Date:
October 2nd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
276/12:05:20
216 -1
8 2
3 2
3
N/A -1
0 0
0 193
8
000/00:04:40
432 1
0 0
1 187
0
Coasting Arc #1 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2008/273/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2185661
61 A = 6725116
38 meter
Y = -3616238
68 meter E =
0006372
Z = 5227715
27 I = 51
50215
XDOT = 6958
241095 Wp = 136
84833
YDOT = 3233
080740 meter/sec RA = 200
89831 deg
ZDOT = -676
806813 TA = 319
57439
MA = 319
62173
Ha = 194
156 n
mi
Hp = 185
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7170805
81 X = 2200540
87
Y = -11864300
14 feet Y = -3591713
66 meter
Z = 17151296
81 Z = 5238369
85
XDOT = 22828
874983 XDOT = 6924
858962
YDOT = 10607
220275 feet/sec YDOT = 3310
705096 meter/sec
ZDOT = -2220
494794 ZDOT = -643
084588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11033344
44 X = -3362963
39
Y = 8309326
36 feet Y = 2532682
67 meter
Z = 17192133
72 Z = 5240162
36
XDOT = -16528
915607 XDOT = -5038
013477
YDOT = -17651
645922 feet/sec YDOT = -5380
221677 meter/sec
ZDOT = -2089
683219 ZDOT = -636
935445
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 08273
46328580
00020000 00000-0 20000-3 0 9005
2 25544 51
6400 201
6607 0006143 163
6041 196
5321 15
72286188 4947
Satellite: ISS
Catalog Number: 25544
Epoch time: 08273
46328580 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 201
6607 deg
Eccentricity:
0006143
Arg of perigee: 163
6041 deg
Mean anomaly: 196
5321 deg
Mean motion: 15
72286188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 494
Checksum: 274
Coasting Arc #2 (Orbit 509)
---------------------------------------
Vector Time (GMT): 2008/274/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6471844
38 A = 6736943
57 meter
Y = -1864476
98 meter E =
0010404
Z = 43975
50 I = 51
57010
XDOT = 1369
164420 Wp = 76
16773
YDOT = -4582
387041 meter/sec RA = 195
77436 deg
ZDOT = 6026
944968 TA = 284
30982
MA = 284
42532
Ha = 194
067 n
mi
Hp = 185
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21233085
24 X = -6450728
12
Y = -6117050
47 feet Y = -1936730
81 meter
Z = 144276
56 Z = 12586
14
XDOT = 4492
009252 XDOT = 1391
025290
YDOT = -15034
078219 feet/sec YDOT = -4566
953520 meter/sec
ZDOT = 19773
441495 ZDOT = 6033
649976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17577247
83 X = 5357545
14
Y = 13391149
23 feet Y = 4081622
29 meter
Z = 22630
95 Z = 6897
91
XDOT = -8549
198950 XDOT = -2605
795840
YDOT = 11146
255049 feet/sec YDOT = 3397
378539 meter/sec
ZDOT = 19798
897771 ZDOT = 6034
704041
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 08274
48021352
00020000 00000-0 20000-3 0 9016
2 25544 51
6399 196
4514 0006199 167
6859 192
4456 15
72327461 5107
Satellite: ISS
Catalog Number: 25544
Epoch time: 08274
48021352 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 196
4514 deg
Eccentricity:
0006199
Arg of perigee: 167
6859 deg
Mean anomaly: 192
4456 deg
Mean motion: 15
72327461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 510
Checksum: 305
Coasting Arc #3 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2008/275/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -178225
26 A = 6724986
07 meter
Y = 4210079
24 meter E =
0016398
Z = -5254124
44 I = 51
55904
XDOT = -7603
602176 Wp = 107
54687
YDOT = -991
531641 meter/sec RA = 190
65080 deg
ZDOT = -542
823621 TA = 157
31687
MA = 157
24432
Ha = 193
911 n
mi
Hp = 185
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -584728
54 X = -199765
66
Y = 13812595
92 feet Y = 4207965
43 meter
Z = -17237941
06 Z = -5255042
88
XDOT = -24946
201364 XDOT = -7589
312592
YDOT = -3253
056565 feet/sec YDOT = -1076
479650 meter/sec
ZDOT = -1780
917392 ZDOT = -579
727934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5235629
93 X = 1595820
00
Y = -12791038
50 feet Y = -3898708
53 meter
Z = -17241050
99 Z = -5255072
34
XDOT = 21336
623343 XDOT = 6503
402795
YDOT = 11299
030118 feet/sec YDOT = 3443
944380 meter/sec
ZDOT = -1923
816281 ZDOT = -586
379202
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 08275
43357122
00020000 00000-0 20000-3 0 9020
2 25544 51
6406 191
5675 0006068 171
9662 188
1598 15
72328442 5250
Satellite: ISS
Catalog Number: 25544
Epoch time: 08275
43357122 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 191
5675 deg
Eccentricity:
0006068
Arg of perigee: 171
9662 deg
Mean anomaly: 188
1598 deg
Mean motion: 15
72328442 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 525
Checksum: 302
Coasting Arc #4 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2008/276/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6650525
14 A = 6736432
54 meter
Y = -147883
03 meter E =
0018157
Z = 992479
97 I = 51
62723
XDOT = 999
181237 Wp = 139
48753
YDOT = 4814
621397 meter/sec RA = 185
51071 deg
ZDOT = -5931
192023 TA = 29
66349
MA = 29
56064
Ha = 193
786 n
mi
Hp = 185
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21819308
21 X = 6646863
11
Y = -485180
56 feet Y = -73533
45 meter
Z = 3256167
87 Z = 1024780
06
XDOT = 3278
153664 XDOT = 974
082410
YDOT = 15796
001959 feet/sec YDOT = 4825
654202 meter/sec
ZDOT = -19459
291414 ZDOT = -5926
399087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20740228
70 X = -6321621
71
Y = -6732832
90 feet Y = -2052167
47 meter
Z = 3381141
06 Z = 1030571
79
XDOT = 1519
444049 XDOT = 463
126546
YDOT = -14517
548177 feet/sec YDOT = -4424
948684 meter/sec
ZDOT = -19440
240772 ZDOT = -5925
385387
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 08276
45047190
00020000 00000-0 20000-3 0 9035
2 25544 51
6410 186
3586 0006075 175
5132 184
6086 15
72347264 5412
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
45047190 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 186
3586 deg
Eccentricity:
0006075
Arg of perigee: 175
5132 deg
Mean anomaly: 184
6086 deg
Mean motion: 15
72347264 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 541
Checksum: 289
Coasting Arc #5 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4702650
69 A = 6731159
80 meter
Y = 2742308
44 meter E =
0009166
Z = -3969238
99 I = 51
60941
XDOT = -5480
960844 Wp = 142
42995
YDOT = -3644
139850 meter/sec RA = 185
04103 deg
ZDOT = 3973
680340 TA = 168
83525
MA = 168
81490
Ha = 193
769 n
mi
Hp = 187
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15428644
00 X = -4713683
83
Y = 8997074
92 feet Y = 2689658
81 meter
Z = -13022437
63 Z = -3992111
91
XDOT = -17982
155000 XDOT = -5459
107980
YDOT = -11955
839404 feet/sec YDOT = -3705
308751 meter/sec
ZDOT = 13037
008988 ZDOT = 3947
106483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12990385
38 X = 3959469
46
Y = -12162843
30 feet Y = -3707234
64 meter
Z = -13110660
74 Z = -3996129
39
XDOT = 19362
494479 XDOT = 5901
688317
YDOT = 6730
054272 feet/sec YDOT = 2051
320542 meter/sec
ZDOT = 12933
796731 ZDOT = 3942
221244
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 08276
51402691
00020000 00000-0 20000-3 0 9044
2 25544 51
6422 186
0337 0005142 192
2946 167
8092 15
71930040 5429
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51402691 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 186
0337 deg
Eccentricity:
0005142
Arg of perigee: 192
2946 deg
Mean anomaly: 167
8092 deg
Mean motion: 15
71930040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 275
Coasting Arc #6 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5573397
28 A = 6734325
17 meter
Y = 2340524
59 meter E =
0007239
Z = -2961894
89 I = 51
64941
XDOT = -4312
475000 Wp = 158
93490
YDOT = 3956
897473 meter/sec RA = 179
97030 deg
ZDOT = -4998
389023 TA = 55
19451
MA = 55
12642
Ha = 193
693 n
mi
Hp = 187
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18285424
16 X = 5561199
59
Y = 7678886
45 feet Y = 2402781
25 meter
Z = -9717502
93 Z = -2934848
43
XDOT = -14148
540025 XDOT = -4332
119350
YDOT = 12981
947091 feet/sec YDOT = 3908
562915 meter/sec
ZDOT = -16398
914116 ZDOT = -5019
387307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19639363
87 X = -5986078
11
Y = -3105702
38 feet Y = -946618
08 meter
Z = -9612590
52 Z = -2929917
59
XDOT = 10344
571235 XDOT = 3153
025313
YDOT = -14514
876762 feet/sec YDOT = -4424
134437 meter/sec
ZDOT = -16479
766715 ZDOT = -5023
032895
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 08277
53119560
00020000 00000-0 20000-3 0 9058
2 25544 51
6424 180
8263 0005175 197
4322 162
6663 15
71938136 5580
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53119560 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 180
8263 deg
Eccentricity:
0005175
Arg of perigee: 197
4322 deg
Mean anomaly: 162
6663 deg
Mean motion: 15
71938136 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 300
Coasting Arc #7 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2008/278/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2691610
78 A = 6728209
00 meter
Y = -3980928
32 meter E =
0004980
Z = 4704520
58 I = 51
65828
XDOT = 7036
143488 Wp = 102
80568
YDOT = 1529
025928 meter/sec RA = 174
80706 deg
ZDOT = -2730
426382 TA = 14
07781
MA = 14
06393
Ha = 193
340 n
mi
Hp = 187
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8830744
04 X = 2713071
95
Y = -13060788
44 feet Y = -3950709
12 meter
Z = 15434778
82 Z = 4717648
87
XDOT = 23084
460261 XDOT = 7031
786909
YDOT = 5016
489265 feet/sec YDOT = 1607
683752 meter/sec
ZDOT = -8958
091806 ZDOT = -2696
254719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5137238
71 X = -1565830
36
Y = 14853168
03 feet Y = 4527245
62 meter
Z = 15485180
33 Z = 4719882
97
XDOT = -22567
688052 XDOT = -6878
631318
YDOT = 1400
312760 feet/sec YDOT = 426
815329 meter/sec
ZDOT = -8825
676497 ZDOT = -2690
066196
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 08278
54834945
00020000 00000-0 20000-3 0 9062
2 25544 51
6418 175
6188 0005065 202
0589 158
0355 15
71995809 5742
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
54834945 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 175
6188 deg
Eccentricity:
0005065
Arg of perigee: 202
0589 deg
Mean anomaly: 158
0355 deg
Mean motion: 15
71995809 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 574
Checksum: 326
Coasting Arc #8 (Orbit 589)
---------------------------------------
Vector Time (GMT): 2008/279/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6487962
83 A = 6736620
02 meter
Y = -254449
82 meter E =
0010692
Z = 1783126
50 I = 51
71551
XDOT = 1761
338693 Wp = 82
73469
YDOT = -4879
375142 meter/sec RA = 169
72682 deg
ZDOT = 5684
730467 TA = 296
98232
MA = 297
09147
Ha = 193
306 n
mi
Hp = 187
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21285967
31 X = -6493297
59
Y = -834809
12 feet Y = -327031
79 meter
Z = 5850152
55 Z = 1751594
47
XDOT = 5778
670253 XDOT = 1788
153873
YDOT = -16008
448630 feet/sec YDOT = -4859
528884 meter/sec
ZDOT = 18650
690509 ZDOT = 5693
352352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20749401
81 X = 6324417
67
Y = -4966398
63 feet Y = -1513758
30 meter
Z = 5728071
60 Z = 1745916
22
XDOT = -1489
496508 XDOT = -453
998536
YDOT = 15432
880246 feet/sec YDOT = 4703
941899 meter/sec
ZDOT = 18683
564360 ZDOT = 5694
750417
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 08279
56549066
00020000 00000-0 20000-3 0 9073
2 25544 51
6420 170
4105 0005033 205
9505 154
1405 15
71978936 5905
Satellite: ISS
Catalog Number: 25544
Epoch time: 08279
56549066 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 170
4105 deg
Eccentricity:
0005033
Arg of perigee: 205
9505 deg
Mean anomaly: 154
1405 deg
Mean motion: 15
71978936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 590
Checksum: 290
Coasting Arc #9 (Orbit 604)
---------------------------------------
Vector Time (GMT): 2008/280/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -362414
29 A = 6726299
62 meter
Y = 4320371
87 meter E =
0013242
Z = -5153617
54 I = 51
71015
XDOT = -7507
981918 Wp = 121
44325
YDOT = 973
218935 meter/sec RA = 164
58432 deg
ZDOT = 1339
598416 TA = 161
40687
MA = 161
35844
Ha = 193
074 n
mi
Hp = 187
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1189023
27 X = -385662
75
Y = 14174448
40 feet Y = 4316189
15 meter
Z = -16908194
04 Z = -5155434
66
XDOT = -24632
486609 XDOT = -7524
814218
YDOT = 3192
975507 feet/sec YDOT = 889
166236 meter/sec
ZDOT = 4395
007927 ZDOT = 1303
083223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3024349
91 X = -921821
85
Y = -13890970
39 feet Y = -4233967
77 meter
Z = -16914787
57 Z = -5155627
25
XDOT = 21688
826675 XDOT = 6610
754371
YDOT = -9918
778183 feet/sec YDOT = -3023
243590 meter/sec
ZDOT = 4253
747390 ZDOT = 1296
542204
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 08280
51904580
00020000 00000-0 20000-3 0 9087
2 25544 51
6422 165
5281 0005099 210
6660 149
4205 15
72024298 6050
Satellite: ISS
Catalog Number: 25544
Epoch time: 08280
51904580 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 165
5281 deg
Eccentricity:
0005099
Arg of perigee: 210
6660 deg
Mean anomaly: 149
4205 deg
Mean motion: 15
72024298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 605
Checksum: 279
Coasting Arc #10 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2008/281/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6420159
81 A = 6737791
29 meter
Y = -1941030
68 meter E =
0013479
Z = -548139
32 I = 51
77648
XDOT = 916
900968 Wp = 161
45211
YDOT = 4717
190529 meter/sec RA = 159
48776 deg
ZDOT = -6017
614797 TA = 24
49912
MA = 24
43513
Ha = 193
097 n
mi
Hp = 187
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21063516
44 X = 6444050
36
Y = -6368210
89 feet Y = -1869103
17 meter
Z = -1798357
35 Z = -516891
77
XDOT = 3008
205277 XDOT = 893
317267
YDOT = 15476
346881 feet/sec YDOT = 4727
311938 meter/sec
ZDOT = -19742
830698 ZDOT = -6013
217759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145361
17 X = -5530706
09
Y = 12465614
15 feet Y = 3799519
19 meter
Z = -1677574
36 Z = -511324
66
XDOT = -6763
629322 XDOT = -2061
554217
YDOT = -12474
940342 feet/sec YDOT = -3802
361816 meter/sec
ZDOT = -19725
326010 ZDOT = -6012
279368
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 08281
53615945
00020000 00000-0 20000-3 0 9095
2 25544 51
6423 160
3204 0005272 214
0180 146
0645 15
71991135 6218
Satellite: ISS
Catalog Number: 25544
Epoch time: 08281
53615945 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 160
3204 deg
Eccentricity:
0005272
Arg of perigee: 214
0180 deg
Mean anomaly: 146
0645 deg
Mean motion: 15
71991135 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 621
Checksum: 265
Coasting Arc #11 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2008/282/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1907845
06 A = 6725630
44 meter
Y = -3701234
93 meter E =
0004336
Z = 5282389
27 I = 51
76335
XDOT = 6903
715797 Wp = 191
58733
YDOT = -3403
303529 meter/sec RA = 154
37215 deg
ZDOT = 104
664926 TA = 257
39654
MA = 257
44504
Ha = 192
816 n
mi
Hp = 187
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6259334
20 X = -1891976
60
Y = -12143159
23 feet Y = -3722480
73 meter
Z = 17330673
45 Z = 5273159
48
XDOT = 22649
986212 XDOT = 6940
750537
YDOT = -11165
693992 feet/sec YDOT = -3325
895119 meter/sec
ZDOT = 343
388866 ZDOT = 138
293530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9909492
27 X = 3020413
24
Y = 9470377
63 feet Y = 2886571
10 meter
Z = 17294557
91 Z = 5271381
25
XDOT = -17194
138833 XDOT = -5240
773516
YDOT = 17102
230290 feet/sec YDOT = 5212
759792 meter/sec
ZDOT = 473
254877 ZDOT = 144
248087
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 08282
55325672
00020000 00000-0 20000-3 0 9105
2 25544 51
6424 155
1122 0005106 219
4456 140
6335 15
72063636 6371
Satellite: ISS
Catalog Number: 25544
Epoch time: 08282
55325672 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 155
1122 deg
Eccentricity:
0005106
Arg of perigee: 219
4456 deg
Mean anomaly: 140
6335 deg
Mean motion: 15
72063636 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 637
Checksum: 268
Coasting Arc #12 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2008/283/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5445981
92 A = 6737385
47 meter
Y = 3896395
30 meter E =
0005444
Z = -718116
56 I = 51
82864
XDOT = -3303
364536 Wp = 35
36298
YDOT = -3517
385561 meter/sec RA = 149
25366 deg
ZDOT = 5993
772969 TA = 316
84186
MA = 316
88452
Ha = 192
533 n
mi
Hp = 187
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17867394
75 X = -5485658
77
Y = 12783449
15 feet Y = 3835273
31 meter
Z = -2356025
47 Z = -744669
90
XDOT = -10837
810157 XDOT = -3292
903977
YDOT = -11539
978876 feet/sec YDOT = -3554
266977 meter/sec
ZDOT = 19664
609477 ZDOT = 5977
750622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12516594
46 X = 3815057
99
Y = -18041676
46 feet Y = -5499102
99 meter
Z = -2458454
14 Z = -749336
82
XDOT = 12877
021121 XDOT = 3924
916038
YDOT = 6273
970704 feet/sec YDOT = 1912
306271 meter/sec
ZDOT = 19602
205558 ZDOT = 5974
752254
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 08283
50677369
00020000 00000-0 20000-3 0 9115
2 25544 51
6420 150
2290 0005110 224
4991 135
5762 15
72084055 6526
Satellite: ISS
Catalog Number: 25544
Epoch time: 08283
50677369 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 150
2290 deg
Eccentricity:
0005110
Arg of perigee: 224
4991 deg
Mean anomaly: 135
5762 deg
Mean motion: 15
72084055 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 652
Checksum: 273
Coasting Arc #13 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2008/284/12:07:40
432
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3717746
02 A = 6726276
70 meter
Y = 2287678
45 meter E =
0009646
Z = -5125500
22 I = 51
81493
XDOT = -5345
481809 Wp = 93
55889
YDOT = 5320
805076 meter/sec RA = 144
16476 deg
ZDOT = -1505
466787 TA = 162
03792
MA = 162
00381
Ha = 192
365 n
mi
Hp = 188
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12197329
47 X = 3716787
52
Y = 7505506
72 feet Y = 2329246
77 meter
Z = -16815945
60 Z = -5107441
69
XDOT = -17537
669976 XDOT = -5397
269263
YDOT = 17456
709566 feet/sec YDOT = 5260
739164 meter/sec
ZDOT = -4939
195496 ZDOT = -1531
561497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14149658
68 X = -4312815
97
Y = -2692510
52 feet Y = -820677
21 meter
Z = -16745777
08 Z = -5104112
85
XDOT = 10039
015815 XDOT = 3059
892021
YDOT = -21474
656830 feet/sec YDOT = -6545
475402 meter/sec
ZDOT = -5039
710149 ZDOT = -1536
103653
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 08284
52384439
00020000 00000-0 20000-3 0 9122
2 25544 51
6411 145
0202 0005123 229
4960 130
5756 15
72108597 6689
Satellite: ISS
Catalog Number: 25544
Epoch time: 08284
52384439 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 145
0202 deg
Eccentricity:
0005123
Arg of perigee: 229
4960 deg
Mean anomaly: 130
5756 deg
Mean motion: 15
72108597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 668
Checksum: 283
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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