Date:
November 22nd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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
326/17:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 193
3
000/00:00:00
000 0
0 0
0 185
4
326/17:24:41
759 1
0 2
0 2
0
N/A 0
9 0
0 194
7
000/00:29:23
518 1
5 0
0 186
1
326/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 194
8
000/00:00:00
000 0
0 0
0 186
1
329/00:05:20
980 1
0 -1
4 5
1
N/A 4
6 -0
0 195
0
000/02:38:41
960 1
9 4
9 185
8
Coasting Arc #1 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2008/325/01:53:38
826
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4802667
02 A = 6729932
63 meter
Y = -2710158
32 meter E =
0011686
Z = 3846029
89 I = 51
34653
XDOT = 392
078010 Wp = 79
38655
YDOT = 6514
710020 meter/sec RA = 296
65887 deg
ZDOT = 4092
681365 TA = 327
71086
MA = 327
78235
Ha = 192
901 n
mi
Hp = 185
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15756781
55 X = 4813931
97
Y = -8891595
55 feet Y = -2656389
32 meter
Z = 12618208
29 Z = 3869388
75
XDOT = 1286
345178 XDOT = 299
318583
YDOT = 21373
720537 feet/sec YDOT = 6518
575630 meter/sec
ZDOT = 13427
432300 ZDOT = 4094
361086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8090583
06 X = -2466009
72
Y = -16111811
14 feet Y = -4910880
04 meter
Z = 12708572
86 Z = 3873573
01
XDOT = 20232
712804 XDOT = 6166
930863
YDOT = 458
394907 feet/sec YDOT = 139
718768 meter/sec
ZDOT = 13434
422305 ZDOT = 4094
811919
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
13413709
00020000 00000-0 20000-3 0 9005
2 25544 51
6422 296
9868 0003956 5
5171 354
6035 15
72499369 13074
Satellite: ISS
Catalog Number: 25544
Epoch time: 08325
13413709 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 296
9868 deg
Eccentricity:
0003956
Arg of perigee: 5
5171 deg
Mean anomaly: 354
6035 deg
Mean motion: 15
72499369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1307
Checksum: 301
Coasting Arc #2 (Orbit 1321)
---------------------------------------
Vector Time (GMT): 2008/326/01:53:38
826
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1275275
27 A = 6729853
61 meter
Y = -5324468
83 meter E =
0007389
Z = -3917885
44 I = 51
33371
XDOT = 5081
182857 Wp = 73
56570
YDOT = -4159
768904 meter/sec RA = 291
46262 deg
ZDOT = 4007
571830 TA = 238
24831
MA = 238
32033
Ha = 193
137 n
mi
Hp = 185
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4183973
97 X = -1196608
74
Y = -17468729
75 feet Y = -5338289
71 meter
Z = -12853954
85 Z = -3923889
92
XDOT = 16670
547432 XDOT = 5107
852069
YDOT = -13647
535775 feet/sec YDOT = -4102
799201 meter/sec
ZDOT = 13148
201543 ZDOT = 4032
321229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17595516
21 X = -5363113
34
Y = 3528563
32 feet Y = 1075506
10 meter
Z = -12877630
34 Z = -3925101
73
XDOT = -12832
346296 XDOT = -3911
299151
YDOT = -15755
079869 feet/sec YDOT = -4802
148344 meter/sec
ZDOT = 13243
847440 ZDOT = 4036
724700
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
08740585
00020000 00000-0 20000-3 0 9016
2 25544 51
6421 292
1033 0004099 8
7811 351
3423 15
72468296 13227
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
08740585 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 292
1033 deg
Eccentricity:
0004099
Arg of perigee: 8
7811 deg
Mean anomaly: 351
3423 deg
Mean motion: 15
72468296 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1322
Checksum: 275
Coasting Arc #3 (Orbit 1331)
---------------------------------------
Vector Time (GMT): 2008/326/17:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 857604
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3695626
54 A = 6724556
30 meter
Y = -2125140
76 meter E =
0015798
Z = -5213576
32 I = 51
31111
XDOT = 2972
959477 Wp = 78
88620
YDOT = -7047
429046 meter/sec RA = 288
24680 deg
ZDOT = 770
251975 TA = 198
46018
MA = 198
51757
Ha = 193
264 n
mi
Hp = 185
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12124758
99 X = -3646261
14
Y = -6972246
57 feet Y = -2166191
21 meter
Z = -17104909
17 Z = -5231410
15
XDOT = 9753
804060 XDOT = 3047
802208
YDOT = -23121
486370 feet/sec YDOT = -7013
765250 meter/sec
ZDOT = 2527
073408 ZDOT = 784
876442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3645910
57 X = -1111273
54
Y = -13414683
25 feet Y = -4088795
46 meter
Z = -17174211
19 Z = -5234699
57
XDOT = 22206
471887 XDOT = 6768
532631
YDOT = -9321
789335 feet/sec YDOT = -2841
281389 meter/sec
ZDOT = 2583
246522 ZDOT = 787
373540
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
72291175
00020000 00000-0 20000-3 0 9024
2 25544 51
6433 288
8509 0004648 10
8406 349
2856 15
72510451 13322
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
72291175 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 288
8509 deg
Eccentricity:
0004648
Arg of perigee: 10
8406 deg
Mean anomaly: 349
2856 deg
Mean motion: 15
72510451 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1332
Checksum: 288
Coasting Arc #4 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2008/326/17:39:23
518
Vector Time (MET): N/A
Weight (LBS) : 857153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4439167
38 A = 6727092
89 meter
Y = -687439
06 meter E =
0006791
Z = 5001492
14 I = 51
31396
XDOT = -898
720137 Wp = 60
25406
YDOT = 7430
350277 meter/sec RA = 288
12751 deg
ZDOT = 1820
430112 TA = 12
13011
MA = 12
11377
Ha = 194
692 n
mi
Hp = 186
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14564197
45 X = 4422227
72
Y = -2255377
48 feet Y = -637892
59 meter
Z = 16409094
95 Z = 5023016
83
XDOT = -2948
556881 XDOT = -990
584209
YDOT = 24377
789622 feet/sec YDOT = 7419
786572 meter/sec
ZDOT = 5972
539737 ZDOT = 1815
841145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13167017
95 X = 4013307
07
Y = 6410005
72 feet Y = 1953769
74 meter
Z = 16492496
38 Z = 5026912
90
XDOT = -15900
009308 XDOT = -4846
322837
YDOT = 17350
588558 feet/sec YDOT = 5288
459393 meter/sec
ZDOT = 5955
303739 ZDOT = 1815
176580
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
78648517
00020000 00000-0 20000-3 0 9037
2 25544 51
6433 288
5252 0006647 12
6996 347
4332 15
71928324 13330
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
78648517 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 288
5252 deg
Eccentricity:
0006647
Arg of perigee: 12
6996 deg
Mean anomaly: 347
4332 deg
Mean motion: 15
71928324 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1333
Checksum: 309
Coasting Arc #5 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2008/326/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -82564
91 A = 6735717
69 meter
Y = 6311593
61 meter E =
0015024
Z = 2342452
22 I = 51
34255
XDOT = -5153
600651 Wp = 80
42968
YDOT = 1939
785077 meter/sec RA = 288
01842 deg
ZDOT = -5376
496379 TA = 73
11255
MA = 72
94787
Ha = 194
836 n
mi
Hp = 186
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -270882
26 X = -164515
46
Y = 20707328
12 feet Y = 6310212
04 meter
Z = 7685210
70 Z = 2341852
25
XDOT = -16908
138619 XDOT = -5148
790096
YDOT = 6364
124268 feet/sec YDOT = 1882
181601 meter/sec
ZDOT = -17639
423817 ZDOT = -5401
521276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10517909
57 X = -3205858
84
Y = 17840092
10 feet Y = 5437660
07 meter
Z = 7683356
74 Z = 2341887
13
XDOT = -16453
268084 XDOT = -5014
956112
YDOT = -2016
705645 feet/sec YDOT = -614
691880 meter/sec
ZDOT = -17736
302044 ZDOT = -5406
024863
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
78648543
00020000 00000-0 20000-3 0 9047
2 25544 51
6432 288
5254 0006652 12
8688 347
2643 15
71924425 13338
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
78648543 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 288
5254 deg
Eccentricity:
0006652
Arg of perigee: 12
8688 deg
Mean anomaly: 347
2643 deg
Mean motion: 15
71924425 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1333
Checksum: 307
Coasting Arc #6 (Orbit 1348)
---------------------------------------
Vector Time (GMT): 2008/327/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239594
99 A = 6729727
15 meter
Y = -2863856
31 meter E =
0011116
Z = 4360854
21 I = 51
31424
XDOT = 1177
634940 Wp = 73
01484
YDOT = 6840
345872 meter/sec RA = 282
92012 deg
ZDOT = 3343
482673 TA = 343
18969
MA = 343
22649
Ha = 194
812 n
mi
Hp = 185
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13909432
38 X = 4250119
28
Y = -9395854
04 feet Y = -2816388
02 meter
Z = 14307264
45 Z = 4381476
08
XDOT = 3863
631694 XDOT = 1084
815155
YDOT = 22442
079632 feet/sec YDOT = 6852
995765 meter/sec
ZDOT = 10969
431341 ZDOT = 3348
978532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16639390
12 X = 5071686
11
Y = -1611543
35 feet Y = -491198
41 meter
Z = 14387001
87 Z = 4385158
17
XDOT = -7547
974118 XDOT = -2300
622511
YDOT = 20301
367079 feet/sec YDOT = 6187
856686 meter/sec
ZDOT = 10991
254107 ZDOT = 3350
134252
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 08327
80365290
00020000 00000-0 20000-3 0 9057
2 25544 51
6428 283
3170 0006745 16
0700 344
0674 15
71926053 13492
Satellite: ISS
Catalog Number: 25544
Epoch time: 08327
80365290 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 283
3170 deg
Eccentricity:
0006745
Arg of perigee: 16
0700 deg
Mean anomaly: 344
0674 deg
Mean motion: 15
71926053 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1349
Checksum: 281
Coasting Arc #7 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2008/328/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 611773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2053894
68 A = 6732776
08 meter
Y = -5404767
54 meter E =
0009312
Z = -3449772
58 I = 51
31895
XDOT = 4276
236441 Wp = 49
47318
YDOT = -4510
858578 meter/sec RA = 277
72681 deg
ZDOT = 4535
208819 TA = 269
50375
MA = 269
61045
Ha = 194
842 n
mi
Hp = 185
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6738499
59 X = -1976546
23
Y = -17732176
96 feet Y = -5427302
73 meter
Z = -11318151
52 Z = -3459563
04
XDOT = 14029
647117 XDOT = 4304
327981
YDOT = -14799
404785 feet/sec YDOT = -4462
882381 meter/sec
ZDOT = 14879
294025 ZDOT = 4556
051330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2327367
82 X = 709381
71
Y = -18802948
76 feet Y = -5731138
78 meter
Z = -11356518
27 Z = -3461466
77
XDOT = 17851
688884 XDOT = 5441
194772
YDOT = -6798
091575 feet/sec YDOT = -2072
058312 meter/sec
ZDOT = 14959
763283 ZDOT = 4559
735849
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 08328
75723599
00020000 00000-0 20000-3 0 9063
2 25544 51
6422 278
4343 0006655 17
8365 342
3029 15
71963777 13645
Satellite: ISS
Catalog Number: 25544
Epoch time: 08328
75723599 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 278
4343 deg
Eccentricity:
0006655
Arg of perigee: 17
8365 deg
Mean anomaly: 342
3029 deg
Mean motion: 15
71963777 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1364
Checksum: 320
Coasting Arc #8 (Orbit 1368)
---------------------------------------
Vector Time (GMT): 2008/329/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213518
96 A = 6726290
50 meter
Y = -200060
84 meter E =
0018428
Z = -5254433
21 I = 51
29294
XDOT = 647
012892 Wp = 71
17093
YDOT = -7653
971511 meter/sec RA = 276
16017 deg
ZDOT = -222
195733 TA = 196
67522
MA = 196
73590
Ha = 194
978 n
mi
Hp = 185
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13823881
09 X = -4185442
92
Y = -656367
58 feet Y = -247021
58 meter
Z = -17238954
10 Z = -5274834
84
XDOT = 2122
745708 XDOT = 733
632177
YDOT = -25111
455088 feet/sec YDOT = -7646
251913 meter/sec
ZDOT = -728
988624 ZDOT = -218
842468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2134964
60 X = -650737
21
Y = 13573445
54 feet Y = 4137186
20 meter
Z = -17318069
98 Z = -5278547
73
XDOT = -23745
076111 XDOT = -7237
499199
YDOT = -4670
859259 feet/sec YDOT = -1423
677902 meter/sec
ZDOT = -716
564778 ZDOT = -218
408944
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 08329
07510057
00020000 00000-0 20000-3 0 9073
2 25544 51
6404 276
8008 0006003 24
0977 336
0464 15
71839047 13691
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
07510057 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 276
8008 deg
Eccentricity:
0006003
Arg of perigee: 24
0977 deg
Mean anomaly: 336
0464 deg
Mean motion: 15
71839047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1369
Checksum: 286
Coasting Arc #9 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2008/330/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 575737
54 A = 6738001
42 meter
Y = 6653943
07 meter E =
0014135
Z = 865442
92 I = 51
33046
XDOT = -4763
253509 Wp = 101
09543
YDOT = 1193
062699 meter/sec RA = 271
00706 deg
ZDOT = -5924
872255 TA = 69
43112
MA = 69
27953
Ha = 195
053 n
mi
Hp = 185
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1888902
68 X = 497084
99
Y = 21830521
87 feet Y = 6659941
46 meter
Z = 2839379
67 Z = 868049
37
XDOT = -15627
472142 XDOT = -4747
457740
YDOT = 3914
247701 feet/sec YDOT = 1139
885999 meter/sec
ZDOT = -19438
557266 ZDOT = -5947
974339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21910387
16 X = 6678286
01
Y = 119263
02 feet Y = 36351
37 meter
Z = 2849987
05 Z = 868676
05
XDOT = 2496
435478 XDOT = 760
913534
YDOT = 14209
340143 feet/sec YDOT = 4331
006876 meter/sec
ZDOT = -19528
041327 ZDOT = -5952
146996
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 08330
09233083
00020000 00000-0 20000-3 0 9089
2 25544 51
6403 271
5933 0005939 28
8327 331
3162 15
71841487 13859
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
09233083 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 271
5933 deg
Eccentricity:
0005939
Arg of perigee: 28
8327 deg
Mean anomaly: 331
3162 deg
Mean motion: 15
71841487 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1385
Checksum: 290
Coasting Arc #10 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/331/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3866145
26 A = 6727128
95 meter
Y = -2256315
84 meter E =
0007785
Z = 5014563
50 I = 51
29590
XDOT = 1938
429785 Wp = 75
20806
YDOT = 7243
873481 meter/sec RA = 265
88720 deg
ZDOT = 1764
583049 TA = 357
72123
MA = 357
72477
Ha = 194
905 n
mi
Hp = 185
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12684203
61 X = 3866727
88
Y = -7402611
04 feet Y = -2213079
59 meter
Z = 16451980
00 Z = 5033346
97
XDOT = 6359
677771 XDOT = 1848
711273
YDOT = 23765
989110 feet/sec YDOT = 7265
048314 meter/sec
ZDOT = 5789
314465 ZDOT = 1773
782960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6453934
15 X = -1967159
13
Y = -13101076
51 feet Y = -3993208
12 meter
Z = 16524643
59 Z = 5036711
37
XDOT = 23212
504624 XDOT = 7075
171409
YDOT = -4085
915758 feet/sec YDOT = -1245
387123 meter/sec
ZDOT = 5825
532093 ZDOT = 1775
622182
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 08331
10954821
00020000 00000-0 20000-3 0 9093
2 25544 51
6411 266
3856 0005975 31
9589 328
1934 15
71899725 14017
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
10954821 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 266
3856 deg
Eccentricity:
0005975
Arg of perigee: 31
9589 deg
Mean anomaly: 328
1934 deg
Mean motion: 15
71899725 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 312
Coasting Arc #11 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/332/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2717731
34 A = 6736187
20 meter
Y = -5756977
54 meter E =
0012215
Z = -2190212
47 I = 51
32933
XDOT = 3800
231844 Wp = 38
42630
YDOT = -3863
481962 meter/sec RA = 260
71116 deg
ZDOT = 5465
388537 TA = 296
94865
MA = 297
07337
Ha = 195
149 n
mi
Hp = 185
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8916441
40 X = -2642513
95
Y = -18887721
59 feet Y = -5786947
97 meter
Z = -7185736
45 Z = -2203233
51
XDOT = 12467
952244 XDOT = 3816
600913
YDOT = -12675
465756 feet/sec YDOT = -3820
894669 meter/sec
ZDOT = 17931
064755 ZDOT = 5483
889879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19359652
78 X = -5900822
17
Y = 7792196
75 feet Y = 2375061
57 meter
Z = -7236661
98 Z = -2205734
57
XDOT = -11387
225069 XDOT = -3470
826201
YDOT = -11650
319569 feet/sec YDOT = -3551
017405 meter/sec
ZDOT = 18002
518911 ZDOT = 5487
167764
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 08332
06318207
00020000 00000-0 20000-3 0 9103
2 25544 51
6410 261
5047 0006128 34
0834 326
0720 15
71849571 14163
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
06318207 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 261
5047 deg
Eccentricity:
0006128
Arg of perigee: 34
0834 deg
Mean anomaly: 326
0720 deg
Mean motion: 15
71849571 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 258
Coasting Arc #12 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/333/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2585121
00 A = 6729506
67 meter
Y = 4330618
62 meter E =
0015240
Z = -4470714
27 I = 51
31242
XDOT = -4075
062061 Wp = 58
02841
YDOT = -5696
474450 meter/sec RA = 255
61224 deg
ZDOT = -3161
576508 TA = 180
16280
MA = 180
16330
Ha = 195
180 n
mi
Hp = 185
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8481368
10 X = -2611636
11
Y = 14208066
34 feet Y = 4301562
62 meter
Z = -14667697
73 Z = -4483336
94
XDOT = -13369
626184 XDOT = -3995
701556
YDOT = -18689
220637 feet/sec YDOT = -5741
600017 meter/sec
ZDOT = -10372
626339 ZDOT = -3181
181588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13866102
58 X = 4226388
07
Y = 8950145
49 feet Y = 2728004
34 meter
Z = -14716324
46 Z = -4485535
70
XDOT = -18546
488549 XDOT = -5652
969710
YDOT = 11552
097459 feet/sec YDOT = 3521
079305 meter/sec
ZDOT = -10449
086139 ZDOT = -3184
881455
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 08333
08038010
00020000 00000-0 20000-3 0 9118
2 25544 51
6404 256
2975 0006018 39
1453 321
0143 15
71884302 14321
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
08038010 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 256
2975 deg
Eccentricity:
0006018
Arg of perigee: 39
1453 deg
Mean anomaly: 321
0143 deg
Mean motion: 15
71884302 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 251
Coasting Arc #13 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/334/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243475
46 A = 6733276
46 meter
Y = 4043997
72 meter E =
0017411
Z = 3303040
00 I = 51
33413
XDOT = -1894
669080 Wp = 75
64975
YDOT = 5821
950463 meter/sec RA = 250
42160 deg
ZDOT = -4669
039291 TA = 65
39399
MA = 65
21269
Ha = 195
177 n
mi
Hp = 185
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13922163
58 X = 4181893
54
Y = 13267709
05 feet Y = 4091105
94 meter
Z = 10836745
40 Z = 3323506
19
XDOT = -6216
105904 XDOT = -1936
948467
YDOT = 19100
887346 feet/sec YDOT = 5800
527424 meter/sec
ZDOT = -15318
370377 ZDOT = -4678
345675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13572236
57 X = 4136817
71
Y = -13561701
58 feet Y = -4133606
64 meter
Z = 10916429
72 Z = 3327327
78
XDOT = 17971
048634 XDOT = 5477
575624
YDOT = 5560
813213 feet/sec YDOT = 1694
935867 meter/sec
ZDOT = -15354
025577 ZDOT = -4679
906996
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 08334
09756688
00020000 00000-0 20000-3 0 9129
2 25544 51
6404 251
0901 0006215 42
6567 317
5075 15
71930048 14487
Satellite: ISS
Catalog Number: 25544
Epoch time: 08334
09756688 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 251
0901 deg
Eccentricity:
0006215
Arg of perigee: 42
6567 deg
Mean anomaly: 317
5075 deg
Mean motion: 15
71930048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 288
Coasting Arc #14 (Orbit 1463)
---------------------------------------
Vector Time (GMT): 2008/335/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 597362
87 A = 6732327
42 meter
Y = -5634776
54 meter E =
0016696
Z = 3618423
51 I = 51
34161
XDOT = 5384
902375 Wp = 78
75216
YDOT = 3376
614126 meter/sec RA = 245
33182 deg
ZDOT = 4355
476675 TA = 324
81662
MA = 324
92675
Ha = 195
180 n
mi
Hp = 185
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1959851
94 X = 642749
54
Y = -18486799
67 feet Y = -5627843
22 meter
Z = 11871468
22 Z = 3621435
00
XDOT = 17667
002542 XDOT = 5325
585854
YDOT = 11078
130336 feet/sec YDOT = 3436
498948 meter/sec
ZDOT = 14289
621636 ZDOT = 4381
493341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18476991
05 X = -5631786
87
Y = -1984009
07 feet Y = -604725
96 meter
Z = 11882720
60 Z = 3621853
24
XDOT = 11021
381844 XDOT = 3359
317186
YDOT = -16181
623197 feet/sec YDOT = -4932
158751 meter/sec
ZDOT = 14390
796048 ZDOT = 4386
314635
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 08335
11474254
00020000 00000-0 20000-3 0 9130
2 25544 51
6399 245
8826 0006118 46
4991 313
6678 15
71948290 14644
Satellite: ISS
Catalog Number: 25544
Epoch time: 08335
11474254 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 245
8826 deg
Eccentricity:
0006118
Arg of perigee: 46
4991 deg
Mean anomaly: 313
6678 deg
Mean motion: 15
71948290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1464
Checksum: 316
Coasting Arc #15 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/336/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4927155
95 A = 6730083
14 meter
Y = -1777192
07 meter E =
0012839
Z = -4236349
36 I = 51
34676
XDOT = -608
223338 Wp = 85
48384
YDOT = -6785
192810 meter/sec RA = 240
14095 deg
ZDOT = 3564
145988 TA = 220
88146
MA = 220
97782
Ha = 195
250 n
mi
Hp = 184
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16165209
80 X = -4886337
23
Y = -5830682
66 feet Y = -1832061
57 meter
Z = -13898783
98 Z = -4260186
87
XDOT = -1995
483394 XDOT = -549
619185
YDOT = -22261
131267 feet/sec YDOT = -6791
667132 meter/sec
ZDOT = 11693
392349 ZDOT = 3561
332622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5634120
36 X = -1717279
89
Y = 16155017
99 feet Y = 4924049
48 meter
Z = -13991395
43 Z = -4264577
33
XDOT = -21056
145315 XDOT = -6417
913092
YDOT = 2744
972046 feet/sec YDOT = 836
667480 meter/sec
ZDOT = 11681
955900 ZDOT = 3560
660158
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 08336
06833656
00020000 00000-0 20000-3 0 9141
2 25544 51
6389 241
0011 0006303 50
3428 309
8290 15
71969741 14799
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
06833656 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 241
0011 deg
Eccentricity:
0006303
Arg of perigee: 50
3428 deg
Mean anomaly: 309
8290 deg
Mean motion: 15
71969741 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 292
Coasting Arc #16 (Orbit 1493)
---------------------------------------
Vector Time (GMT): 2008/337/01:24:41
960
Vector Time (MET): N/A
Weight (LBS) : 611735
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1664952
78 A = 6735090
26 meter
Y = 5993852
46 meter E =
0009175
Z = -2590070
79 I = 51
37884
XDOT = -5590
419320 Wp = 86
41527
YDOT = -701
516716 meter/sec RA = 235
04777 deg
ZDOT = -5232
458390 TA = 123
05490
MA = 122
96674
Ha = 195
365 n
mi
Hp = 184
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5462443
51 X = 1610387
01
Y = 19664870
26 feet Y = 6012166
16 meter
Z = -8497607
59 Z = -2582114
16
XDOT = -18341
270736 XDOT = -5556
740782
YDOT = -2301
564030 feet/sec YDOT = -763
843046 meter/sec
ZDOT = -17166
858236 ZDOT = -5259
535186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19494254
53 X = 5941848
78
Y = -6086958
19 feet Y = -1855304
86 meter
Z = -8466269
94 Z = -2580519
08
XDOT = -2208
282811 XDOT = -673
084601
YDOT = 16880
546384 feet/sec YDOT = 5145
190538 meter/sec
ZDOT = -17271
965077 ZDOT = -5264
494955
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 08337
08549307
00020000 00000-0 20000-3 0 9152
2 25544 51
6386 235
7928 0006365 53
8273 306
3477 15
71963166 14948
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
08549307 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 235
7928 deg
Eccentricity:
0006365
Arg of perigee: 53
8273 deg
Mean anomaly: 306
3477 deg
Mean motion: 15
71963166 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1494
Checksum: 322
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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