Date:
May 29th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 269)
---------------------------------------
Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2749647
18 A = 6733337
74 meter
Y = -5882697
39 meter E =
0011573
Z = -1791928
04 I = 51
92199
XDOT = 5119
888226 Wp = 87
37188
YDOT = -666
281893 meter/sec RA = 52
46184 deg
ZDOT = -5699
901882 TA = 112
37907
MA = 112
25640
Ha = 194
624 n
mi
Hp = 182
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9021152
17 X = -2674956
63
Y = -19300188
29 feet Y = -5913027
61 meter
Z = -5879029
01 Z = -1805105
50
XDOT = 16797
533551 XDOT = 5154
647313
YDOT = -2185
964215 feet/sec YDOT = -608
832932 meter/sec
ZDOT = -18700
465492 ZDOT = -5674
945112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21288792
96 X = -6488824
09
Y = -230035
56 feet Y = -70114
84 meter
Z = -5930920
22 Z = -1807744
48
XDOT = 5312
744239 XDOT = 1619
324444
YDOT = -14639
498756 feet/sec YDOT = -4462
119221 meter/sec
ZDOT = -18602
728858 ZDOT = -5670
111756
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 09147
52829137
00010596 00000-0 82463-4 0 9008
2 25544 51
6427 52
9019 0009397 48
2766 311
9199 15
73090892 2700
Satellite: ISS
Catalog Number: 25544
Epoch time: 09147
52829137 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 52
9019 deg
Eccentricity:
0009397
Arg of perigee: 48
2766 deg
Mean anomaly: 311
9199 deg
Mean motion: 15
73090892 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 270
Checksum: 328
Coasting Arc #2 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4233013
49 A = 6723484
83 meter
Y = 1268244
01 meter E =
0014745
Z = 5059782
06 I = 51
86998
XDOT = -3999
247871 Wp = 51
99472
YDOT = -6353
003547 meter/sec RA = 47
32019 deg
ZDOT = -1741
066278 TA = 54
76576
MA = 54
62783
Ha = 194
669 n
mi
Hp = 182
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13887839
53 X = -4271460
05
Y = 4160905
55 feet Y = 1220692
21 meter
Z = 16600334
83 Z = 5039124
93
XDOT = -13120
891966 XDOT = -3919
452512
YDOT = -20843
187490 feet/sec YDOT = -6397
279034 meter/sec
ZDOT = -5712
159706 ZDOT = -1760
301778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2038197
67 X = -621242
65
Y = 14446777
42 feet Y = 4403377
76 meter
Z = 16519464
61 Z = 5035132
81
XDOT = -23346
189128 XDOT = -7115
918446
YDOT = 3370
846151 feet/sec YDOT = 1027
433907 meter/sec
ZDOT = -5787
806721 ZDOT = -1764
123489
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 09148
54469169
00010596 00000-0 82463-4 0 9017
2 25544 51
6423 47
6891 0009409 51
0088 309
1911 15
73172882 2866
Satellite: ISS
Catalog Number: 25544
Epoch time: 09148
54469169 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 47
6891 deg
Eccentricity:
0009409
Arg of perigee: 51
0088 deg
Mean anomaly: 309
1911 deg
Mean motion: 15
73172882 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 286
Checksum: 323
Coasting Arc #3 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183447
22 A = 6733922
50 meter
Y = 5113529
23 meter E =
0023398
Z = 1241684
58 I = 51
88427
XDOT = -4455
437008 Wp = 56
88348
YDOT = 2198
175665 meter/sec RA = 42
23387 deg
ZDOT = 5891
711364 TA = 316
69447
MA = 316
87813
Ha = 194
655 n
mi
Hp = 182
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13725220
54 X = 4119924
09
Y = 16776670
69 feet Y = 5159955
63 meter
Z = 4073768
30 Z = 1261854
10
XDOT = -14617
575487 XDOT = -4508
307027
YDOT = 7211
862417 feet/sec YDOT = 2148
055969 meter/sec
ZDOT = 19329
761692 ZDOT = 5869
938780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20860562
01 X = 6358299
30
Y = -5832951
68 feet Y = -1777883
67 meter
Z = 4153019
84 Z = 1265840
45
XDOT = 282
059126 XDOT = 85
971622
YDOT = 14863
896685 feet/sec YDOT = 4530
515710 meter/sec
ZDOT = 19244
560915 ZDOT = 5865
742167
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 09149
56107861
00010596 00000-0 82463-4 0 9029
2 25544 51
6427 42
4758 0009477 54
8824 305
3226 15
73145740 3028
Satellite: ISS
Catalog Number: 25544
Epoch time: 09149
56107861 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 42
4758 deg
Eccentricity:
0009477
Arg of perigee: 54
8824 deg
Mean anomaly: 305
3226 deg
Mean motion: 15
73145740 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 302
Checksum: 307
Coasting Arc #4 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2009/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3479900
76 A = 6722858
08 meter
Y = -2495280
63 meter E =
0022260
Z = -5201156
86 I = 51
82487
XDOT = 5475
688892 Wp = 82
70683
YDOT = 5267
824827 meter/sec RA = 37
09786 deg
ZDOT = 1143
235839 TA = 198
16323
MA = 198
24287
Ha = 194
582 n
mi
Hp = 182
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11416997
26 X = 3532811
03
Y = -8186616
25 feet Y = -2456069
93 meter
Z = -17064162
93 Z = -5184123
27
XDOT = 17964
858568 XDOT = 5410
822591
YDOT = 17282
889851 feet/sec YDOT = 5328
694364 meter/sec
ZDOT = 3750
773750 ZDOT = 1169
679738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3125392
79 X = -952619
72
Y = -13779320
52 feet Y = -4199936
89 meter
Z = -16997541
42 Z = -5180850
62
XDOT = 21851
634444 XDOT = 6660
378178
YDOT = -9683
092197 feet/sec YDOT = -2951
406502 meter/sec
ZDOT = 3854
613367 ZDOT = 1174
886154
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 09150
51392399
00010596 00000-0 82463-4 0 9039
2 25544 51
6430 37
5884 0009354 58
1839 302
0233 15
73194254 3176
Satellite: ISS
Catalog Number: 25544
Epoch time: 09150
51392399 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 37
5884 deg
Eccentricity:
0009354
Arg of perigee: 58
1839 deg
Mean anomaly: 302
0233 deg
Mean motion: 15
73194254 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 317
Checksum: 305
Coasting Arc #5 (Orbit 332)
---------------------------------------
Vector Time (GMT): 2009/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5324936
28 A = 6734244
59 meter
Y = -4046990
57 meter E =
0015213
Z = -776693
48 I = 51
83889
XDOT = 3440
228893 Wp = 104
05549
YDOT = -3397
124500 meter/sec RA = 31
99924 deg
ZDOT = -5986
015675 TA = 84
38066
MA = 84
20718
Ha = 194
587 n
mi
Hp = 181
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17470263
39 X = -5275513
34
Y = -13277528
12 feet Y = -4106260
71 meter
Z = -2548206
95 Z = -802442
44
XDOT = 11286
840199 XDOT = 3507
039486
YDOT = -11145
421587 feet/sec YDOT = -3358
279708 meter/sec
ZDOT = -19639
159038 ZDOT = -5969
141044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18779766
57 X = -5724072
85
Y = 11326869
54 feet Y = 3452429
84 meter
Z = -2649265
65 Z = -807496
17
XDOT = -5328
691573 XDOT = -1624
185191
YDOT = -13338
369650 feet/sec YDOT = -4065
535069 meter/sec
ZDOT = -19573
200639 ZDOT = -5965
911555
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 09151
53027853
00010596 00000-0 82463-4 0 9043
2 25544 51
6432 32
3751 0009207 62
6792 297
5307 15
73171715 3334
Satellite: ISS
Catalog Number: 25544
Epoch time: 09151
53027853 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 32
3751 deg
Eccentricity:
0009207
Arg of perigee: 62
6792 deg
Mean anomaly: 297
5307 deg
Mean motion: 15
73171715 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 333
Checksum: 297
Coasting Arc #6 (Orbit 348)
---------------------------------------
Vector Time (GMT): 2009/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2464817
81 A = 6722338
00 meter
Y = 3386198
33 meter E =
0012154
Z = 5249214
67 I = 51
77386
XDOT = -6629
288347 Wp = 64
47302
YDOT = -3887
442714 meter/sec RA = 26
86835 deg
ZDOT = -598
897600 TA = 31
23900
MA = 31
16683
Ha = 194
587 n
mi
Hp = 181
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8086672
61 X = -2527999
58
Y = 11109574
57 feet Y = 3358281
53 meter
Z = 17221832
89 Z = 5237087
35
XDOT = -21749
633683 XDOT = -6582
416242
YDOT = -12754
077145 feet/sec YDOT = -3961
313156 meter/sec
ZDOT = -1964
887140 ZDOT = -630
989439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7507151
55 X = 2288179
79
Y = 11579665
22 feet Y = 3529481
96 meter
Z = 17174471
70 Z = 5234778
97
XDOT = -18758
932684 XDOT = -5717
722682
YDOT = 15292
762677 feet/sec YDOT = 4661
234064 meter/sec
ZDOT = -2090
782424 ZDOT = -637
270483
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 09152
54661458
00010596 00000-0 82463-4 0 9051
2 25544 51
6434 27
1616 0009222 65
2502 294
9620 15
73257301 3495
Satellite: ISS
Catalog Number: 25544
Epoch time: 09152
54661458 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 27
1616 deg
Eccentricity:
0009222
Arg of perigee: 65
2502 deg
Mean anomaly: 294
9620 deg
Mean motion: 15
73257301 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 349
Checksum: 296
Coasting Arc #7 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2009/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6159511
54 A = 6734205
67 meter
Y = 2686961
01 meter E =
0021661
Z = 269862
90 I = 51
78664
XDOT = -2141
654421 Wp = 56
31885
YDOT = 4268
928235 meter/sec RA = 21
75648 deg
ZDOT = 6044
293917 TA = 306
60845
MA = 306
80751
Ha = 194
491 n
mi
Hp = 181
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20208371
18 X = 6127696
73
Y = 8815488
87 feet Y = 2755662
35 meter
Z = 885376
97 Z = 299709
16
XDOT = -7026
425265 XDOT = -2218
593548
YDOT = 14005
670061 feet/sec YDOT = 4244
548181 meter/sec
ZDOT = 19830
360619 ZDOT = 6033
703199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15102502
36 X = 4603242
72
Y = -16055671
48 feet Y = -4893768
67 meter
Z = 1002416
22 Z = 305536
47
XDOT = 9613
353117 XDOT = 2930
150030
YDOT = 10338
464811 feet/sec YDOT = 3151
164074 meter/sec
ZDOT = 19789
055030 ZDOT = 6031
703973
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 09153
56293618
00010596 00000-0 82463-4 0 9064
2 25544 51
6431 21
9481 0009177 68
7918 291
4225 15
73275271 3659
Satellite: ISS
Catalog Number: 25544
Epoch time: 09153
56293618 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 21
9481 deg
Eccentricity:
0009177
Arg of perigee: 68
7918 deg
Mean anomaly: 291
4225 deg
Mean motion: 15
73275271 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 365
Checksum: 323
Coasting Arc #8 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2009/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1268644
69 A = 6722123
59 meter
Y = -3977518
43 meter E =
0023863
Z = -5288756
21 I = 51
71724
XDOT = 7344
365122 Wp = 83
26629
YDOT = 2252
137798 meter/sec RA = 16
63023 deg
ZDOT = 70
980119 TA = 187
39051
MA = 187
42574
Ha = 194
450 n
mi
Hp = 181
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4162220
12 X = 1338719
88
Y = -13049601
14 feet Y = -3962939
24 meter
Z = -17351562
37 Z = -5282423
32
XDOT = 24095
686097 XDOT = 7318
290670
YDOT = 7388
903538 feet/sec YDOT = 2334
120980 meter/sec
ZDOT = 232
874407 ZDOT = 106
596507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10995972
18 X = -3351572
32
Y = -8219447
23 feet Y = -2505287
52 meter
Z = -17326920
27 Z = -5281245
30
XDOT = 14120
094410 XDOT = 4303
804776
YDOT = -19654
230666 feet/sec YDOT = -5990
609507 meter/sec
ZDOT = 372
494112 ZDOT = 113
536205
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 09154
51572373
00010596 00000-0 82463-4 0 9079
2 25544 51
6423 17
0599 0009137 71
8262 288
3895 15
73295042 3802
Satellite: ISS
Catalog Number: 25544
Epoch time: 09154
51572373 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 17
0599 deg
Eccentricity:
0009137
Arg of perigee: 71
8262 deg
Mean anomaly: 288
3895 deg
Mean motion: 15
73295042 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 380
Checksum: 321
Coasting Arc #9 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2009/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6613309
23 A = 6734227
44 meter
Y = -1238771
38 meter E =
0018946
Z = 133503
43 I = 51
72915
XDOT = 746
881259 Wp = 109
45875
YDOT = -4712
426728 meter/sec RA = 11
50635 deg
ZDOT = -6042
012653 TA = 69
09332
MA = 68
89062
Ha = 194
476 n
mi
Hp = 181
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21697208
75 X = -6599614
10
Y = -4064210
56 feet Y = -1312648
71 meter
Z = 438003
38 Z = 101408
55
XDOT = 2450
397833 XDOT = 828
872363
YDOT = -15460
717613 feet/sec YDOT = -4703
615358 meter/sec
ZDOT = -19822
876158 ZDOT = -6038
185767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10470020
35 X = -3191262
20
Y = 19436041
57 feet Y = 5924105
47 meter
Z = 312224
02 Z = 95165
88
XDOT = -12531
576217 XDOT = -3819
624431
YDOT = -6381
699111 feet/sec YDOT = -1945
141889 meter/sec
ZDOT = -19808
076173 ZDOT = -6037
501618
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 09155
53201566
00010596 00000-0 82463-4 0 9086
2 25544 51
6424 11
8469 0009094 76
3297 283
8878 15
73277845 3960
Satellite: ISS
Catalog Number: 25544
Epoch time: 09155
53201566 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 11
8469 deg
Eccentricity:
0009094
Arg of perigee: 76
3297 deg
Mean anomaly: 283
8878 deg
Mean motion: 15
73277845 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 396
Checksum: 346
Coasting Arc #10 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2009/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -8819
08 A = 6722087
67 meter
Y = 4180589
84 meter E =
0011407
Z = 5254146
14 I = 51
65856
XDOT = -7679
873190 Wp = 84
82005
YDOT = -532
250551 meter/sec RA = 6
38381 deg
ZDOT = 410
859270 TA = 1
28522
MA = 1
28230
Ha = 194
451 n
mi
Hp = 181
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -28934
00 X = -81090
56
Y = 13715845
92 feet Y = 4180086
25 meter
Z = 17238012
29 Z = 5253928
44
XDOT = -25196
434349 XDOT = -7675
346594
YDOT = -1746
228843 feet/sec YDOT = -618
106136 meter/sec
ZDOT = 1347
963485 ZDOT = 373
560788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13099372
20 X = 3992688
65
Y = 4068835
76 feet Y = 1240181
14 meter
Z = 17237324
55 Z = 5253936
52
XDOT = -8625
442928 XDOT = -2629
035004
YDOT = 22681
138932 feet/sec YDOT = 6913
211147 meter/sec
ZDOT = 1201
827871 ZDOT = 366
317135
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 09156
54829043
00010596 00000-0 82463-4 0 9095
2 25544 51
6417 6
6325 0009069 79
4497 280
7687 15
73312701 4127
Satellite: ISS
Catalog Number: 25544
Epoch time: 09156
54829043 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 6
6325 deg
Eccentricity:
0009069
Arg of perigee: 79
4497 deg
Mean anomaly: 280
7687 deg
Mean motion: 15
73312701 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 412
Checksum: 322
Coasting Arc #11 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2009/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6696804
39 A = 6733927
51 meter
Y = -309685
51 meter E =
0018742
Z = -575681
39 I = 51
66777
XDOT = 723
388267 Wp = 59
03243
YDOT = 4764
775286 meter/sec RA = 1
24546 deg
ZDOT = 6004
970366 TA = 294
70590
MA = 294
90089
Ha = 194
388 n
mi
Hp = 181
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21971143
01 X = 6702566
21
Y = -1016028
57 feet Y = -234765
61 meter
Z = -1888718
48 Z = -543133
96
XDOT = 2373
321087 XDOT = 640
882555
YDOT = 15632
464848 feet/sec YDOT = 4772
402220 meter/sec
ZDOT = 19701
346345 ZDOT = 6008
285097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4981848
35 X = 1518467
38
Y = -21433851
02 feet Y = -6533037
79 meter
Z = -1761225
28 Z = -536821
46
XDOT = 14096
746409 XDOT = 4296
688305
YDOT = 1700
809651 feet/sec YDOT = 518
406782 meter/sec
ZDOT = 19714
515405 ZDOT = 6008
984295
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 09157
50103331
00010596 00000-0 82463-4 0 9109
2 25544 51
6405 1
7437 0008957 82
5174 277
7006 15
73339588 4275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09157
50103331 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 1
7437 deg
Eccentricity:
0008957
Arg of perigee: 82
5174 deg
Mean anomaly: 277
7006 deg
Mean motion: 15
73339588 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 427
Checksum: 304
Coasting Arc #12 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2009/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1229012
04 A = 6722111
21 meter
Y = -4069877
23 meter E =
0023673
Z = -5227465
15 I = 51
59746
XDOT = 7542
277929 Wp = 84
43744
YDOT = -1186
493652 meter/sec RA = 356
12585 deg
ZDOT = -850
534325 TA = 177
44686
MA = 177
43476
Ha = 194
322 n
mi
Hp = 181
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4032191
74 X = -1158016
33
Y = -13352615
58 feet Y = -4083222
78 meter
Z = -17150476
22 Z = -5233264
09
XDOT = 24745
006329 XDOT = 7559
116719
YDOT = -3892
695710 feet/sec YDOT = -1102
057181 meter/sec
ZDOT = -2790
466947 ZDOT = -813
852923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13914104
80 X = -4241019
14
Y = 404392
39 feet Y = 123258
80 meter
Z = -17173348
60 Z = -5234436
65
XDOT = 2567
322527 XDOT = 782
519906
YDOT = -23921
464451 feet/sec YDOT = -7291
262365 meter/sec
ZDOT = -2646
807572 ZDOT = -806
746948
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 09158
51727777
00010596 00000-0 82463-4 0 9118
2 25544 51
6394 356
5286 0008976 86
7408 273
4782 15
73373814 4434
Satellite: ISS
Catalog Number: 25544
Epoch time: 09158
51727777 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 356
5286 deg
Eccentricity:
0008976
Arg of perigee: 86
7408 deg
Mean anomaly: 273
4782 deg
Mean motion: 15
73373814 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 443
Checksum: 352
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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