Date:
November 11th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7265 64 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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 1155)
---------------------------------------
Vector Time (GMT): 2008/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4459884
67 A = 6731733
28 meter
Y = 3817460
46 meter E =
0011137
Z = 3288394
73 I = 51
56621
XDOT = -5577
421456 Wp = 74
14742
YDOT = -2445
800187 meter/sec RA = 345
82977 deg
ZDOT = -4708
902472 TA = 67
25251
MA = 67
13485
Ha = 192
186 n
mi
Hp = 186
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14632167
55 X = -4518215
60
Y = 12524476
58 feet Y = 3767261
32 meter
Z = 10788696
64 Z = 3266586
22
XDOT = -18298
626823 XDOT = -5526
781863
YDOT = -8024
278830 feet/sec YDOT = -2507
887019 meter/sec
ZDOT = -15449
155092 ZDOT = -4735
875429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 99591
73 X = 30355
56
Y = -19307088
06 feet Y = -5884800
44 meter
Z = 10704449
93 Z = 3262716
34
XDOT = 16555
942494 XDOT = 5046
251272
YDOT = -8567
798793 feet/sec YDOT = -2611
465072 meter/sec
ZDOT = -15553
872260 ZDOT = -4740
820265
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 08315
53854975
00020000 00000-0 20000-3 0 9002
2 25544 51
6422 346
1587 0004008 329
4103 30
6825 15
72534995 11567
Satellite: ISS
Catalog Number: 25544
Epoch time: 08315
53854975 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 346
1587 deg
Eccentricity:
0004008
Arg of perigee: 329
4103 deg
Mean anomaly: 30
6825 deg
Mean motion: 15
72534995 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 291
Coasting Arc #2 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2008/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5391055
71 A = 6730018
48 meter
Y = 1313974
94 meter E =
0009855
Z = 3798360
03 I = 51
53191
XDOT = -4155
499680 Wp = 78
29395
YDOT = 4963
690770 meter/sec RA = 340
74988 deg
ZDOT = 4173
709187 TA = 327
88034
MA = 327
94034
Ha = 192
218 n
mi
Hp = 186
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17687190
64 X = 5357509
53
Y = 4310941
39 feet Y = 1374073
20 meter
Z = 12461811
11 Z = 3824469
26
XDOT = -13633
529133 XDOT = -4230
971486
YDOT = 16285
074704 feet/sec YDOT = 4916
799507 meter/sec
ZDOT = 13693
271612 ZDOT = 4153
337805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14579042
10 X = -4443692
03
Y = 10786002
03 feet Y = 3287573
42 meter
Z = 12563095
01 Z = 3829231
36
XDOT = -2965
133515 XDOT = -903
772695
YDOT = -19892
740188 feet/sec YDOT = -6063
307209 meter/sec
ZDOT = 13614
675966 ZDOT = 4149
753234
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 08316
55533905
00020000 00000-0 20000-3 0 9013
2 25544 51
6417 340
9482 0003952 335
9213 24
1764 15
72521996 11723
Satellite: ISS
Catalog Number: 25544
Epoch time: 08316
55533905 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 340
9482 deg
Eccentricity:
0003952
Arg of perigee: 335
9213 deg
Mean anomaly: 24
1764 deg
Mean motion: 15
72521996 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1172
Checksum: 288
Coasting Arc #3 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2008/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2725166
04 A = 6729517
87 meter
Y = -4704847
60 meter E =
0005367
Z = -3968448
15 I = 51
50399
XDOT = 6578
228154 Wp = 71
12740
YDOT = 472
910944 meter/sec RA = 335
56563 deg
ZDOT = 3962
725093 TA = 239
99798
MA = 240
05125
Ha = 192
380 n
mi
Hp = 186
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8940833
47 X = 2796852
61
Y = -15435851
71 feet Y = -4673972
19 meter
Z = -13019843
02 Z = -3955034
90
XDOT = 21582
113366 XDOT = 6553
200137
YDOT = 1551
545092 feet/sec YDOT = 546
332346 meter/sec
ZDOT = 13001
066579 ZDOT = 3994
622574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6390197
16 X = 1947732
09
Y = 16694661
66 feet Y = 5088532
87 meter
Z = -12968191
31 Z = -3952704
71
XDOT = -13459
352334 XDOT = -4102
410591
YDOT = 15331
406188 feet/sec YDOT = 4673
012606 meter/sec
ZDOT = 13124
722203 ZDOT = 4000
415328
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 08317
50856416
00020000 00000-0 20000-3 0 9025
2 25544 51
6427 336
0640 0004058 338
5118 21
5874 15
72552348 11871
Satellite: ISS
Catalog Number: 25544
Epoch time: 08317
50856416 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 336
0640 deg
Eccentricity:
0004058
Arg of perigee: 338
5118 deg
Mean anomaly: 21
5874 deg
Mean motion: 15
72552348 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1187
Checksum: 288
Coasting Arc #4 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2008/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5946405
04 A = 6731926
21 meter
Y = 513545
61 meter E =
0004333
Z = -3119923
90 I = 51
48524
XDOT = 2060
286269 Wp = 47
32009
YDOT = -5602
613384 meter/sec RA = 330
48069 deg
ZDOT = -4850
369981 TA = 168
98313
MA = 168
97364
Ha = 192
408 n
mi
Hp = 186
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19509202
89 X = -5936549
06
Y = 1684860
94 feet Y = 447104
86 meter
Z = -10235970
81 Z = -3148788
60
XDOT = 6759
469387 XDOT = 2146
345553
YDOT = -18381
277508 feet/sec YDOT = -5579
092460 meter/sec
ZDOT = -15913
287338 ZDOT = -4840
152197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10584694
73 X = 3226214
95
Y = -16404572
49 feet Y = -5000113
69 meter
Z = -10347806
09 Z = -3154011
30
XDOT = 9134
345156 XDOT = 2784
148404
YDOT = 15904
098403 feet/sec YDOT = 4847
569193 meter/sec
ZDOT = -15874
076800 ZDOT = -4838
418609
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 08318
52532435
00020000 00000-0 20000-3 0 9031
2 25544 51
6417 330
8530 0004031 342
0261 18
0758 15
72573223 12036
Satellite: ISS
Catalog Number: 25544
Epoch time: 08318
52532435 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 330
8530 deg
Eccentricity:
0004031
Arg of perigee: 342
0261 deg
Mean anomaly: 18
0758 deg
Mean motion: 15
72573223 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1203
Checksum: 249
Coasting Arc #5 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -856237
37 A = 6727403
86 meter
Y = 4939813
52 meter E =
0010418
Z = 4483562
19 I = 51
44440
XDOT = -6824
918884 Wp = 44
16509
YDOT = 1679
964997 meter/sec RA = 325
29503 deg
ZDOT = -3142
553644 TA = 77
35631
MA = 77
23984
Ha = 192
481 n
mi
Hp = 186
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2809177
74 X = -933192
55
Y = 16206737
26 feet Y = 4929807
77 meter
Z = 14709849
70 Z = 4479216
10
XDOT = -22391
466155 XDOT = -6827
930845
YDOT = 5511
696186 feet/sec YDOT = 1603
628338 meter/sec
ZDOT = -10310
215369 ZDOT = -3175
717258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11244801
00 X = -3427415
34
Y = -12024538
95 feet Y = -3665079
47 meter
Z = 14693345
57 Z = 4478531
73
XDOT = 8085
798759 XDOT = 2464
551462
YDOT = -20364
042429 feet/sec YDOT = -6206
960132 meter/sec
ZDOT = -10438
638426 ZDOT = -3181
696992
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 08319
54206971
00020000 00000-0 20000-3 0 9048
2 25544 51
6408 325
6419 0004127 346
4899 13
6152 15
72618074 12195
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54206971 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 325
6419 deg
Eccentricity:
0004127
Arg of perigee: 346
4899 deg
Mean anomaly: 13
6152 deg
Mean motion: 15
72618074 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 295
Coasting Arc #6 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5821250
46 A = 6733590
00 meter
Y = -2407910
49 meter E =
0014889
Z = 2353843
77 I = 51
44207
XDOT = 94
213415 Wp = 57
62989
YDOT = 5508
265011 meter/sec RA = 320
20057 deg
ZDOT = 5384
913645 TA = 328
95997
MA = 329
04786
Ha = 192
423 n
mi
Hp = 185
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19098590
75 X = 5836308
63
Y = -7899968
80 feet Y = -2342730
01 meter
Z = 7722584
54 Z = 2382160
35
XDOT = 309
099130 XDOT = 6
452534
YDOT = 18071
735601 feet/sec YDOT = 5508
827169 meter/sec
ZDOT = 17667
039517 ZDOT = 5385
158879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4742156
26 X = -1445409
23
Y = 20074185
30 feet Y = 6118611
68 meter
Z = 7832178
89 Z = 2387248
13
XDOT = -13313
156508 XDOT = -4057
850104
YDOT = -10059
809443 feet/sec YDOT = -3066
229918 meter/sec
ZDOT = 17668
369035 ZDOT = 5385
318882
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 08320
55880096
00020000 00000-0 20000-3 0 9058
2 25544 51
6407 320
4316 0004117 349
6131 10
4945 15
72637767 12359
Satellite: ISS
Catalog Number: 25544
Epoch time: 08320
55880096 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 320
4316 deg
Eccentricity:
0004117
Arg of perigee: 349
6131 deg
Mean anomaly: 10
4945 deg
Mean motion: 15
72637767 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 279
Coasting Arc #7 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2008/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -978289
46 A = 6725761
04 meter
Y = -4532540
11 meter E =
0011360
Z = -4881350
86 I = 51
39346
XDOT = 6313
180513 Wp = 86
28582
YDOT = -3774
628502 meter/sec RA = 315
02050 deg
ZDOT = 2244
869606 TA = 205
62010
MA = 205
67643
Ha = 192
628 n
mi
Hp = 185
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3209611
10 X = -903820
03
Y = -14870538
43 feet Y = -4543062
93 meter
Z = -16014930
66 Z = -4885923
15
XDOT = 20712
534491 XDOT = 6344
014454
YDOT = -12383
951779 feet/sec YDOT = -3703
858745 meter/sec
ZDOT = 7365
057761 ZDOT = 2275
613997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13987707
98 X = 4263453
39
Y = 5932997
82 feet Y = 1808377
74 meter
Z = -16032968
63 Z = -4886848
84
XDOT = -1205
442253 XDOT = -367
418799
YDOT = 23020
012914 feet/sec YDOT = 7016
499936 meter/sec
ZDOT = 7483
975932 ZDOT = 2281
115864
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 08321
51197400
00020000 00000-0 20000-3 0 9066
2 25544 51
6406 315
5463 0004227 353
6436 6
4673 15
72618059 12504
Satellite: ISS
Catalog Number: 25544
Epoch time: 08321
51197400 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 315
5463 deg
Eccentricity:
0004227
Arg of perigee: 353
6436 deg
Mean anomaly: 6
4673 deg
Mean motion: 15
72618059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1250
Checksum: 272
Coasting Arc #8 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5088254
65 A = 6734857
02 meter
Y = 4119709
89 meter E =
0005211
Z = -1578307
56 I = 51
40427
XDOT = -2034
823918 Wp = 113
36891
YDOT = -4704
708538 meter/sec RA = 309
91063 deg
ZDOT = -5737
275001 TA = 84
08036
MA = 84
02097
Ha = 192
698 n
mi
Hp = 185
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16693748
85 X = -5126276
52
Y = 13516108
57 feet Y = 4062597
66 meter
Z = -5178174
41 Z = -1603118
53
XDOT = -6675
931490 XDOT = -1954
192886
YDOT = -15435
395465 feet/sec YDOT = -4727
011686 meter/sec
ZDOT = -18823
080712 ZDOT = -5746
964932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1946968
99 X = -593436
15
Y = -21367578
80 feet Y = -6512838
02 meter
Z = -5274070
52 Z = -1607536
70
XDOT = 14920
000106 XDOT = 4547
616032
YDOT = 3282
370043 feet/sec YDOT = 1000
466389 meter/sec
ZDOT = -18860
975649 ZDOT = -5748
825378
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 08322
52867737
00020000 00000-0 20000-3 0 9076
2 25544 51
6401 310
3349 0004266 358
9480 1
1672 15
72663971 12666
Satellite: ISS
Catalog Number: 25544
Epoch time: 08322
52867737 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 310
3349 deg
Eccentricity:
0004266
Arg of perigee: 358
9480 deg
Mean anomaly: 1
1672 deg
Mean motion: 15
72663971 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 294
Coasting Arc #9 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2008/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2505104
41 A = 6724471
67 meter
Y = 3568926
36 meter E =
0007777
Z = 5117396
80 I = 51
35103
XDOT = -5159
508965 Wp = 27
71134
YDOT = 5556
805313 meter/sec RA = 304
74016 deg
ZDOT = -1342
048323 TA = 75
22589
MA = 75
13973
Ha = 192
662 n
mi
Hp = 185
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8218846
50 X = 2440150
28
Y = 11709075
98 feet Y = 3596576
30 meter
Z = 16789359
57 Z = 5129409
23
XDOT = -16927
522852 XDOT = -5214
743107
YDOT = 18230
988560 feet/sec YDOT = 5498
799978 meter/sec
ZDOT = -4403
045678 ZDOT = -1367
247193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14242736
84 X = -4341186
19
Y = 470966
18 feet Y = 143550
49 meter
Z = 16836185
17 Z = 5131669
24
XDOT = -6111
430541 XDOT = -1862
764029
YDOT = -23050
262981 feet/sec YDOT = -7025
720157 meter/sec
ZDOT = -4500
342611 ZDOT = -1371
704428
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 08323
54536529
00020000 00000-0 20000-3 0 9082
2 25544 51
6396 305
1239 0004317
7977 359
3191 15
72686251 12827
Satellite: ISS
Catalog Number: 25544
Epoch time: 08323
54536529 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 305
1239 deg
Eccentricity:
0004317
Arg of perigee:
7977 deg
Mean anomaly: 359
3191 deg
Mean motion: 15
72686251 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1282
Checksum: 301
Coasting Arc #10 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2008/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3817573
28 A = 6735464
25 meter
Y = -5485328
63 meter E =
0016559
Z = 761206
29 I = 51
37291
XDOT = 3581
045068 Wp = 42
46929
YDOT = 3327
246863 meter/sec RA = 299
61442 deg
ZDOT = 5953
778069 TA = 325
85999
MA = 325
96638
Ha = 192
643 n
mi
Hp = 185
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12524846
73 X = 3874929
55
Y = -17996485
00 feet Y = -5442317
66 meter
Z = 2497395
97 Z = 779891
27
XDOT = 11748
835525 XDOT = 3514
650421
YDOT = 10916
164249 feet/sec YDOT = 3366
920612 meter/sec
ZDOT = 19533
392614 ZDOT = 5971
013881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8678736
07 X = 2645278
75
Y = 20126096
65 feet Y = 6134434
26 meter
Z = 2569439
31 Z = 783165
10
XDOT = -13946
900066 XDOT = -4251
015140
YDOT = 3486
104325 feet/sec YDOT = 1062
564598 meter/sec
ZDOT = 19600
457601 ZDOT = 5974
219477
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 08324
56203684
00020000 00000-0 20000-3 0 9099
2 25544 51
6394 299
9134 0004132 5
9126 354
2085 15
72756385 12986
Satellite: ISS
Catalog Number: 25544
Epoch time: 08324
56203684 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 299
9134 deg
Eccentricity:
0004132
Arg of perigee: 5
9126 deg
Mean anomaly: 354
2085 deg
Mean motion: 15
72756385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1298
Checksum: 307
Coasting Arc #11 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2008/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625883
94 A = 6723825
76 meter
Y = -2168333
98 meter E =
0015970
Z = -5244002
84 I = 51
31993
XDOT = 3483
694636 Wp = 77
38239
YDOT = -6839
941009 meter/sec RA = 294
45588 deg
ZDOT = 424
011891 TA = 196
64282
MA = 196
69530
Ha = 192
839 n
mi
Hp = 185
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11895944
67 X = -3575893
04
Y = -7113956
63 feet Y = -2208600
99 meter
Z = -17204733
74 Z = -5261496
27
XDOT = 11429
444344 XDOT = 3557
861254
YDOT = -22440
751341 feet/sec YDOT = -6800
569650 meter/sec
ZDOT = 1391
115128 ZDOT = 441
115780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12160604
19 X = 3706552
16
Y = -6472843
55 feet Y = -1972922
71 meter
Z = -17272716
74 Z = -5264724
06
XDOT = 12924
788941 XDOT = 3939
475669
YDOT = 20433
599368 feet/sec YDOT = 6228
161087 meter/sec
ZDOT = 1456
923203 ZDOT = 444
070192
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 08325
51515617
00020000 00000-0 20000-3 0 9109
2 25544 51
6395 295
0274 0004387 8
9913 351
1327 15
72718171 13132
Satellite: ISS
Catalog Number: 25544
Epoch time: 08325
51515617 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 295
0274 deg
Eccentricity:
0004387
Arg of perigee: 8
9913 deg
Mean anomaly: 351
1327 deg
Mean motion: 15
72718171 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1313
Checksum: 283
Coasting Arc #12 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2008/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2221634
52 A = 6735695
51 meter
Y = 6355762
31 meter E =
0010505
Z = 6570
70 I = 51
34965
XDOT = -4541
780517 Wp = 113
48826
YDOT = -1573
503005 meter/sec RA = 289
31161 deg
ZDOT = -6010
282757 TA = 66
44014
MA = 66
32984
Ha = 192
876 n
mi
Hp = 185
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7288827
15 X = -2292572
49
Y = 20852238
54 feet Y = 6330522
07 meter
Z = 21557
41 Z = -4394
29
XDOT = -14900
854715 XDOT = -4494
650431
YDOT = -5162
411433 feet/sec YDOT = -1624
028110 meter/sec
ZDOT = -19718
775449 ZDOT = -6032
232670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14444224
40 X = -4402599
60
Y = -16712488
74 feet Y = -5093966
57 meter
Z = -20480
21 Z = -6242
37
XDOT = 10627
498639 XDOT = 3239
261585
YDOT = -9192
958722 feet/sec YDOT = -2802
013819 meter/sec
ZDOT = -19803
994241 ZDOT = -6036
257445
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 08326
53179971
00020000 00000-0 20000-3 0 9112
2 25544 51
6397 289
8158 0004499 12
0166 348
1103 15
72764084 13295
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
53179971 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 289
8158 deg
Eccentricity:
0004499
Arg of perigee: 12
0166 deg
Mean anomaly: 348
1103 deg
Mean motion: 15
72764084 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1329
Checksum: 309
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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