Date:
April 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
113/20:49:49
025 -7
0 7
9 7
9
N/A 3
2 -0
4 189
0
000/00:19:38
051 1
9 0
2 188
0
Coasting Arc #1 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2010/107/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3970433
86 A = 6721751
90 meter
Y = 3370236
88 meter E =
0008007
Z = -4255864
25 I = 51
63561
XDOT = -6209
514834 Wp = 96
38039
YDOT = 2820
606208 meter/sec RA = 180
01998 deg
ZDOT = -3566
000518 TA = 137
42632
MA = 137
36422
Ha = 189
201 n
mi
Hp = 182
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13026357
81 X = 3953126
71
Y = 11057207
60 feet Y = 3414539
94 meter
Z = -13962809
23 Z = -4236617
56
XDOT = -20372
423997 XDOT = -6223
270596
YDOT = 9253
957376 feet/sec YDOT = 2751
090875 meter/sec
ZDOT = -11699
476764 ZDOT = -3596
200166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8953200
96 X = 2728935
65
Y = -14626093
07 feet Y = -4458033
17 meter
Z = -13886161
22 Z = -4232501
94
XDOT = 11143
591254 XDOT = 3396
566614
YDOT = 18022
291679 feet/sec YDOT = 5493
194504 meter/sec
ZDOT = -11819
458690 ZDOT = -3602
571009
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 10107
72717798
00016717 00000-0 10270-3 0 9004
2 25544 51
6439 180
9197 0003747 178
0364 182
0815 15
74924930 13952
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
72717798 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 180
9197 deg
Eccentricity:
0003747
Arg of perigee: 178
0364 deg
Mean anomaly: 182
0815 deg
Mean motion: 15
74924930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 330
Coasting Arc #2 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2010/108/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5439077
09 A = 6725742
11 meter
Y = -2741082
01 meter E =
0014231
Z = 2834062
16 I = 51
67979
XDOT = 4495
640661 Wp = 113
37067
YDOT = 3636
984433 meter/sec RA = 174
83022 deg
ZDOT = -5095
724604 TA = 34
10073
MA = 34
00938
Ha = 188
831 n
mi
Hp = 182
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17844741
10 X = 5455556
59
Y = -8993051
20 feet Y = -2680166
97 meter
Z = 9298104
19 Z = 2860525
44
XDOT = 14749
477235 XDOT = 4479
391514
YDOT = 11932
363626 feet/sec YDOT = 3687
166679 meter/sec
ZDOT = -16718
256574 ZDOT = -5073
923877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11850627
43 X = -3612071
24
Y = -16028289
05 feet Y = -4885422
50 meter
Z = 9403248
18 Z = 2866110
04
XDOT = 8102
276591 XDOT = 2469
573905
YDOT = -15775
278681 feet/sec YDOT = -4808
304942 meter/sec
ZDOT = -16631
435055 ZDOT = -5069
261405
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 10108
74239002
00016717 00000-0 10270-3 0 9015
2 25544 51
6433 175
6991 0003521 183
2603 176
8538 15
75004465 14118
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
74239002 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 175
6991 deg
Eccentricity:
0003521
Arg of perigee: 183
2603 deg
Mean anomaly: 176
8538 deg
Mean motion: 15
75004465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 287
Coasting Arc #3 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2010/109/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3839530
71 A = 6720036
26 meter
Y = -3011996
44 meter E =
0009986
Z = 4617399
90 I = 51
69004
XDOT = 6233
439820 Wp = 135
51836
YDOT = -3466
254787 meter/sec RA = 169
73658 deg
ZDOT = 2911
460421 TA = 285
63387
MA = 285
74405
Ha = 188
838 n
mi
Hp = 182
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12596885
53 X = -3827995
30
Y = -9881878
07 feet Y = -3054868
03 meter
Z = 15148949
80 Z = 4598775
24
XDOT = 20450
918045 XDOT = 6257
593374
YDOT = -11372
226991 feet/sec YDOT = -3396
413817 meter/sec
ZDOT = 9552
035502 ZDOT = 2941
801212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7367717
23 X = -2245680
21
Y = 14293065
51 feet Y = 4356526
37 meter
Z = 15074771
65 Z = 4594790
40
XDOT = -13901
724463 XDOT = -4237
245616
YDOT = -17405
063270 feet/sec YDOT = -5305
063285 meter/sec
ZDOT = 9672
592817 ZDOT = 2948
206291
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 10109
75757255
00016717 00000-0 10270-3 0 9023
2 25544 51
6428 170
4784 0003527 188
3909 171
7196 15
75034029 14276
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
75757255 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 170
4784 deg
Eccentricity:
0003527
Arg of perigee: 188
3909 deg
Mean anomaly: 171
7196 deg
Mean motion: 15
75034029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 323
Coasting Arc #4 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2010/110/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5420723
89 A = 6726927
60 meter
Y = 3310681
71 meter E =
0003717
Z = -2216436
08 I = 51
74337
XDOT = -4262
627611 Wp = 75
30425
YDOT = -3311
424104 meter/sec RA = 164
55690 deg
ZDOT = 5487
371358 TA = 259
88828
MA = 259
93022
Ha = 188
659 n
mi
Hp = 182
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17784527
21 X = -5446574
58
Y = 10861816
63 feet Y = 3249919
48 meter
Z = -7271771
90 Z = -2242832
70
XDOT = -13984
998723 XDOT = -4251
938580
YDOT = -10864
252311 feet/sec YDOT = -3359
031745 meter/sec
ZDOT = 18003
186869 ZDOT = 5466
689328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14215650
41 X = 4332930
24
Y = 15187075
86 feet Y = 4629020
72 meter
Z = -7376662
22 Z = -2248406
64
XDOT = -6692
171456 XDOT = -2039
773860
YDOT = 14955
170138 feet/sec YDOT = 4558
335858 meter/sec
ZDOT = 17920
805393 ZDOT = 5462
261484
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 10110
70927849
00016717 00000-0 10270-3 0 9039
2 25544 51
6427 165
5839 0003430 188
8549 171
2555 15
75069835 14423
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
70927849 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 165
5839 deg
Eccentricity:
0003430
Arg of perigee: 188
8549 deg
Mean anomaly: 171
2555 deg
Mean motion: 15
75069835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 326
Coasting Arc #5 (Orbit 1457)
---------------------------------------
Vector Time (GMT): 2010/111/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3576220
09 A = 6718478
68 meter
Y = 2824797
06 meter E =
0011313
Z = -4946228
87 I = 51
74427
XDOT = -6160
304991 Wp = 89
40189
YDOT = 4093
737593 meter/sec RA = 159
45710 deg
ZDOT = -2120
119741 TA = 160
07812
MA = 160
03391
Ha = 188
506 n
mi
Hp = 182
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11733005
53 X = 3568394
77
Y = 9267706
88 feet Y = 2864744
79 meter
Z = -16227785
01 Z = -4928874
58
XDOT = -20210
974381 XDOT = -6195
324899
YDOT = 13430
897616 feet/sec YDOT = 4024
653618 meter/sec
ZDOT = -6955
773430 ZDOT = -2150
131492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6459658
88 X = 1968904
03
Y = -13567081
12 feet Y = -4135246
33 meter
Z = -16158648
86 Z = -4925156
17
XDOT = 16522
939001 XDOT = 5036
191807
YDOT = 16277
677460 feet/sec YDOT = 4961
436090 meter/sec
ZDOT = -7075
032431 ZDOT = -2156
469885
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 10111
72440221
00016717 00000-0 10270-3 0 9047
2 25544 51
6431 160
3618 0003364 194
5863 165
5204 15
75108029 14588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
72440221 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 160
3618 deg
Eccentricity:
0003364
Arg of perigee: 194
5863 deg
Mean anomaly: 165
5204 deg
Mean motion: 15
75108029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 279
Coasting Arc #6 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2010/112/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5313062
55 A = 6727866
26 meter
Y = -3841935
02 meter E =
0014854
Z = 1470415
61 I = 51
80493
XDOT = 3923
798550 Wp = 130
99118
YDOT = 3189
503802 meter/sec RA = 154
29180 deg
ZDOT = -5815
945803 TA = 32
84166
MA = 32
74944
Ha = 188
234 n
mi
Hp = 182
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17431307
57 X = 5348485
87
Y = -12604773
67 feet Y = -3782323
11 meter
Z = 4824198
19 Z = 1496312
52
XDOT = 12873
354824 XDOT = 3916
094099
YDOT = 10464
251319 feet/sec YDOT = 3233
338914 meter/sec
ZDOT = -19081
187019 ZDOT = -5796
902762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16344078
47 X = -4981675
12
Y = -13949853
65 feet Y = -4251915
39 meter
Z = 4927105
97 Z = 1501781
90
XDOT = 6098
845670 XDOT = 1858
928160
YDOT = -13890
443914 feet/sec YDOT = -4233
807305 meter/sec
ZDOT = -19005
312274 ZDOT = -5792
819181
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 10112
73949529
00016717 00000-0 10270-3 0 9055
2 25544 51
6435 155
1407 0003230 200
5705 159
5329 15
75171769 14745
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
73949529 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 155
1407 deg
Eccentricity:
0003230
Arg of perigee: 200
5705 deg
Mean anomaly: 159
5329 deg
Mean motion: 15
75171769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 304
Coasting Arc #7 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2010/113/16:54:56
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3263253
34 A = 6717140
19 meter
Y = -2787948
26 meter E =
0005699
Z = 5166329
95 I = 51
79633
XDOT = 5978
986466 Wp = 159
80564
YDOT = -4698
534400 meter/sec RA = 149
18435 deg
ZDOT = 1235
404367 TA = 278
38712
MA = 278
45173
Ha = 188
158 n
mi
Hp = 182
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10706211
73 X = -3256932
59
Y = -9146811
87 feet Y = -2824404
40 meter
Z = 16949901
42 Z = 5150492
49
XDOT = 19616
097329 XDOT = 6025
080571
YDOT = -15415
139109 feet/sec YDOT = -4631
416050 meter/sec
ZDOT = 4053
163934 ZDOT = 1264
562419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6129700
23 X = -1868332
63
Y = 12761246
06 feet Y = 3889627
80 meter
Z = 16886789
78 Z = 5147093
52
XDOT = -18922
264952 XDOT = -5767
506357
YDOT = -14630
491216 feet/sec YDOT = -4459
373723 meter/sec
ZDOT = 4169
028138 ZDOT = 1270
719776
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 10113
75455828
00016717 00000-0 10270-3 0 9063
2 25544 51
6439 149
9198 0003257 206
0780 154
0220 15
75225063 14905
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
75455828 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 149
9198 deg
Eccentricity:
0003257
Arg of perigee: 206
0780 deg
Mean anomaly: 154
0220 deg
Mean motion: 15
75225063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 302
Coasting Arc #8 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2010/113/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3205259
31 A = 6729063
76 meter
Y = 4960295
06 meter E =
0003447
Z = -3223054
79 I = 51
82766
XDOT = -5974
409479 Wp = 259
09581
YDOT = -740
318573 meter/sec RA = 148
27609 deg
ZDOT = 4797
119767 TA = 63
36117
MA = 63
32587
Ha = 189
039 n
mi
Hp = 187
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10515942
63 X = -3244830
96
Y = 16273933
93 feet Y = 4924230
58 meter
Z = -10574326
75 Z = -3238722
26
XDOT = -19601
080968 XDOT = -5988
990649
YDOT = -2428
866710 feet/sec YDOT = -807
209340 meter/sec
ZDOT = 15738
581914 ZDOT = 4768
060650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14096556
52 X = 4296630
43
Y = -13243649
51 feet Y = -4036664
37 meter
Z = -10636503
32 Z = -3242006
21
XDOT = 17546
264966 XDOT = 5348
101562
YDOT = 6115
902885 feet/sec YDOT = 1864
127199 meter/sec
ZDOT = 15622
927728 ZDOT = 4761
868371
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 10113
88144070
00016717 00000-0 10270-3 0 9072
2 25544 51
6471 149
2666 0008080 261
2612 98
7636 15
73488453 14929
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
88144070 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 149
2666 deg
Eccentricity:
0008080
Arg of perigee: 261
2612 deg
Mean anomaly: 98
7636 deg
Mean motion: 15
73488453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 315
Coasting Arc #9 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2010/114/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5331798
52 A = 6726326
91 meter
Y = 35984
63 meter E =
0002130
Z = -4100876
51 I = 51
84374
XDOT = -2981
960767 Wp = 330
05540
YDOT = 5979
691426 meter/sec RA = 143
20919 deg
ZDOT = -3821
902449 TA = 260
77845
MA = 260
80255
Ha = 188
843 n
mi
Hp = 188
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17492777
28 X = 5350921
30
Y = 118059
80 feet Y = 95714
72 meter
Z = -13454319
25 Z = -4074928
02
XDOT = -9783
335850 XDOT = -3030
038895
YDOT = 19618
410189 feet/sec YDOT = 5946
076379 meter/sec
ZDOT = -12539
050031 ZDOT = -3836
505948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17088729
16 X = -5208644
65
Y = -4093217
39 feet Y = -1247612
66 meter
Z = -13351060
20 Z = -4069403
15
XDOT = 13600
579365 XDOT = 4145
456591
YDOT = -15664
103714 feet/sec YDOT = -4774
418812 meter/sec
ZDOT = -12596
965757 ZDOT = -3839
555163
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 10114
89759725
00016717 00000-0 10270-3 0 9084
2 25544 51
6472 144
0530 0008169 265
7831 94
2399 15
73526475 15085
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
89759725 = yrday
fracday
Element set: 908
Inclination: 51
6472 deg
RA of node: 144
0530 deg
Eccentricity:
0008169
Arg of perigee: 265
7831 deg
Mean anomaly: 94
2399 deg
Mean motion: 15
73526475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 333
Coasting Arc #10 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2010/115/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1989928
94 A = 6728225
09 meter
Y = -5424227
45 meter E =
0004346
Z = 3444250
25 I = 51
87356
XDOT = 6140
047494 Wp = 87
13366
YDOT = -669
314460 meter/sec RA = 138
04196 deg
ZDOT = -4596
350371 TA = 52
25528
MA = 52
21591
Ha = 187
839 n
mi
Hp = 187
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6528638
25 X = 2033703
98
Y = -17796021
81 feet Y = -5401729
98 meter
Z = 11300033
64 Z = 3454023
99
XDOT = 20144
512775 XDOT = 6169
404048
YDOT = -2195
913583 feet/sec YDOT = -600
488835 meter/sec
ZDOT = -15079
889668 ZDOT = -4566
450334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10048914
63 X = -3062909
18
Y = 16045690
71 feet Y = 4890726
53 meter
Z = 11338756
28 Z = 3456052
91
XDOT = -19073
760850 XDOT = -5813
682307
YDOT = -1361
165256 feet/sec YDOT = -414
883170 meter/sec
ZDOT = -14960
922644 ZDOT = -4560
089222
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 10115
91372765
00016717 00000-0 10270-3 0 9094
2 25544 51
6466 138
8389 0008050 269
8453 90
1788 15
73564518 15240
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
91372765 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 138
8389 deg
Eccentricity:
0008050
Arg of perigee: 269
8453 deg
Mean anomaly: 90
1788 deg
Mean motion: 15
73564518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1524
Checksum: 338
Coasting Arc #11 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2010/116/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323767
78 A = 6726726
57 meter
Y = 1185028
73 meter E =
0003268
Z = 3935784
67 I = 51
89009
XDOT = 1581
159878 Wp = 114
86253
YDOT = -6354
809973 meter/sec RA = 132
97733 deg
ZDOT = 4048
190228 TA = 293
18587
MA = 293
22029
Ha = 188
497 n
mi
Hp = 187
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17466429
71 X = -5355742
96
Y = 3887889
52 feet Y = 1125316
50 meter
Z = 12912679
36 Z = 3909843
67
XDOT = 5187
532407 XDOT = 1632
437278
YDOT = -20849
114085 feet/sec YDOT = -6336
841698 meter/sec
ZDOT = 13281
464001 ZDOT = 4055
996339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17962697
82 X = 5475030
30
Y = -433505
65 feet Y = -132132
52 meter
Z = 12809476
96 Z = 3904328
58
XDOT = -9064
218993 XDOT = -2762
773949
YDOT = 18162
863492 feet/sec YDOT = 5536
040792 meter/sec
ZDOT = 13312
338591 ZDOT = 4057
600803
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 10116
92983031
00016717 00000-0 10270-3 0 9102
2 25544 51
6466 133
6236 0008074 274
2406 85
7834 15
73587374 15403
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
92983031 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 133
6236 deg
Eccentricity:
0008074
Arg of perigee: 274
2406 deg
Mean anomaly: 85
7834 deg
Mean motion: 15
73587374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 309
Coasting Arc #12 (Orbit 1554)
---------------------------------------
Vector Time (GMT): 2010/117/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -770577
29 A = 6727482
68 meter
Y = 5617801
33 meter E =
0002741
Z = -3617622
16 I = 51
91263
XDOT = -5964
848796 Wp = 274
60071
YDOT = 2031
926405 meter/sec RA = 127
81139 deg
ZDOT = 4423
288773 TA = 42
29311
MA = 42
27198
Ha = 188
858 n
mi
Hp = 187
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2528140
71 X = -815765
17
Y = 18431106
72 feet Y = 5608931
61 meter
Z = -11868839
12 Z = -3621475
47
XDOT = -19569
713898 XDOT = -6008
614807
YDOT = 6666
425212 feet/sec YDOT = 1964
979208 meter/sec
ZDOT = 14512
102272 ZDOT = 4394
204644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5661352
60 X = 1725580
27
Y = -17711176
07 feet Y = -5398366
47 meter
Z = -11884017
05 Z = -3622248
40
XDOT = 19229
481423 XDOT = 5861
145938
YDOT = -3518
966434 feet/sec YDOT = -1072
580969 meter/sec
ZDOT = 14396
405722 ZDOT = 4388
024464
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 10117
88240038
00016717 00000-0 10270-3 0 9112
2 25544 51
6461 128
7346 0008286 277
8361 82
1861 15
73644357 15551
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
88240038 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 128
7346 deg
Eccentricity:
0008286
Arg of perigee: 277
8361 deg
Mean anomaly: 82
1861 deg
Mean motion: 15
73644357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1555
Checksum: 317
Coasting Arc #13 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2010/118/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5038268
04 A = 6726930
97 meter
Y = -2329799
67 meter E =
0003828
Z = -3800554
62 I = 51
92792
XDOT = -210
289499 Wp = 323
72122
YDOT = 6435
013308 meter/sec RA = 122
74990 deg
ZDOT = -4218
370568 TA = 262
13821
MA = 262
18167
Ha = 189
077 n
mi
Hp = 187
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16529750
77 X = 5082408
61
Y = -7643699
69 feet Y = -2273211
85 meter
Z = -12469011
21 Z = -3775971
04
XDOT = -689
926177 XDOT = -261
738836
YDOT = 21112
248387 feet/sec YDOT = 6432
374167 meter/sec
ZDOT = -13839
798450 ZDOT = -4219
516982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17606670
78 X = -5366513
25
Y = 4908465
51 feet Y = 1496100
29 meter
Z = -12371222
93 Z = -3770748
75
XDOT = 4313
563092 XDOT = 1314
774030
YDOT = -19463
012020 feet/sec YDOT = -5932
326064 meter/sec
ZDOT = -13844
194485 ZDOT = -4219
710479
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 10118
89844950
00016717 00000-0 10270-3 0 9128
2 25544 51
6456 123
5197 0008365 281
2307 78
7916 15
73672075 15717
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
89844950 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 123
5197 deg
Eccentricity:
0008365
Arg of perigee: 281
2307 deg
Mean anomaly: 78
7916 deg
Mean motion: 15
73672075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 329
Coasting Arc #14 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2010/119/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -391929
33 A = 6726745
56 meter
Y = -5576084
40 meter E =
0005118
Z = 3742085
80 I = 51
94420
XDOT = 5494
612105 Wp = 44
49359
YDOT = -3268
302584 meter/sec RA = 117
58561 deg
ZDOT = -4287
536350 TA = 90
55646
MA = 90
49781
Ha = 189
151 n
mi
Hp = 187
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1285857
38 X = -347726
15
Y = -18294240
15 feet Y = -5580220
22 meter
Z = 12277184
38 Z = 3740288
86
XDOT = 18026
942603 XDOT = 5551
578950
YDOT = -10722
777505 feet/sec YDOT = -3206
539826 meter/sec
ZDOT = -14066
720309 ZDOT = -4260
704804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1251633
70 X = -381497
95
Y = 18301499
91 feet Y = 5578297
17 meter
Z = 12269899
03 Z = 3739865
22
XDOT = -18113
353137 XDOT = -5520
950036
YDOT = 8136
037278 feet/sec YDOT = 2479
864162 meter/sec
ZDOT = -13959
992470 ZDOT = -4255
005705
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 10119
91447000
00016717 00000-0 10270-3 0 9138
2 25544 51
6461 118
3043 0008355 286
2324 73
7919 15
73772856 15871
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
91447000 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 118
3043 deg
Eccentricity:
0008355
Arg of perigee: 286
2324 deg
Mean anomaly: 73
7919 deg
Mean motion: 15
73772856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 313
Coasting Arc #15 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2010/120/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4517065
90 A = 6727014
99 meter
Y = 3336189
75 meter E =
0004328
Z = 3698989
19 I = 51
95693
XDOT = -1075
600950 Wp = 66
89204
YDOT = -6270
118309 meter/sec RA = 112
52468 deg
ZDOT = 4339
331279 TA = 337
41359
MA = 337
43263
Ha = 189
487 n
mi
Hp = 187
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14819770
02 X = -4572005
36
Y = 10945504
45 feet Y = 3285369
79 meter
Z = 12135791
31 Z = 3676911
73
XDOT = -3528
874508 XDOT = -1026
487433
YDOT = -20571
254295 feet/sec YDOT = -6281
872015 meter/sec
ZDOT = 14236
651179 ZDOT = 4334
224787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16141164
81 X = 4919827
03
Y = -9000899
94 feet Y = -2743474
30 meter
Z = 12047974
13 Z = 3672222
52
XDOT = 359
589622 XDOT = 109
602917
YDOT = 19683
926638 feet/sec YDOT = 5999
660839 meter/sec
ZDOT = 14216
185884 ZDOT = 4333
093457
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 10120
93046527
00016717 00000-0 10270-3 0 9142
2 25544 51
6453 113
0881 0008325 290
0056 70
0210 15
73753214 16036
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
93046527 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 113
0881 deg
Eccentricity:
0008325
Arg of perigee: 290
0056 deg
Mean anomaly: 70
0210 deg
Mean motion: 15
73753214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 262
Coasting Arc #16 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2010/121/20:59:38
051
Vector Time (MET): N/A
Weight (LBS) : 796736
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471226
32 A = 6726334
16 meter
Y = 5329625
75 meter E =
0002226
Z = -3828056
08 I = 51
96537
XDOT = -4789
969533 Wp = 314
21443
YDOT = 4332
836349 meter/sec RA = 107
36121 deg
ZDOT = 4191
518080 TA = 359
50612
MA = 359
50634
Ha = 189
476 n
mi
Hp = 187
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4826857
99 X = 1430116
35
Y = 17485648
78 feet Y = 5345848
33 meter
Z = -12559239
11 Z = -3821008
21
XDOT = -15715
123140 XDOT = -4858
425949
YDOT = 14215
342351 feet/sec YDOT = 4278
888961 meter/sec
ZDOT = 13751
699737 ZDOT = 4168
082211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2987757
49 X = -910668
48
Y = -17911630
13 feet Y = -5459464
86 meter
Z = -12531072
17 Z = -3819470
80
XDOT = 15929
813934 XDOT = 4855
407287
YDOT = -12212
665573 feet/sec YDOT = -3722
420467 meter/sec
ZDOT = 13658
479880 ZDOT = 4163
104667
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 10121
88293265
00016717 00000-0 10270-3 0 9151
2 25544 51
6448 108
1981 0008335 292
4975 67
5305 15
73822536 16189
Satellite: ISS
Catalog Number: 25544
Epoch time: 10121
88293265 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 108
1981 deg
Eccentricity:
0008335
Arg of perigee: 292
4975 deg
Mean anomaly: 67
5305 deg
Mean motion: 15
73822536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 324
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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