Date:
April 2nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 3356)
---------------------------------------
Vector Time (GMT): 2009/089/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5910692
49 A = 6734607
00 meter
Y = -1307154
07 meter E =
0011895
Z = -2941441
07 I = 51
59226
XDOT = 3516
932625 Wp = 156
31946
YDOT = -4667
949203 meter/sec RA = 349
81214 deg
ZDOT = -5010
390068 TA = 57
57964
MA = 57
46464
Ha = 195
543 n
mi
Hp = 186
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19392035
73 X = -5881347
24
Y = -4288563
22 feet Y = -1373086
86 meter
Z = -9650397
21 Z = -2970084
20
XDOT = 11538
492865 XDOT = 3593
208849
YDOT = -15314
793974 feet/sec YDOT = -4628
194438 meter/sec
ZDOT = -16438
287626 ZDOT = -4993
119256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19315222
04 X = -5887279
68
Y = -4380919
16 feet Y = -1335304
16 meter
Z = -9762312
00 Z = -2975552
70
XDOT = 11386
860046 XDOT = 3470
714942
YDOT = -13850
751388 feet/sec YDOT = -4221
709023 meter/sec
ZDOT = -16371
153603 ZDOT = -4989
927618
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 09089
50494112
00010596 00000-0 82463-4 0 9002
2 25544 51
6437 350
1567 0009325 177
2902 182
8313 15
71796784 33571
Satellite: ISS
Catalog Number: 25544
Epoch time: 09089
50494112 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 350
1567 deg
Eccentricity:
0009325
Arg of perigee: 177
2902 deg
Mean anomaly: 182
8313 deg
Mean motion: 15
71796784 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3357
Checksum: 323
Coasting Arc #2 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2009/090/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1853260
04 A = 6728629
53 meter
Y = 4404179
51 meter E =
0008609
Z = 4729423
01 I = 51
54290
XDOT = -7229
904913 Wp = 129
94815
YDOT = -197
950036 meter/sec RA = 344
64400 deg
ZDOT = -2651
016668 TA = 346
11084
MA = 346
13451
Ha = 195
417 n
mi
Hp = 186
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6080249
46 X = -1925345
40
Y = 14449407
85 feet Y = 4383052
23 meter
Z = 15516479
70 Z = 4720244
72
XDOT = -23720
160477 XDOT = -7214
275814
YDOT = -649
442374 feet/sec YDOT = -278
711658 meter/sec
ZDOT = -8697
561248 ZDOT = -2686
101812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5989811
61 X = -1825694
58
Y = 14525122
98 feet Y = 4427257
48 meter
Z = 15480921
24 Z = 4718584
79
XDOT = -22616
530122 XDOT = -6893
518381
YDOT = 81
463820 feet/sec YDOT = 24
830172 meter/sec
ZDOT = -8834
559769 ZDOT = -2692
773818
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 09090
52218784
00010596 00000-0 82463-4 0 9016
2 25544 51
6431 344
9500 0009210 181
3630 178
7509 15
71846129 33738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09090
52218784 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 344
9500 deg
Eccentricity:
0009210
Arg of perigee: 181
3630 deg
Mean anomaly: 178
7509 deg
Mean motion: 15
71846129 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3373
Checksum: 304
Coasting Arc #3 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2009/091/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6451367
03 A = 6737092
89 meter
Y = -994232
25 meter E =
0012298
Z = 1664656
35 I = 51
54368
XDOT = -697
745481 Wp = 103
99251
YDOT = 5103
114425 meter/sec RA = 339
55369 deg
ZDOT = 5713
825679 TA = 274
40230
MA = 274
54281
Ha = 195
281 n
mi
Hp = 186
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21165902
34 X = 6453918
61
Y = -3261916
85 feet Y = -922075
06 meter
Z = 5461470
95 Z = 1696003
31
XDOT = -2289
191209 XDOT = -782
514268
YDOT = 16742
501394 feet/sec YDOT = 5094
837806 meter/sec
ZDOT = 18746
147242 ZDOT = 5710
230174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21028055
32 X = 6409351
26
Y = -3886543
27 feet Y = -1184618
39 meter
Z = 5583803
31 Z = 1701943
25
XDOT = -2183
892285 XDOT = -665
650369
YDOT = 15272
979804 feet/sec YDOT = 4655
204244 meter/sec
ZDOT = 18732
428865 ZDOT = 5709
644318
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 09091
53942173
00010596 00000-0 82463-4 0 9025
2 25544 51
6435 339
7423 0009181 185
2378 174
8689 15
71834034 33892
Satellite: ISS
Catalog Number: 25544
Epoch time: 09091
53942173 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 339
7423 deg
Eccentricity:
0009181
Arg of perigee: 185
2378 deg
Mean anomaly: 174
8689 deg
Mean motion: 15
71834034 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3389
Checksum: 337
Coasting Arc #4 (Orbit 3403)
---------------------------------------
Vector Time (GMT): 2009/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -607870
89 A = 6726635
52 meter
Y = -4273420
44 meter E =
0016939
Z = -5171850
88 I = 51
48183
XDOT = 7200
124770 Wp = 131
65820
YDOT = -2431
249568 meter/sec RA = 334
39965 deg
ZDOT = 1154
009040 TA = 149
45392
MA = 149
35516
Ha = 195
070 n
mi
Hp = 186
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1994327
08 X = -534915
80
Y = -14020408
27 feet Y = -4279810
07 meter
Z = -16968014
70 Z = -5174626
72
XDOT = 23622
456596 XDOT = 7221
170336
YDOT = -7976
540577 feet/sec YDOT = -2350
615910 meter/sec
ZDOT = 3786
118897 ZDOT = 1189
038209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2550468
70 X = -777382
86
Y = -13916436
04 feet Y = -4241729
70 meter
Z = -16979123
32 Z = -5175236
79
XDOT = 22186
065330 XDOT = 6762
312712
YDOT = -8886
622694 feet/sec YDOT = -2708
642597 meter/sec
ZDOT = 3922
742082 ZDOT = 1195
651787
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 09092
49306408
00010596 00000-0 82463-4 0 9037
2 25544 51
6438 334
8604 0009187 189
5724 170
5264 15
71878411 34047
Satellite: ISS
Catalog Number: 25544
Epoch time: 09092
49306408 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 334
8604 deg
Eccentricity:
0009187
Arg of perigee: 189
5724 deg
Mean anomaly: 170
5264 deg
Mean motion: 15
71878411 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3404
Checksum: 324
Coasting Arc #5 (Orbit 3419)
---------------------------------------
Vector Time (GMT): 2009/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5908392
65 A = 6738264
03 meter
Y = 3197679
95 meter E =
0018433
Z = -338005
52 I = 51
49470
XDOT = -2024
305909 Wp = 162
22717
YDOT = -4365
435532 meter/sec RA = 329
28330 deg
ZDOT = -6016
919770 TA = 21
45438
MA = 21
37722
Ha = 194
993 n
mi
Hp = 186
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19384490
31 X = -5942068
56
Y = 10491075
95 feet Y = 3131420
56 meter
Z = -1108941
98 Z = -366790
10
XDOT = -6641
423587 XDOT = -1946
111556
YDOT = -14322
295051 feet/sec YDOT = -4387
635378 meter/sec
ZDOT = -19740
550427 ZDOT = -6026
563773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18666705
05 X = -5689611
70
Y = 11709562
15 feet Y = 3569074
54 meter
Z = -1221134
13 Z = -372201
68
XDOT = -6576
403867 XDOT = -2004
487899
YDOT = -12514
261777 feet/sec YDOT = -3814
346990 meter/sec
ZDOT = -19778
487300 ZDOT = -6028
482929
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 09093
51027093
00010596 00000-0 82463-4 0 9042
2 25544 51
6439 329
6534 0009362 193
5590 166
5322 15
71844488 34208
Satellite: ISS
Catalog Number: 25544
Epoch time: 09093
51027093 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 329
6534 deg
Eccentricity:
0009362
Arg of perigee: 193
5590 deg
Mean anomaly: 166
5322 deg
Mean motion: 15
71844488 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3420
Checksum: 320
Coasting Arc #6 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2009/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2816161
67 A = 6726080
96 meter
Y = 3127701
54 meter E =
0009460
Z = 5247377
87 I = 51
42961
XDOT = -6039
882597 Wp = 181
63519
YDOT = 4755
305221 meter/sec RA = 324
15101 deg
ZDOT = 397
788377 TA = 264
52099
MA = 264
62891
Ha = 194
632 n
mi
Hp = 187
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9239375
57 X = 2755487
32
Y = 10261487
99 feet Y = 3158854
46 meter
Z = 17215806
67 Z = 5260911
15
XDOT = -19815
887786 XDOT = -6094
540684
YDOT = 15601
395081 feet/sec YDOT = 4687
458138 meter/sec
ZDOT = 1305
079976 ZDOT = 368
313958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9942217
84 X = 3030388
00
Y = 9486155
11 feet Y = 2891380
08 meter
Z = 17268855
25 Z = 5263547
08
XDOT = -17799
973126 XDOT = -5425
431809
YDOT = 16433
552581 feet/sec YDOT = 5008
946827 meter/sec
ZDOT = 1190
298059 ZDOT = 362
802848
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 09094
52746147
00010596 00000-0 82463-4 0 9053
2 25544 51
6439 324
4461 0009147 197
9535 162
1305 15
71917604 34369
Satellite: ISS
Catalog Number: 25544
Epoch time: 09094
52746147 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 324
4461 deg
Eccentricity:
0009147
Arg of perigee: 197
9535 deg
Mean anomaly: 162
1305 deg
Mean motion: 15
71917604 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3436
Checksum: 322
Coasting Arc #7 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2009/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4464397
71 A = 6737615
56 meter
Y = -4945474
50 meter E =
0002757
Z = -1008633
26 I = 51
44487
XDOT = 4196
142606 Wp = 103
63550
YDOT = 2586
604516 meter/sec RA = 319
00347 deg
ZDOT = 5903
282803 TA = 245
32940
MA = 245
35811
Ha = 194
490 n
mi
Hp = 187
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14646974
13 X = 4524266
75
Y = -16225310
05 feet Y = -4895216
33 meter
Z = -3309164
25 Z = -986799
66
XDOT = 13766
872066 XDOT = 4138
230049
YDOT = 8486
235288 feet/sec YDOT = 2633
204810 meter/sec
ZDOT = 19367
725733 ZDOT = 5923
526656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13000239
84 X = 3962473
10
Y = -17588154
06 feet Y = -5360869
36 meter
Z = -3224237
32 Z = -982747
53
XDOT = 13140
015780 XDOT = 4005
076810
YDOT = 6155
367746 feet/sec YDOT = 1876
156089 meter/sec
ZDOT = 19446
945027 ZDOT = 5927
428844
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 09095
48106598
00010596 00000-0 82463-4 0 9060
2 25544 51
6434 319
5636 0009093 202
3661 157
7105 15
71940759 34516
Satellite: ISS
Catalog Number: 25544
Epoch time: 09095
48106598 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 319
5636 deg
Eccentricity:
0009093
Arg of perigee: 202
3661 deg
Mean anomaly: 157
7105 deg
Mean motion: 15
71940759 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3451
Checksum: 326
Coasting Arc #8 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2009/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4326386
92 A = 6727034
51 meter
Y = -1263055
63 meter E =
0010047
Z = -5000205
70 I = 51
38695
XDOT = 3992
431566 Wp = 118
91170
YDOT = -6303
741012 meter/sec RA = 313
89206 deg
ZDOT = -1869
703074 TA = 133
00698
MA = 132
92275
Ha = 194
190 n
mi
Hp = 187
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14194182
80 X = -4287651
68
Y = -4143883
28 feet Y = -1311219
64 meter
Z = -16404874
33 Z = -5021129
00
XDOT = 13098
528760 XDOT = 4071
706968
YDOT = -20681
565000 feet/sec YDOT = -6258
652216 meter/sec
ZDOT = -6134
196437 ZDOT = -1850
114847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14483047
88 X = -4414432
99
Y = -2489561
53 feet Y = -758818
35 meter
Z = -16486658
35 Z = -5025133
46
XDOT = 10478
206463 XDOT = 3193
757330
YDOT = -21002
793974 feet/sec YDOT = -6401
651603 meter/sec
ZDOT = -6058
136075 ZDOT = -1846
519876
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 09096
49823014
00010596 00000-0 82463-4 0 9072
2 25544 51
6423 314
3556 0009057 207
0747 152
9944 15
71962092 34674
Satellite: ISS
Catalog Number: 25544
Epoch time: 09096
49823014 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 314
3556 deg
Eccentricity:
0009057
Arg of perigee: 207
0747 deg
Mean anomaly: 152
9944 deg
Mean motion: 15
71962092 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3467
Checksum: 326
Coasting Arc #9 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2009/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2407092
83 A = 6735750
45 meter
Y = 5865979
92 meter E =
0014925
Z = 2243547
91 I = 51
39699
XDOT = -5449
084006 Wp = 144
09075
YDOT = -151
500603 meter/sec RA = 308
71979 deg
ZDOT = -5443
828794 TA = 10
64209
MA = 10
61054
Ha = 194
044 n
mi
Hp = 187
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7897286
19 X = -2483407
06
Y = 19245340
93 feet Y = 5838635
91 meter
Z = 7360721
49 Z = 2231668
35
XDOT = -17877
572197 XDOT = -5420
539745
YDOT = -497
049224 feet/sec YDOT = -212
276329 meter/sec
ZDOT = -17860
330688 ZDOT = -5470
231119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5320661
10 X = -1621737
50
Y = 20127485
57 feet Y = 6134857
60 meter
Z = 7314737
71 Z = 2229532
06
XDOT = -16215
507503 XDOT = -4942
486687
YDOT = 2249
365025 feet/sec YDOT = 685
606460 meter/sec
ZDOT = -17963
430119 ZDOT = -5475
253500
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 09097
51538089
00010596 00000-0 82463-4 0 9082
2 25544 51
6424 309
1484 0008980 210
9197 149
1437 15
71988817 34839
Satellite: ISS
Catalog Number: 25544
Epoch time: 09097
51538089 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 309
1484 deg
Eccentricity:
0008980
Arg of perigee: 210
9197 deg
Mean anomaly: 149
1437 deg
Mean motion: 15
71988817 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3483
Checksum: 351
Coasting Arc #10 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2009/098/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4952687
84 A = 6729336
71 meter
Y = -1038639
10 meter E =
0011198
Z = 4438797
37 I = 51
35643
XDOT = -1459
018076 Wp = 162
99977
YDOT = 6836
197631 meter/sec RA = 303
62303 deg
ZDOT = 3214
942061 TA = 254
59540
MA = 254
71913
Ha = 193
868 n
mi
Hp = 187
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16248975
85 X = 4942370
96
Y = -3407608
60 feet Y = -983312
56 meter
Z = 14562983
49 Z = 4462832
71
XDOT = -4786
804711 XDOT = -1550
970858
YDOT = 22428
469919 feet/sec YDOT = 6819
368179 meter/sec
ZDOT = 10547
710173 ZDOT = 3207
630167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15473493
58 X = 4716320
84
Y = -5785498
86 feet Y = -1763420
05 meter
Z = 14656756
12 Z = 4467379
26
XDOT = -1862
455529 XDOT = -567
676445
YDOT = 21772
879193 feet/sec YDOT = 6636
373578 meter/sec
ZDOT = 10519
631231 ZDOT = 3206
383599
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 09098
53251839
00010596 00000-0 82463-4 0 9091
2 25544 51
6411 303
9393 0008947 215
2420 144
8152 15
71960706 34996
Satellite: ISS
Catalog Number: 25544
Epoch time: 09098
53251839 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 303
9393 deg
Eccentricity:
0008947
Arg of perigee: 215
2420 deg
Mean anomaly: 144
8152 deg
Mean motion: 15
71960706 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3499
Checksum: 327
Coasting Arc #11 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2009/099/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 146817
50 A = 6733023
52 meter
Y = -5856249
08 meter E =
0006901
Z = -3325465
50 I = 51
35290
XDOT = 5587
447729 Wp = 188
21529
YDOT = -2506
269093 meter/sec RA = 298
43223 deg
ZDOT = 4652
381141 TA = 132
57962
MA = 132
52137
Ha = 193
693 n
mi
Hp = 188
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 481684
71 X = 228446
84
Y = -19213415
62 feet Y = -5854151
11 meter
Z = -10910319
88 Z = -3324553
55
XDOT = 18331
521420 XDOT = 5592
457290
YDOT = -8222
667628 feet/sec YDOT = -2443
758649 meter/sec
ZDOT = 15263
717653 ZDOT = 4679
537615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2661277
86 X = -811157
49
Y = -19036119
55 feet Y = -5802209
24 meter
Z = -10907162
44 Z = -3324503
11
XDOT = 15231
448911 XDOT = 4642
545628
YDOT = -10950
606043 feet/sec YDOT = -3337
744722 meter/sec
ZDOT = 15369
572686 ZDOT = 4684
645755
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 09099
48606922
00010596 00000-0 82463-4 0 9105
2 25544 51
6400 299
0556 0009121 219
1631 140
8872 15
72021306 35140
Satellite: ISS
Catalog Number: 25544
Epoch time: 09099
48606922 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 299
0556 deg
Eccentricity:
0009121
Arg of perigee: 219
1631 deg
Mean anomaly: 140
8872 deg
Mean motion: 15
72021306 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3514
Checksum: 295
Coasting Arc #12 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2009/100/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4598525
12 A = 6731904
70 meter
Y = 3291104
51 meter E =
0005519
Z = -3647104
19 I = 51
33560
XDOT = -1063
246949 Wp = 185
86753
YDOT = -6276
751287 meter/sec RA = 293
34205 deg
ZDOT = -4328
284751 TA = 38
09141
MA = 38
05241
Ha = 193
355 n
mi
Hp = 188
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15087024
68 X = -4617267
80
Y = 10797586
97 feet Y = 3239576
13 meter
Z = -11965564
92 Z = -3669489
84
XDOT = -3488
343007 XDOT = -971
953911
YDOT = -20593
016032 feet/sec YDOT = -6288
130911 meter/sec
ZDOT = -14200
409289 ZDOT = -4333
228002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12782505
87 X = -3896107
79
Y = 13368618
98 feet Y = 4074755
06 meter
Z = -12052738
78 Z = -3673674
78
XDOT = -6150
420556 XDOT = -1874
648186
YDOT = -18687
021560 feet/sec YDOT = -5695
804171 meter/sec
ZDOT = -14220
140506 ZDOT = -4334
298826
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 09100
50317794
00010596 00000-0 82463-4 0 9118
2 25544 51
6391 293
8475 0009049 223
3383 136
7068 15
72037926 35305
Satellite: ISS
Catalog Number: 25544
Epoch time: 09100
50317794 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 293
8475 deg
Eccentricity:
0009049
Arg of perigee: 223
3383 deg
Mean anomaly: 136
7068 deg
Mean motion: 15
72037926 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3530
Checksum: 313
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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