Date:
April 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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
There are no maneuvers
Coasting Arc #1 (Orbit 1316)
---------------------------------------
Vector Time (GMT): 2010/102/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1668998
74 A = 6721758
05 meter
Y = -4739030
11 meter E =
0012570
Z = 4461052
47 I = 51
48908
XDOT = 6993
704543 Wp = 129
06153
YDOT = 547
110388 meter/sec RA = 205
64500 deg
ZDOT = 3183
947180 TA = 288
98787
MA = 289
12403
Ha = 190
196 n
mi
Hp = 182
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5475717
65 X = -1637553
19
Y = -15547999
05 feet Y = -4757517
68 meter
Z = 14635998
93 Z = 4453021
16
XDOT = 22945
224879 XDOT = 6971
599690
YDOT = 1794
981587 feet/sec YDOT = 625
194810 meter/sec
ZDOT = 10446
020933 ZDOT = 3217
869151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14242317
87 X = -4341058
49
Y = 8355768
05 feet Y = 2546838
10 meter
Z = 14603894
85 Z = 4451267
15
XDOT = -1881
760896 XDOT = -573
560721
YDOT = -21779
506765 feet/sec YDOT = -6638
393662 meter/sec
ZDOT = 10580
867498 ZDOT = 3225
048413
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 10102
77743184
00016717 00000-0 10270-3 0 9002
2 25544 51
6458 206
3604 0004677 162
8688 197
2634 15
74628882 13170
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
77743184 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 206
3604 deg
Eccentricity:
0004677
Arg of perigee: 162
8688 deg
Mean anomaly: 197
2634 deg
Mean motion: 15
74628882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1317
Checksum: 326
Coasting Arc #2 (Orbit 1331)
---------------------------------------
Vector Time (GMT): 2010/103/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6215372
56 A = 6727164
31 meter
Y = -132978
53 meter E =
0005319
Z = -2576953
82 I = 51
53734
XDOT = -2064
478293 Wp = 106
49146
YDOT = -5226
335858 meter/sec RA = 200
45069 deg
ZDOT = 5256
482767 TA = 224
23137
MA = 224
27390
Ha = 189
932 n
mi
Hp = 182
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20391642
27 X = -6200905
09
Y = -436281
25 feet Y = -202401
80 meter
Z = -8454572
90 Z = -2607113
34
XDOT = -6773
222745 XDOT = -2031
418408
YDOT = -17146
771188 feet/sec YDOT = -5249
236878 meter/sec
ZDOT = 17245
678368 ZDOT = 5246
534061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3698190
30 X = 1127208
40
Y = 20007281
48 feet Y = 6098219
40 meter
Z = -8574455
94 Z = -2613494
17
XDOT = -13936
736668 XDOT = -4247
917337
YDOT = 9939
647609 feet/sec YDOT = 3029
604591 meter/sec
ZDOT = 17205
933426 ZDOT = 5244
368508
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 10103
72937367
00016717 00000-0 10270-3 0 9017
2 25544 51
6469 201
4683 0004627 166
5201 193
6087 15
74715780 13325
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
72937367 = yrday
fracday
Element set: 901
Inclination: 51
6469 deg
RA of node: 201
4683 deg
Eccentricity:
0004627
Arg of perigee: 166
5201 deg
Mean anomaly: 193
6087 deg
Mean motion: 15
74715780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1332
Checksum: 306
Coasting Arc #3 (Orbit 1347)
---------------------------------------
Vector Time (GMT): 2010/104/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1885438
80 A = 6720445
87 meter
Y = 4405616
85 meter E =
0011295
Z = -4721002
22 I = 51
54230
XDOT = -7210
131181 Wp = 94
29199
YDOT = 225
094401 meter/sec RA = 195
34585 deg
ZDOT = -2675
786099 TA = 149
37371
MA = 149
30772
Ha = 189
776 n
mi
Hp = 182
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6185822
82 X = 1858968
42
Y = 14454123
52 feet Y = 4426552
71 meter
Z = -15488852
42 Z = -4711907
13
XDOT = -23655
286027 XDOT = -7199
113651
YDOT = 738
498691 feet/sec YDOT = 144
527892 meter/sec
ZDOT = -8778
825783 ZDOT = -2710
786733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12722216
46 X = 3877731
58
Y = -9298123
49 feet Y = -2834068
04 meter
Z = -15452532
10 Z = -4709931
78
XDOT = 5226
215936 XDOT = 1592
950617
YDOT = 21937
010178 feet/sec YDOT = 6686
400702 meter/sec
ZDOT = -8917
946818 ZDOT = -2718
190190
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
74474687
00016717 00000-0 10270-3 0 9022
2 25544 51
6459 196
2488 0004461 171
4304 188
6937 15
74734244 13484
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
74474687 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 196
2488 deg
Eccentricity:
0004461
Arg of perigee: 171
4304 deg
Mean anomaly: 188
6937 deg
Mean motion: 15
74734244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1348
Checksum: 330
Coasting Arc #4 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2010/105/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6363125
49 A = 6727932
35 meter
Y = -540946
86 meter E =
0016362
Z = 2087722
09 I = 51
59679
XDOT = 2239
430793 Wp = 123
84104
YDOT = 4865
122589 meter/sec RA = 190
15995 deg
ZDOT = -5542
964920 TA = 32
79832
MA = 32
69686
Ha = 189
489 n
mi
Hp = 182
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20876395
96 X = 6358559
57
Y = -1774760
04 feet Y = -469816
08 meter
Z = 6849481
92 Z = 2118623
63
XDOT = 7347
213888 XDOT = 2211
788885
YDOT = 15961
688284 feet/sec YDOT = 4890
010533 meter/sec
ZDOT = -18185
580445 ZDOT = -5532
152845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6649437
69 X = -2026748
61
Y = -19825765
86 feet Y = -6042893
43 meter
Z = 6972307
42 Z = 2125159
30
XDOT = 12301
168671 XDOT = 3749
396211
YDOT = -10530
929654 feet/sec YDOT = -3209
827359 meter/sec
ZDOT = -18142
418027 ZDOT = -5529
809015
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
76008726
00016717 00000-0 10270-3 0 9033
2 25544 51
6448 191
0291 0004258 174
5338 185
5873 15
74802139 13644
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
76008726 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 191
0291 deg
Eccentricity:
0004258
Arg of perigee: 174
5338 deg
Mean anomaly: 185
5873 deg
Mean motion: 15
74802139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 311
Coasting Arc #5 (Orbit 1379)
---------------------------------------
Vector Time (GMT): 2010/106/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986254
85 A = 6719266
18 meter
Y = -4102567
32 meter E =
0009291
Z = 4934767
11 I = 51
59656
XDOT = 7342
198699 Wp = 145
63222
YDOT = -1020
211436 meter/sec RA = 185
05176 deg
ZDOT = 2097
635979 TA = 283
98441
MA = 284
08770
Ha = 189
452 n
mi
Hp = 182
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6516584
16 X = -1964204
21
Y = -13459866
53 feet Y = -4124655
50 meter
Z = 16190180
81 Z = 4925171
29
XDOT = 24088
578409 XDOT = 7342
871076
YDOT = -3347
150379 feet/sec YDOT = -938
102837 meter/sec
ZDOT = 6882
007804 ZDOT = 2133
306645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11348186
35 X = -3458927
20
Y = 9802612
35 feet Y = 2987836
24 meter
Z = 16151881
89 Z = 4923093
60
XDOT = -8608
680968 XDOT = -2623
925959
YDOT = -21590
412067 feet/sec YDOT = -6580
757598 meter/sec
ZDOT = 7023
789826 ZDOT = 2140
851139
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
77539567
00016717 00000-0 10270-3 0 9048
2 25544 51
6438 185
8092 0004188 179
5775 180
5393 15
74825358 13803
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
77539567 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 185
8092 deg
Eccentricity:
0004188
Arg of perigee: 179
5775 deg
Mean anomaly: 180
5393 deg
Mean motion: 15
74825358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1380
Checksum: 345
Coasting Arc #6 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2010/107/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6429989
93 A = 6728495
32 meter
Y = 1236900
02 meter E =
0005287
Z = -1546550
47 I = 51
65858
XDOT = -2261
743487 Wp = 65
61956
YDOT = -4561
258974 meter/sec RA = 179
87802 deg
ZDOT = 5773
053509 TA = 277
33834
MA = 277
39842
Ha = 189
221 n
mi
Hp = 182
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21095767
48 X = -6435830
29
Y = 4058070
94 feet Y = 1164963
42 meter
Z = -5073984
47 Z = -1577802
00
XDOT = -7420
418264 XDOT = -2238
615453
YDOT = -14964
760415 feet/sec YDOT = -4586
421931 meter/sec
ZDOT = 18940
464269 ZDOT = 5762
121881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9588199
67 X = 2922483
26
Y = 19190876
88 feet Y = 5849379
27 meter
Z = -5198205
01 Z = -1584412
89
XDOT = -10979
445890 XDOT = -3346
535107
YDOT = 10588
911112 feet/sec YDOT = 3227
500107 meter/sec
ZDOT = 18896
836982 ZDOT = 5759
755912
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
72721705
00016717 00000-0 10270-3 0 9052
2 25544 51
6435 180
9162 0004208 181
4164 178
6989 15
74907583 13957
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
72721705 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 180
9162 deg
Eccentricity:
0004208
Arg of perigee: 181
4164 deg
Mean anomaly: 178
6989 deg
Mean motion: 15
74907583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 323
Coasting Arc #7 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2010/108/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1924114
69 A = 6718167
35 meter
Y = 3900160
94 meter E =
0013299
Z = -5131615
94 I = 51
65324
XDOT = -7350
034282 Wp = 96
13019
YDOT = 1787
407919 meter/sec RA = 174
76278 deg
ZDOT = -1401
932123 TA = 160
45926
MA = 160
40824
Ha = 189
054 n
mi
Hp = 182
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6312712
23 X = 1905288
13
Y = 12795803
61 feet Y = 3921572
44 meter
Z = -16836010
29 Z = -5122314
08
XDOT = -24114
285702 XDOT = -7362
664712
YDOT = 5864
199208 feet/sec YDOT = 1705
144891 meter/sec
ZDOT = -4599
514838 ZDOT = -1437
669616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10425226
03 X = 3177608
89
Y = -9805421
94 feet Y = -2988692
61 meter
Z = -16798884
82 Z = -5120300
09
XDOT = 11797
107040 XDOT = 3595
758226
YDOT = 20640
884138 feet/sec YDOT = 6291
341485 meter/sec
ZDOT = -4741
573376 ZDOT = -1445
231565
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
74246273
00016717 00000-0 10270-3 0 9068
2 25544 51
6428 175
6948 0004018 187
0100 173
1008 15
74920123 14119
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
74246273 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 175
6948 deg
Eccentricity:
0004018
Arg of perigee: 187
0100 deg
Mean anomaly: 173
1008 deg
Mean motion: 15
74920123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 281
Coasting Arc #8 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2010/109/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6388122
72 A = 6728980
88 meter
Y = -1886442
56 meter E =
0015554
Z = 890303
98 I = 51
72055
XDOT = 2134
549810 Wp = 138
53982
YDOT = 4392
036204 meter/sec RA = 169
60284 deg
ZDOT = -5962
140088 TA = 31
74387
MA = 31
65019
Ha = 188
772 n
mi
Hp = 182
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20958407
89 X = 6404417
52
Y = -6189116
03 feet Y = -1814915
70 meter
Z = 2920944
80 Z = 921377
19
XDOT = 7003
116173 XDOT = 2114
241817
YDOT = 14409
567597 feet/sec YDOT = 4415
792689 meter/sec
ZDOT = -19560
827060 ZDOT = -5951
819537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12236083
78 X = -3729558
34
Y = -18085944
78 feet Y = -5512595
97 meter
Z = 3044469
11 Z = 927954
18
XDOT = 10260
403778 XDOT = 3127
371072
YDOT = -10252
693825 feet/sec YDOT = -3125
021078 meter/sec
ZDOT = -19519
630027 ZDOT = -5949
583232
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
75767588
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 170
4741 0003809 192
2389 167
8683 15
74993561 14279
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
75767588 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 170
4741 deg
Eccentricity:
0003809
Arg of perigee: 192
2389 deg
Mean anomaly: 167
8683 deg
Mean motion: 15
74993561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 351
Coasting Arc #9 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2010/110/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1785531
19 A = 6717332
85 meter
Y = -3799727
31 meter E =
0005227
Z = 5242854
72 I = 51
71089
XDOT = 7249
423425 Wp = 163
03295
YDOT = -2529
688922 meter/sec RA = 164
48018 deg
ZDOT = 630
456623 TA = 280
95294
MA = 281
01174
Ha = 188
695 n
mi
Hp = 182
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5858041
95 X = -1768378
14
Y = -12466296
95 feet Y = -3819598
43 meter
Z = 17200966
92 Z = 5234222
14
XDOT = 23784
197589 XDOT = 7274
109414
YDOT = -8299
504338 feet/sec YDOT = -2448
483550 meter/sec
ZDOT = 2068
427242 ZDOT = 665
734284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9913805
28 X = -3021727
85
Y = 9624251
92 feet Y = 2933471
98 meter
Z = 17166499
88 Z = 5232349
16
XDOT = -14746
678212 XDOT = -4494
787519
YDOT = -19159
582622 feet/sec YDOT = -5839
840783 meter/sec
ZDOT = 2208
671590 ZDOT = 673
203101
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
77285817
00016717 00000-0 10270-3 0 9083
2 25544 51
6427 165
2535 0003802 197
1513 162
9523 15
75021754 14431
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
77285817 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 165
2535 deg
Eccentricity:
0003802
Arg of perigee: 197
1513 deg
Mean anomaly: 162
9523 deg
Mean motion: 15
75021754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 298
Coasting Arc #10 (Orbit 1457)
---------------------------------------
Vector Time (GMT): 2010/111/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237294
45 A = 6729027
68 meter
Y = 2509749
79 meter E =
0008455
Z = -187090
33 I = 51
77999
XDOT = -1930
045869 Wp = 54
62555
YDOT = -4360
477632 meter/sec RA = 159
33689 deg
ZDOT = 6045
849666 TA = 303
34541
MA = 303
42632
Ha = 188
466 n
mi
Hp = 182
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20463564
46 X = -6263986
50
Y = 8234087
23 feet Y = 2439851
41 meter
Z = -613813
41 Z = -217455
88
XDOT = -6332
171486 XDOT = -1910
512403
YDOT = -14306
028977 feet/sec YDOT = -4381
951411 meter/sec
ZDOT = 19835
464784 ZDOT = 6036
520903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14616322
33 X = 4455055
05
Y = 16515387
12 feet Y = 5033890
00 meter
Z = -734533
54 Z = -223885
82
XDOT = -10111
536437 XDOT = -3081
996306
YDOT = 9805
544054 feet/sec YDOT = 2988
729828 meter/sec
ZDOT = 19798
205039 ZDOT = 6034
492896
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
72456202
00016717 00000-0 10270-3 0 9098
2 25544 51
6427 160
3589 0003849 198
9121 161
1900 15
75097567 14582
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
72456202 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 160
3589 deg
Eccentricity:
0003849
Arg of perigee: 198
9121 deg
Mean anomaly: 161
1900 deg
Mean motion: 15
75097567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 314
Coasting Arc #11 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2010/112/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1569846
44 A = 6716936
32 meter
Y = 3860700
26 meter E =
0013978
Z = -5279247
69 I = 51
76811
XDOT = -7002
392544 Wp = 105
90470
YDOT = 3176
736094 meter/sec RA = 154
20259 deg
ZDOT = 237
661894 TA = 166
36817
MA = 166
33038
Ha = 188
277 n
mi
Hp = 182
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5150414
81 X = 1552204
32
Y = 12666339
44 feet Y = 3878156
52 meter
Z = -17320366
45 Z = -5271664
28
XDOT = -22973
728818 XDOT = -7038
549459
YDOT = 10422
362512 feet/sec YDOT = 3098
229011 meter/sec
ZDOT = 779
730623 ZDOT = 203
556454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10012569
95 X = 3051831
32
Y = -9368038
73 feet Y = -2855378
20 meter
Z = -17290064
05 Z = -5270011
52
XDOT = 17148
792044 XDOT = 5226
951815
YDOT = 17120
181120 feet/sec YDOT = 5218
231205 meter/sec
ZDOT = 644
140594 ZDOT = 196
334053
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
73968273
00016717 00000-0 10270-3 0 9108
2 25544 51
6436 155
1373 0003690 205
3174 154
7809 15
75115245 14748
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
73968273 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 155
1373 deg
Eccentricity:
0003690
Arg of perigee: 205
3174 deg
Mean anomaly: 154
7809 deg
Mean motion: 15
75115245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 300
Coasting Arc #12 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2010/113/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974944
86 A = 6728698
72 meter
Y = -3016753
91 meter E =
0012644
Z = -613754
89 I = 51
83560
XDOT = 1666
830466 Wp = 155
47143
YDOT = 4514
317020 meter/sec RA = 149
07811 deg
ZDOT = -6017
461019 TA = 31
19790
MA = 31
12291
Ha = 188
113 n
mi
Hp = 182
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19602837
45 X = 6011216
18
Y = -9897486
60 feet Y = -2949735
74 meter
Z = -2013631
52 Z = -584640
38
XDOT = 5468
603891 XDOT = 1645
458448
YDOT = 14810
751377 feet/sec YDOT = 4532
836822 meter/sec
ZDOT = -19742
326178 ZDOT = -6009
415605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16412290
43 X = -5002466
12
Y = -14605510
88 feet Y = -4451759
72 meter
Z = -1897884
03 Z = -578475
05
XDOT = 10657
085216 XDOT = 3248
279574
YDOT = -9439
196483 feet/sec YDOT = -2877
067088 meter/sec
ZDOT = -19710
161606 ZDOT = -6007
657258
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
75477191
00016717 00000-0 10270-3 0 9116
2 25544 51
6442 149
9161 0003632 210
2546 149
8408 15
75172244 14905
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
75477191 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 149
9161 deg
Eccentricity:
0003632
Arg of perigee: 210
2546 deg
Mean anomaly: 149
8408 deg
Mean motion: 15
75172244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 295
Coasting Arc #13 (Orbit 1505)
---------------------------------------
Vector Time (GMT): 2010/114/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1353262
90 A = 6717037
30 meter
Y = -4053973
03 meter E =
0001416
Z = 5180818
15 I = 51
82228
XDOT = 6650
922912 Wp = 124
83814
YDOT = -3709
765155 meter/sec RA = 143
93247 deg
ZDOT = -1166
184504 TA = 336
26052
MA = 336
26705
Ha = 187
961 n
mi
Hp = 182
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4439838
92 X = -1332997
69
Y = -13300436
46 feet Y = -4068992
49 meter
Z = 16997434
86 Z = 5174293
36
XDOT = 21820
613229 XDOT = 6697
577003
YDOT = -12171
145523 feet/sec YDOT = -3635
129769 meter/sec
ZDOT = -3826
064646 ZDOT = -1133
760664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10543207
68 X = -3213569
70
Y = 9291989
21 feet Y = 2832198
31 meter
Z = 16971337
01 Z = 5172863
52
XDOT = -18937
822036 XDOT = -5772
248157
YDOT = -14738
646584 feet/sec YDOT = -4492
339479 meter/sec
ZDOT = -3697
162489 ZDOT = -1126
895127
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
76982975
00016717 00000-0 10270-3 0 9120
2 25544 51
6443 144
6953 0003594 214
5464 145
5467 15
75219357 15063
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
76982975 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 144
6953 deg
Eccentricity:
0003594
Arg of perigee: 214
5464 deg
Mean anomaly: 145
5467 deg
Mean motion: 15
75219357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1506
Checksum: 327
Coasting Arc #14 (Orbit 1521)
---------------------------------------
Vector Time (GMT): 2010/115/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5611752
95 A = 6727699
20 meter
Y = 3414033
13 meter E =
0010763
Z = 1433525
66 I = 51
88200
XDOT = -1436
299905 Wp = 68
08391
YDOT = -4822
430056 meter/sec RA = 138
82548 deg
ZDOT = 5831
545729 TA = 307
64075
MA = 307
73836
Ha = 187
719 n
mi
Hp = 182
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18411262
97 X = -5656476
09
Y = 11200896
11 feet Y = 3351029
17 meter
Z = 4703168
16 Z = 1406154
69
XDOT = -4712
270028 XDOT = -1410
596784
YDOT = -15821
620918 feet/sec YDOT = -4838
347663 meter/sec
ZDOT = 19132
367878 ZDOT = 5824
630740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17630715
74 X = 5373842
16
Y = 12433995
33 feet Y = 3789881
78 meter
Z = 4594354
31 Z = 1400359
19
XDOT = -11672
848935 XDOT = -3557
884355
YDOT = 9454
096817 feet/sec YDOT = 2881
608710 meter/sec
ZDOT = 19104
695450 ZDOT = 5823
111173
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
78485524
00016717 00000-0 10270-3 0 9132
2 25544 51
6440 139
4731 0003611 218
8956 141
1949 15
75275425 15222
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
78485524 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 139
4731 deg
Eccentricity:
0003611
Arg of perigee: 218
8956 deg
Mean anomaly: 141
1949 deg
Mean motion: 15
75275425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1522
Checksum: 308
Coasting Arc #15 (Orbit 1536)
---------------------------------------
Vector Time (GMT): 2010/116/17:22:44
831
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1169382
16 A = 6717811
28 meter
Y = 4401070
79 meter E =
0011521
Z = -4949167
51 I = 51
87128
XDOT = -6183
759122 Wp = 121
61996
YDOT = 4048
987239 meter/sec RA = 133
66631 deg
ZDOT = 2137
205075 TA = 169
07044
MA = 169
04539
Ha = 187
525 n
mi
Hp = 182
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3836555
65 X = 1144124
24
Y = 14439208
62 feet Y = 4414006
16 meter
Z = -16237426
23 Z = -4943548
04
XDOT = -20287
923629 XDOT = -6238
958355
YDOT = 13284
078869 feet/sec YDOT = 3979
528186 meter/sec
ZDOT = 7011
827674 ZDOT = 2107
029696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11505647
82 X = 3506921
46
Y = -9568702
91 feet Y = -2916540
65 meter
Z = -16214928
56 Z = -4942310
23
XDOT = 19823
983184 XDOT = 6042
350075
YDOT = 12145
315706 feet/sec YDOT = 3701
892227 meter/sec
ZDOT = 6891
861858 ZDOT = 2100
639494
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
73641318
00016717 00000-0 10270-3 0 9144
2 25544 51
6441 134
5772 0003554 223
5724 136
5159 15
75316899 15374
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
73641318 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 134
5772 deg
Eccentricity:
0003554
Arg of perigee: 223
5724 deg
Mean anomaly: 136
5159 deg
Mean motion: 15
75316899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1537
Checksum: 312
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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