Date:
January 21st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9902 8 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 2256)
---------------------------------------
Vector Time (GMT): 2009/019/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -859769
88 A = 6730277
74 meter
Y = -4099237
52 meter E =
0007386
Z = -5274263
00 I = 51
54805
XDOT = 7514
656335 Wp = 73
91166
YDOT = -1633
687561 meter/sec RA = 347
45781 deg
ZDOT = 46
809239 TA = 196
52163
MA = 196
54571
Ha = 194
186 n
mi
Hp = 192
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2820767
31 X = -788246
44
Y = -13448942
00 feet Y = -4108451
62 meter
Z = -17304012
48 Z = -5278266
34
XDOT = 24654
384302 XDOT = 7532
138605
YDOT = -5359
867325 feet/sec YDOT = -1549
556570 meter/sec
ZDOT = 153
573620 ZDOT = 83
357444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9320903
81 X = 2841011
48
Y = -10069934
11 feet Y = -3069315
92 meter
Z = -17319838
23 Z = -5279086
69
XDOT = 18026
440118 XDOT = 5494
458948
YDOT = 16188
538540 feet/sec YDOT = 4934
266547 meter/sec
ZDOT = 295
751854 ZDOT = 90
145165
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 09019
53659256
00010596 00000-0 82463-4 0 9000
2 25544 51
6402 347
8788 0008205 285
4453 74
5802 15
70436401 22574
Satellite: ISS
Catalog Number: 25544
Epoch time: 09019
53659256 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 347
8788 deg
Eccentricity:
0008205
Arg of perigee: 285
4453 deg
Mean anomaly: 74
5802 deg
Mean motion: 15
70436401 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2257
Checksum: 314
Coasting Arc #2 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2009/020/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6012909
38 A = 6741765
21 meter
Y = 2833750
32 meter E =
0006114
Z = 1102802
67 I = 51
55894
XDOT = -2953
133016 Wp = 142
07414
YDOT = -3968
175123 meter/sec RA = 342
33371 deg
ZDOT = -5892
517982 TA = 25
86443
MA = 25
83388
Ha = 194
413 n
mi
Hp = 192
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19727392
98 X = -6049507
11
Y = 9297081
10 feet Y = 2766305
74 meter
Z = 3618119
01 Z = 1073503
65
XDOT = -9688
756614 XDOT = -2879
916266
YDOT = -13018
947254 feet/sec YDOT = -4000
788818 meter/sec
ZDOT = -19332
408077 ZDOT = -5906
686696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19266862
87 X = -5872539
80
Y = -10256944
62 feet Y = -3126316
72 meter
Z = 3504228
57 Z = 1068088
87
XDOT = 3950
687251 XDOT = 1204
169474
YDOT = -14059
291224 feet/sec YDOT = -4285
271965 meter/sec
ZDOT = -19387
797626 ZDOT = -5909
400716
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 09020
55471930
00010596 00000-0 82463-4 0 9016
2 25544 51
6407 342
6779 0008220 289
5526 70
4748 15
70463187 22738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09020
55471930 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 342
6779 deg
Eccentricity:
0008220
Arg of perigee: 289
5526 deg
Mean anomaly: 70
4748 deg
Mean motion: 15
70463187 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2273
Checksum: 314
Coasting Arc #3 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2009/021/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051655
34 A = 6732032
98 meter
Y = 2436098
65 meter E =
0001646
Z = 4794217
33 I = 51
49983
XDOT = -5686
253868 Wp = 254
37347
YDOT = 4540
124786 meter/sec RA = 337
24746 deg
ZDOT = 2498
816024 TA = 171
10761
MA = 171
10469
Ha = 194
422 n
mi
Hp = 192
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13292832
49 X = 4000824
24
Y = 7992449
63 feet Y = 2481121
88 meter
Z = 15729059
47 Z = 4813776
80
XDOT = -18655
688542 XDOT = -5748
738307
YDOT = 14895
422525 feet/sec YDOT = 4476
188161 meter/sec
ZDOT = 8198
215302 ZDOT = 2471
041292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1761664
60 X = 536955
37
Y = 15331976
72 feet Y = 4673186
51 meter
Z = 15805346
76 Z = 4817469
69
XDOT = -22109
377416 XDOT = -6738
938236
YDOT = -5798
820768 feet/sec YDOT = -1767
480570 meter/sec
ZDOT = 8090
355880 ZDOT = 2465
940472
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 09021
57282938
00010596 00000-0 82463-4 0 9028
2 25544 51
6412 337
4771 0008330 292
5420 67
4859 15
70524866 22895
Satellite: ISS
Catalog Number: 25544
Epoch time: 09021
57282938 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 337
4771 deg
Eccentricity:
0008330
Arg of perigee: 292
5420 deg
Mean anomaly: 67
4859 deg
Mean motion: 15
70524866 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2289
Checksum: 323
Coasting Arc #4 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2009/022/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3576721
38 A = 6737871
97 meter
Y = -4746371
57 meter E =
0005610
Z = -3166573
13 I = 51
49207
XDOT = 5879
262377 Wp = 327
71233
YDOT = 1219
440359 meter/sec RA = 332
08399 deg
ZDOT = 4813
696132 TA = 355
35220
MA = 355
35741
Ha = 194
810 n
mi
Hp = 191
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11734650
20 X = 3644912
63
Y = -15572085
20 feet Y = -4705992
97 meter
Z = -10389019
45 Z = -3149032
60
XDOT = 19288
918560 XDOT = 5841
805778
YDOT = 4000
788578 feet/sec YDOT = 1284
975720 meter/sec
ZDOT = 15792
966311 ZDOT = 4842
166249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19527058
20 X = 5951847
34
Y = -542469
06 feet Y = -165344
57 meter
Z = -10321012
71 Z = -3145844
67
XDOT = 8850
700816 XDOT = 2697
693609
YDOT = 16055
095526 feet/sec YDOT = 4893
593116 meter/sec
ZDOT = 15903
875408 ZDOT = 4847
501224
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 09022
52729673
00010596 00000-0 82463-4 0 9037
2 25544 51
6409 332
6006 0008337 297
2478 62
7834 15
70497843 23044
Satellite: ISS
Catalog Number: 25544
Epoch time: 09022
52729673 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 332
6006 deg
Eccentricity:
0008337
Arg of perigee: 297
2478 deg
Mean anomaly: 62
7834 deg
Mean motion: 15
70497843 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2304
Checksum: 321
Coasting Arc #5 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2009/023/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5772829
82 A = 6736793
27 meter
Y = 478442
15 meter E =
0005057
Z = -3442336
25 I = 51
46470
XDOT = 2240
591448 Wp = 336
30648
YDOT = -5778
023329 meter/sec RA = 327
01382 deg
ZDOT = -4553
695958 TA = 244
46862
MA = 244
52092
Ha = 194
870 n
mi
Hp = 191
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18939730
37 X = -5761028
90
Y = 1569692
10 feet Y = 413953
37 meter
Z = -11293754
08 Z = -3470351
34
XDOT = 7351
021811 XDOT = 2327
156292
YDOT = -18956
769452 feet/sec YDOT = -5752
483244 meter/sec
ZDOT = -14939
947370 ZDOT = -4542
601747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13267953
10 X = -4044072
10
Y = -13515319
94 feet Y = -4119469
52 meter
Z = -11402795
65 Z = -3475572
11
XDOT = 18348
541811 XDOT = 5592
635544
YDOT = -5425
282890 feet/sec YDOT = -1653
626225 meter/sec
ZDOT = -14897
100035 ZDOT = -4540
636091
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 09023
54537940
00010596 00000-0 82463-4 0 9045
2 25544 51
6419 327
3992 0008281 301
4272 58
6079 15
70547465 23207
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023
54537940 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 327
3992 deg
Eccentricity:
0008281
Arg of perigee: 301
4272 deg
Mean anomaly: 58
6079 deg
Mean motion: 15
70547465 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2320
Checksum: 312
Coasting Arc #6 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2009/024/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -264783
95 A = 6732773
61 meter
Y = 4893635
60 meter E =
0008326
Z = 4619902
39 I = 51
42709
XDOT = -6728
427995 Wp = 4
35543
YDOT = 2364
095021 meter/sec RA = 321
84416 deg
ZDOT = -2881
290041 TA = 114
31709
MA = 114
23012
Ha = 195
044 n
mi
Hp = 191
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -868713
76 X = -341927
81
Y = 16055234
91 feet Y = 4890242
86 meter
Z = 15157160
06 Z = 4618429
19
XDOT = -22074
894997 XDOT = -6740
367190
YDOT = 7756
217260 feet/sec YDOT = 2288
787357 meter/sec
ZDOT = -9453
051315 ZDOT = -2914
004707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12795161
42 X = -3899965
20
Y = 9745455
12 feet Y = 2970414
72 meter
Z = 15151722
06 Z = 4618244
88
XDOT = -19529
296960 XDOT = -5952
529714
YDOT = -10702
376836 feet/sec YDOT = -3262
084460 meter/sec
ZDOT = -9580
279385 ZDOT = -2920
069157
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 09024
56344749
00010596 00000-0 82463-4 0 9052
2 25544 51
6420 322
1984 0008266 304
9897 55
0488 15
70553297 23369
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024
56344749 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 322
1984 deg
Eccentricity:
0008266
Arg of perigee: 304
9897 deg
Mean anomaly: 55
0488 deg
Mean motion: 15
70553297 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2336
Checksum: 331
Coasting Arc #7 (Orbit 2351)
---------------------------------------
Vector Time (GMT): 2009/025/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5518110
57 A = 6740944
95 meter
Y = -3555883
01 meter E =
0013192
Z = 1492802
29 I = 51
43263
XDOT = 1561
614425 Wp = 26
36677
YDOT = 4850
073646 meter/sec RA = 316
75547 deg
ZDOT = 5772
634646 TA = 350
10851
MA = 350
13445
Ha = 195
128 n
mi
Hp = 191
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18104037
31 X = 5550211
36
Y = -11666282
84 feet Y = -3493996
93 meter
Z = 4897645
31 Z = 1519686
22
XDOT = 5123
406906 XDOT = 1479
222399
YDOT = 15912
315111 feet/sec YDOT = 4867
075384 meter/sec
ZDOT = 18939
090045 ZDOT = 5780
021024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20733650
32 X = 6319616
62
Y = 5739338
80 feet Y = 1749350
47 meter
Z = 5002098
18 Z = 1524639
52
XDOT = -8129
759793 XDOT = -2477
950785
YDOT = 12815
547567 feet/sec YDOT = 3906
178898 meter/sec
ZDOT = 18968
151051 ZDOT = 5781
492440
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 09025
58150037
00010596 00000-0 82463-4 0 9061
2 25544 51
6421 316
9964 0008330 309
0769 50
9651 15
70572843 23527
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025
58150037 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 316
9964 deg
Eccentricity:
0008330
Arg of perigee: 309
0769 deg
Mean anomaly: 50
9651 deg
Mean motion: 15
70572843 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2352
Checksum: 308
Coasting Arc #8 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2791686
15 A = 6729858
29 meter
Y = -3169469
71 meter E =
0009902
Z = -5246667
46 I = 51
37565
XDOT = 5367
995032 Wp = 61
80246
YDOT = -5486
343980 meter/sec RA = 311
61116 deg
ZDOT = 463
282629 TA = 212
58982
MA = 212
65097
Ha = 195
243 n
mi
Hp = 190
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9159075
29 X = -2730550
51
Y = -10398522
66 feet Y = -3200345
82 meter
Z = -17213475
92 Z = -5260080
78
XDOT = 17611
532257 XDOT = 5426
694799
YDOT = -17999
816208 feet/sec YDOT = -5425
987765 meter/sec
ZDOT = 1519
956132 ZDOT = 489
501848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1504505
12 X = 458573
16
Y = -13709364
46 feet Y = -4178614
29 meter
Z = -17265905
06 Z = -5262647
86
XDOT = 24165
565552 XDOT = 7365
664380
YDOT = 631
303620 feet/sec YDOT = 192
421343 meter/sec
ZDOT = 1621
694726 ZDOT = 494
292553
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 09026
53591083
00010596 00000-0 82463-4 0 9078
2 25544 51
6426 312
1202 0008315 312
6517 47
3943 15
70609936 23673
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026
53591083 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 312
1202 deg
Eccentricity:
0008315
Arg of perigee: 312
6517 deg
Mean anomaly: 47
3943 deg
Mean motion: 15
70609936 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 301
Coasting Arc #9 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3535247
45 A = 6741643
39 meter
Y = 5697389
74 meter E =
0005246
Z = 682513
91 I = 51
39670
XDOT = -4420
396135 Wp = 115
15337
YDOT = -2024
907483 meter/sec RA = 306
48117 deg
ZDOT = -5959
735488 TA = 57
40114
MA = 57
35050
Ha = 195
450 n
mi
Hp = 190
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11598580
87 X = -3602009
29
Y = 18692223
57 feet Y = 5657483
24 meter
Z = 2239218
88 Z = 665178
22
XDOT = -14502
611992 XDOT = -4368
474261
YDOT = -6643
397255 feet/sec YDOT = -2074
048390 meter/sec
ZDOT = -19552
937952 ZDOT = -5981
083121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21539108
46 X = -6565120
26
Y = 4504356
24 feet Y = 1372927
78 meter
Z = 2172091
77 Z = 662053
57
XDOT = -4799
370342 XDOT = -1462
848080
YDOT = -13426
114642 feet/sec YDOT = -4092
279743 meter/sec
ZDOT = -19636
192188 ZDOT = -5985
111379
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 09027
55393509
00010596 00000-0 82463-4 0 9085
2 25544 51
6426 306
9187 0008277 316
1125 43
9379 15
70611498 23836
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027
55393509 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 306
9187 deg
Eccentricity:
0008277
Arg of perigee: 316
1125 deg
Mean anomaly: 43
9379 deg
Mean motion: 15
70611498 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 331
Coasting Arc #10 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4546090
58 A = 6730919
18 meter
Y = 165972
88 meter E =
0003126
Z = 4960478
51 I = 51
34445
XDOT = -2422
927796 Wp = 349
69399
YDOT = 7028
522561 meter/sec RA = 301
37463 deg
ZDOT = 1988
577895 TA = 81
00081
MA = 80
96542
Ha = 195
443 n
mi
Hp = 190
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14914995
33 X = 4519800
29
Y = 544530
44 feet Y = 216662
83 meter
Z = 16274535
78 Z = 4982498
98
XDOT = -7949
238177 XDOT = -2511
001718
YDOT = 23059
457220 feet/sec YDOT = 7000
935499 meter/sec
ZDOT = 6524
205691 ZDOT = 1976
593800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10027307
37 X = 3056323
29
Y = 10927404
59 feet Y = 3330672
92 meter
Z = 16360288
80 Z = 4986616
03
XDOT = -21221
762626 XDOT = -6468
393248
YDOT = 9790
713594 feet/sec YDOT = 2984
209503 meter/sec
ZDOT = 6478
014814 ZDOT = 1974
498915
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 09028
57194326
00010596 00000-0 82463-4 0 9095
2 25544 51
6424 301
7168 0008339 319
9937 40
0610 15
70659740 23992
Satellite: ISS
Catalog Number: 25544
Epoch time: 09028
57194326 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 301
7168 deg
Eccentricity:
0008339
Arg of perigee: 319
9937 deg
Mean anomaly: 40
0610 deg
Mean motion: 15
70659740 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2399
Checksum: 327
Coasting Arc #11 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 588726
96 A = 6738421
38 meter
Y = -6128722
06 meter E =
0009434
Z = -2724177
24 I = 51
35584
XDOT = 5449
788351 Wp = 354
23955
YDOT = -1759
444280 meter/sec RA = 296
20493 deg
ZDOT = 5143
779960 TA = 334
55869
MA = 334
60510
Ha = 195
666 n
mi
Hp = 190
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1931518
90 X = 670448
85
Y = -20107355
83 feet Y = -6121681
65 meter
Z = -8937589
37 Z = -2721118
76
XDOT = 17879
883040 XDOT = 5444
070726
YDOT = -5772
454987 feet/sec YDOT = -1698
533542 meter/sec
ZDOT = 16875
918504 ZDOT = 5170
240541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15478290
70 X = 4717783
00
Y = -12987080
56 feet Y = -3958462
16 meter
Z = -8926101
23 Z = -2720675
65
XDOT = 15801
020515 XDOT = 4816
151053
YDOT = 7179
746396 feet/sec YDOT = 2188
386701 meter/sec
ZDOT = 16978
827773 ZDOT = 5175
146705
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 09029
52631344
00010596 00000-0 82463-4 0 9109
2 25544 51
6427 296
8401 0008409 323
7233 36
3357 15
70683041 24144
Satellite: ISS
Catalog Number: 25544
Epoch time: 09029
52631344 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 296
8401 deg
Eccentricity:
0008409
Arg of perigee: 323
7233 deg
Mean anomaly: 36
3357 deg
Mean motion: 15
70683041 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2414
Checksum: 293
Coasting Arc #12 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531296
50 A = 6735077
53 meter
Y = 3165702
96 meter E =
0009115
Z = -3856559
00 I = 51
33287
XDOT = -1015
482113 Wp = 10
19730
YDOT = -6434
777430 meter/sec RA = 291
12237 deg
ZDOT = -4081
552610 TA = 216
92748
MA = 216
99027
Ha = 195
829 n
mi
Hp = 189
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14866458
34 X = -4547625
02
Y = 10386164
58 feet Y = 3114940
04 meter
Z = -12652752
62 Z = -3878611
32
XDOT = -3331
634230 XDOT = -923
624816
YDOT = -21111
474507 feet/sec YDOT = -6445
619579 meter/sec
ZDOT = -13390
920638 ZDOT = -4086
262552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17885251
71 X = -5451424
72
Y = -2612885
94 feet Y = -796407
64 meter
Z = -12738396
49 Z = -3882663
25
XDOT = 11945
433068 XDOT = 3640
967999
YDOT = -16274
435400 feet/sec YDOT = -4960
447910 meter/sec
ZDOT = -13409
709196 ZDOT = -4087
279363
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 09030
54429355
00010596 00000-0 82463-4 0 9111
2 25544 51
6426 291
6382 0008526 327
0308 33
0321 15
70696248 24300
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54429355 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 291
6382 deg
Eccentricity:
0008526
Arg of perigee: 327
0308 deg
Mean anomaly: 33
0321 deg
Mean motion: 15
70696248 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 291
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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