Date:
February 6th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13347 25 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 744)
---------------------------------------
Vector Time (GMT): 2008/035/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5580633
87 A = 6719310
89 meter
Y = -3165359
33 meter E =
0012141
Z = -1977160
81 I = 51
56890
XDOT = 3968
035197 Wp = 23
32798
YDOT = 3513
522925 meter/sec RA = 344
59162 deg
ZDOT = 5597
571625 TA = 314
58906
MA = 314
68808
Ha = 185
169 n
mi
Hp = 177
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18309166
23 X = 5625219
07
Y = -10385037
18 feet Y = -3102704
08 meter
Z = -6486748
06 Z = -1949942
75
XDOT = 13018
488179 XDOT = 3901
260273
YDOT = 11527
306186 feet/sec YDOT = 3557
521987 meter/sec
ZDOT = 18364
736302 ZDOT = 5616
685887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19366076
92 X = 5902780
25
Y = -8328602
49 feet Y = -2538558
04 meter
Z = -6382939
04 Z = -1945519
82
XDOT = 10976
900251 XDOT = 3345
759196
YDOT = 11451
009222 feet/sec YDOT = 3490
267611 meter/sec
ZDOT = 18438
190715 ZDOT = 5619
960530
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 08035
61591913
00020000 00000-0 20000-3 0 9000
2 25544 51
6411 345
0863 0005766 5
0302 355
0920 15
77946243 7451
Satellite: ISS
Catalog Number: 25544
Epoch time: 08035
61591913 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 345
0863 deg
Eccentricity:
0005766
Arg of perigee: 5
0302 deg
Mean anomaly: 355
0920 deg
Mean motion: 15
77946243 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 745
Checksum: 273
Coasting Arc #2 (Orbit 760)
---------------------------------------
Vector Time (GMT): 2008/036/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2273844
90 A = 6708858
55 meter
Y = -3576384
95 meter E =
0017201
Z = -5214939
47 I = 51
50718
XDOT = 6927
111625 Wp = 64
95911
YDOT = -3259
891692 meter/sec RA = 339
44331 deg
ZDOT = -779
615595 TA = 197
57399
MA = 197
63358
Ha = 185
095 n
mi
Hp = 176
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7460121
05 X = -2208351
75
Y = -11733546
42 feet Y = -3601445
90 meter
Z = -17109381
47 Z = -5225826
59
XDOT = 22726
744176 XDOT = 6966
836518
YDOT = -10695
182718 feet/sec YDOT = -3182
206633 meter/sec
ZDOT = -2557
793946 ZDOT = -745
868391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6257060
74 X = -1907152
11
Y = -12358798
93 feet Y = -3766961
91 meter
Z = -17151376
97 Z = -5227739
70
XDOT = 22723
912813 XDOT = 6926
248625
YDOT = -8110
361844 feet/sec YDOT = -2472
038290 meter/sec
ZDOT = -2429
018041 ZDOT = -740
364699
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 08036
62919323
00020000 00000-0 20000-3 0 9012
2 25544 51
6417 339
8519 0005761 9
1290 350
9979 15
78017968 7612
Satellite: ISS
Catalog Number: 25544
Epoch time: 08036
62919323 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 339
8519 deg
Eccentricity:
0005761
Arg of perigee: 9
1290 deg
Mean anomaly: 350
9979 deg
Mean motion: 15
78017968 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 761
Checksum: 316
Coasting Arc #3 (Orbit 776)
---------------------------------------
Vector Time (GMT): 2008/037/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237407
00 A = 6720504
71 meter
Y = 2404069
32 meter E =
0008429
Z = -682298
05 I = 51
51989
XDOT = -1169
159069 Wp = 108
65931
YDOT = -4712
653362 meter/sec RA = 334
26834 deg
ZDOT = -5979
514869 TA = 78
79362
MA = 78
69889
Ha = 185
093 n
mi
Hp = 176
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20463933
72 X = -6260511
72
Y = 7887366
54 feet Y = 2334189
92 meter
Z = -2238510
65 Z = -712654
45
XDOT = -3835
823718 XDOT = -1087
328088
YDOT = -15461
461162 feet/sec YDOT = -4725
269851 meter/sec
ZDOT = -19617
830934 ZDOT = -5984
995837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20981568
60 X = -6395182
11
Y = 6342290
75 feet Y = 1933130
22 meter
Z = -2354398
30 Z = -717620
60
XDOT = -2100
233068 XDOT = -640
151039
YDOT = -14165
903619 feet/sec YDOT = -4317
767423 meter/sec
ZDOT = -19639
263878 ZDOT = -5986
047630
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 08037
64243083
00020000 00000-0 20000-3 0 9029
2 25544 51
6418 334
6172 0005561 12
3610 347
7691 15
78030114 7771
Satellite: ISS
Catalog Number: 25544
Epoch time: 08037
64243083 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 334
6172 deg
Eccentricity:
0005561
Arg of perigee: 12
3610 deg
Mean anomaly: 347
7691 deg
Mean motion: 15
78030114 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 777
Checksum: 272
Coasting Arc #4 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2008/038/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -210350
76 A = 6710079
84 meter
Y = 4629742
06 meter E =
0011600
Z = 4849571
86 I = 51
46000
XDOT = -7055
202152 Wp = 37
96232
YDOT = 2096
438554 meter/sec RA = 329
06550 deg
ZDOT = -2295
512197 TA = 74
47621
MA = 74
34816
Ha = 185
007 n
mi
Hp = 176
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -690127
18 X = -285663
22
Y = 15189442
44 feet Y = 4626968
69 meter
Z = 15910668
83 Z = 4848367
09
XDOT = -23146
988688 XDOT = -7066
969664
YDOT = 6878
079247 feet/sec YDOT = 2017
477475 meter/sec
ZDOT = -7531
207995 ZDOT = -2329
813870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1649553
08 X = -502783
78
Y = 15119730
80 feet Y = 4608493
95 meter
Z = 15906524
92 Z = 4848308
79
XDOT = -22357
638218 XDOT = -6814
608129
YDOT = 5662
872970 feet/sec YDOT = 1726
043681 meter/sec
ZDOT = -7662
215849 ZDOT = -2335
443391
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 08038
65562856
00020000 00000-0 20000-3 0 9034
2 25544 51
6418 329
3825 0005717 14
6070 345
5260 15
78159979 7932
Satellite: ISS
Catalog Number: 25544
Epoch time: 08038
65562856 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 329
3825 deg
Eccentricity:
0005717
Arg of perigee: 14
6070 deg
Mean anomaly: 345
5260 deg
Mean motion: 15
78159979 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 793
Checksum: 318
Coasting Arc #5 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2008/039/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5799862
34 A = 6715831
89 meter
Y = -1081394
25 meter E =
0015941
Z = 3189073
05 I = 51
45517
XDOT = -1549
312388 Wp = 67
53005
YDOT = 5847
621434 meter/sec RA = 323
92930 deg
ZDOT = 4787
627343 TA = 329
91366
MA = 330
00514
Ha = 184
998 n
mi
Hp = 176
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19028419
74 X = 5796032
10
Y = -3547881
41 feet Y = -1016558
23 meter
Z = 10462838
08 Z = 3217238
69
XDOT = -5083
045891 XDOT = -1637
843010
YDOT = 19185
109690 feet/sec YDOT = 5829
801247 meter/sec
ZDOT = 15707
438790 ZDOT = 4779
885832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19095941
95 X = 5820443
11
Y = -2783759
64 feet Y = -848489
94 meter
Z = 10570472
28 Z = 3221879
95
XDOT = -6140
744712 XDOT = -1871
698988
YDOT = 17569
561314 feet/sec YDOT = 5355
202288 meter/sec
ZDOT = 15678
420018 ZDOT = 4778
782421
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 08039
66879243
00020000 00000-0 20000-3 0 9048
2 25544 51
6418 324
1473 0005728 19
4641 340
6742 15
78158799 8091
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
66879243 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 324
1473 deg
Eccentricity:
0005728
Arg of perigee: 19
4641 deg
Mean anomaly: 340
6742 deg
Mean motion: 15
78158799 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 809
Checksum: 321
Coasting Arc #6 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2008/040/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2346264
21 A = 6715798
36 meter
Y = -5431852
47 meter E =
0008918
Z = -3175382
10 I = 51
43241
XDOT = 6023
130251 Wp = 46
47064
YDOT = -196
377022 meter/sec RA = 318
69697 deg
ZDOT = 4800
808111 TA = 276
31560
MA = 276
41716
Ha = 185
005 n
mi
Hp = 176
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7697717
22 X = 2422254
71
Y = -17821038
28 feet Y = -5405190
44 meter
Z = -10417920
26 Z = -3163799
43
XDOT = 19760
926019 XDOT = 6001
557613
YDOT = -644
281569 feet/sec YDOT = -129
143382 meter/sec
ZDOT = 15750
682778 ZDOT = 4830
015391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8163388
95 X = 2488200
95
Y = -17638393
90 feet Y = -5376182
46 meter
Z = -10374172
73 Z = -3162047
85
XDOT = 18394
761477 XDOT = 5606
723298
YDOT = -788
167005 feet/sec YDOT = -240
233303 meter/sec
ZDOT = 15862
388948 ZDOT = 4834
856151
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
61859677
00020000 00000-0 20000-3 0 9055
2 25544 51
6415 319
2393 0005624 20
9817 339
1578 15
78226802 8249
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
61859677 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 319
2393 deg
Eccentricity:
0005624
Arg of perigee: 20
9817 deg
Mean anomaly: 339
1578 deg
Mean motion: 15
78226802 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 824
Checksum: 306
Coasting Arc #7 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2008/041/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525025
53 A = 6709456
02 meter
Y = -903486
21 meter E =
0016734
Z = -4886035
68 I = 51
38992
XDOT = 3659
263171 Wp = 58
93452
YDOT = -6400
983445 meter/sec RA = 313
55536 deg
ZDOT = -2202
328623 TA = 189
56414
MA = 189
59604
Ha = 184
922 n
mi
Hp = 175
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14845884
28 X = -4490851
25
Y = -2964193
60 feet Y = -953896
75 meter
Z = -16030300
78 Z = -4907934
80
XDOT = 12005
456599 XDOT = 3741
266312
YDOT = -21000
601853 feet/sec YDOT = -6359
605071 meter/sec
ZDOT = -7225
487608 ZDOT = -2184
352789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14737565
13 X = -4492009
85
Y = -3048801
38 feet Y = -929274
66 meter
Z = -16114163
05 Z = -4911596
90
XDOT = 11944
217382 XDOT = 3640
597458
YDOT = -19856
421213 feet/sec YDOT = -6052
237186 meter/sec
ZDOT = -7157
391090 ZDOT = -2181
572804
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
63168591
00020000 00000-0 20000-3 0 9067
2 25544 51
6407 314
0033 0005569 24
2578 335
8848 15
78299970 8400
Satellite: ISS
Catalog Number: 25544
Epoch time: 08041
63168591 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 314
0033 deg
Eccentricity:
0005569
Arg of perigee: 24
2578 deg
Mean anomaly: 335
8848 deg
Mean motion: 15
78299970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 840
Checksum: 309
Coasting Arc #8 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2008/042/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3830690
83 A = 6719826
27 meter
Y = 5493736
03 meter E =
0013264
Z = 506349
46 I = 51
40569
XDOT = -4218
735353 Wp = 106
12842
YDOT = -2377
614990 meter/sec RA = 308
34683 deg
ZDOT = -5993
715198 TA = 68
33643
MA = 68
19523
Ha = 184
938 n
mi
Hp = 176
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12567883
29 X = -3894297
65
Y = 18024068
34 feet Y = 5450543
44 meter
Z = 1661251
50 Z = 487585
52
XDOT = -13840
995252 XDOT = -4162
718945
YDOT = -7800
574113 feet/sec YDOT = -2424
478292 meter/sec
ZDOT = -19664
419940 ZDOT = -6014
073402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12369671
32 X = -3770275
82
Y = 18167043
23 feet Y = 5537314
78 meter
Z = 1590049
76 Z = 484647
17
XDOT = -12493
104543 XDOT = -3807
898265
YDOT = -6740
645071 feet/sec YDOT = -2054
548618 meter/sec
ZDOT = -19742
540438 ZDOT = -6017
526325
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
64473945
00020000 00000-0 20000-3 0 9072
2 25544 51
6405 308
7675 0005398 29
6236 330
5235 15
78314385 8567
Satellite: ISS
Catalog Number: 25544
Epoch time: 08042
64473945 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 308
7675 deg
Eccentricity:
0005398
Arg of perigee: 29
6236 deg
Mean anomaly: 330
5235 deg
Mean motion: 15
78314385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 856
Checksum: 311
Coasting Arc #9 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2008/043/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2784086
55 A = 6707949
91 meter
Y = 3268707
72 meter E =
0009041
Z = 5149687
92 I = 51
34889
XDOT = -4875
643893 Wp = 41
24362
YDOT = 5875
891285 meter/sec RA = 303
15367 deg
ZDOT = -1085
934916 TA = 59
18812
MA = 59
09918
Ha = 184
747 n
mi
Hp = 175
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9134142
22 X = 2722312
43
Y = 10724106
71 feet Y = 3299495
64 meter
Z = 16895301
58 Z = 5163062
79
XDOT = -15996
206998 XDOT = -4935
711423
YDOT = 19277
858547 feet/sec YDOT = 5821
033189 meter/sec
ZDOT = -3562
778595 ZDOT = -1109
766539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9341912
99 X = 2847415
08
Y = 10460628
88 feet Y = 3188399
68 meter
Z = 16946803
22 Z = 5165385
62
XDOT = -14653
880947 XDOT = -4466
502913
YDOT = 19046
599839 feet/sec YDOT = 5805
403631 meter/sec
ZDOT = -3653
324293 ZDOT = -1113
533244
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
65775302
00020000 00000-0 20000-3 0 9087
2 25544 51
6400 303
5304 0005411 31
4445 328
7043 15
78415853 8729
Satellite: ISS
Catalog Number: 25544
Epoch time: 08043
65775302 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 303
5304 deg
Eccentricity:
0005411
Arg of perigee: 31
4445 deg
Mean anomaly: 328
7043 deg
Mean motion: 15
78415853 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 872
Checksum: 268
Coasting Arc #10 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2008/044/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4466344
76 A = 6717033
78 meter
Y = -4425224
97 meter E =
0018387
Z = 2335385
44 I = 51
36423
XDOT = 2187
603254 Wp = 62
80733
YDOT = 5065
978854 meter/sec RA = 297
99360 deg
ZDOT = 5391
494225 TA = 323
66467
MA = 323
78937
Ha = 184
666 n
mi
Hp = 175
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14653362
07 X = 4504151
58
Y = -14518454
63 feet Y = -4375068
40 meter
Z = 7662025
72 Z = 2357174
51
XDOT = 7177
176029 XDOT = 2104
601453
YDOT = 16620
665530 feet/sec YDOT = 5089
977719 meter/sec
ZDOT = 17688
629346 ZDOT = 5401
919961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13928663
07 X = 4245456
50
Y = -15173063
95 feet Y = -4624749
89 meter
Z = 7744911
77 Z = 2360649
11
XDOT = 6725
020505 XDOT = 2049
786250
YDOT = 15262
986551 feet/sec YDOT = 4652
158301 meter/sec
ZDOT = 17729
038607 ZDOT = 5403
810967
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
67073072
00020000 00000-0 20000-3 0 9096
2 25544 51
6389 298
2929 0005307 34
2119 325
9387 15
78479303 8888
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
67073072 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 298
2929 deg
Eccentricity:
0005307
Arg of perigee: 34
2119 deg
Mean anomaly: 325
9387 deg
Mean motion: 15
78479303 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 888
Checksum: 326
Coasting Arc #11 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2008/045/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1066420
80 A = 6712869
26 meter
Y = -5404841
71 meter E =
0009789
Z = -3841973
24 I = 51
33706
XDOT = 5203
477644 Wp = 75
67205
YDOT = -3931
142080 meter/sec RA = 292
75448 deg
ZDOT = 4097
035778 TA = 237
22451
MA = 237
31887
Ha = 184
696 n
mi
Hp = 175
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3498755
89 X = -987240
38
Y = -17732420
29 feet Y = -5416324
16 meter
Z = -12604899
07 Z = -3846961
73
XDOT = 17071
777046 XDOT = 5227
147125
YDOT = -12897
447770 feet/sec YDOT = -3872
821646 meter/sec
ZDOT = 13441
718431 ZDOT = 4122
371313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4538081
86 X = -1383207
35
Y = -17481136
64 feet Y = -5328250
45 meter
Z = -12624546
64 Z = -3847961
81
XDOT = 14873
906272 XDOT = 4533
566632
YDOT = -13612
069894 feet/sec YDOT = -4148
958904 meter/sec
ZDOT = 13538
226330 ZDOT = 4126
451386
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
62036488
00020000 00000-0 20000-3 0 9104
2 25544 51
6380 293
3824 0005284 38
1934 321
9605 15
78520467 9036
Satellite: ISS
Catalog Number: 25544
Epoch time: 08045
62036488 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 293
3824 deg
Eccentricity:
0005284
Arg of perigee: 38
1934 deg
Mean anomaly: 321
9605 deg
Mean motion: 15
78520467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 903
Checksum: 292
Coasting Arc #12 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2008/046/14:41:25
713
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4482210
08 A = 6710162
12 meter
Y = 2137369
68 meter E =
0015128
Z = -4528139
24 I = 51
31734
XDOT = -305
169305 Wp = 60
27872
YDOT = -7066
005945 meter/sec RA = 287
61098 deg
ZDOT = -3033
400986 TA = 179
39443
MA = 179
39260
Ha = 184
687 n
mi
Hp = 175
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14705413
64 X = -4483780
83
Y = 7012367
71 feet Y = 2087238
51 meter
Z = -14856099
88 Z = -4549917
16
XDOT = -1001
211630 XDOT = -211
397990
YDOT = -23182
434202 feet/sec YDOT = -7068
894056 meter/sec
ZDOT = -9952
102974 ZDOT = -3034
656088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14011617
21 X = -4270740
93
Y = 8162190
56 feet Y = 2487835
68 meter
Z = -14939190
84 Z = -4553465
37
XDOT = -2205
440368 XDOT = -672
218224
YDOT = -22010
272751 feet/sec YDOT = -6708
731134 meter/sec
ZDOT = -9957
645624 ZDOT = -3035
090386
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
63327185
00020000 00000-0 20000-3 0 9114
2 25544 51
6369 288
1451 0005270 42
0201 318
1368 15
78570420 9192
Satellite: ISS
Catalog Number: 25544
Epoch time: 08046
63327185 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 288
1451 deg
Eccentricity:
0005270
Arg of perigee: 42
0201 deg
Mean anomaly: 318
1368 deg
Mean motion: 15
78570420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 919
Checksum: 278
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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