Date:
December 6th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12809 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 ET - UTC (sec) : 66 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 3215)
---------------------------------------
Vector Time (GMT): 2009/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 810697
94 A = 6713900
98 meter
Y = 4094455
67 meter E =
0019850
Z = -5274894
51 I = 51
67024
XDOT = -7579
076642 Wp = 70
03356
YDOT = 1296
449751 meter/sec RA = 171
19051 deg
ZDOT = -152
319550 TA = 198
48357
MA = 198
55578
Ha = 188
866 n
mi
Hp = 178
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2659770
14 X = 790478
01
Y = 13433253
52 feet Y = 4103408
88 meter
Z = -17306084
36 Z = -5271004
71
XDOT = -24865
737014 XDOT = -7592
270506
YDOT = 4253
444066 feet/sec YDOT = 1211
622291 meter/sec
ZDOT = -499
736056 ZDOT = -189
171712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13519070
12 X = -4120612
57
Y = -2301954
08 feet Y = -701635
61 meter
Z = -17290546
08 Z = -5270158
45
XDOT = 4891
057192 XDOT = 1490
794232
YDOT = -23725
251821 feet/sec YDOT = -7231
456755 meter/sec
ZDOT = -645
267457 ZDOT = -196
677521
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 09334
51620127
00016717 00000-0 10270-3 0 9000
2 25544 51
6413 172
1354 0007417 28
7332 331
4239 15
76183689 32160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
51620127 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 172
1354 deg
Eccentricity:
0007417
Arg of perigee: 28
7332 deg
Mean anomaly: 331
4239 deg
Mean motion: 15
76183689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 294
Coasting Arc #2 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2009/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6599960
28 A = 6725706
33 meter
Y = -1128334
82 meter E =
0011241
Z = -629290
96 I = 51
74008
XDOT = 259
356961 Wp = 100
44633
YDOT = 4813
556656 meter/sec RA = 166
04794 deg
ZDOT = -6003
013708 TA = 86
39775
MA = 86
26920
Ha = 188
899 n
mi
Hp = 178
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21653413
01 X = 6615144
06
Y = -3701885
89 feet Y = -1054445
19 meter
Z = -2064602
88 Z = -597190
74
XDOT = 850
908665 XDOT = 234
673997
YDOT = 15792
508713 feet/sec YDOT = 4816
319736 meter/sec
ZDOT = -19694
926863 ZDOT = -6001
813027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4041527
04 X = -1231857
44
Y = 21604345
77 feet Y = 6585004
59 meter
Z = -1937818
84 Z = -590647
18
XDOT = -13571
548886 XDOT = -4136
608100
YDOT = -4276
000663 feet/sec YDOT = -1303
325002 meter/sec
ZDOT = -19689
987857 ZDOT = -6001
508299
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 09335
53061988
00016717 00000-0 10270-3 0 9018
2 25544 51
6414 166
9094 0007489 31
9452 328
2165 15
76220580 32323
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335
53061988 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 166
9094 deg
Eccentricity:
0007489
Arg of perigee: 31
9452 deg
Mean anomaly: 328
2165 deg
Mean motion: 15
76220580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 315
Coasting Arc #3 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2009/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 330567
69 A = 6714558
92 meter
Y = -4362863
15 meter E =
0011974
Z = 5088186
37 I = 51
73067
XDOT = 7440
718801 Wp = 43
66316
YDOT = -1273
035218 meter/sec RA = 160
88262 deg
ZDOT = -1564
289161 TA = 61
37518
MA = 61
25479
Ha = 188
915 n
mi
Hp = 178
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1084539
65 X = 354611
39
Y = -14313855
49 feet Y = -4359032
91 meter
Z = 16693524
85 Z = 5089850
03
XDOT = 24411
807089 XDOT = 7462
000287
YDOT = -4176
624730 feet/sec YDOT = -1189
709478 meter/sec
ZDOT = -5132
182286 ZDOT = -1528
089850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13182210
30 X = 4017937
70
Y = 5663762
31 feet Y = 1726314
75 meter
Z = 16699927
70 Z = 5090137
96
XDOT = -3726
101631 XDOT = -1135
715777
YDOT = 23486
552207 feet/sec YDOT = 7158
701113 meter/sec
ZDOT = -4989
185120 ZDOT = -1520
703624
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 09336
54502166
00016717 00000-0 10270-3 0 9029
2 25544 51
6406 161
6819 0007359 36
2920 323
8742 15
76213695 32483
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336
54502166 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 161
6819 deg
Eccentricity:
0007359
Arg of perigee: 36
2920 deg
Mean anomaly: 323
8742 deg
Mean motion: 15
76213695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 316
Coasting Arc #4 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2009/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6298865
16 A = 6723953
45 meter
Y = 1047559
28 meter E =
0020882
Z = 2070418
77 I = 51
79011
XDOT = 968
953504 Wp = 59
59273
YDOT = -5244
949165 meter/sec RA = 155
76949 deg
ZDOT = 5570
629921 TA = 323
51966
MA = 323
66175
Ha = 188
977 n
mi
Hp = 178
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20665568
11 X = -6320168
87
Y = 3436874
27 feet Y = 977002
20 meter
Z = 6792712
51 Z = 2039766
84
XDOT = 3178
981311 XDOT = 1000
469903
YDOT = -17207
838467 feet/sec YDOT = -5233
938450 meter/sec
ZDOT = 18276
344886 ZDOT = 5575
412866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3245646
30 X = 989272
99
Y = -20735819
02 feet Y = -6320277
64 meter
Z = 6671607
21 Z = 2033505
88
XDOT = 13857
403257 XDOT = 4223
736513
YDOT = 8088
625464 feet/sec YDOT = 2465
413041 meter/sec
ZDOT = 18295
047170 ZDOT = 5576
330377
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 09337
55940493
00016717 00000-0 10270-3 0 9031
2 25544 51
6401 156
4544 0007361 40
5464 319
6247 15
76261343 32643
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337
55940493 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 156
4544 deg
Eccentricity:
0007361
Arg of perigee: 40
5464 deg
Mean anomaly: 319
6247 deg
Mean motion: 15
76261343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 308
Coasting Arc #5 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2009/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1320899
19 A = 6716812
53 meter
Y = 4814984
80 meter E =
0014707
Z = -4504585
02 I = 51
79390
XDOT = -6934
324134 Wp = 83
52601
YDOT = 1049
388722 meter/sec RA = 150
58515 deg
ZDOT = 3165
492611 TA = 217
99207
MA = 218
09589
Ha = 188
961 n
mi
Hp = 178
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4333658
77 X = -1352760
38
Y = 15797194
24 feet Y = 4800036
29 meter
Z = -14778822
23 Z = -4511078
64
XDOT = -22750
407265 XDOT = -6960
920728
YDOT = 3442
876383 feet/sec YDOT = 971
695816 meter/sec
ZDOT = 10385
474445 ZDOT = 3131
740925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13813783
78 X = -4210441
30
Y = -8761127
19 feet Y = -2670391
57 meter
Z = -14804308
78 Z = -4512353
32
XDOT = 2871
266355 XDOT = 875
161985
YDOT = -21793
252425 feet/sec YDOT = -6642
583339 meter/sec
ZDOT = 10252
096045 ZDOT = 3124
838874
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 09338
51037394
00016717 00000-0 10270-3 0 9046
2 25544 51
6405 151
5537 0007412 45
0429 315
1335 15
76286506 32796
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338
51037394 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 151
5537 deg
Eccentricity:
0007412
Arg of perigee: 45
0429 deg
Mean anomaly: 315
1335 deg
Mean motion: 15
76286506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 306
Coasting Arc #6 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2009/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5754094
50 A = 6720567
36 meter
Y = -697998
17 meter E =
0011667
Z = -3415417
73 I = 51
83305
XDOT = -2033
942889 Wp = 64
80935
YDOT = 5805
149156 meter/sec RA = 145
49371 deg
ZDOT = -4620
411933 TA = 155
40953
MA = 155
35385
Ha = 189
005 n
mi
Hp = 178
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18878262
80 X = 5778063
52
Y = -2290020
24 feet Y = -633518
01 meter
Z = -11205438
74 Z = -3387406
10
XDOT = -6673
040975 XDOT = -2076
260704
YDOT = 19045
764949 feet/sec YDOT = 5782
168424 meter/sec
ZDOT = -15158
831801 ZDOT = -4630
394868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3134985
47 X = -955543
57
Y = 18822164
98 feet Y = 5736995
89 meter
Z = -11094720
72 Z = -3381670
88
XDOT = -15049
197316 XDOT = -4586
995342
YDOT = -11450
687161 feet/sec YDOT = -3490
169447 meter/sec
ZDOT = -15198
080672 ZDOT = -4632
374989
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 09339
52472315
00016717 00000-0 10270-3 0 9055
2 25544 51
6411 146
3271 0007571 48
4037 311
7775 15
76332230 32952
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339
52472315 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 146
3271 deg
Eccentricity:
0007571
Arg of perigee: 48
4037 deg
Mean anomaly: 311
7775 deg
Mean motion: 15
76332230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 301
Coasting Arc #7 (Orbit 3310)
---------------------------------------
Vector Time (GMT): 2009/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2152522
50 A = 6720275
04 meter
Y = -5329658
21 meter E =
0018840
Z = 3471032
50 I = 51
85602
XDOT = 6194
051357 Wp = 75
12965
YDOT = -485
727139 meter/sec RA = 140
30303 deg
ZDOT = -4561
810763 TA = 63
77680
MA = 63
58325
Ha = 188
976 n
mi
Hp = 177
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7062081
71 X = 2195098
02
Y = -17485755
27 feet Y = -5305349
76 meter
Z = 11387901
90 Z = 3481592
31
XDOT = 20321
690803 XDOT = 6221
182976
YDOT = -1593
592975 feet/sec YDOT = -416
309400 meter/sec
ZDOT = -14966
570744 ZDOT = -4531
654153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15007112
31 X = 4574167
83
Y = 11378184
69 feet Y = 3468070
69 meter
Z = 11429454
85 Z = 3483697
84
XDOT = -3040
768221 XDOT = -926
826154
YDOT = 19007
517203 feet/sec YDOT = 5793
491243 meter/sec
ZDOT = -14847
349687 ZDOT = -4525
472184
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 09340
53905512
00016717 00000-0 10270-3 0 9069
2 25544 51
6408 141
0995 0007400 52
4293 307
7543 15
76325098 33114
Satellite: ISS
Catalog Number: 25544
Epoch time: 09340
53905512 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 141
0995 deg
Eccentricity:
0007400
Arg of perigee: 52
4293 deg
Mean anomaly: 307
7543 deg
Mean motion: 15
76325098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3311
Checksum: 297
Coasting Arc #8 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2009/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5025275
94 A = 6716858
08 meter
Y = 73392
79 meter E =
0014730
Z = 4443228
54 I = 51
86792
XDOT = 2804
367146 Wp = 87
32595
YDOT = -6398
832809 meter/sec RA = 135
21503 deg
ZDOT = 3268
866927 TA = 330
03154
MA = 330
11578
Ha = 189
061 n
mi
Hp = 177
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16487125
77 X = -5047307
59
Y = 240789
98 feet Y = 17073
62 meter
Z = 14577521
44 Z = 4418762
17
XDOT = 9200
679614 XDOT = 2859
831983
YDOT = -20993
545961 feet/sec YDOT = -6367
162879 meter/sec
ZDOT = 10724
629027 ZDOT = 3282
624758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3881780
03 X = 1183166
55
Y = -16112925
72 feet Y = -4911219
76 meter
Z = 14480774
70 Z = 4413740
13
XDOT = 16891
534727 XDOT = 5148
539785
YDOT = 13781
717035 feet/sec YDOT = 4200
667352 meter/sec
ZDOT = 10778
792989 ZDOT = 3285
376103
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 09341
55336832
00016717 00000-0 10270-3 0 9076
2 25544 51
6414 135
8725 0007365 56
3069 303
8797 15
76391220 33272
Satellite: ISS
Catalog Number: 25544
Epoch time: 09341
55336832 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 135
8725 deg
Eccentricity:
0007365
Arg of perigee: 56
3069 deg
Mean anomaly: 303
8797 deg
Mean motion: 15
76391220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 322
Coasting Arc #9 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2009/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2661596
14 A = 6723323
16 meter
Y = 5785632
52 meter E =
0013584
Z = -2148515
13 I = 51
91166
XDOT = -5332
546646 Wp = 52
29773
YDOT = -406
601076 meter/sec RA = 130
03650 deg
ZDOT = 5542
864577 TA = 283
73902
MA = 283
89019
Ha = 189
002 n
mi
Hp = 177
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8732270
81 X = -2715657
13
Y = 18981734
00 feet Y = 5755566
86 meter
Z = -7048934
16 Z = -2161576
16
XDOT = -17495
231778 XDOT = -5354
530015
YDOT = -1333
993031 feet/sec YDOT = -466
356056 meter/sec
ZDOT = 18185
251238 ZDOT = 5516
905495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16452268
72 X = -5014651
51
Y = -12851218
60 feet Y = -3917051
43 meter
Z = -7100372
28 Z = -2164193
47
XDOT = 4437
184946 XDOT = 1352
453972
YDOT = -15614
063521 feet/sec YDOT = -4759
166561 meter/sec
ZDOT = 18082
576107 ZDOT = 5511
569198
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 09342
50427249
00016717 00000-0 10270-3 0 9086
2 25544 51
6426 130
9726 0007512 60
4161 299
7752 15
76393541 33424
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342
50427249 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 130
9726 deg
Eccentricity:
0007512
Arg of perigee: 60
4161 deg
Mean anomaly: 299
7752 deg
Mean motion: 15
76393541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 314
Coasting Arc #10 (Orbit 3357)
---------------------------------------
Vector Time (GMT): 2009/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4280333
27 A = 6713997
73 meter
Y = 878065
94 meter E =
0021208
Z = -5116328
02 I = 51
89902
XDOT = -3254
223601 Wp = 73
16029
YDOT = 6790
060766 meter/sec RA = 124
93480 deg
ZDOT = -1556
456004 TA = 181
92899
MA = 181
93719
Ha = 189
007 n
mi
Hp = 177
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14043088
15 X = 4295050
89
Y = 2880793
78 feet Y = 926013
77 meter
Z = -16785853
07 Z = -5095498
15
XDOT = -10676
586618 XDOT = -3322
348333
YDOT = 22277
102250 feet/sec YDOT = 6753
289310 meter/sec
ZDOT = -5106
482953 ZDOT = -1572
430221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5851517
96 X = -1783542
68
Y = 13191927
96 feet Y = 4020899
64 meter
Z = -16703440
82 Z = -5091208
76
XDOT = -18507
172634 XDOT = -5640
986219
YDOT = -14757
653382 feet/sec YDOT = -4498
132751 meter/sec
ZDOT = -5169
414569 ZDOT = -1575
637561
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 09343
51855162
00016717 00000-0 10270-3 0 9098
2 25544 51
6428 125
7462 0007592 63
6759 296
5185 15
76435137 33581
Satellite: ISS
Catalog Number: 25544
Epoch time: 09343
51855162 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 125
7462 deg
Eccentricity:
0007592
Arg of perigee: 63
6759 deg
Mean anomaly: 296
5185 deg
Mean motion: 15
76435137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3358
Checksum: 343
Coasting Arc #11 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2009/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2960847
42 A = 6725055
89 meter
Y = -6009461
84 meter E =
0017964
Z = 530327
75 I = 51
95223
XDOT = 4489
482822 Wp = 107
69702
YDOT = 1665
138051 meter/sec RA = 119
78136 deg
ZDOT = -6035
557721 TA = 66
55171
MA = 66
36296
Ha = 188
974 n
mi
Hp = 177
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9714066
34 X = 3025249
94
Y = -19716082
14 feet Y = -5975991
84 meter
Z = 1739920
45 Z = 544867
76
XDOT = 14729
274349 XDOT = 4499
849336
YDOT = 5463
051349 feet/sec YDOT = 1715
400485 meter/sec
ZDOT = -19801
698560 ZDOT = -6013
722214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17403935
33 X = 5304719
49
Y = 13415936
06 feet Y = 4089177
31 meter
Z = 1797219
40 Z = 547792
47
XDOT = -7315
853326 XDOT = -2229
872094
YDOT = 12200
051962 feet/sec YDOT = 3718
575838 meter/sec
ZDOT = -19715
278066 ZDOT = -6009
216755
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 09344
53281245
00016717 00000-0 10270-3 0 9108
2 25544 51
6421 120
5174 0007516 66
8409 293
3547 15
76459814 33743
Satellite: ISS
Catalog Number: 25544
Epoch time: 09344
53281245 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 120
5174 deg
Eccentricity:
0007516
Arg of perigee: 66
8409 deg
Mean anomaly: 293
3547 deg
Mean motion: 15
76459814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 315
Coasting Arc #12 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2009/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3598023
77 A = 6713071
25 meter
Y = -2060363
43 meter E =
0010088
Z = 5271621
68 I = 51
92695
XDOT = 3450
179038 Wp = 71
48598
YDOT = -6890
040812 meter/sec RA = 114
65117 deg
ZDOT = -334
411582 TA = 21
69261
MA = 21
64992
Ha = 189
115 n
mi
Hp = 177
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11804539
93 X = -3600326
02
Y = -6759722
52 feet Y = -2100611
98 meter
Z = 17295346
71 Z = 5254136
41
XDOT = 11319
485032 XDOT = 3528
592792
YDOT = -22605
120773 feet/sec YDOT = -6851
020410 meter/sec
ZDOT = -1097
150860 ZDOT = -317
460451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8804081
02 X = 2683483
90
Y = -10484228
50 feet Y = -3195592
85 meter
Z = 17226117
94 Z = 5250520
75
XDOT = 19415
111468 XDOT = 5917
725975
YDOT = 14591
077986 feet/sec YDOT = 4447
360570 meter/sec
ZDOT = -1030
330363 ZDOT = -314
044695
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 09345
54705638
00016717 00000-0 10270-3 0 9118
2 25544 51
6432 115
2903 0007583 70
1846 290
0135 15
76475222 33909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09345
54705638 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 115
2903 deg
Eccentricity:
0007583
Arg of perigee: 70
1846 deg
Mean anomaly: 290
0135 deg
Mean motion: 15
76475222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 301
Coasting Arc #13 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2009/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3014549
47 A = 6724519
17 meter
Y = 5896956
32 meter E =
0021229
Z = 1111976
88 I = 51
97828
XDOT = -3827
927812 Wp = 63
10521
YDOT = -3090
557410 meter/sec RA = 109
53268 deg
ZDOT = 5935
498947 TA = 309
02831
MA = 309
21710
Ha = 188
982 n
mi
Hp = 177
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9890254
18 X = -3085668
10
Y = 19346969
56 feet Y = 5862848
09 meter
Z = 3648218
11 Z = 1097159
81
XDOT = -12558
818281 XDOT = -3821
918252
YDOT = -10139
624050 feet/sec YDOT = -3133
330591 meter/sec
ZDOT = 19473
421742 ZDOT = 5916
916805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17457029
98 X = -5320902
74
Y = -12953662
19 feet Y = -3948276
23 meter
Z = 3589790
31 Z = 1094168
09
XDOT = 11137
753421 XDOT = 3394
787243
YDOT = -9562
778426 feet/sec YDOT = -2914
734864 meter/sec
ZDOT = 19399
821488 ZDOT = 5913
065589
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 09346
56128095
00016717 00000-0 10270-3 0 9128
2 25544 51
6441 110
0631 0007611 74
3346 285
8658 15
76513879 34064
Satellite: ISS
Catalog Number: 25544
Epoch time: 09346
56128095 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 110
0631 deg
Eccentricity:
0007611
Arg of perigee: 74
3346 deg
Mean anomaly: 285
8658 deg
Mean motion: 15
76513879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 316
Coasting Arc #14 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2009/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3124343
84 A = 6714451
28 meter
Y = 3346327
92 meter E =
0019535
Z = -4928874
53 I = 51
95386
XDOT = -3461
167744 Wp = 95
42445
YDOT = 6497
701154 meter/sec RA = 104
37373 deg
ZDOT = 2223
145556 TA = 196
08013
MA = 196
14222
Ha = 188
924 n
mi
Hp = 177
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10250471
91 X = 3110636
39
Y = 10978766
15 feet Y = 3381190
17 meter
Z = -16170848
20 Z = -4913729
08
XDOT = -11355
537219 XDOT = -3544
368755
YDOT = 21317
917172 feet/sec YDOT = 6458
530848 meter/sec
ZDOT = 7293
784632 ZDOT = 2206
129645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12381606
49 X = -3773913
66
Y = 8616181
24 feet Y = 2626212
04 meter
Z = -16110836
53 Z = -4910582
97
XDOT = -18779
695125 XDOT = -5724
051074
YDOT = -13509
133543 feet/sec YDOT = -4117
583904 meter/sec
ZDOT = 7226
659134 ZDOT = 2202
685704
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 09347
51210112
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 105
1634 0007596 77
2714 282
9299 15
76548478 34217
Satellite: ISS
Catalog Number: 25544
Epoch time: 09347
51210112 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 105
1634 deg
Eccentricity:
0007596
Arg of perigee: 77
2714 deg
Mean anomaly: 282
9299 deg
Mean motion: 15
76548478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 318
Coasting Arc #15 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 759223
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3039601
80 A = 6721675
67 meter
Y = -5338446
62 meter E =
0011638
Z = -2735983
74 I = 51
98535
XDOT = 3368
788676 Wp = 96
97592
YDOT = 4570
971989 meter/sec RA = 99
28233 deg
ZDOT = -5196
347637 TA = 114
11503
MA = 113
99326
Ha = 188
927 n
mi
Hp = 177
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9972446
84 X = 3112362
43
Y = -17514588
63 feet Y = -5304048
77 meter
Z = -8976324
61 Z = -2721041
18
XDOT = 11052
456285 XDOT = 3342
668164
YDOT = 14996
627260 feet/sec YDOT = 4608
498479 meter/sec
ZDOT = -17048
384635 ZDOT = -5180
044609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16060857
51 X = 4895349
37
Y = 12219435
54 feet Y = 3724483
95 meter
Z = -8917351
94 Z = -2718008
87
XDOT = -15429
221964 XDOT = -4702
826855
YDOT = 7933
956376 feet/sec YDOT = 2418
269903 meter/sec
ZDOT = -16983
761298 ZDOT = -5176
650444
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 09348
52629195
00016717 00000-0 10270-3 0 9145
2 25544 51
6451 99
9351 0007594 80
8522 279
3502 15
76559863 34370
Satellite: ISS
Catalog Number: 25544
Epoch time: 09348
52629195 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 99
9351 deg
Eccentricity:
0007594
Arg of perigee: 80
8522 deg
Mean anomaly: 279
3502 deg
Mean motion: 15
76559863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 349
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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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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