Date:
April 17th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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
113/20:50:20
149 -7
6 8
3 8
3
N/A 2
9 0
1 189
4
000/00:20:36
298 1
7 0
0 188
5
Coasting Arc #1 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3022557
63 A = 6722546
82 meter
Y = -4334318
53 meter E =
0012839
Z = 4151811
43 I = 51
54512
XDOT = 6667
316204 Wp = 125
67185
YDOT = -1089
883077 meter/sec RA = 196
50295 deg
ZDOT = 3700
725875 TA = 286
41503
MA = 286
55612
Ha = 189
777 n
mi
Hp = 182
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9916527
66 X = -2994034
92
Y = -14220205
17 feet Y = -4367958
87 meter
Z = 13621428
56 Z = 4137197
13
XDOT = 21874
396994 XDOT = 6661
030197
YDOT = -3575
731881 feet/sec YDOT = -1015
360124 meter/sec
ZDOT = 12141
489090 ZDOT = 3733
100992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14559080
16 X = -4437607
63
Y = -9495715
92 feet Y = -2894294
21 meter
Z = 13563172
04 Z = 4134054
84
XDOT = 18227
166151 XDOT = 5555
640243
YDOT = -10348
116791 feet/sec YDOT = -3154
105998 meter/sec
ZDOT = 12270
138550 ZDOT = 3739
938230
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 10104
55434997
00016717 00000-0 10270-3 0 9009
2 25544 51
6478 197
2265 0004777 175
1375 184
9836 15
74769774 13458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
55434997 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 197
2265 deg
Eccentricity:
0004777
Arg of perigee: 175
1375 deg
Mean anomaly: 184
9836 deg
Mean motion: 15
74769774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 351
Coasting Arc #2 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5885345
50 A = 6725895
45 meter
Y = 1257931
17 meter E =
0005436
Z = -3010763
08 I = 51
58580
XDOT = -3537
496010 Wp = 126
88579
YDOT = -4710
313216 meter/sec RA = 191
30788 deg
ZDOT = 4949
899949 TA = 198
29373
MA = 198
31329
Ha = 189
544 n
mi
Hp = 182
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19308876
32 X = -5884348
50
Y = 4127070
78 feet Y = 1192123
22 meter
Z = -9877831
62 Z = -3039352
21
XDOT = -11605
958037 XDOT = -3508
607673
YDOT = -15453
783518 feet/sec YDOT = -4749
709918 meter/sec
ZDOT = 16239
829229 ZDOT = 4932
784813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16153843
04 X = -4923691
36
Y = 11254401
39 feet Y = 3430341
54 meter
Z = -9991435
33 Z = -3045389
49
XDOT = -15948
904013 XDOT = -4861
225943
YDOT = -8543
642923 feet/sec YDOT = -2604
102363 meter/sec
ZDOT = 16171
615857 ZDOT = 4929
108513
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 10105
50622559
00016717 00000-0 10270-3 0 9019
2 25544 51
6474 192
3344 0004571 179
3364 180
7806 15
74789031 13600
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
50622559 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 192
3344 deg
Eccentricity:
0004571
Arg of perigee: 179
3364 deg
Mean anomaly: 180
7806 deg
Mean motion: 15
74789031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 303
Coasting Arc #3 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3106819
18 A = 6721078
04 meter
Y = 3921837
21 meter E =
0008997
Z = -4494760
93 I = 51
59858
XDOT = -6792
144722 Wp = 97
56399
YDOT = 1774
639305 meter/sec RA = 186
21108 deg
ZDOT = -3152
888118 TA = 140
94914
MA = 140
88415
Ha = 189
416 n
mi
Hp = 182
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10192976
32 X = 3084568
71
Y = 12866919
97 feet Y = 3956455
06 meter
Z = -14746590
98 Z = -4479721
81
XDOT = -22283
939378 XDOT = -6796
167810
YDOT = 5822
307430 feet/sec YDOT = 1698
662983 meter/sec
ZDOT = -10344
121121 ZDOT = -3185
894733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14591126
75 X = 4447375
43
Y = 7636585
90 feet Y = 2327631
38 meter
Z = -14686657
79 Z = -4476493
29
XDOT = -17438
753580 XDOT = -5315
332091
YDOT = 13215
358716 feet/sec YDOT = 4028
041337 meter/sec
ZDOT = -10475
280669 ZDOT = -3192
865548
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 10106
52152449
00016717 00000-0 10270-3 0 9029
2 25544 51
6463 187
1149 0004553 182
7455 177
3685 15
74837599 13769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
52152449 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 187
1149 deg
Eccentricity:
0004553
Arg of perigee: 182
7455 deg
Mean anomaly: 177
3685 deg
Mean motion: 15
74837599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 332
Coasting Arc #4 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5960125
65 A = 6726802
96 meter
Y = -1857452
77 meter E =
0015117
Z = 2481801
29 I = 51
64893
XDOT = 3560
250085 Wp = 120
94713
YDOT = 4281
146548 meter/sec RA = 181
02335 deg
ZDOT = -5329
719448 TA = 30
94934
MA = 30
86033
Ha = 189
084 n
mi
Hp = 182
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19554218
01 X = 5968396
71
Y = -6094005
15 feet Y = -1790756
89 meter
Z = 8142392
69 Z = 2510776
11
XDOT = 11680
610516 XDOT = 3538
004158
YDOT = 14045
756390 feet/sec YDOT = 4320
835078 meter/sec
ZDOT = -17485
956195 ZDOT = -5312
477448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15166188
35 X = 4622654
21
Y = -13696815
16 feet Y = -4174789
26 meter
Z = 8257535
04 Z = 2516896
68
XDOT = 15580
548046 XDOT = 4748
951044
YDOT = 6719
899279 feet/sec YDOT = 2048
225300 meter/sec
ZDOT = -17417
248172 ZDOT = -5308
777243
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
53678756
00016717 00000-0 10270-3 0 9036
2 25544 51
6462 181
8952 0004319 185
3880 174
7237 15
74919993 13923
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
53678756 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 181
8952 deg
Eccentricity:
0004319
Arg of perigee: 185
3880 deg
Mean anomaly: 174
7237 deg
Mean motion: 15
74919993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 343
Coasting Arc #5 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2010/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3066684
85 A = 6719484
38 meter
Y = -3578565
11 meter E =
0009684
Z = 4788009
06 I = 51
65446
XDOT = 6843
813882 Wp = 145
00046
YDOT = -2483
708819 meter/sec RA = 175
92334 deg
ZDOT = 2516
789605 TA = 280
32620
MA = 280
43535
Ha = 189
023 n
mi
Hp = 182
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10061302
00 X = -3049700
34
Y = -11740699
18 feet Y = -3612763
79 meter
Z = 15708691
14 Z = 4773152
06
XDOT = 22453
457618 XDOT = 6858
852247
YDOT = -8148
650980 feet/sec YDOT = -2407
093217 meter/sec
ZDOT = 8257
183742 ZDOT = 2550
073716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14242858
58 X = -4341223
29
Y = -6170198
27 feet Y = -1880676
43 meter
Z = 15649486
42 Z = 4769963
46
XDOT = 16197
970401 XDOT = 4937
141378
YDOT = -16026
080316 feet/sec YDOT = -4884
749280 meter/sec
ZDOT = 8389
457387 ZDOT = 2557
106611
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
55201477
00016717 00000-0 10270-3 0 9042
2 25544 51
6458 176
6747 0004326 190
4700 169
6375 15
74976842 14088
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
55201477 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 176
6747 deg
Eccentricity:
0004326
Arg of perigee: 190
4700 deg
Mean anomaly: 169
6375 deg
Mean motion: 15
74976842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 324
Coasting Arc #6 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5966111
46 A = 6727751
47 meter
Y = 2476041
76 meter E =
0003740
Z = -1880454
27 I = 51
71197
XDOT = -3419
507353 Wp = 67
02280
YDOT = -3959
013699 meter/sec RA = 170
74653 deg
ZDOT = 5646
420386 TA = 272
11585
MA = 272
15868
Ha = 188
788 n
mi
Hp = 182
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19573856
51 X = -5984220
61
Y = 8123496
58 feet Y = 2409223
97 meter
Z = -6169469
37 Z = -1909481
75
XDOT = -11218
856145 XDOT = -3402
412305
YDOT = -12988
890088 feet/sec YDOT = -3997
157296 meter/sec
ZDOT = 18525
001267 ZDOT = 5629
849664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13801835
19 X = -4206799
37
Y = 16037444
37 feet Y = 4888213
05 meter
Z = -6284833
40 Z = -1915617
22
XDOT = -14787
228011 XDOT = -4507
147098
YDOT = -5505
100124 feet/sec YDOT = -1677
954518 meter/sec
ZDOT = 18458
961645 ZDOT = 5626
291509
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
50375996
00016717 00000-0 10270-3 0 9057
2 25544 51
6450 171
7806 0004097 193
9473 166
1578 15
74992020 14232
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
50375996 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 171
7806 deg
Eccentricity:
0004097
Arg of perigee: 193
9473 deg
Mean anomaly: 166
1578 deg
Mean motion: 15
74992020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 323
Coasting Arc #7 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2870043
36 A = 6718165
43 meter
Y = 3384092
65 meter E =
0011901
Z = -5054183
57 I = 51
70967
XDOT = -6793
923062 Wp = 94
33078
YDOT = 3161
709312 meter/sec RA = 165
64007 deg
ZDOT = -1745
392981 TA = 158
89451
MA = 158
84536
Ha = 188
662 n
mi
Hp = 182
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9416152
76 X = 2856540
91
Y = 11102666
18 feet Y = 3416111
86 meter
Z = -16581967
09 Z = -5040273
54
XDOT = -22289
773825 XDOT = -6820
294091
YDOT = 10373
062046 feet/sec YDOT = 3085
588233 meter/sec
ZDOT = -5726
354923 ZDOT = -1778
461910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13583468
59 X = 4140241
23
Y = 5409084
29 feet Y = 1648688
89 meter
Z = -16526522
62 Z = -5037284
09
XDOT = -14491
093694 XDOT = -4416
885358
YDOT = 18537
224237 feet/sec YDOT = 5650
145947 meter/sec
ZDOT = -5857
788027 ZDOT = -1785
453791
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
51892087
00016717 00000-0 10270-3 0 9066
2 25544 51
6450 166
5593 0004091 196
6078 163
4952 15
75047820 14395
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
51892087 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 166
5593 deg
Eccentricity:
0004091
Arg of perigee: 196
6078 deg
Mean anomaly: 163
4952 deg
Mean motion: 15
75047820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 315
Coasting Arc #8 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5877490
08 A = 6728315
24 meter
Y = -3046388
72 meter E =
0015169
Z = 1151792
03 I = 51
77455
XDOT = 3145
300515 Wp = 136
82930
YDOT = 3821
673682 meter/sec RA = 160
47810 deg
ZDOT = -5907
552864 TA = 30
56769
MA = 30
47938
Ha = 188
363 n
mi
Hp = 182
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19283103
94 X = 5905523
32
Y = -9994713
66 feet Y = -2980506
41 meter
Z = 3778845
24 Z = 1180412
91
XDOT = 10319
227412 XDOT = 3131
029923
YDOT = 12538
299480 feet/sec YDOT = 3856
766613 meter/sec
ZDOT = -19381
735118 ZDOT = -5892
307596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12101256
48 X = 3688462
97
Y = -18011643
46 feet Y = -5489948
93 meter
Z = 3892603
48 Z = 1186465
54
XDOT = 13856
745067 XDOT = 4223
535896
YDOT = 5110
347466 feet/sec YDOT = 1557
633908 meter/sec
ZDOT = -19320
957201 ZDOT = -5889
027755
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
53404601
00016717 00000-0 10270-3 0 9071
2 25544 51
6456 161
3383 0003849 200
1951 159
9061 15
75143876 14559
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
53404601 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 161
3383 deg
Eccentricity:
0003849
Arg of perigee: 200
1951 deg
Mean anomaly: 159
9061 deg
Mean motion: 15
75143876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 294
Coasting Arc #9 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2010/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2605646
02 A = 6717006
20 meter
Y = -3329192
90 meter E =
0005555
Z = 5219183
33 I = 51
76441
XDOT = 6638
952043 Wp = 165
47362
YDOT = -3807
727027 meter/sec RA = 155
36256 deg
ZDOT = 880
123494 TA = 276
13156
MA = 276
19484
Ha = 188
339 n
mi
Hp = 182
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8548707
43 X = -2593578
55
Y = -10922548
90 feet Y = -3358263
29 meter
Z = 17123304
90 Z = 5206554
45
XDOT = 21781
338725 XDOT = 6676
761832
YDOT = -12492
542741 feet/sec YDOT = -3733
274904 meter/sec
ZDOT = 2887
544272 ZDOT = 912
467340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12921377
28 X = -3938435
79
Y = -5209850
42 feet Y = -1587962
41 meter
Z = 17072946
78 Z = 5203834
18
XDOT = 12348
826009 XDOT = 3763
922168
YDOT = -20684
378650 feet/sec YDOT = -6304
598612 meter/sec
ZDOT = 3016
101399 ZDOT = 919
307706
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
54913744
00016717 00000-0 10270-3 0 9087
2 25544 51
6452 156
1172 0003860 203
0021 157
0970 15
75182161 14712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
54913744 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 156
1172 deg
Eccentricity:
0003860
Arg of perigee: 203
0021 deg
Mean anomaly: 157
0970 deg
Mean motion: 15
75182161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 273
Coasting Arc #10 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2010/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5683775
67 A = 6728685
17 meter
Y = 3577428
14 meter E =
0007952
Z = -358482
06 I = 51
83141
XDOT = -2807
183887 Wp = 49
07625
YDOT = -3863
923973 meter/sec RA = 150
21793 deg
ZDOT = 6040
334514 TA = 307
03625
MA = 307
10896
Ha = 188
085 n
mi
Hp = 182
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18647557
98 X = -5721615
24
Y = 11736968
95 feet Y = 3513657
19 meter
Z = -1176122
24 Z = -386185
86
XDOT = -9209
920888 XDOT = -2793
111021
YDOT = -12676
915921 feet/sec YDOT = -3895
236721 meter/sec
ZDOT = 19817
370453 ZDOT = 6026
731501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10052748
10 X = -3064077
62
Y = 19599973
88 feet Y = 5974072
04 meter
Z = -1286235
65 Z = -392044
63
XDOT = -13056
644629 XDOT = -3979
665283
YDOT = -5417
804265 feet/sec YDOT = -1651
346740 meter/sec
ZDOT = 19763
114257 ZDOT = 6023
797226
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
50075476
00016717 00000-0 10270-3 0 9096
2 25544 51
6456 151
2220 0003649 207
3059 152
7914 15
75202218 14861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
50075476 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 151
2220 deg
Eccentricity:
0003649
Arg of perigee: 207
3059 deg
Mean anomaly: 152
7914 deg
Mean motion: 15
75202218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 291
Coasting Arc #11 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2010/113/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3579661
25 A = 6730164
52 meter
Y = 4899493
28 meter E =
0004641
Z = -2906554
19 I = 51
83002
XDOT = -5689
713740 Wp = 278
50285
YDOT = -1154
290966 meter/sec RA = 148
27181 deg
ZDOT = 5055
437572 TA = 48
16468
MA = 48
12507
Ha = 189
354 n
mi
Hp = 188
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11744295
45 X = -3620062
68
Y = 16074453
02 feet Y = 4859237
38 meter
Z = -9535938
95 Z = -2924042
52
XDOT = -18667
039829 XDOT = -5700
941819
YDOT = -3787
043851 feet/sec YDOT = -1217
979339 meter/sec
ZDOT = 16586
081273 ZDOT = 5027
769668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15189303
04 X = 4629699
57
Y = -12816892
07 feet Y = -3906588
70 meter
Z = -9605362
97 Z = -2927714
63
XDOT = 16382
022291 XDOT = 4993
240394
YDOT = 7051
734233 feet/sec YDOT = 2149
368594 meter/sec
ZDOT = 16475
949013 ZDOT = 5021
869259
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
88139484
00016717 00000-0 10270-3 0 9109
2 25544 51
6466 149
2648 0008863 262
5970 97
4186 15
73397791 14923
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
88139484 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 149
2648 deg
Eccentricity:
0008863
Arg of perigee: 262
5970 deg
Mean anomaly: 97
4186 deg
Mean motion: 15
73397791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 346
Coasting Arc #12 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2010/114/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5143520
86 A = 6725771
48 meter
Y = 388825
81 meter E =
0002717
Z = -4317011
71 I = 51
84059
XDOT = -3387
150104 Wp = 342
68615
YDOT = 5963
563981 meter/sec RA = 143
20342 deg
ZDOT = -3495
405643 TA = 252
02428
MA = 252
05389
Ha = 188
881 n
mi
Hp = 188
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16875068
45 X = 5159762
06
Y = 1275675
23 feet Y = 446434
34 meter
Z = -14163424
24 Z = -4291984
90
XDOT = -11112
697192 XDOT = -3436
603849
YDOT = 19565
498626 feet/sec YDOT = 5925
410189 meter/sec
ZDOT = -11467
866283 ZDOT = -3511
980904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16251208
47 X = -4953368
34
Y = -5010491
37 feet Y = -1527197
77 meter
Z = -14063821
24 Z = -4286652
71
XDOT = 14749
794686 XDOT = 4495
737420
YDOT = -15437
816260 feet/sec YDOT = -4705
446396 meter/sec
ZDOT = -11533
628868 ZDOT = -3515
450079
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
89760914
00016717 00000-0 10270-3 0 9110
2 25544 51
6467 144
0515 0008932 267
1752 92
8389 15
73444640 15084
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
89760914 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 144
0515 deg
Eccentricity:
0008932
Arg of perigee: 267
1752 deg
Mean anomaly: 92
8389 deg
Mean motion: 15
73444640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 318
Coasting Arc #13 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2010/115/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2320530
66 A = 6729211
95 meter
Y = -5450727
81 meter E =
0004124
Z = 3187528
22 I = 51
87554
XDOT = 5985
657438 Wp = 98
50395
YDOT = -281
026063 meter/sec RA = 138
03837 deg
ZDOT = -4833
445140 TA = 44
46011
MA = 44
42702
Ha = 188
443 n
mi
Hp = 188
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7613289
57 X = 2365824
59
Y = -17882965
27 feet Y = -5424524
88 meter
Z = 10457769
75 Z = 3198911
73
XDOT = 19637
983720 XDOT = 6011
835334
YDOT = -922
001520 feet/sec YDOT = -213
944702 meter/sec
ZDOT = -15857
759647 ZDOT = -4804
302876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11062558
00 X = -3371867
68
Y = 15951066
53 feet Y = 4861885
08 meter
Z = 10502897
70 Z = 3201283
22
XDOT = -18336
849626 XDOT = -5589
071766
YDOT = -2341
975823 feet/sec YDOT = -713
834231 meter/sec
ZDOT = -15741
795864 ZDOT = -4798
099379
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
91379384
00016717 00000-0 10270-3 0 9122
2 25544 51
6461 138
8377 0008813 270
9945 89
0208 15
73477064 15241
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
91379384 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 138
8377 deg
Eccentricity:
0008813
Arg of perigee: 270
9945 deg
Mean anomaly: 89
0208 deg
Mean motion: 15
73477064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1524
Checksum: 327
Coasting Arc #14 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2010/116/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5235680
80 A = 6726250
49 meter
Y = 863050
18 meter E =
0002240
Z = 4133433
13 I = 51
88730
XDOT = 1928
857747 Wp = 141
46168
YDOT = -6421
967022 meter/sec RA = 132
97314 deg
ZDOT = 3781
303444 TA = 269
89440
MA = 269
92006
Ha = 189
182 n
mi
Hp = 188
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17177430
43 X = -5265022
26
Y = 2831529
47 feet Y = 804337
73 meter
Z = 13561132
32 Z = 4107926
47
XDOT = 6328
273448 XDOT = 1982
156777
YDOT = -21069
445610 feet/sec YDOT = -6400
099285 meter/sec
ZDOT = 12405
851194 ZDOT = 3790
803613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17481469
16 X = 5328351
80
Y = 471249
99 feet Y = 143637
00 meter
Z = 13459648
76 Z = 4102500
94
XDOT = -10079
480545 XDOT = -3072
225670
YDOT = 18237
894618 feet/sec YDOT = 5558
910279 meter/sec
ZDOT = 12443
465660 ZDOT = 3792
768333
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
92994665
00016717 00000-0 10270-3 0 9130
2 25544 51
6461 133
6228 0008846 275
4361 84
5792 15
73512765 15401
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
92994665 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 133
6228 deg
Eccentricity:
0008846
Arg of perigee: 275
4361 deg
Mean anomaly: 84
5792 deg
Mean motion: 15
73512765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 325
Coasting Arc #15 (Orbit 1554)
---------------------------------------
Vector Time (GMT): 2010/117/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1045861
84 A = 6728323
24 meter
Y = 5703877
07 meter E =
0004208
Z = -3407322
22 I = 51
91427
XDOT = -5910
077447 Wp = 288
34482
YDOT = 1688
513729 meter/sec RA = 127
80844 deg
ZDOT = 4637
303843 TA = 31
59191
MA = 31
56666
Ha = 189
194 n
mi
Hp = 188
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3431305
24 X = -1093013
39
Y = 18713507
46 feet Y = 5691917
99 meter
Z = -11178878
69 Z = -3412517
66
XDOT = -19390
017871 XDOT = -5951
047094
YDOT = 5539
743205 feet/sec YDOT = 1622
194654 meter/sec
ZDOT = 15214
251455 ZDOT = 4608
492592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6525700
34 X = 1989033
46
Y = -17858480
18 feet Y = -5443264
76 meter
Z = -11199395
83 Z = -3413575
85
XDOT = 18838
665717 XDOT = 5742
025311
YDOT = -2592
274598 feet/sec YDOT = -790
125298 meter/sec
ZDOT = 15099
631273 ZDOT = 4602
367612
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
88256051
00016717 00000-0 10270-3 0 9147
2 25544 51
6456 128
7340 0009060 279
0835 80
9303 15
73573222 15559
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
88256051 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 128
7340 deg
Eccentricity:
0009060
Arg of perigee: 279
0835 deg
Mean anomaly: 80
9303 deg
Mean motion: 15
73573222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1555
Checksum: 300
Coasting Arc #16 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2010/118/21:00:38
298
Vector Time (MET): N/A
Weight (LBS) : 796682
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5023370
83 A = 6726519
39 meter
Y = -2053496
54 meter E =
0004668
Z = -3975319
76 I = 51
92540
XDOT = -490
544507 Wp = 329
87797
YDOT = 6557
258033 meter/sec RA = 122
74687 deg
ZDOT = -4001
133457 TA = 258
77100
MA = 258
82347
Ha = 189
339 n
mi
Hp = 187
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16480875
42 X = 5065271
83
Y = -6737193
38 feet Y = -1997087
84 meter
Z = -13042387
67 Z = -3950813
99
XDOT = -1609
397990 XDOT = -544
395298
YDOT = 21513
313756 feet/sec YDOT = 6551
471480 meter/sec
ZDOT = -13127
078271 ZDOT = -4003
647209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17399865
63 X = -5303479
04
Y = 4097205
92 feet Y = 1248828
36 meter
Z = -12944901
89 Z = -3945606
10
XDOT = 5137
770494 XDOT = 1565
992447
YDOT = -19748
760633 feet/sec YDOT = -6019
422241 meter/sec
ZDOT = -13136
913489 ZDOT = -4004
131232
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
89865258
00016717 00000-0 10270-3 0 9155
2 25544 51
6451 123
5193 0009134 282
5247 77
4894 15
73610910 15711
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
89865258 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 123
5193 deg
Eccentricity:
0009134
Arg of perigee: 282
5247 deg
Mean anomaly: 77
4894 deg
Mean motion: 15
73610910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 320
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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