Date:
January 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 1672)
---------------------------------------
Vector Time (GMT): 2011/014/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3694176
51 A = 6726224
02 meter
Y = 2137641
64 meter E =
0015810
Z = -5211788
00 I = 51
36696
XDOT = -4671
870036 Wp = 114
65501
YDOT = -6047
475794 meter/sec RA = 227
35361 deg
ZDOT = 826
548154 TA = 163
28345
MA = 163
23127
Ha = 193
953 n
mi
Hp = 186
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12120001
67 X = -3692487
70
Y = 7013259
96 feet Y = 2096341
01 meter
Z = -17099041
98 Z = -5229729
90
XDOT = -15327
657599 XDOT = -4607
913995
YDOT = -19840
799849 feet/sec YDOT = -6099
361935 meter/sec
ZDOT = 2711
772159 ZDOT = 804
007192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13891924
11 X = -4234258
47
Y = -785976
53 feet Y = -239565
65 meter
Z = -17171318
47 Z = -5233817
87
XDOT = -1900
238807 XDOT = -579
192788
YDOT = -24000
611290 feet/sec YDOT = -7315
386321 meter/sec
ZDOT = 2621
117778 ZDOT = 798
916699
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 11014
60785656
00016717 00000-0 10270-3 0 9007
2 25544 51
6400 228
2504 0004942 182
5109 177
6029 15
71930151 16738
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
60785656 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 228
2504 deg
Eccentricity:
0004942
Arg of perigee: 182
5109 deg
Mean anomaly: 177
6029 deg
Mean motion: 15
71930151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 289
Coasting Arc #2 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2011/015/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4941733
06 A = 6737867
29 meter
Y = 4566502
39 meter E =
0015425
Z = -75949
48 I = 51
42841
XDOT = -3304
468905 Wp = 149
34559
YDOT = 3484
990978 meter/sec RA = 222
22430 deg
ZDOT = -6020
757535 TA = 31
48159
MA = 31
38938
Ha = 193
647 n
mi
Hp = 186
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16213034
98 X = 4890671
24
Y = 14981963
23 feet Y = 4621478
34 meter
Z = -249178
09 Z = -52066
31
XDOT = -10841
433414 XDOT = -3313
945640
YDOT = 11433
697433 feet/sec YDOT = 3447
986044 meter/sec
ZDOT = -19753
141519 ZDOT = -6036
833167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5618896
61 X = 1712639
69
Y = 21349200
97 feet Y = 6507236
45 meter
Z = -153081
82 Z = -46659
34
XDOT = -13631
241696 XDOT = -4154
802469
YDOT = 3466
524017 feet/sec YDOT = 1056
596520 meter/sec
ZDOT = -19817
932718 ZDOT = -6040
505893
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 11015
62501635
00016717 00000-0 10270-3 0 9014
2 25544 51
6400 223
0429 0004662 188
0758 172
0329 15
72003574 16897
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
62501635 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 223
0429 deg
Eccentricity:
0004662
Arg of perigee: 188
0758 deg
Mean anomaly: 172
0329 deg
Mean motion: 15
72003574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 285
Coasting Arc #3 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/016/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1917029
43 A = 6726117
80 meter
Y = -3776734
61 meter E =
0006457
Z = 5224094
33 I = 51
41089
XDOT = 6424
038261 Wp = 163
01902
YDOT = 4190
908594 meter/sec RA = 217
09357 deg
ZDOT = 666
147318 TA = 280
58927
MA = 280
66200
Ha = 193
704 n
mi
Hp = 187
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6289466
64 X = 1933741
73
Y = -12390861
58 feet Y = -3755204
39 meter
Z = 17139417
09 Z = 5233447
30
XDOT = 21076
241014 XDOT = 6373
461302
YDOT = 13749
700111 feet/sec YDOT = 4262
463195 meter/sec
ZDOT = 2185
522698 ZDOT = 697
232539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11753198
54 X = 3582374
91
Y = -7325192
82 feet Y = -2232718
77 meter
Z = 17177145
68 Z = 5235594
00
XDOT = 10228
240807 XDOT = 3117
567798
YDOT = 21877
725298 feet/sec YDOT = 6668
330671 meter/sec
ZDOT = 2310
644688 ZDOT = 704
284501
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 11016
64216132
00016717 00000-0 10270-3 0 9023
2 25544 51
6392 217
8346 0004820 189
5341 170
5730 15
71947372 17056
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
64216132 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 217
8346 deg
Eccentricity:
0004820
Arg of perigee: 189
5341 deg
Mean anomaly: 170
5730 deg
Mean motion: 15
71947372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 293
Coasting Arc #4 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/017/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6074313
69 A = 6737133
54 meter
Y = -2645807
99 meter E =
0005022
Z = -1216374
03 I = 51
47451
XDOT = 963
167708 Wp = 61
65997
YDOT = -4894
226420 meter/sec RA = 211
94150 deg
ZDOT = 5856
533424 TA = 284
99516
MA = 285
05075
Ha = 193
557 n
mi
Hp = 187
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19928850
69 X = -6038367
49
Y = -8680472
42 feet Y = -2713533
50 meter
Z = -3990728
46 Z = -1245795
53
XDOT = 3159
999041 XDOT = 989
374816
YDOT = -16057
173295 feet/sec YDOT = -4883
309864 meter/sec
ZDOT = 19214
348505 ZDOT = 5861
275482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12730718
95 X = -3880323
14
Y = -17592013
07 feet Y = -5362045
59 meter
Z = -4109194
07 Z = -1252482
35
XDOT = 9500
089793 XDOT = 2895
627369
YDOT = -11352
123940 feet/sec YDOT = -3460
127377 meter/sec
ZDOT = 19233
524854 ZDOT = 5862
378376
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 11017
59571317
00016717 00000-0 10270-3 0 9038
2 25544 51
6399 212
9520 0004938 193
2299 166
8735 15
72018684 17203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
59571317 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 212
9520 deg
Eccentricity:
0004938
Arg of perigee: 193
2299 deg
Mean anomaly: 166
8735 deg
Mean motion: 15
72018684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 325
Coasting Arc #5 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2011/018/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 281686
92 A = 6727098
79 meter
Y = 4558570
76 meter E =
0010949
Z = -4947978
44 I = 51
46765
XDOT = -7187
163194 Wp = 96
65226
YDOT = -1792
705985 meter/sec RA = 206
83839 deg
ZDOT = -2065
937973 TA = 153
29001
MA = 153
23357
Ha = 193
366 n
mi
Hp = 187
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 924169
67 X = 254727
00
Y = 14955940
81 feet Y = 4561570
55 meter
Z = -16233525
05 Z = -4946675
02
XDOT = -23579
931740 XDOT = -7156
546938
YDOT = -5881
581314 feet/sec YDOT = -1872
905766 meter/sec
ZDOT = -6778
011722 ZDOT = -2100
778224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6489822
03 X = -1978097
75
Y = 13512393
14 feet Y = 4118577
43 meter
Z = -16228340
41 Z = -4946398
16
XDOT = -16588
164874 XDOT = -5056
072654
YDOT = -16255
656486 feet/sec YDOT = -4954
724097 meter/sec
ZDOT = -6918
339391 ZDOT = -2108
709846
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 11018
61281758
00016717 00000-0 10270-3 0 9040
2 25544 51
6401 207
7446 0004804 196
6119 163
4887 15
72061766 17363
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
61281758 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 207
7446 deg
Eccentricity:
0004804
Arg of perigee: 196
6119 deg
Mean anomaly: 163
4887 deg
Mean motion: 15
72061766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 317
Coasting Arc #6 (Orbit 1751)
---------------------------------------
Vector Time (GMT): 2011/019/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6276193
71 A = 6735170
84 meter
Y = 461864
42 meter E =
0014250
Z = 2375628
50 I = 51
52205
XDOT = 1654
729148 Wp = 126
01698
YDOT = 5258
491600 meter/sec RA = 201
66849 deg
ZDOT = -5379
814835 TA = 27
16667
MA = 27
09219
Ha = 193
167 n
mi
Hp = 187
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20591186
72 X = 6259022
55
Y = 1515303
22 feet Y = 531952
39 meter
Z = 7794056
75 Z = 2406075
72
XDOT = 5428
901405 XDOT = 1621
938153
YDOT = 17252
269028 feet/sec YDOT = 5276
812909 meter/sec
ZDOT = -17650
311139 ZDOT = -5371
855571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17317039
24 X = 5278233
56
Y = 11157331
98 feet Y = 3400754
79 meter
Z = 7916724
72 Z = 2413017
69
XDOT = -2577
724631 XDOT = -785
690468
YDOT = 16534
445860 feet/sec YDOT = 5039
699098 meter/sec
ZDOT = -17618
312278 ZDOT = -5370
061582
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 11019
62990233
00016717 00000-0 10270-3 0 9058
2 25544 51
6393 202
5351 0004877 201
7159 158
3797 15
72062677 17526
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
62990233 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 202
5351 deg
Eccentricity:
0004877
Arg of perigee: 201
7159 deg
Mean anomaly: 158
3797 deg
Mean motion: 15
72062677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1752
Checksum: 318
Coasting Arc #7 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2011/020/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2574202
80 A = 6729199
00 meter
Y = -4403831
27 meter E =
0010144
Z = 4387454
35 I = 51
53244
XDOT = 6903
558130 Wp = 138
87295
YDOT = -705
192574 meter/sec RA = 196
58442 deg
ZDOT = 3330
754141 TA = 277
51981
MA = 277
63504
Ha = 193
052 n
mi
Hp = 187
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8445547
25 X = -2546079
82
Y = -14448265
33 feet Y = -4432460
58 meter
Z = 14394535
28 Z = 4375017
30
XDOT = 22649
468929 XDOT = 6894
750931
YDOT = -2313
623932 feet/sec YDOT = -628
042262 meter/sec
ZDOT = 10927
671067 ZDOT = 3364
269174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -870214
42 X = -265241
36
Y = -16755929
00 feet Y = -5107207
16 meter
Z = 14344471
25 Z = 4372194
84
XDOT = 19865
371993 XDOT = 6054
965383
YDOT = 8472
371738 feet/sec YDOT = 2582
378906 meter/sec
ZDOT = 11062
731345 ZDOT = 3371
920514
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 11020
64696595
00016717 00000-0 10270-3 0 9067
2 25544 51
6406 197
3266 0004873 206
5054 153
5860 15
72133813 17686
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
64696595 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 197
3266 deg
Eccentricity:
0004873
Arg of perigee: 206
5054 deg
Mean anomaly: 153
5860 deg
Mean motion: 15
72133813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 317
Coasting Arc #8 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2011/021/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5586580
48 A = 6732404
08 meter
Y = 1621077
06 meter E =
0004986
Z = -3395905
98 I = 51
57416
XDOT = -4128
435804 Wp = 148
69462
YDOT = -4565
054960 meter/sec RA = 191
40814 deg
ZDOT = 4611
317606 TA = 171
24852
MA = 171
23983
Ha = 192
880 n
mi
Hp = 187
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18328676
10 X = -5587796
25
Y = 5318494
28 feet Y = 1558597
85 meter
Z = -11141423
81 Z = -3423047
68
XDOT = -13544
736890 XDOT = -4099
481949
YDOT = -14977
214435 feet/sec YDOT = -4611
059870 meter/sec
ZDOT = 15128
994771 ZDOT = 4591
332450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18709934
04 X = -5702787
89
Y = -3422780
12 feet Y = -1043263
38 meter
Z = -11250822
99 Z = -3429250
85
XDOT = -5734
227071 XDOT = -1747
792411
YDOT = -18132
437227 feet/sec YDOT = -5526
766867 meter/sec
ZDOT = 15048
502008 ZDOT = 4586
783412
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 11021
60044665
00016717 00000-0 10270-3 0 9070
2 25544 51
6417 192
4441 0004705 209
9308 150
1586 15
72130374 17836
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
60044665 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 192
4441 deg
Eccentricity:
0004705
Arg of perigee: 209
9308 deg
Mean anomaly: 150
1586 deg
Mean motion: 15
72130374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 290
Coasting Arc #9 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2011/022/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4526678
41 A = 6731749
69 meter
Y = 3403687
97 meter E =
0004101
Z = -3638373
20 I = 51
60255
XDOT = -5654
351977 Wp = 137
87713
YDOT = 2856
008707 meter/sec RA = 186
33440 deg
ZDOT = -4368
889846 TA = 85
72557
MA = 85
67872
Ha = 192
752 n
mi
Hp = 187
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14851307
11 X = 4505955
39
Y = 11166955
27 feet Y = 3454192
18 meter
Z = -11936919
96 Z = -3616433
49
XDOT = -18551
023547 XDOT = -5664
645444
YDOT = 9370
107308 feet/sec YDOT = 2792
720813 meter/sec
ZDOT = -14333
628105 ZDOT = -4396
382940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8627482
52 X = 2629656
67
Y = 16520630
49 feet Y = 5035488
17 meter
Z = -11848526
68 Z = -3611430
93
XDOT = -19496
350196 XDOT = -5942
487540
YDOT = -164
231083 feet/sec YDOT = -50
057634 meter/sec
ZDOT = -14444
463752 ZDOT = -4402
672552
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 11022
61747204
00016717 00000-0 10270-3 0 9082
2 25544 51
6421 187
2355 0004711 214
4784 145
6074 15
72162684 17990
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
61747204 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 187
2355 deg
Eccentricity:
0004711
Arg of perigee: 214
4784 deg
Mean anomaly: 145
6074 deg
Mean motion: 15
72162684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 306
Coasting Arc #10 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2011/023/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4136388
12 A = 6729635
52 meter
Y = -3240780
68 meter E =
0006907
Z = 4197799
19 I = 51
62694
XDOT = 6072
533509 Wp = 97
11636
YDOT = 3015
140949 meter/sec RA = 181
16094 deg
ZDOT = -3651
675957 TA = 30
12191
MA = 30
08221
Ha = 192
506 n
mi
Hp = 187
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13570827
16 X = 4151928
01
Y = -10632482
54 feet Y = -3194438
20 meter
Z = 13772307
05 Z = 4217931
07
XDOT = 19923
010200 XDOT = 6056
105107
YDOT = 9892
194715 feet/sec YDOT = 3082
955828 meter/sec
ZDOT = -11980
564162 ZDOT = -3622
216138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16692249
19 X = 5087797
55
Y = -4042685
75 feet Y = -1232210
62 meter
Z = 13853482
78 Z = 4222541
55
XDOT = 13757
244830 XDOT = 4193
208224
YDOT = 16107
690738 feet/sec YDOT = 4909
624137 meter/sec
ZDOT = -11861
847136 ZDOT = -3615
491007
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 11023
63447773
00016717 00000-0 10270-3 0 9094
2 25544 51
6427 182
0274 0004615 217
2544 142
8298 15
72172687 18157
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
63447773 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 182
0274 deg
Eccentricity:
0004615
Arg of perigee: 217
2544 deg
Mean anomaly: 142
8298 deg
Mean motion: 15
72172687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 315
Coasting Arc #11 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2011/024/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5906360
71 A = 6734018
78 meter
Y = -1746790
81 meter E =
0010308
Z = 2714408
39 I = 51
67365
XDOT = 3674
474456 Wp = 93
85667
YDOT = -4352
991924 meter/sec RA = 176
08740 deg
ZDOT = 5176
626418 TA = 297
07822
MA = 297
18335
Ha = 192
318 n
mi
Hp = 187
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19377823
85 X = -5899574
67
Y = -5730940
98 feet Y = -1812801
37 meter
Z = 8905539
33 Z = 2685732
26
XDOT = 12055
362387 XDOT = 3697
730656
YDOT = -14281
469567 feet/sec YDOT = -4311
771719 meter/sec
ZDOT = 16983
682474 ZDOT = 5194
533177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15500743
72 X = -4724626
69
Y = -13042848
91 feet Y = -3975460
35 meter
Z = 8789960
68 Z = 2679180
01
XDOT = 15726
897245 XDOT = 4793
558280
YDOT = -7156
894079 feet/sec YDOT = -2181
421315 meter/sec
ZDOT = 17055
905451 ZDOT = 5198
639982
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 11024
65145921
00016717 00000-0 10270-3 0 9109
2 25544 51
6436 176
8186 0004585 222
6263 137
4544 15
72261263 18315
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
65145921 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 176
8186 deg
Eccentricity:
0004585
Arg of perigee: 222
6263 deg
Mean anomaly: 137
4544 deg
Mean motion: 15
72261263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 298
Coasting Arc #12 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2011/025/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2207595
62 A = 6727052
62 meter
Y = 4186156
98 meter E =
0010327
Z = -4790195
82 I = 51
68100
XDOT = -7203
087630 Wp = 130
40265
YDOT = -885
029924 meter/sec RA = 170
92678 deg
ZDOT = 2543
187159 TA = 164
54395
MA = 164
51239
Ha = 192
076 n
mi
Hp = 187
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7242767
78 X = -2230972
37
Y = 13734110
84 feet Y = 4161339
70 meter
Z = -15715865
55 Z = -4800976
87
XDOT = -23632
177264 XDOT = -7205
009877
YDOT = -2903
641484 feet/sec YDOT = -965
589995 meter/sec
ZDOT = 8343
789892 ZDOT = 2508
190371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11888098
06 X = -3623492
29
Y = 9919038
54 feet Y = 3023322
95 meter
Z = -15759369
10 Z = -4803455
70
XDOT = -20011
535743 XDOT = -6099
516095
YDOT = -10936
137096 feet/sec YDOT = -3333
334587 meter/sec
ZDOT = 8202
712627 ZDOT = 2500
186809
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 11025
60486294
00016717 00000-0 10270-3 0 9117
2 25544 51
6435 171
9365 0004463 227
4300 132
6486 15
72289702 18465
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
60486294 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 171
9365 deg
Eccentricity:
0004463
Arg of perigee: 227
4300 deg
Mean anomaly: 132
6486 deg
Mean motion: 15
72289702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 306
Coasting Arc #13 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2011/026/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6501917
84 A = 6735782
17 meter
Y = -239134
23 meter E =
0008951
Z = -1722211
37 I = 51
74024
XDOT = -1327
548321 Wp = 172
44696
YDOT = 4983
651338 meter/sec RA = 165
84487 deg
ZDOT = -5715
966273 TA = 26
57203
MA = 26
52617
Ha = 191
990 n
mi
Hp = 187
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21331751
46 X = 6512474
73
Y = -784561
12 feet Y = -166366
77 meter
Z = -5650299
76 Z = -1690599
83
XDOT = -4355
473495 XDOT = -1355
411018
YDOT = 16350
562133 feet/sec YDOT = 4968
650326 meter/sec
ZDOT = -18753
170186 ZDOT = -5722
482901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20144300
80 X = 6139982
88
Y = 7161729
10 feet Y = 2182895
03 meter
Z = -5522845
76 Z = -1683363
39
XDOT = -9459
849214 XDOT = -2883
362040
YDOT = 12157
528191 feet/sec YDOT = 3705
614593 meter/sec
ZDOT = -18779
496786 ZDOT = -5723
990620
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 11026
62180505
00016717 00000-0 10270-3 0 9127
2 25544 51
6434 166
7275 0004431 232
2044 127
8717 15
72302030 18621
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
62180505 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 166
7275 deg
Eccentricity:
0004431
Arg of perigee: 232
2044 deg
Mean anomaly: 127
8717 deg
Mean motion: 15
72302030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1862
Checksum: 272
Coasting Arc #14 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2011/027/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 97548
15 A = 6725349
61 meter
Y = -4332387
16 meter E =
0000257
Z = 5143251
39 I = 51
73545
XDOT = 7433
929739 Wp = 322
39625
YDOT = -1458
551803 meter/sec RA = 160
70230 deg
ZDOT = -1369
432024 TA = 140
69920
MA = 140
69733
Ha = 191
675 n
mi
Hp = 187
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 320039
86 X = 121001
84
Y = -14213868
63 feet Y = -4331165
48 meter
Z = 16874184
35 Z = 5143781
99
XDOT = 24389
533266 XDOT = 7456
339391
YDOT = -4785
274944 feet/sec YDOT = -1375
295734 meter/sec
ZDOT = -4492
887218 ZDOT = -1333
264167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5226716
44 X = 1593103
17
Y = -13219077
83 feet Y = -4029174
92 meter
Z = 16876374
05 Z = 5143918
81
XDOT = 23568
076459 XDOT = 7183
549705
YDOT = 3768
223250 feet/sec YDOT = 1148
554447 meter/sec
ZDOT = -4347
031610 ZDOT = -1324
975235
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 11027
63872458
00016717 00000-0 10270-3 0 9135
2 25544 51
6437 161
5184 0004319 238
3520 121
7221 15
72361292 18782
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
63872458 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 161
5184 deg
Eccentricity:
0004319
Arg of perigee: 238
3520 deg
Mean anomaly: 121
7221 deg
Mean motion: 15
72361292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 301
Coasting Arc #15 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2011/028/14:14:19
830
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6299774
14 A = 6736678
89 meter
Y = 2275785
48 meter E =
0009205
Z = 672518
55 I = 51
80190
XDOT = -1054
552837 Wp = 47
09393
YDOT = -4705
600057 meter/sec RA = 155
60652 deg
ZDOT = 5999
813584 TA = 320
20922
MA = 320
27669
Ha = 191
544 n
mi
Hp = 187
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20668550
33 X = -6328021
11
Y = 7466487
80 feet Y = 2205179
62 meter
Z = 2206425
69 Z = 641846
34
XDOT = -3459
819018 XDOT = -1031
001044
YDOT = -15438
320397 feet/sec YDOT = -4717
261448 meter/sec
ZDOT = 19684
427768 ZDOT = 5994
747526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21987834
91 X = -6701892
08
Y = 56509
66 feet Y = 17224
14 meter
Z = 2082702
52 Z = 634807
73
XDOT = 1841
195343 XDOT = 561
196340
YDOT = -14136
343473 feet/sec YDOT = -4308
757490 meter/sec
ZDOT = 19664
055996 ZDOT = 5993
604268
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 11028
65562397
00016717 00000-0 10270-3 0 9147
2 25544 51
6437 156
3095 0004205 242
8674 117
2060 15
72358757 18940
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
65562397 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 156
3095 deg
Eccentricity:
0004205
Arg of perigee: 242
8674 deg
Mean anomaly: 117
2060 deg
Mean motion: 15
72358757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 321
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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