Date:
February 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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
059/05:22:06
064 -8
2 10
5 10
5
N/A -6
5 0
0 187
4
000/00:02:12
128 -0
9 0
0 181
5
Coasting Arc #1 (Orbit 1029)
---------------------------------------
Vector Time (GMT): 2008/053/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516558
83 A = 6712995
90 meter
Y = 1710518
83 meter E =
0015244
Z = 4653501
13 I = 51
31525
XDOT = 120
710295 Wp = 64
94305
YDOT = 7204
236518 meter/sec RA = 251
23297 deg
ZDOT = -2751
868852 TA = 52
32436
MA = 52
18620
Ha = 187
415 n
mi
Hp = 176
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14818106
40 X = 4474490
52
Y = 5611938
42 feet Y = 1760790
70 meter
Z = 15267392
15 Z = 4675339
75
XDOT = 396
031151 XDOT = 53
510211
YDOT = 23635
946582 feet/sec YDOT = 7205
210429 meter/sec
ZDOT = -9028
441115 ZDOT = -2751
446219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15695113
03 X = 4783870
45
Y = 1472545
06 feet Y = 448831
73 meter
Z = 15351170
36 Z = 4679036
72
XDOT = 6852
568156 XDOT = 2088
662774
YDOT = 21512
976650 feet/sec YDOT = 6557
155283 meter/sec
ZDOT = -9025
989463 ZDOT = -2751
121588
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 08053
66596817
00020000 00000-0 20000-3 0 9003
2 25544 51
6348 251
8612 0007413 67
5550 292
6399 15
77379235 10300
Satellite: ISS
Catalog Number: 25544
Epoch time: 08053
66596817 = yrday
fracday
Element set: 900
Inclination: 51
6348 deg
RA of node: 251
8612 deg
Eccentricity:
0007413
Arg of perigee: 67
5550 deg
Mean anomaly: 292
6399 deg
Mean motion: 15
77379235 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1030
Checksum: 305
Coasting Arc #2 (Orbit 1045)
---------------------------------------
Vector Time (GMT): 2008/054/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 347467
42 A = 6717504
73 meter
Y = -5807429
92 meter E =
0019724
Z = 3338885
89 I = 51
34280
XDOT = 5386
360837 Wp = 82
84644
YDOT = 2999
918022 meter/sec RA = 246
09607 deg
ZDOT = 4636
397210 TA = 316
75318
MA = 316
90787
Ha = 187
382 n
mi
Hp = 175
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1139984
96 X = 396161
76
Y = -19053247
75 feet Y = -5803271
81 meter
Z = 10954350
03 Z = 3340692
59
XDOT = 17671
787523 XDOT = 5329
892594
YDOT = 9842
250727 feet/sec YDOT = 3059
836016 meter/sec
ZDOT = 15211
276936 ZDOT = 4662
426276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4371483
16 X = -1332428
07
Y = -18576309
56 feet Y = -5662059
15 meter
Z = 10960586
58 Z = 3340786
79
XDOT = 18300
284806 XDOT = 5577
926809
YDOT = 4768
033981 feet/sec YDOT = 1453
296757 meter/sec
ZDOT = 15311
246638 ZDOT = 4666
867975
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 08054
67959557
00020000 00000-0 20000-3 0 9010
2 25544 51
6359 246
6286 0007312 71
1936 289
0021 15
77449738 10463
Satellite: ISS
Catalog Number: 25544
Epoch time: 08054
67959557 = yrday
fracday
Element set: 901
Inclination: 51
6359 deg
RA of node: 246
6286 deg
Eccentricity:
0007312
Arg of perigee: 71
1936 deg
Mean anomaly: 289
0021 deg
Mean motion: 15
77449738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1046
Checksum: 315
Coasting Arc #3 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2008/055/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4832138
12 A = 6717801
86 meter
Y = -3390196
05 meter E =
0012019
Z = -3214451
39 I = 51
35803
XDOT = 1030
648797 Wp = 77
87062
YDOT = -5964
067594 meter/sec RA = 240
86231 deg
ZDOT = 4758
269133 TA = 244
37298
MA = 244
49720
Ha = 187
425 n
mi
Hp = 175
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15853471
52 X = -4778254
28
Y = -11122690
46 feet Y = -3443930
73 meter
Z = -10546100
37 Z = -3237794
46
XDOT = 3381
393690 XDOT = 1074
148828
YDOT = -19567
150898 feet/sec YDOT = -5952
298724 meter/sec
ZDOT = 15611
119204 ZDOT = 4763
382049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18403594
31 X = -5609415
55
Y = -5869723
91 feet Y = -1789091
85 meter
Z = -10635840
01 Z = -3241804
03
XDOT = -3159
790168 XDOT = -963
104043
YDOT = -18311
365234 feet/sec YDOT = -5581
304123 meter/sec
ZDOT = 15629
987901 ZDOT = 4764
020312
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 08055
62986159
00020000 00000-0 20000-3 0 9025
2 25544 51
6369 241
7236 0007410 74
2140 285
9842 15
77444035 10613
Satellite: ISS
Catalog Number: 25544
Epoch time: 08055
62986159 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 241
7236 deg
Eccentricity:
0007410
Arg of perigee: 74
2140 deg
Mean anomaly: 285
9842 deg
Mean motion: 15
77444035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1061
Checksum: 290
Coasting Arc #4 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/056/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1559119
45 A = 6712400
60 meter
Y = 4480145
42 meter E =
0019000
Z = -4766868
15 I = 51
35558
XDOT = -5598
467933 Wp = 74
14382
YDOT = -4630
847788 meter/sec RA = 235
72576 deg
ZDOT = -2524
414692 TA = 171
02487
MA = 170
99085
Ha = 187
419 n
mi
Hp = 175
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5115221
31 X = -1585944
92
Y = 14698639
83 feet Y = 4462560
19 meter
Z = -15639331
22 Z = -4774507
70
XDOT = -18367
676944 XDOT = -5534
005967
YDOT = -15193
070169 feet/sec YDOT = -4693
092772 meter/sec
ZDOT = -8282
200433 ZDOT = -2551
454908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -115969
96 X = -35347
64
Y = 15533934
80 feet Y = 4734743
33 meter
Z = -15668044
02 Z = -4775619
82
XDOT = -21054
450370 XDOT = -6417
396473
YDOT = -8605
182116 feet/sec YDOT = -2622
859509 meter/sec
ZDOT = -8386
241182 ZDOT = -2556
126312
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 08056
64346492
00020000 00000-0 20000-3 0 9039
2 25544 51
6373 236
4913 0007367 77
3597 282
8391 15
77468929 10772
Satellite: ISS
Catalog Number: 25544
Epoch time: 08056
64346492 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 236
4913 deg
Eccentricity:
0007367
Arg of perigee: 77
3597 deg
Mean anomaly: 282
8391 deg
Mean motion: 15
77468929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 333
Coasting Arc #5 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/057/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4844657
14 A = 6721742
75 meter
Y = 4521924
79 meter E =
0019948
Z = 1081884
30 I = 51
40496
XDOT = -2611
509982 Wp = 109
02533
YDOT = 4227
451910 meter/sec RA = 230
51347 deg
ZDOT = -5893
293151 TA = 59
07807
MA = 58
88212
Ha = 187
388 n
mi
Hp = 175
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15894544
44 X = 4788476
67
Y = 14835711
27 feet Y = 4575786
44 meter
Z = 3549489
18 Z = 1105282
79
XDOT = -8567
946136 XDOT = -2629
959613
YDOT = 13869
592882 feet/sec YDOT = 4198
145119 meter/sec
ZDOT = -19334
951282 ZDOT = -5906
024737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19906327
34 X = 6067448
57
Y = 8707772
74 feet Y = 2654129
13 meter
Z = 3639583
85 Z = 1109345
16
XDOT = -2725
781837 XDOT = -830
818304
YDOT = 14442
212979 feet/sec YDOT = 4401
986516 meter/sec
ZDOT = -19383
185408 ZDOT = -5907
994912
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 08057
65705513
00020000 00000-0 20000-3 0 9045
2 25544 51
6373 231
2580 0007352 81
3090 278
8908 15
77486808 10935
Satellite: ISS
Catalog Number: 25544
Epoch time: 08057
65705513 = yrday
fracday
Element set: 904
Inclination: 51
6373 deg
RA of node: 231
2580 deg
Eccentricity:
0007352
Arg of perigee: 81
3090 deg
Mean anomaly: 278
8908 deg
Mean motion: 15
77486808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 302
Coasting Arc #6 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2008/058/14:57:22
125
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3041279
74 A = 6710037
37 meter
Y = -2873548
02 meter E =
0009675
Z = 5237493
22 I = 51
38653
XDOT = 5374
380677 Wp = 84
82187
YDOT = 5534
178988 meter/sec RA = 225
34425 deg
ZDOT = -83
448480 TA = 5
97708
MA = 5
96554
Ha = 187
230 n
mi
Hp = 175
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9977951
89 X = 3047743
59
Y = -9427651
00 feet Y = -2839502
44 meter
Z = 17183376
70 Z = 5252283
39
XDOT = 17632
482536 XDOT = 5312
502571
YDOT = 18156
755211 feet/sec YDOT = 5593
932397 meter/sec
ZDOT = -273
781103 ZDOT = -57
490399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5969632
79 X = 1819544
08
Y = -12282767
77 feet Y = -3743787
62 meter
Z = 17239653
78 Z = 5254646
47
XDOT = 21965
330909 XDOT = 6695
032861
YDOT = 10427
073848 feet/sec YDOT = 3178
172109 meter/sec
ZDOT = -173
762529 ZDOT = -52
962819
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 08058
67063089
00020000 00000-0 20000-3 0 9054
2 25544 51
6383 226
0259 0007312 83
7752 276
4239 15
77533558 11092
Satellite: ISS
Catalog Number: 25544
Epoch time: 08058
67063089 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 226
0259 deg
Eccentricity:
0007312
Arg of perigee: 83
7752 deg
Mean anomaly: 276
4239 deg
Mean motion: 15
77533558 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 308
Coasting Arc #7 (Orbit 1117)
---------------------------------------
Vector Time (GMT): 2008/059/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2625286
60 A = 6715636
29 meter
Y = 3279202
23 meter E =
0014218
Z = -5251934
33 I = 51
40019
XDOT = -5816
518129 Wp = 87
77549
YDOT = -5029
849202 meter/sec RA = 222
23790 deg
ZDOT = -233
030610 TA = 180
00327
MA = 180
00328
Ha = 187
381 n
mi
Hp = 181
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8613145
00 X = -2636247
32
Y = 10758537
51 feet Y = 3249783
42 meter
Z = -17230755
66 Z = -5264714
52
XDOT = -19083
064729 XDOT = -5758
709273
YDOT = -16502
129929 feet/sec YDOT = -5094
569602 meter/sec
ZDOT = -764
536123 ZDOT = -261
146503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4492417
53 X = -1369288
86
Y = -12964395
60 feet Y = -3951547
78 meter
Z = -17279293
05 Z = -5266728
52
XDOT = 23226
545527 XDOT = 7079
451077
YDOT = -6885
211425 feet/sec YDOT = -2098
612442 meter/sec
ZDOT = -872
760844 ZDOT = -266
017505
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 08059
24076705
00020000 00000-0 20000-3 0 9068
2 25544 51
6392 223
0875 0000821 276
0154 84
0916 15
75576732 11188
Satellite: ISS
Catalog Number: 25544
Epoch time: 08059
24076705 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 223
0875 deg
Eccentricity:
0000821
Arg of perigee: 276
0154 deg
Mean anomaly: 84
0916 deg
Mean motion: 15
75576732 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1118
Checksum: 288
Coasting Arc #8 (Orbit 1133)
---------------------------------------
Vector Time (GMT): 2008/060/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5185485
36 A = 6727729
19 meter
Y = 4263848
24 meter E =
0010983
Z = -346002
94 I = 51
46315
XDOT = -3287
183635 Wp = 140
96729
YDOT = 3518
832427 meter/sec RA = 217
07663 deg
ZDOT = -6012
926871 TA = 42
80562
MA = 42
72015
Ha = 187
410 n
mi
Hp = 181
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17012747
24 X = 5139101
75
Y = 13989003
40 feet Y = 4321575
94 meter
Z = -1135180
24 Z = -320924
81
XDOT = -10784
723211 XDOT = -3297
078070
YDOT = 11544
725810 feet/sec YDOT = 3482
017928 meter/sec
ZDOT = -19727
450365 ZDOT = -6028
919871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20825081
08 X = -6347484
71
Y = 7186904
19 feet Y = 2190568
40 meter
Z = -1038665
00 Z = -316585
09
XDOT = -3732
184175 XDOT = -1137
569736
YDOT = -13616
539453 feet/sec YDOT = -4150
321225 meter/sec
ZDOT = -19788
263559 ZDOT = -6031
462733
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 08060
25558724
00020000 00000-0 20000-3 0 9078
2 25544 51
6391 217
8635 0000884 273
4717 86
6346 15
75549635 11342
Satellite: ISS
Catalog Number: 25544
Epoch time: 08060
25558724 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 217
8635 deg
Eccentricity:
0000884
Arg of perigee: 273
4717 deg
Mean anomaly: 86
6346 deg
Mean motion: 15
75549635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1134
Checksum: 312
Coasting Arc #9 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2008/061/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3138668
07 A = 6715747
24 meter
Y = -2905304
80 meter E =
0003013
Z = 5176361
45 I = 51
44764
XDOT = 6022
348574 Wp = 41
93398
YDOT = 4698
927996 meter/sec RA = 211
90399 deg
ZDOT = -1011
744031 TA = 57
74636
MA = 57
71716
Ha = 187
131 n
mi
Hp = 181
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10297467
42 X = 3145776
89
Y = -9531839
91 feet Y = -2870166
70 meter
Z = 16982813
16 Z = 5191626
14
XDOT = 19758
361464 XDOT = 5974
271642
YDOT = 15416
430434 feet/sec YDOT = 4766
004523 meter/sec
ZDOT = -3319
370180 ZDOT = -982
604641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3022389
92 X = 921224
45
Y = 13630190
87 feet Y = 4154482
18 meter
Z = 17040915
65 Z = 5194071
09
XDOT = -22335
724541 XDOT = -6807
928840
YDOT = 8972
984676 feet/sec YDOT = 2734
965729 meter/sec
ZDOT = -3207
241509 ZDOT = -977
567212
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 08061
27039250
00020000 00000-0 20000-3 0 9080
2 25544 51
6391 212
6395 0001054 289
3410 70
7640 15
75638526 11501
Satellite: ISS
Catalog Number: 25544
Epoch time: 08061
27039250 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 212
6395 deg
Eccentricity:
0001054
Arg of perigee: 289
3410 deg
Mean anomaly: 70
7640 deg
Mean motion: 15
75638526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1150
Checksum: 273
Coasting Arc #10 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2008/062/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5271943
05 A = 6726757
25 meter
Y = -3919371
87 meter E =
0013515
Z = 1415057
30 I = 51
50983
XDOT = 3936
500691 Wp = 56
83102
YDOT = -3186
480075 meter/sec RA = 206
76622 deg
ZDOT = 5807
493260 TA = 318
77575
MA = 318
87773
Ha = 187
305 n
mi
Hp = 181
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17296401
10 X = -5234598
18
Y = -12858831
58 feet Y = -3978116
94 meter
Z = 4642576
45 Z = 1389537
36
XDOT = 12915
028514 XDOT = 3943
628581
YDOT = -10454
330955 feet/sec YDOT = -3142
420031 meter/sec
ZDOT = 19053
455579 ZDOT = 5826
633753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19732369
58 X = 6014426
25
Y = -8720705
72 feet Y = -2658071
10 meter
Z = 4544385
44 Z = 1385128
68
XDOT = 2136
923228 XDOT = 651
334200
YDOT = 14858
897058 feet/sec YDOT = 4528
991823 meter/sec
ZDOT = 19126
370926 ZDOT = 5829
717858
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 08062
28518865
00020000 00000-0 20000-3 0 9097
2 25544 51
6391 207
4150 0001070 300
2320 59
8738 15
75615861 11663
Satellite: ISS
Catalog Number: 25544
Epoch time: 08062
28518865 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 207
4150 deg
Eccentricity:
0001070
Arg of perigee: 300
2320 deg
Mean anomaly: 59
8738 deg
Mean motion: 15
75615861 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 282
Coasting Arc #11 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2008/063/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3748978
57 A = 6717007
02 meter
Y = 2697560
03 meter E =
0011418
Z = -4887622
43 I = 51
50404
XDOT = -5991
119424 Wp = 104
86914
YDOT = -4280
336403 meter/sec RA = 201
57724 deg
ZDOT = 2234
465201 TA = 186
90251
MA = 186
91825
Ha = 187
217 n
mi
Hp = 181
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12299798
44 X = -3755121
78
Y = 8850262
56 feet Y = 2655602
42 meter
Z = -16035506
66 Z = -4905849
53
XDOT = -19655
903623 XDOT = -5953
665169
YDOT = -14043
098434 feet/sec YDOT = -4347
123079 meter/sec
ZDOT = 7330
922575 ZDOT = 2205
451971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1930384
03 X = -588381
05
Y = -14955020
49 feet Y = -4558290
24 meter
Z = -16104988
14 Z = -4908800
38
XDOT = 20665
010591 XDOT = 6298
695228
YDOT = -10436
733523 feet/sec YDOT = -3181
116378 meter/sec
ZDOT = 7219
295640 ZDOT = 2200
441311
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 08063
23654702
00020000 00000-0 20000-3 0 9106
2 25544 51
6390 202
5170 0001166 302
5623 57
5429 15
75649057 11810
Satellite: ISS
Catalog Number: 25544
Epoch time: 08063
23654702 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 202
5170 deg
Eccentricity:
0001166
Arg of perigee: 302
5623 deg
Mean anomaly: 57
5429 deg
Mean motion: 15
75649057 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1181
Checksum: 268
Coasting Arc #12 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2008/064/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5134879
84 A = 6724934
95 meter
Y = 3566227
92 meter E =
0004234
Z = -2475509
68 I = 51
55797
XDOT = -4665
849748 Wp = 135
69340
YDOT = 3028
244351 meter/sec RA = 196
46102 deg
ZDOT = -5324
177946 TA = 72
34377
MA = 72
29754
Ha = 187
253 n
mi
Hp = 181
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16846718
62 X = 5106645
38
Y = 11700222
85 feet Y = 3623491
15 meter
Z = -8121750
90 Z = -2450633
70
XDOT = -15307
905999 XDOT = -4673
501990
YDOT = 9935
184877 feet/sec YDOT = 2976
025227 meter/sec
ZDOT = -17467
775412 ZDOT = -5346
862773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18194773
78 X = -5545767
05
Y = 9550018
82 feet Y = 2910845
74 meter
Z = -8026040
64 Z = -2446337
19
XDOT = -1062
643491 XDOT = -323
893736
YDOT = -16754
022534 feet/sec YDOT = -5106
626068 meter/sec
ZDOT = -17554
295045 ZDOT = -5350
549130
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 08064
25131813
00020000 00000-0 20000-3 0 9113
2 25544 51
6390 197
2929 0001228 301
2377 58
8667 15
75629648 11972
Satellite: ISS
Catalog Number: 25544
Epoch time: 08064
25131813 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 197
2929 deg
Eccentricity:
0001228
Arg of perigee: 301
2377 deg
Mean anomaly: 58
8667 deg
Mean motion: 15
75629648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1197
Checksum: 307
Coasting Arc #13 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2008/065/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4383341
41 A = 6718947
16 meter
Y = -2644582
02 meter E =
0008899
Z = 4347318
65 I = 51
56763
XDOT = 5721
802588 Wp = 62
12203
YDOT = 3886
578932 meter/sec RA = 191
26104 deg
ZDOT = -3395
549270 TA = 62
15519
MA = 62
06506
Ha = 187
038 n
mi
Hp = 181
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14381041
37 X = 4391469
79
Y = -8676450
18 feet Y = -2595519
32 meter
Z = 14262856
48 Z = 4368632
28
XDOT = 18772
318202 XDOT = 5694
411565
YDOT = 12751
243216 feet/sec YDOT = 3950
410070 meter/sec
ZDOT = -11140
253512 ZDOT = -3367
820171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1351465
38 X = 411926
65
Y = 16671604
40 feet Y = 5081505
02 meter
Z = 14344175
18 Z = 4372104
59
XDOT = -18622
021225 XDOT = -5675
992069
YDOT = 11029
081880 feet/sec YDOT = 3361
664157 meter/sec
ZDOT = -11033
562400 ZDOT = -3363
029819
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 08065
26607481
00020000 00000-0 20000-3 0 9125
2 25544 51
6394 192
0680 0001406 313
8040 46
3008 15
75721556 12138
Satellite: ISS
Catalog Number: 25544
Epoch time: 08065
26607481 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 192
0680 deg
Eccentricity:
0001406
Arg of perigee: 313
8040 deg
Mean anomaly: 46
3008 deg
Mean motion: 15
75721556 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1213
Checksum: 265
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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