Date:
April 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 1564)
---------------------------------------
Vector Time (GMT): 2010/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197423
35 A = 6722460
89 meter
Y = 1032680
68 meter E =
0004490
Z = -5152080
43 I = 51
90073
XDOT = -3367
873798 Wp = 100
19265
YDOT = 6780
868086 meter/sec RA = 124
66761 deg
ZDOT = -1386
461353 TA = 156
58548
MA = 156
56503
Ha = 190
232 n
mi
Hp = 187
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13771073
98 X = 4210592
16
Y = 3388059
97 feet Y = 1079692
48 meter
Z = -16903151
02 Z = -5131656
92
XDOT = -11049
454718 XDOT = -3436
713053
YDOT = 22246
942541 feet/sec YDOT = 6742
821639 meter/sec
ZDOT = -4548
757720 ZDOT = -1402
989932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13252053
63 X = 4039225
95
Y = -5314779
60 feet Y = -1619944
82 meter
Z = -16821835
09 Z = -5127295
34
XDOT = 3591
138703 XDOT = 1094
579077
YDOT = 23540
495446 feet/sec YDOT = 7175
143012 meter/sec
ZDOT = -4614
362074 ZDOT = -1406
457560
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
51826167
00016717 00000-0 10270-3 0 9004
2 25544 51
6424 125
4876 0009948 250
1908 109
8183 15
73399243 15655
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
51826167 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 125
4876 deg
Eccentricity:
0009948
Arg of perigee: 250
1908 deg
Mean anomaly: 109
8183 deg
Mean motion: 15
73399243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 323
Coasting Arc #2 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2010/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2256899
20 A = 6732904
17 meter
Y = -6183088
66 meter E =
0009874
Z = 1385044
12 I = 51
95196
XDOT = 4979
136126 Wp = 164
29454
YDOT = 506
003436 meter/sec RA = 119
53171 deg
ZDOT = -5854
150022 TA =
54740
MA =
54632
Ha = 189
788 n
mi
Hp = 187
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7404524
94 X = 2319143
44
Y = -20285723
94 feet Y = -6157502
70 meter
Z = 4544107
99 Z = 1396159
29
XDOT = 16335
748444 XDOT = 5001
546811
YDOT = 1660
116260 feet/sec YDOT = 561
808649 meter/sec
ZDOT = -19206
528943 ZDOT = -5829
906436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6158838
06 X = -1877213
84
Y = -20688248
87 feet Y = -6305778
26 meter
Z = 4588199
57 Z = 1398483
23
XDOT = 12691
447896 XDOT = 3868
353319
YDOT = -8016
647282 feet/sec YDOT = -2443
474092 meter/sec
ZDOT = -19110
015898 ZDOT = -5824
732846
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
53446743
00016717 00000-0 10270-3 0 9016
2 25544 51
6417 120
2732 0009837 254
7794 105
2282 15
73446342 15812
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
53446743 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 120
2732 deg
Eccentricity:
0009837
Arg of perigee: 254
7794 deg
Mean anomaly: 105
2282 deg
Mean motion: 15
73446342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 302
Coasting Arc #3 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2010/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424205
65 A = 6722714
69 meter
Y = 145012
90 meter E =
0007336
Z = 5065551
78 I = 51
93103
XDOT = 1787
373879 Wp = 226
91087
YDOT = -7273
249944 meter/sec RA = 114
44893 deg
ZDOT = 1765
986057 TA = 206
12223
MA = 206
15926
Ha = 189
507 n
mi
Hp = 188
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14515110
39 X = -4450106
34
Y = 475764
12 feet Y = 95393
66 meter
Z = 16619264
37 Z = 5043995
72
XDOT = 5864
087529 XDOT = 1859
992837
YDOT = -23862
368583 feet/sec YDOT = -7252
856544 meter/sec
ZDOT = 5793
917510 ZDOT = 1774
845199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11295166
56 X = -3442766
77
Y = 9283251
12 feet Y = 2829534
94 meter
Z = 16533456
70 Z = 5039397
60
XDOT = -9243
715804 XDOT = -2817
484577
YDOT = -21647
939677 feet/sec YDOT = -6598
292014 meter/sec
ZDOT = 5829
020676 ZDOT = 1776
685502
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
55065547
00016717 00000-0 10270-3 0 9020
2 25544 51
6413 115
0586 0009927 258
9708 101
0338 15
73450415 15977
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
55065547 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 115
0586 deg
Eccentricity:
0009927
Arg of perigee: 258
9708 deg
Mean anomaly: 101
0338 deg
Mean motion: 15
73450415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 301
Coasting Arc #4 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2010/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -859925
93 A = 6732331
14 meter
Y = 6454988
31 meter E =
0006913
Z = -1691858
19 I = 51
97569
XDOT = -5054
799849 Wp = 313
82745
YDOT = 835
520574 meter/sec RA = 109
31000 deg
ZDOT = 5747
213657 TA = 27
55739
MA = 27
52075
Ha = 188
973 n
mi
Hp = 187
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2821279
30 X = -923824
01
Y = 21177783
18 feet Y = 6445014
97 meter
Z = -5550715
86 Z = -1696190
48
XDOT = -16583
989005 XDOT = -5091
686387
YDOT = 2741
209231 feet/sec YDOT = 778
788103 meter/sec
ZDOT = 18855
687851 ZDOT = 5722
567586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11012265
07 X = 3356538
39
Y = 18302946
42 feet Y = 5578738
07 meter
Z = -5567830
28 Z = -1697074
67
XDOT = -10016
356321 XDOT = -3052
985407
YDOT = 11742
374281 feet/sec YDOT = 3579
075681 meter/sec
ZDOT = 18757
583716 ZDOT = 5717
311517
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
50331438
00016717 00000-0 10270-3 0 9032
2 25544 51
6415 110
1708 0009807 262
1973 97
8077 15
73505196 16126
Satellite: ISS
Catalog Number: 25544
Epoch time: 10121
50331438 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 110
1708 deg
Eccentricity:
0009807
Arg of perigee: 262
1973 deg
Mean anomaly: 97
8077 deg
Mean motion: 15
73505196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 292
Coasting Arc #5 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2010/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4341488
89 A = 6722954
62 meter
Y = -1299314
95 meter E =
0003734
Z = -4968981
75 I = 51
95301
XDOT = -185
562519 Wp = 40
35199
YDOT = 7404
189532 meter/sec RA = 104
23310 deg
ZDOT = -2096
304423 TA = 209
40550
MA = 209
42651
Ha = 188
492 n
mi
Hp = 187
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14243729
96 X = 4379834
01
Y = -4262844
31 feet Y = -1250551
03 meter
Z = -16302433
55 Z = -4947797
58
XDOT = -608
800916 XDOT = -258
160151
YDOT = 24291
960406 feet/sec YDOT = 7401
708719 meter/sec
ZDOT = -6877
639182 ZDOT = -2097
381626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8348461
77 X = 2544611
15
Y = -12413745
01 feet Y = -3783709
48 meter
Z = -16218111
65 Z = -4943280
43
XDOT = 14114
647549 XDOT = 4302
144573
YDOT = 18491
386933 feet/sec YDOT = 5636
174737 meter/sec
ZDOT = -6881
786483 ZDOT = -2097
568520
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 10122
51946690
00016717 00000-0 10270-3 0 9047
2 25544 51
6416 104
9558 0009891 266
8556 93
1475 15
73508332 16285
Satellite: ISS
Catalog Number: 25544
Epoch time: 10122
51946690 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 104
9558 deg
Eccentricity:
0009891
Arg of perigee: 266
8556 deg
Mean anomaly: 93
1475 deg
Mean motion: 15
73508332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 326
Coasting Arc #6 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2010/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -527683
53 A = 6731755
49 meter
Y = -6413385
16 meter E =
0005901
Z = 1963117
78 I = 51
98976
XDOT = 4799
316844 Wp = 148
79889
YDOT = -2120
463959 meter/sec RA = 99
09037 deg
ZDOT = -5634
816270 TA = 9
46459
MA = 9
45347
Ha = 188
123 n
mi
Hp = 187
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1731245
18 X = -465465
20
Y = -21041289
90 feet Y = -6418938
30 meter
Z = 6440675
12 Z = 1960704
92
XDOT = 15745
790170 XDOT = 4850
044607
YDOT = -6956
902754 feet/sec YDOT = -2066
511079 meter/sec
ZDOT = -18486
930021 ZDOT = -5611
378017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15012024
15 X = -4575664
96
Y = -14849153
75 feet Y = -4526022
06 meter
Z = 6430952
52 Z = 1960154
33
XDOT = 6452
799722 XDOT = 1966
813355
YDOT = -14493
234935 feet/sec YDOT = -4417
538008 meter/sec
ZDOT = -18393
638279 ZDOT = -5606
380947
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 10123
53560006
00016717 00000-0 10270-3 0 9054
2 25544 51
6419 99
7417 0010006 271
7006 88
3011 15
73561220 16443
Satellite: ISS
Catalog Number: 25544
Epoch time: 10123
53560006 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 99
7417 deg
Eccentricity:
0010006
Arg of perigee: 271
7006 deg
Mean anomaly: 88
3011 deg
Mean motion: 15
73561220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1644
Checksum: 271
Coasting Arc #7 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2010/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987371
20 A = 6723121
84 meter
Y = 2367347
38 meter E =
0005001
Z = 4872525
14 I = 51
96490
XDOT = -1360
762234 Wp = 237
38035
YDOT = -7191
365503 meter/sec RA = 94
01902 deg
ZDOT = 2379
530214 TA = 189
50150
MA = 189
51096
Ha = 188
610 n
mi
Hp = 187
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13081926
51 X = -4037216
86
Y = 7766887
74 feet Y = 2322479
22 meter
Z = 15985974
86 Z = 4853033
51
XDOT = -4464
443024 XDOT = -1291
805313
YDOT = -23593
718841 feet/sec YDOT = -7206
196947 meter/sec
ZDOT = 7806
857657 ZDOT = 2373
086657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4723424
74 X = -1439699
86
Y = 14547335
46 feet Y = 4434027
85 meter
Z = 15908394
89 Z = 4848878
76
XDOT = -17948
711517 XDOT = -5470
767270
YDOT = -14340
072730 feet/sec YDOT = -4370
854168 meter/sec
ZDOT = 7781
076691 ZDOT = 2371
672176
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 10124
55171475
00016717 00000-0 10270-3 0 9066
2 25544 51
6423 94
5275 0010108 275
1686 84
8323 15
73593066 16606
Satellite: ISS
Catalog Number: 25544
Epoch time: 10124
55171475 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 94
5275 deg
Eccentricity:
0010108
Arg of perigee: 275
1686 deg
Mean anomaly: 84
8323 deg
Mean motion: 15
73593066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1660
Checksum: 306
Coasting Arc #8 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1830981
93 A = 6731260
70 meter
Y = 6090390
54 meter E =
0008382
Z = -2189144
14 I = 51
99318
XDOT = -4254
660365 Wp = 317
47446
YDOT = 3267
453067 meter/sec RA = 88
87233 deg
ZDOT = 5525
611940 TA = 18
12718
MA = 18
09732
Ha = 189
060 n
mi
Hp = 187
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6007158
56 X = 1773376
49
Y = 19981596
25 feet Y = 6110543
68 meter
Z = -7182231
45 Z = -2180388
86
XDOT = -13958
859464 XDOT = -4317
723870
YDOT = 10719
990377 feet/sec YDOT = 3219
522057 meter/sec
ZDOT = 18128
648098 ZDOT = 5504
789732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17955128
01 X = 5472723
02
Y = 10651973
74 feet Y = 3246721
60 meter
Z = -7147266
93 Z = -2178486
96
XDOT = -2357
545018 XDOT = -718
579722
YDOT = 16095
918403 feet/sec YDOT = 4906
035929 meter/sec
ZDOT = 18045
777185 ZDOT = 5500
352886
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 10125
50430580
00016717 00000-0 10270-3 0 9078
2 25544 51
6422 89
6386 0009953 279
1698 80
8338 15
73596360 16754
Satellite: ISS
Catalog Number: 25544
Epoch time: 10125
50430580 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 89
6386 deg
Eccentricity:
0009953
Arg of perigee: 279
1698 deg
Mean anomaly: 80
8338 deg
Mean motion: 15
73596360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1675
Checksum: 336
Coasting Arc #9 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3400245
07 A = 6723386
45 meter
Y = -3295835
01 meter E =
0006022
Z = -4776199
66 I = 51
96600
XDOT = 2786
707583 Wp = 10
84938
YDOT = 6679
327454 meter/sec RA = 83
80320 deg
ZDOT = -2619
948931 TA = 233
51828
MA = 233
57378
Ha = 189
301 n
mi
Hp = 187
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11155659
69 X = 3460048
96
Y = -10813106
98 feet Y = -3257476
91 meter
Z = -15669946
38 Z = -4759536
06
XDOT = 9142
741415 XDOT = 2724
538302
YDOT = 21913
803983 feet/sec YDOT = 6710
142554 meter/sec
ZDOT = -8595
632977 ZDOT = -2606
561862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 725347
89 X = 221086
04
Y = -15585884
00 feet Y = -4750577
44 meter
Z = -15603632
13 Z = -4755987
07
XDOT = 20610
141236 XDOT = 6281
971049
YDOT = 9528
431462 feet/sec YDOT = 2904
265910 meter/sec
ZDOT = -8542
217411 ZDOT = -2603
667867
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 10126
52038387
00016717 00000-0 10270-3 0 9081
2 25544 51
6430 84
4237 0010038 283
1871 76
8172 15
73634718 16914
Satellite: ISS
Catalog Number: 25544
Epoch time: 10126
52038387 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 84
4237 deg
Eccentricity:
0010038
Arg of perigee: 283
1871 deg
Mean anomaly: 76
8172 deg
Mean motion: 15
73634718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 309
Coasting Arc #10 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3005940
59 A = 6730708
38 meter
Y = -5530528
70 meter E =
0003867
Z = 2378431
11 I = 51
98676
XDOT = 3473
423170 Wp = 104
52524
YDOT = -4221
172858 meter/sec RA = 78
65365 deg
ZDOT = -5419
262692 TA = 48
81904
MA = 48
78570
Ha = 189
576 n
mi
Hp = 187
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9862009
82 X = -2955427
87
Y = -18144779
20 feet Y = -5563860
54 meter
Z = 7803251
66 Z = 2363950
75
XDOT = 11395
745309 XDOT = 3546
692870
YDOT = -13848
992316 feet/sec YDOT = -4181
921185 meter/sec
ZDOT = -17779
733242 ZDOT = -5402
210828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19779080
61 X = -6028663
77
Y = -6014825
72 feet Y = -1833318
88 meter
Z = 7745503
76 Z = 2360829
54
XDOT = -1927
182371 XDOT = -587
405187
YDOT = -16497
862877 feet/sec YDOT = -5028
548605 meter/sec
ZDOT = -17711
881251 ZDOT = -5398
581405
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 10127
53644276
00016717 00000-0 10270-3 0 9094
2 25544 51
6433 79
2091 0010082 287
3421 72
6638 15
73664792 17077
Satellite: ISS
Catalog Number: 25544
Epoch time: 10127
53644276 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 79
2091 deg
Eccentricity:
0010082
Arg of perigee: 287
3421 deg
Mean anomaly: 72
6638 deg
Mean motion: 15
73664792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 315
Coasting Arc #11 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2642188
02 A = 6723441
37 meter
Y = 4027173
89 meter E =
0002526
Z = 4693199
87 I = 51
95646
XDOT = -4036
674944 Wp = 267
11219
YDOT = -5921
763898 meter/sec RA = 73
58620 deg
ZDOT = 2809
978129 TA = 155
28029
MA = 155
26818
Ha = 189
782 n
mi
Hp = 187
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8668595
86 X = -2709823
14
Y = 13212512
75 feet Y = 3997249
13 meter
Z = 15397637
37 Z = 4680199
78
XDOT = -13243
684201 XDOT = -3983
807184
YDOT = -19428
359247 feet/sec YDOT = -5966
608845 meter/sec
ZDOT = 9219
088349 ZDOT = 2790
496117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3266971
95 X = 995773
05
Y = 15512320
24 feet Y = 4728155
21 meter
Z = 15345914
73 Z = 4677434
81
XDOT = -22041
718924 XDOT = -6718
315928
YDOT = -4397
467185 feet/sec YDOT = -1340
347998 meter/sec
ZDOT = 9141
421697 ZDOT = 2786
305333
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 10128
55248063
00016717 00000-0 10270-3 0 9103
2 25544 51
6439 73
9943 0010192 290
3459 69
6609 15
73727620 17239
Satellite: ISS
Catalog Number: 25544
Epoch time: 10128
55248063 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 73
9943 deg
Eccentricity:
0010192
Arg of perigee: 290
3459 deg
Mean anomaly: 69
6609 deg
Mean motion: 15
73727620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 316
Coasting Arc #12 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4010713
17 A = 6730278
86 meter
Y = 4768350
47 meter E =
0009341
Z = -2527747
79 I = 51
96928
XDOT = -2526
496948 Wp = 325
73630
YDOT = 4952
401085 meter/sec RA = 68
43255 deg
ZDOT = 5331
576493 TA = 5
75714
MA = 5
74641
Ha = 190
117 n
mi
Hp = 186
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13158507
78 X = 3969374
03
Y = 15644194
44 feet Y = 4812969
55 meter
Z = -8293135
78 Z = -2508363
83
XDOT = -8289
031981 XDOT = -2607
587978
YDOT = 16248
035057 feet/sec YDOT = 4923
694805 meter/sec
ZDOT = 17492
048861 ZDOT = 5319
105718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20437255
78 X = 6229275
56
Y = 1217008
98 feet Y = 370944
34 meter
Z = -8215881
75 Z = -2504200
76
XDOT = 6074
224270 XDOT = 1851
423557
YDOT = 15790
137615 feet/sec YDOT = 4812
833945 meter/sec
ZDOT = 17442
439783 ZDOT = 5316
455646
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 10129
50500114
00016717 00000-0 10270-3 0 9118
2 25544 51
6436 69
1048 0010217 294
9533 65
0568 15
73707771 17385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10129
50500114 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 69
1048 deg
Eccentricity:
0010217
Arg of perigee: 294
9533 deg
Mean anomaly: 65
0568 deg
Mean motion: 15
73707771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 297
Coasting Arc #13 (Orbit 1753)
---------------------------------------
Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1756345
10 A = 6723615
59 meter
Y = -4564989
35 meter E =
0008559
Z = -4618297
64 I = 51
93633
XDOT = 5083
222439 Wp = 6
77171
YDOT = 4960
683850 meter/sec RA = 63
36482 deg
ZDOT = -2962
509381 TA = 233
91765
MA = 233
99695
Ha = 190
174 n
mi
Hp = 186
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5762287
07 X = 1829696
33
Y = -14976999
18 feet Y = -4544938
62 meter
Z = -15151895
15 Z = -4609587
10
XDOT = 16677
238973 XDOT = 5041
764957
YDOT = 16275
209480 feet/sec YDOT = 5017
295737 meter/sec
ZDOT = -9719
518968 ZDOT = -2937
915259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7065518
82 X = -2153570
14
Y = -14444430
44 feet Y = -4402662
40 meter
Z = -15117250
29 Z = -4607737
89
XDOT = 22253
502050 XDOT = 6782
867425
YDOT = -788
951544 feet/sec YDOT = -240
472431 meter/sec
ZDOT = -9621
521832 ZDOT = -2932
639854
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 10130
52100295
00016717 00000-0 10270-3 0 9129
2 25544 51
6447 63
8895 0010155 298
9934 61
0211 15
73767495 17546
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
52100295 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 63
8895 deg
Eccentricity:
0010155
Arg of perigee: 298
9934 deg
Mean anomaly: 61
0211 deg
Mean motion: 15
73767495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1754
Checksum: 309
Coasting Arc #14 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4830091
74 A = 6729825
19 meter
Y = -3873193
86 meter E =
0005390
Z = 2637580
40 I = 51
94323
XDOT = 1476
264654 Wp = 62
81722
YDOT = -5426
294533 meter/sec RA = 58
20842 deg
ZDOT = -5254
326963 TA = 87
33106
MA = 87
26936
Ha = 190
348 n
mi
Hp = 186
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15846757
69 X = -4799235
16
Y = -12707328
94 feet Y = -3927034
40 meter
Z = 8653478
99 Z = 2614190
14
XDOT = 4843
387973 XDOT = 1562
357825
YDOT = -17802
803585 feet/sec YDOT = -5409
304489 meter/sec
ZDOT = -17238
605521 ZDOT = -5246
946206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20057619
64 X = -6113562
47
Y = 3448459
54 feet Y = 1051090
47 meter
Z = 8560295
44 Z = 2609178
05
XDOT = -9776
369808 XDOT = -2979
837517
YDOT = -14056
775699 feet/sec YDOT = -4284
505233 meter/sec
ZDOT = -17209
255350 ZDOT = -5245
381031
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 10131
53698541
00016717 00000-0 10270-3 0 9138
2 25544 51
6452 58
6745 0010200 302
6569 57
3609 15
73786976 17708
Satellite: ISS
Catalog Number: 25544
Epoch time: 10131
53698541 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 58
6745 deg
Eccentricity:
0010200
Arg of perigee: 302
6569 deg
Mean anomaly: 57
3609 deg
Mean motion: 15
73786976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 320
Coasting Arc #15 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823246
45 A = 6723637
50 meter
Y = 4866965
44 meter E =
0002484
Z = 4564502
82 I = 51
90625
XDOT = -5907
399031 Wp = 349
18969
YDOT = -3872
322179 meter/sec RA = 53
13943 deg
ZDOT = 3066
123342 TA = 70
42905
MA = 70
40224
Ha = 190
519 n
mi
Hp = 186
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2700939
78 X = -899782
57
Y = 15967734
38 feet Y = 4857331
20 meter
Z = 14975402
95 Z = 4560317
78
XDOT = -19381
230417 XDOT = -5878
553978
YDOT = -12704
469090 feet/sec YDOT = -3938
221136 meter/sec
ZDOT = 10059
459782 ZDOT = 3037
494382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10303995
65 X = 3140657
87
Y = 12513565
35 feet Y = 3814134
72 meter
Z = 14958765
54 Z = 4559431
74
XDOT = -21387
213359 XDOT = -6518
822632
YDOT = 5732
414290 feet/sec YDOT = 1747
239876 meter/sec
ZDOT = 9945
421250 ZDOT = 3031
364397
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 10132
55294803
00016717 00000-0 10270-3 0 9145
2 25544 51
6455 53
4590 0010188 306
1756 53
8464 15
73822558 17868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
55294803 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 53
4590 deg
Eccentricity:
0010188
Arg of perigee: 306
1756 deg
Mean anomaly: 53
8464 deg
Mean motion: 15
73822558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 317
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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