDOT = 1027
533429
YDOT = -15719
825336 feet/sec YDOT = -4780
374253 meter/sec
ZDOT = -19620
001192 ZDOT = -5975
385006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17090935
67 X = -5209317
19
Y = -13553488
12 feet Y = -4131103
18 meter
Z = -2795193
79 Z = -851975
07
XDOT = 10832
549275 XDOT = 3301
761019
YDOT = -9601
471804 feet/sec YDOT = -2926
528606 meter/sec
ZDOT = -19602
602472 ZDOT = -5974
873233
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 07049
52097377
00020000 00000-0 20000-3 0 9111
2 25544 51
6337 357
2461 0021106 222
3407 137
6130 15
78389763 32031
Satellite: ISS
Catalog Number: 25544
Epoch time: 07049
52097377 = yrday
fracday
Element set: 911
Inclination: 51
6337 deg
RA of node: 357
2461 deg
Eccentricity:
0021106
Arg of perigee: 222
3407 deg
Mean anomaly: 137
6130 deg
Mean motion: 15
78389763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3203
Checksum: 284
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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