Date:
January 20th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 1718)
---------------------------------------
Vector Time (GMT): 2011/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5737218
59 A = 6737828
60 meter
Y = 3513377
12 meter E =
0015057
Z = 140633
91 I = 51
47546
XDOT = -2393
462816 Wp = 149
05326
YDOT = 4160
421511 meter/sec RA = 212
43621 deg
ZDOT = -6022
981148 TA = 29
41594
MA = 29
33128
Ha = 193
351 n
mi
Hp = 187
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18822895
64 X = 5696821
78
Y = 11526827
83 feet Y = 3577308
27 meter
Z = 461397
36 Z = 168407
14
XDOT = -7852
568295 XDOT = -2410
549503
YDOT = 13649
676872 feet/sec YDOT = 4133
561548 meter/sec
ZDOT = -19760
436837 ZDOT = -6034
649395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2194584
84 X = -668909
46
Y = 21959901
57 feet Y = 6693378
00 meter
Z = 573208
62 Z = 174713
99
XDOT = -14052
930944 XDOT = -4283
333352
YDOT = -868
607319 feet/sec YDOT = -264
751511 meter/sec
ZDOT = -19807
499429 ZDOT = -6037
325826
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
53215239
00016717 00000-0 10270-3 0 9007
2 25544 51
6411 213
2831 0004496 197
8524 162
2481 15
72012911 17190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
53215239 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 213
2831 deg
Eccentricity:
0004496
Arg of perigee: 197
8524 deg
Mean anomaly: 162
2481 deg
Mean motion: 15
72012911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 281
Coasting Arc #2 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2011/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1003700
70 A = 6726185
37 meter
Y = -4144535
09 meter E =
0006289
Z = 5201248
60 I = 51
46104
XDOT = 7092
411798 Wp = 167
37340
YDOT = 2855
391591 meter/sec RA = 207
31218 deg
ZDOT = 900
385430 TA = 273
99122
MA = 274
06311
Ha = 193
368 n
mi
Hp = 187
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3292981
30 X = 1024704
93
Y = -13597556
07 feet Y = -4133194
24 meter
Z = 17064463
92 Z = 5206175
03
XDOT = 23269
067578 XDOT = 7055
581341
YDOT = 9368
082649 feet/sec YDOT = 2934
497187 meter/sec
ZDOT = 2954
020439 ZDOT = 934
750434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13577127
44 X = 4138308
44
Y = -3274001
76 feet Y = -997915
74 meter
Z = 17084370
32 Z = 5207316
07
XDOT = 1867
649040 XDOT = 569
259427
YDOT = 23988
666929 feet/sec YDOT = 7311
745680 meter/sec
ZDOT = 3092
415946 ZDOT = 942
568380
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
54927776
00016717 00000-0 10270-3 0 9016
2 25544 51
6400 208
0741 0004551 200
0525 160
0458 15
71969601 17354
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
54927776 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 208
0741 deg
Eccentricity:
0004551
Arg of perigee: 200
0525 deg
Mean anomaly: 160
0458 deg
Mean motion: 15
71969601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1735
Checksum: 284
Coasting Arc #3 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2011/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6433860
34 A = 6736847
85 meter
Y = -1411019
99 meter E =
0004105
Z = -1409165
74 I = 51
52497
XDOT = -161
467173 Wp = 52
72820
YDOT = -5046
559596 meter/sec RA = 202
15891 deg
ZDOT = 5804
432493 TA = 291
77261
MA = 291
81629
Ha = 193
178 n
mi
Hp = 187
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21108465
68 X = -6410758
59
Y = -4629330
67 feet Y = -1482838
00 meter
Z = -4623247
18 Z = -1440364
58
XDOT = -529
747944 XDOT = -133
219691
YDOT = -16556
954056 feet/sec YDOT = -5048
207805 meter/sec
ZDOT = 19043
413692 ZDOT = 5803
716262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5718717
76 X = -1743065
17
Y = -20811448
29 feet Y = -6343329
44 meter
Z = -4748929
07 Z = -1447473
58
XDOT = 12834
687779 XDOT = 3912
012835
YDOT = -7861
431106 feet/sec YDOT = -2396
164201 meter/sec
ZDOT = 19040
595399 ZDOT = 5803
573478
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
50281483
00016717 00000-0 10270-3 0 9022
2 25544 51
6395 203
1905 0004661 204
0249 156
0697 15
72039023 17508
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
50281483 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 203
1905 deg
Eccentricity:
0004661
Arg of perigee: 204
0249 deg
Mean anomaly: 156
0697 deg
Mean motion: 15
72039023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 284
Coasting Arc #4 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2011/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1290229
86 A = 6727367
01 meter
Y = 4454507
80 meter E =
0009728
Z = -4881548
79 I = 51
52204
XDOT = -7337
944343 Wp = 93
49622
YDOT = -361
591642 meter/sec RA = 197
06197 deg
ZDOT = -2273
905800 TA = 154
33759
MA = 154
28928
Ha = 193
045 n
mi
Hp = 187
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4233037
58 X = 1264035
78
Y = 14614526
89 feet Y = 4468789
77 meter
Z = -16015580
02 Z = -4875344
39
XDOT = -24074
620548 XDOT = -7322
309700
YDOT = -1186
324285 feet/sec YDOT = -443
561405 meter/sec
ZDOT = -7460
320867 ZDOT = -2309
514501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10732904
80 X = -3271389
38
Y = 10821563
37 feet Y = 3298412
51 meter
Z = -15990632
49 Z = -4873944
78
XDOT = -9723
511950 XDOT = -2963
726442
YDOT = -20857
996511 feet/sec YDOT = -6357
517337 meter/sec
ZDOT = -7603
803471 ZDOT = -2317
639298
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
51990697
00016717 00000-0 10270-3 0 9030
2 25544 51
6396 197
9824 0004530 206
2063 153
8860 15
72075031 17665
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
51990697 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 197
9824 deg
Eccentricity:
0004530
Arg of perigee: 206
2063 deg
Mean anomaly: 153
8860 deg
Mean motion: 15
72075031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 309
Coasting Arc #5 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2011/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6180212
44 A = 6734707
54 meter
Y = -761519
47 meter E =
0012954
Z = 2545112
23 I = 51
57686
XDOT = 2780
100976 Wp = 123
14824
YDOT = 4867
474566 meter/sec RA = 191
89383 deg
ZDOT = -5282
081520 TA = 27
97525
MA = 27
90568
Ha = 192
746 n
mi
Hp = 187
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20276287
54 X = 6175905
24
Y = -2498423
46 feet Y = -692432
77 meter
Z = 8350105
73 Z = 2575124
31
XDOT = 9121
066195 XDOT = 2751
123967
YDOT = 15969
404744 feet/sec YDOT = 4898
401486 meter/sec
ZDOT = -17329
663781 ZDOT = -5268
646418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12197469
40 X = 3717788
67
Y = 16326575
32 feet Y = 4976340
16 meter
Z = 8471062
52 Z = 2581979
86
XDOT = -8103
886552 XDOT = -2470
064621
YDOT = 15038
540319 feet/sec YDOT = 4583
747089 meter/sec
ZDOT = -17275
572209 ZDOT = -5265
594409
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
53698169
00016717 00000-0 10270-3 0 9043
2 25544 51
6398 192
7732 0004602 212
9967 147
0908 15
72096403 17827
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
53698169 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 192
7732 deg
Eccentricity:
0004602
Arg of perigee: 212
9967 deg
Mean anomaly: 147
0908 deg
Mean motion: 15
72096403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 324
Coasting Arc #6 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3488694
28 A = 6729599
25 meter
Y = -3838939
49 meter E =
0009578
Z = 4285491
86 I = 51
59019
XDOT = 6546
604731 Wp = 135
39123
YDOT = -2019
513511 meter/sec RA = 186
81500 deg
ZDOT = 3508
890606 TA = 278
98024
MA = 279
08864
Ha = 192
762 n
mi
Hp = 187
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11445847
37 X = -3466324
84
Y = -12594945
84 feet Y = -3877827
15 meter
Z = 14060012
66 Z = 4268598
53
XDOT = 21478
361979 XDOT = 6551
655655
YDOT = -6625
700496 feet/sec YDOT = -1946
277219 meter/sec
ZDOT = 11512
108287 ZDOT = 3540
705407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4940707
68 X = 1505927
70
Y = -16344369
29 feet Y = -4981763
76 meter
Z = 13991963
37 Z = 4264750
44
XDOT = 15437
306475 XDOT = 4705
291014
YDOT = 14663
761986 feet/sec YDOT = 4469
514653 meter/sec
ZDOT = 11640
353276 ZDOT = 3547
979679
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
55404077
00016717 00000-0 10270-3 0 9050
2 25544 51
6401 187
5643 0004634 215
3890 144
6965 15
72134850 17984
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
55404077 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 187
5643 deg
Eccentricity:
0004634
Arg of perigee: 215
3890 deg
Mean anomaly: 144
6965 deg
Mean motion: 15
72134850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 308
Coasting Arc #7 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2011/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5077532
40 A = 6731946
42 meter
Y = 2657234
21 meter E =
0005028
Z = -3538581
07 I = 51
63030
XDOT = -5050
789287 Wp = 149
34339
YDOT = -3689
499791 meter/sec RA = 181
64157 deg
ZDOT = 4475
387638 TA = 168
58102
MA = 168
56961
Ha = 192
629 n
mi
Hp = 187
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16658570
88 X = -5089679
32
Y = 8717960
00 feet Y = 2600386
26 meter
Z = -11609517
93 Z = -3563276
67
XDOT = -16570
830994 XDOT = -5030
897362
YDOT = -12104
658107 feet/sec YDOT = -3745
869544 meter/sec
ZDOT = 14683
030307 ZDOT = 4450
899767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16132906
14 X = -4917309
79
Y = -9535115
96 feet Y = -2906303
35 meter
Z = -11709082
80 Z = -3568928
44
XDOT = 851
879996 XDOT = 259
653023
YDOT = -19356
694002 feet/sec YDOT = -5899
920332 meter/sec
ZDOT = 14584
360792 ZDOT = 4445
313169
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
50751927
00016717 00000-0 10270-3 0 9066
2 25544 51
6415 182
6815 0004515 216
9979 143
0872 15
72142360 18132
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
50751927 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 182
6815 deg
Eccentricity:
0004515
Arg of perigee: 216
9979 deg
Mean anomaly: 143
0872 deg
Mean motion: 15
72142360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 302
Coasting Arc #8 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2011/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5193126
30 A = 6732136
94 meter
Y = 2464407
27 meter E =
0003613
Z = -3503216
40 I = 51
66174
XDOT = -4881
005479 Wp = 144
38960
YDOT = 3871
283560 meter/sec RA = 176
57249 deg
ZDOT = -4517
421198 TA = 77
17673
MA = 77
13637
Ha = 192
480 n
mi
Hp = 187
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17037815
95 X = 5182200
56
Y = 8085325
68 feet Y = 2522418
86 meter
Z = -11493492
13 Z = -3478015
17
XDOT = -16013
797504 XDOT = -4901
987706
YDOT = 12701
061550 feet/sec YDOT = 3816
583905 meter/sec
ZDOT = -14820
935689 ZDOT = -4541
183656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2431086
33 X = 740995
11
Y = 18763630
11 feet Y = 5719154
46 meter
Z = -11391928
26 Z = -3472259
73
XDOT = -17920
287848 XDOT = -5462
103736
YDOT = -6724
097469 feet/sec YDOT = -2049
504909 meter/sec
ZDOT = -14916
757983 ZDOT = -4546
627833
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
52454499
00016717 00000-0 10270-3 0 9074
2 25544 51
6417 177
4733 0004394 222
2199 137
8625 15
72176856 18295
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
52454499 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 177
4733 deg
Eccentricity:
0004394
Arg of perigee: 222
2199 deg
Mean anomaly: 137
8625 deg
Mean motion: 15
72176856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 333
Coasting Arc #9 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2011/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3322177
29 A = 6729243
23 meter
Y = -3949470
90 meter E =
0005947
Z = 4313153
25 I = 51
68221
XDOT = 6635
364823 Wp = 90
40947
YDOT = 1777
522500 meter/sec RA = 171
40320 deg
ZDOT = -3479
131728 TA = 34
77137
MA = 34
73252
Ha = 192
285 n
mi
Hp = 187
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10899531
79 X = 3345141
89
Y = -12957581
69 feet Y = -3912191
98 meter
Z = 14150765
26 Z = 4329347
87
XDOT = 21769
569630 XDOT = 6631
895826
YDOT = 5831
766731 feet/sec YDOT = 1851
703819 meter/sec
ZDOT = -11414
474174 ZDOT = -3446
905987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16779096
59 X = 5114268
64
Y = 1818675
13 feet Y = 554332
18 meter
Z = 14216089
90 Z = 4333064
20
XDOT = 7384
389084 XDOT = 2250
761793
YDOT = 20184
018482 feet/sec YDOT = 6152
088833 meter/sec
ZDOT = -11284
577804 ZDOT = -3439
539315
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
54155457
00016717 00000-0 10270-3 0 9080
2 25544 51
6413 172
2645 0004439 225
1394 134
9408 15
72166556 18456
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
54155457 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 172
2645 deg
Eccentricity:
0004439
Arg of perigee: 225
1394 deg
Mean anomaly: 134
9408 deg
Mean motion: 15
72166556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 310
Coasting Arc #10 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2011/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6204443
08 A = 6734426
07 meter
Y = -560475
54 meter E =
0009993
Z = 2548773
12 I = 51
73132
XDOT = 2626
638522 Wp = 87
63966
YDOT = -4934
650489 meter/sec RA = 166
33246 deg
ZDOT = 5291
492659 TA = 301
19644
MA = 301
29435
Ha = 192
107 n
mi
Hp = 187
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20355784
39 X = -6210095
93
Y = -1838830
50 feet Y = -629889
07 meter
Z = 8362116
54 Z = 2518618
58
XDOT = 8617
580453 XDOT = 2655
918720
YDOT = -16189
798193 feet/sec YDOT = -4905
114313 meter/sec
ZDOT = 17360
540219 ZDOT = 5304
323639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10089395
33 X = -3075247
70
Y = -17831481
81 feet Y = -5435035
66 meter
Z = 8240546
53 Z = 2511718
58
XDOT = 16858
121578 XDOT = 5138
355457
YDOT = -1465
090576 feet/sec YDOT = -446
559608 meter/sec
ZDOT = 17412
323568 ZDOT = 5307
276224
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
55854365
00016717 00000-0 10270-3 0 9097
2 25544 51
6424 167
0560 0004495 229
7515 130
3255 15
72250641 18610
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
55854365 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 167
0560 deg
Eccentricity:
0004495
Arg of perigee: 229
7515 deg
Mean anomaly: 130
3255 deg
Mean motion: 15
72250641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 301
Coasting Arc #11 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2011/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1226734
78 A = 6726826
30 meter
Y = 4480249
74 meter E =
0010221
Z = -4874676
07 I = 51
73542
XDOT = -7306
534182 Wp = 126
77138
YDOT = 543
876486 meter/sec RA = 161
17815 deg
ZDOT = 2335
964184 TA = 166
00324
MA = 165
97489
Ha = 191
920 n
mi
Hp = 187
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4024720
41 X = -1253062
65
Y = 14698982
07 feet Y = 4466384
72 meter
Z = -15993031
73 Z = -4880699
16
XDOT = -23971
568838 XDOT = -7323
420402
YDOT = 1784
371674 feet/sec YDOT = 462
075862 meter/sec
ZDOT = 7663
924488 ZDOT = 2300
428560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14235120
28 X = -4338864
66
Y = 5370356
71 feet Y = 1636884
73 meter
Z = -16017369
68 Z = -4882094
28
XDOT = -15051
909172 XDOT = -4587
821916
YDOT = -17441
503697 feet/sec YDOT = -5316
170327 meter/sec
ZDOT = 7520
630506 ZDOT = 2292
288178
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
51195768
00016717 00000-0 10270-3 0 9101
2 25544 51
6425 162
1738 0004349 234
4926 125
5831 15
72253252 18764
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
51195768 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 162
1738 deg
Eccentricity:
0004349
Arg of perigee: 234
4926 deg
Mean anomaly: 125
5831 deg
Mean motion: 15
72253252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 309
Coasting Arc #12 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6378356
93 A = 6736104
18 meter
Y = -1513969
72 meter E =
0008953
Z = -1525153
41 I = 51
79536
XDOT = -179
465138 Wp = 171
50428
YDOT = 5067
001452 meter/sec RA = 156
09651 deg
ZDOT = -5793
356130 TA = 25
25575
MA = 25
21200
Ha = 191
806 n
mi
Hp = 187
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20926367
88 X = 6402221
16
Y = -4967092
26 feet Y = -1442509
55 meter
Z = -5003784
14 Z = -1494110
03
XDOT = -588
796385 XDOT = -207
969379
YDOT = 16624
020513 feet/sec YDOT = 5064
835599 meter/sec
ZDOT = -19007
073918 ZDOT = -5794
296834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16487465
90 X = 5025379
61
Y = 13855890
62 feet Y = 4223275
46 meter
Z = -4878575
31 Z = -1486989
75
XDOT = -12614
846644 XDOT = -3845
005257
YDOT = 8332
447455 feet/sec YDOT = 2539
729984 meter/sec
ZDOT = -19010
930270 ZDOT = -5794
531546
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
52891395
00016717 00000-0 10270-3 0 9113
2 25544 51
6425 156
9641 0004281 239
5278 120
5462 15
72283962 18923
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
52891395 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 156
9641 deg
Eccentricity:
0004281
Arg of perigee: 239
5278 deg
Mean anomaly: 120
5462 deg
Mean motion: 15
72283962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 320
Coasting Arc #13 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -888801
94 A = 6725329
70 meter
Y = -4181856
99 meter E =
0000714
Z = 5192149
25 I = 51
78784
XDOT = 7043
126053 Wp = 295
26529
YDOT = -2895
812199 meter/sec RA = 150
96196 deg
ZDOT = -1126
508654 TA = 165
46938
MA = 165
46733
Ha = 191
630 n
mi
Hp = 187
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2916016
85 X = -867195
54
Y = -13720003
25 feet Y = -4191675
70 meter
Z = 17034610
39 Z = 5187883
70
XDOT = 23107
368939 XDOT = 7080
456366
YDOT = -9500
696192 feet/sec YDOT = -2816
842902 meter/sec
ZDOT = -3695
894533 ZDOT = -1092
203439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9027096
19 X = 2751458
92
Y = -10762766
73 feet Y = -3280491
30 meter
Z = 17017461
07 Z = 5186922
13
XDOT = 20856
226816 XDOT = 6356
977934
YDOT = 11866
993008 feet/sec YDOT = 3617
059469 meter/sec
ZDOT = -3557
493435 ZDOT = -1084
323999
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 11029
54585288
00016717 00000-0 10270-3 0 9128
2 25544 51
6435 151
7555 0004190 244
9001 115
1727 15
72301220 19084
Satellite: ISS
Catalog Number: 25544
Epoch time: 11029
54585288 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 151
7555 deg
Eccentricity:
0004190
Arg of perigee: 244
9001 deg
Mean anomaly: 115
1727 deg
Mean motion: 15
72301220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 286
Coasting Arc #14 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2011/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5748376
13 A = 6736874
80 meter
Y = 3475121
43 meter E =
0009194
Z = 444564
78 I = 51
85374
XDOT = -2119
997363 Wp = 40
77911
YDOT = -4286
517582 meter/sec RA = 145
86575 deg
ZDOT = 6032
124847 TA = 324
03783
MA = 324
09966
Ha = 191
436 n
mi
Hp = 187
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18859501
73 X = -5788967
92
Y = 11401317
02 feet Y = 3410612
62 meter
Z = 1458545
85 Z = 416541
56
XDOT = -6955
371925 XDOT = -2101
209346
YDOT = -14063
377895 feet/sec YDOT = -4310
120056 meter/sec
ZDOT = 19790
435850 ZDOT = 6021
871500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20680733
69 X = -6303487
63
Y = -7635128
70 feet Y = -2327187
23 meter
Z = 1345457
20 Z = 410095
35
XDOT = 6022
258368 XDOT = 1835
584351
YDOT = -12792
473905 feet/sec YDOT = -3899
146046 meter/sec
ZDOT = 19749
133659 ZDOT = 6019
535939
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 11030
56277322
00016717 00000-0 10270-3 0 9130
2 25544 51
6442 146
5466 0004143 249
6336 110
4381 15
72325791 19247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11030
56277322 = yrday
fracday
Element set: 913
Inclination: 51
6442 deg
RA of node: 146
5466 deg
Eccentricity:
0004143
Arg of perigee: 249
6336 deg
Mean anomaly: 110
4381 deg
Mean motion: 15
72325791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 291
Coasting Arc #15 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2711589
91 A = 6724764
63 meter
Y = 3155448
25 meter E =
0011050
Z = -5292674
63 I = 51
83840
XDOT = -5908
521363 Wp = 94
73235
YDOT = 4921
776957 meter/sec RA = 140
75529 deg
ZDOT = -93
842681 TA = 174
38462
MA = 174
37222
Ha = 191
261 n
mi
Hp = 187
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8896292
37 X = 2701813
64
Y = 10352520
50 feet Y = 3185716
53 meter
Z = -17364418
08 Z = -5279525
69
XDOT = -19384
912608 XDOT = -5962
662611
YDOT = 16147
562195 feet/sec YDOT = 4855
401589 meter/sec
ZDOT = -307
882811 ZDOT = -122
676617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2244602
18 X = -684154
74
Y = 13532125
28 feet Y = 4124591
79 meter
Z = -17311414
16 Z = -5276519
04
XDOT = -23808
388287 XDOT = -7256
796750
YDOT = -4487
460979 feet/sec YDOT = -1367
778106 meter/sec
ZDOT = -424
277777 ZDOT = -129
319866
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 11031
51611951
00016717 00000-0 10270-3 0 9147
2 25544 51
6447 141
6641 0004167 254
6076 105
4626 15
72366586 19395
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
51611951 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 141
6641 deg
Eccentricity:
0004167
Arg of perigee: 254
6076 deg
Mean anomaly: 105
4626 deg
Mean motion: 15
72366586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 306
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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