Date:
February 12th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12852 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 823)
---------------------------------------
Vector Time (GMT): 2008/040/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5757110
42 A = 6717754
66 meter
Y = -2464126
56 meter E =
0018039
Z = 2402948
01 I = 51
43969
XDOT = 128
825553 Wp = 59
41299
YDOT = 5547
587427 meter/sec RA = 319
01711 deg
ZDOT = 5359
543847 TA = 327
85455
MA = 327
96441
Ha = 185
083 n
mi
Hp = 176
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18888157
54 X = 5772563
98
Y = -8084404
72 feet Y = -2399660
77 meter
Z = 7883687
71 Z = 2430953
01
XDOT = 422
656013 XDOT = 40
746929
YDOT = 18200
746152 feet/sec YDOT = 5548
535759 meter/sec
ZDOT = 17583
805273 ZDOT = 5359
955518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20472835
03 X = 6240120
12
Y = -1134274
83 feet Y = -345726
97 meter
Z = 7990561
51 Z = 2435523
15
XDOT = -6019
181945 XDOT = -1834
646657
YDOT = 15715
486509 feet/sec YDOT = 4790
080288 meter/sec
ZDOT = 17585
951188 ZDOT = 5360
197922
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 08040
61868168
00020000 00000-0 20000-3 0 9005
2 25544 51
6414 319
2436 0005830 21
7873 338
3539 15
78169345 8242
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
61868168 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 319
2436 deg
Eccentricity:
0005830
Arg of perigee: 21
7873 deg
Mean anomaly: 338
3539 deg
Mean motion: 15
78169345 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 824
Checksum: 299
Coasting Arc #2 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2008/041/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 925239
11 A = 6713653
61 meter
Y = -5417717
36 meter E =
0009252
Z = -3860141
03 I = 51
40520
XDOT = 6269
038779 Wp = 67
72326
YDOT = -1830
694014 meter/sec RA = 313
78616 deg
ZDOT = 4083
248640 TA = 244
93873
MA = 245
03480
Ha = 185
068 n
mi
Hp = 176
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3035561
37 X = 1004503
61
Y = -17774663
24 feet Y = -5406927
78 meter
Z = -12664504
69 Z = -3855453
54
XDOT = 20567
712528 XDOT = 6269
208634
YDOT = -6006
213957 feet/sec YDOT = -1760
588925 meter/sec
ZDOT = 13396
485040 ZDOT = 4113
703559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8742563
49 X = 2664733
35
Y = -15784818
31 feet Y = -4811212
62 meter
Z = -12647136
42 Z = -3854847
18
XDOT = 20178
341126 XDOT = 6150
358375
YDOT = 378
792979 feet/sec YDOT = 115
456100 meter/sec
ZDOT = 13512
791174 ZDOT = 4118
698750
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 08041
56848233
00020000 00000-0 20000-3 0 9012
2 25544 51
6415 314
3355 0005740 23
9469 336
1962 15
78235537 8393
Satellite: ISS
Catalog Number: 25544
Epoch time: 08041
56848233 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 314
3355 deg
Eccentricity:
0005740
Arg of perigee: 23
9469 deg
Mean anomaly: 336
1962 deg
Mean motion: 15
78235537 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 839
Checksum: 297
Coasting Arc #3 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2008/042/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4989832
27 A = 6711144
26 meter
Y = 518330
04 meter E =
0014633
Z = -4472567
99 I = 51
37793
XDOT = 2129
080534 Wp = 53
91715
YDOT = -6690
966957 meter/sec RA = 308
64973 deg
ZDOT = -3149
410876 TA = 184
48717
MA = 184
50031
Ha = 185
011 n
mi
Hp = 175
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16370840
77 X = -4973530
82
Y = 1700557
86 feet Y = 462621
88 meter
Z = -14673779
49 Z = -4496768
69
XDOT = 6985
172356 XDOT = 2219
040786
YDOT = -21951
991329 feet/sec YDOT = -6666
655481 meter/sec
ZDOT = -10332
712848 ZDOT = -3138
849198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16011075
76 X = -4880175
89
Y = -3437742
92 feet Y = -1047824
04 meter
Z = -14766296
28 Z = -4500767
11
XDOT = 13257
394191 XDOT = 4040
853749
YDOT = -17514
885936 feet/sec YDOT = -5338
537233 meter/sec
ZDOT = -10293
010437 ZDOT = -3137
309581
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 08042
58156984
00020000 00000-0 20000-3 0 9021
2 25544 51
6412 309
0996 0005689 26
7635 333
3823 15
78297999 8553
Satellite: ISS
Catalog Number: 25544
Epoch time: 08042
58156984 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 309
0996 deg
Eccentricity:
0005689
Arg of perigee: 26
7635 deg
Mean anomaly: 333
3823 deg
Mean motion: 15
78297999 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 855
Checksum: 336
Coasting Arc #4 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2008/043/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2618818
86 A = 6719078
84 meter
Y = 6019154
86 meter E =
0015380
Z = 1414867
53 I = 51
38725
XDOT = -5014
391869 Wp = 97
94556
YDOT = -806
979373 meter/sec RA = 303
42548 deg
ZDOT = -5796
694312 TA = 66
41060
MA = 66
24917
Ha = 185
052 n
mi
Hp = 175
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8591925
39 X = -2692804
44
Y = 19747883
41 feet Y = 5989456
08 meter
Z = 4641953
85 Z = 1401965
64
XDOT = -16451
416893 XDOT = -4976
836408
YDOT = -2647
570123 feet/sec YDOT = -862
843261 meter/sec
ZDOT = -19018
025958 ZDOT = -5820
962751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14041814
52 X = -4279945
07
Y = 16342505
73 feet Y = 4981195
75 meter
Z = 4593230
68 Z = 1400016
71
XDOT = -13651
588944 XDOT = -4161
004310
YDOT = -6310
383778 feet/sec YDOT = -1923
404976 meter/sec
ZDOT = -19110
939843 ZDOT = -5825
014464
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 08043
59462446
00020000 00000-0 20000-3 0 9037
2 25544 51
6410 303
8635 0005587 32
4305 327
7202 15
78313294 8711
Satellite: ISS
Catalog Number: 25544
Epoch time: 08043
59462446 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 303
8635 deg
Eccentricity:
0005587
Arg of perigee: 32
4305 deg
Mean anomaly: 327
7202 deg
Mean motion: 15
78313294 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 871
Checksum: 280
Coasting Arc #5 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2008/044/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3674818
52 A = 6707555
11 meter
Y = 2009807
24 meter E =
0007240
Z = 5234376
39 I = 51
33423
XDOT = -3668
268440 Wp = 49
00826
YDOT = 6784
802988 meter/sec RA = 298
24925 deg
ZDOT = -25
074851 TA = 41
25764
MA = 41
20295
Ha = 184
824 n
mi
Hp = 175
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12056491
21 X = 3626644
01
Y = 6593855
79 feet Y = 2050631
74 meter
Z = 17173150
88 Z = 5252111
50
XDOT = -12035
001445 XDOT = -3743
742712
YDOT = 22259
852323 feet/sec YDOT = 6743
360323 meter/sec
ZDOT = -82
266570 ZDOT = -43
078374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9660119
60 X = 2944404
45
Y = 9652880
45 feet Y = 2942197
96 meter
Z = 17241201
07 Z = 5255118
08
XDOT = -17033
789398 XDOT = -5191
899009
YDOT = 17342
756387 feet/sec YDOT = 5286
072147 meter/sec
ZDOT = -150
425751 ZDOT = -45
849769
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 08044
60764152
00020000 00000-0 20000-3 0 9040
2 25544 51
6409 298
6268 0005587 34
1050 326
0473 15
78408841 8870
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
60764152 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 298
6268 deg
Eccentricity:
0005587
Arg of perigee: 34
1050 deg
Mean anomaly: 326
0473 deg
Mean motion: 15
78408841 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 887
Checksum: 302
Coasting Arc #6 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2008/045/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604149
03 A = 6718540
29 meter
Y = -5463882
30 meter E =
0019231
Z = 1469150
23 I = 51
35851
XDOT = 3401
384687 Wp = 54
47181
YDOT = 3809
479291 meter/sec RA = 293
07277 deg
ZDOT = 5781
582934 TA = 321
81156
MA = 321
94765
Ha = 184
815 n
mi
Hp = 175
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11824635
94 X = 3657842
36
Y = -17926123
02 feet Y = -5423278
49 meter
Z = 4820046
68 Z = 1486789
19
XDOT = 11159
398581 XDOT = 3330
448150
YDOT = 12498
291637 feet/sec YDOT = 3847
118668 meter/sec
ZDOT = 18968
447945 ZDOT = 5797
934508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16065080
60 X = 4896636
57
Y = -14227847
26 feet Y = -4336647
85 meter
Z = 4886951
91 Z = 1489542
94
XDOT = 6371
070079 XDOT = 1941
902160
YDOT = 13777
105946 feet/sec YDOT = 4199
261892 meter/sec
ZDOT = 19031
396893 ZDOT = 5800
769773
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 08045
62062532
00020000 00000-0 20000-3 0 9057
2 25544 51
6402 293
3897 0005519 36
5447 323
6094 15
78466721 9036
Satellite: ISS
Catalog Number: 25544
Epoch time: 08045
62062532 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 293
3897 deg
Eccentricity:
0005519
Arg of perigee: 36
5447 deg
Mean anomaly: 323
6094 deg
Mean motion: 15
78466721 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 903
Checksum: 295
Coasting Arc #7 (Orbit 917)
---------------------------------------
Vector Time (GMT): 2008/046/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251579
16 A = 6710819
44 meter
Y = -4536053
38 meter E =
0012415
Z = -4413524
83 I = 51
32187
XDOT = 4461
023123 Wp = 85
85156
YDOT = -5368
031530 meter/sec RA = 287
84247 deg
ZDOT = 3249
980047 TA = 216
83769
MA = 216
92305
Ha = 184
794 n
mi
Hp = 175
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7387070
73 X = -2179249
22
Y = -14882064
90 feet Y = -4560827
17 meter
Z = -14480068
36 Z = -4424287
38
XDOT = 14635
902633 XDOT = 4504
930171
YDOT = -17611
652000 feet/sec YDOT = -5317
900506 meter/sec
ZDOT = 10662
664195 ZDOT = 3271
757704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3449056
01 X = -1051272
27
Y = -16215448
68 feet Y = -4942468
76 meter
Z = -14521717
74 Z = -4426219
57
XDOT = 17252
695907 XDOT = 5258
621712
YDOT = -13267
137920 feet/sec YDOT = -4043
823638 meter/sec
ZDOT = 10745
415155 ZDOT = 3275
202539
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 08046
57026730
00020000 00000-0 20000-3 0 9063
2 25544 51
6395 288
4796 0005485 39
5547 320
6018 15
78509092 9184
Satellite: ISS
Catalog Number: 25544
Epoch time: 08046
57026730 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 288
4796 deg
Eccentricity:
0005485
Arg of perigee: 39
5547 deg
Mean anomaly: 320
6018 deg
Mean motion: 15
78509092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 918
Checksum: 319
Coasting Arc #8 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2008/047/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073003
54 A = 6712266
23 meter
Y = 3563541
90 meter E =
0012226
Z = -3984343
18 I = 51
31844
XDOT = -1768
634109 Wp = 59
10222
YDOT = -6389
704683 meter/sec RA = 282
69958 deg
ZDOT = -3909
547194 TA = 170
31647
MA = 170
29288
Ha = 184
781 n
mi
Hp = 175
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13362872
52 X = -4093194
12
Y = 11691410
45 feet Y = 3517882
59 meter
Z = -13071992
05 Z = -4004178
23
XDOT = -5802
605346 XDOT = -1678
060550
YDOT = -20963
598041 feet/sec YDOT = -6408
975919 meter/sec
ZDOT = -12826
598405 ZDOT = -3917
919381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15600023
94 X = -4754887
30
Y = 8361507
87 feet Y = 2548587
60 meter
Z = -13147503
77 Z = -4007359
15
XDOT = -200
348122 XDOT = -61
066107
YDOT = -20579
848334 feet/sec YDOT = -6272
737772 meter/sec
ZDOT = -12859
305468 ZDOT = -3919
516307
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 08047
58318520
00020000 00000-0 20000-3 0 9077
2 25544 51
6384 283
2428 0005413 42
7932 317
3654 15
78545634 9341
Satellite: ISS
Catalog Number: 25544
Epoch time: 08047
58318520 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 283
2428 deg
Eccentricity:
0005413
Arg of perigee: 42
7932 deg
Mean anomaly: 317
3654 deg
Mean motion: 15
78545634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 934
Checksum: 300
Coasting Arc #9 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2008/048/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 873357
22 A = 6717052
21 meter
Y = 6312640
08 meter E =
0017171
Z = 2106323
28 I = 51
33067
XDOT = -4774
213513 Wp = 93
08654
YDOT = 2510
856993 meter/sec RA = 277
46068 deg
ZDOT = -5507
837847 TA = 63
21383
MA = 63
03827
Ha = 184
683 n
mi
Hp = 175
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2865345
21 X = 792471
54
Y = 20710761
43 feet Y = 6321954
12 meter
Z = 6910509
46 Z = 2110369
74
XDOT = -15663
430162 XDOT = -4775
180142
YDOT = 8237
719792 feet/sec YDOT = 2457
463847 meter/sec
ZDOT = -18070
334143 ZDOT = -5531
032571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1601676
66 X = -488191
05
Y = 20841230
43 feet Y = 6352407
04 meter
Z = 6926667
97 Z = 2111248
40
XDOT = -15427
491385 XDOT = -4702
299374
YDOT = 4890
466104 feet/sec YDOT = 1490
614069 meter/sec
ZDOT = -18158
815272 ZDOT = -5534
806895
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 08048
59606784
00020000 00000-0 20000-3 0 9082
2 25544 51
6388 278
0053 0005497 45
1128 315
0483 15
78643819 9504
Satellite: ISS
Catalog Number: 25544
Epoch time: 08048
59606784 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 278
0053 deg
Eccentricity:
0005497
Arg of perigee: 45
1128 deg
Mean anomaly: 315
0483 deg
Mean motion: 15
78643819 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 950
Checksum: 318
Coasting Arc #10 (Orbit 965)
---------------------------------------
Vector Time (GMT): 2008/049/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189839
44 A = 6707102
88 meter
Y = -635727
62 meter E =
0007160
Z = 5192571
40 I = 51
29301
XDOT = 271
690089 Wp = 73
68632
YDOT = 7675
869626 meter/sec RA = 272
29117 deg
ZDOT = 721
701987 TA = 9
43504
MA = 9
42160
Ha = 184
616 n
mi
Hp = 175
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13746192
40 X = 4171413
08
Y = -2085720
52 feet Y = -588977
57 meter
Z = 17035995
41 Z = 5212880
23
XDOT = 891
371682 XDOT = 182
331352
YDOT = 25183
299298 feet/sec YDOT = 7678
408175 meter/sec
ZDOT = 2367
788670 ZDOT = 722
804917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13794791
06 X = 4204652
31
Y = 600205
31 feet Y = 182942
58 meter
Z = 17113639
83 Z = 5216237
42
XDOT = -3977
548327 XDOT = -1212
356730
YDOT = 23869
721920 feet/sec YDOT = 7275
491241 meter/sec
ZDOT = 2372
843771 ZDOT = 723
242781
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 08049
60891862
00020000 00000-0 20000-3 0 9099
2 25544 51
6373 272
7671 0005412 50
5187 309
6457 15
78628867 9660
Satellite: ISS
Catalog Number: 25544
Epoch time: 08049
60891862 = yrday
fracday
Element set: 909
Inclination: 51
6373 deg
RA of node: 272
7671 deg
Eccentricity:
0005412
Arg of perigee: 50
5187 deg
Mean anomaly: 309
6457 deg
Mean motion: 15
78628867 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 966
Checksum: 331
Coasting Arc #11 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2008/050/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 400571
51 A = 6718448
40 meter
Y = -6633912
07 meter E =
0019005
Z = 919555
65 I = 51
33086
XDOT = 4806
285049 Wp = 54
48015
YDOT = 1122
158460 meter/sec RA = 267
09824 deg
ZDOT = 5927
165250 TA = 315
63000
MA = 315
78213
Ha = 184
599 n
mi
Hp = 174
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1314211
00 X = 470256
28
Y = -21764803
38 feet Y = -6629043
02 meter
Z = 3016914
87 Z = 921670
88
XDOT = 15768
651737 XDOT = 4764
587544
YDOT = 3681
622244 feet/sec YDOT = 1175
671989 meter/sec
ZDOT = 19446
080215 ZDOT = 5950
412120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5128517
03 X = 1563171
99
Y = -21191688
55 feet Y = -6459226
67 meter
Z = 3024275
33 Z = 921799
12
XDOT = 13214
107322 XDOT = 4027
659912
YDOT = 6020
651686 feet/sec YDOT = 1835
094634 meter/sec
ZDOT = 19535
166016 ZDOT = 5954
318602
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 08050
62173203
00020000 00000-0 20000-3 0 9107
2 25544 51
6360 267
5284 0005309 53
7188 306
4467 15
78710553 9827
Satellite: ISS
Catalog Number: 25544
Epoch time: 08050
62173203 = yrday
fracday
Element set: 910
Inclination: 51
6360 deg
RA of node: 267
5284 deg
Eccentricity:
0005309
Arg of perigee: 53
7188 deg
Mean anomaly: 306
4467 deg
Mean motion: 15
78710553 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 982
Checksum: 286
Coasting Arc #12 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2008/051/13:26:41
477
Vector Time (MET): N/A
Weight (LBS) : 540617
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4126769
87 A = 6709113
44 meter
Y = -2545331
74 meter E =
0014944
Z = -4650373
07 I = 51
30185
XDOT = 1238
249884 Wp = 93
25964
YDOT = -7070
957093 meter/sec RA = 261
87129 deg
ZDOT = 2778
216751 TA = 204
25122
MA = 204
32163
Ha = 184
550 n
mi
Hp = 174
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13539271
21 X = -4075410
91
Y = -8350825
92 feet Y = -2591192
64 meter
Z = -15257129
48 Z = -4670295
44
XDOT = 4062
499618 XDOT = 1303
730741
YDOT = -23198
678127 feet/sec YDOT = -7056
744053 meter/sec
ZDOT = 9114
884354 ZDOT = 2784
391285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11942884
95 X = -3640191
33
Y = -10395891
79 feet Y = -3168667
82 meter
Z = -15333658
77 Z = -4673699
19
XDOT = 6913
310507 XDOT = 2107
177042
YDOT = -21387
043529 feet/sec YDOT = -6518
770868 meter/sec
ZDOT = 9137
718058 ZDOT = 2785
176464
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 08051
57121381
00020000 00000-0 20000-3 0 9113
2 25544 51
6350 262
6166 0005309 58
0909 302
0773 15
78766250 9973
Satellite: ISS
Catalog Number: 25544
Epoch time: 08051
57121381 = yrday
fracday
Element set: 911
Inclination: 51
6350 deg
RA of node: 262
6166 deg
Eccentricity:
0005309
Arg of perigee: 58
0909 deg
Mean anomaly: 302
0773 deg
Mean motion: 15
78766250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 997
Checksum: 288
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data may contain past, current and future orbital data These sources include:
NASA Orbital Flight Dynamics 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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