Date:
July 9th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6189 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1381)
---------------------------------------
Vector Time (GMT): 2007/187/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303806
22 A = 6714604
44 meter
Y = -2777254
06 meter E =
0010788
Z = -3054977
92 I = 51
65949
XDOT = 4708
318800 Wp = 57
01541
YDOT = -3585
418360 meter/sec RA = 3
83618 deg
ZDOT = -4921
462559 TA = 158
39956
MA = 158
35402
Ha = 185
405 n
mi
Hp = 174
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17400939
04 X = -5257515
95
Y = -9111725
91 feet Y = -2836305
03 meter
Z = -10022893
44 Z = -3080631
49
XDOT = 15447
240156 XDOT = 4771
968934
YDOT = -11763
183596 feet/sec YDOT = -3532
410853 meter/sec
ZDOT = -16146
530707 ZDOT = -4898
435517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9618246
42 X = -2931641
51
Y = 17068834
26 feet Y = 5202580
68 meter
Z = -10120220
05 Z = -3084643
07
XDOT = -10056
031277 XDOT = -3065
078333
YDOT = -15175
544344 feet/sec YDOT = -4625
505916 meter/sec
ZDOT = -16059
812989 ZDOT = -4895
030999
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 07187
48372591
00020000 00000-0 20000-3 0 9001
2 25544 51
6325 4
1634 0008430 34
2057 325
9650 15
78726316 13828
Satellite: ISS
Catalog Number: 25544
Epoch time: 07187
48372591 = yrday
fracday
Element set: 900
Inclination: 51
6325 deg
RA of node: 4
1634 deg
Eccentricity:
0008430
Arg of perigee: 34
2057 deg
Mean anomaly: 325
9650 deg
Mean motion: 15
78726316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1382
Checksum: 281
Coasting Arc #2 (Orbit 1397)
---------------------------------------
Vector Time (GMT): 2007/188/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5284434
92 A = 6714285
18 meter
Y = 2645254
18 meter E =
0018858
Z = 3178614
99 I = 51
62997
XDOT = -4759
879017 Wp = 71
75168
YDOT = -3694
163605 meter/sec RA = 358
61370 deg
ZDOT = -4809
968708 TA = 71
07720
MA = 70
87287
Ha = 185
383 n
mi
Hp = 174
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17337384
92 X = -5329062
89
Y = 8678655
46 feet Y = 2585910
76 meter
Z = 10428526
87 Z = 3152835
17
XDOT = -15616
400973 XDOT = -4694
850672
YDOT = -12119
959333 feet/sec YDOT = -3747
027091 meter/sec
ZDOT = -15780
737230 ZDOT = -4832
934627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8465133
18 X = 2580172
59
Y = 17500398
03 feet Y = 5334121
32 meter
Z = 10331298
95 Z = 3148979
92
XDOT = -11032
826783 XDOT = -3362
805604
YDOT = 14761
040731 feet/sec YDOT = 4499
165215 meter/sec
ZDOT = -15867
992948 ZDOT = -4836
564250
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 07188
49650828
00020000 00000-0 20000-3 0 9016
2 25544 51
6328 358
9239 0008313 36
6955 323
4779 15
78777521 13981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07188
49650828 = yrday
fracday
Element set: 901
Inclination: 51
6328 deg
RA of node: 358
9239 deg
Eccentricity:
0008313
Arg of perigee: 36
6955 deg
Mean anomaly: 323
4779 deg
Mean motion: 15
78777521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1398
Checksum: 339
Coasting Arc #3 (Orbit 1413)
---------------------------------------
Vector Time (GMT): 2007/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2714044
14 A = 6707927
35 meter
Y = 3629881
84 meter E =
0010950
Z = 4935174
13 I = 51
57868
XDOT = -7022
397064 Wp = 73
91471
YDOT = 2447
749490 meter/sec RA = 353
48056 deg
ZDOT = 2060
770022 TA = 356
15247
MA = 356
16088
Ha = 185
442 n
mi
Hp = 174
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8904344
28 X = 2649278
33
Y = 11909061
14 feet Y = 3659869
00 meter
Z = 16191516
18 Z = 4948202
16
XDOT = -23039
360446 XDOT = -7059
257100
YDOT = 8030
674180 feet/sec YDOT = 2369
014724 meter/sec
ZDOT = 6761
056503 ZDOT = 2026
565963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11865081
11 X = 3616476
72
Y = -8872563
53 feet Y = -2704357
36 meter
Z = 16241174
44 Z = 4950309
97
XDOT = 7498
173049 XDOT = 2285
443145
YDOT = 22171
478226 feet/sec YDOT = 6757
866563 meter/sec
ZDOT = 6631
944389 ZDOT = 2021
416650
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 07189
50927307
00020000 00000-0 20000-3 0 9029
2 25544 51
6319 353
6846 0008437 41
7763 318
4045 15
78753930 14145
Satellite: ISS
Catalog Number: 25544
Epoch time: 07189
50927307 = yrday
fracday
Element set: 902
Inclination: 51
6319 deg
RA of node: 353
6846 deg
Eccentricity:
0008437
Arg of perigee: 41
7763 deg
Mean anomaly: 318
4045 deg
Mean motion: 15
78753930 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1414
Checksum: 306
Coasting Arc #4 (Orbit 1428)
---------------------------------------
Vector Time (GMT): 2007/190/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6524854
09 A = 6718501
21 meter
Y = -1543905
05 meter E =
0020224
Z = -235678
47 I = 51
58627
XDOT = 1299
698491 Wp = 44
11799
YDOT = 4620
341385 meter/sec RA = 348
28477 deg
ZDOT = 6037
974422 TA = 313
31247
MA = 313
48092
Ha = 185
446 n
mi
Hp = 173
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21407001
61 X = 6542778
21
Y = -5065305
28 feet Y = -1470840
21 meter
Z = -773223
33 Z = -203937
35
XDOT = 4264
102662 XDOT = 1218
605089
YDOT = 15158
600346 feet/sec YDOT = 4634
420930 meter/sec
ZDOT = 19809
627368 ZDOT = 6044
092164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5538680
77 X = -1688189
90
Y = -21293451
72 feet Y = -6490244
08 meter
Z = -653329
34 Z = -199134
78
XDOT = 13510
003981 XDOT = 4117
849214
YDOT = -4084
198884 feet/sec YDOT = -1244
863820 meter/sec
ZDOT = 19833
250126 ZDOT = 6045
174638
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 07190
45871729
00020000 00000-0 20000-3 0 9032
2 25544 51
6319 348
7727 0008337 45
9541 314
2310 15
78812133 14293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07190
45871729 = yrday
fracday
Element set: 903
Inclination: 51
6319 deg
RA of node: 348
7727 deg
Eccentricity:
0008337
Arg of perigee: 45
9541 deg
Mean anomaly: 314
2310 deg
Mean motion: 15
78812133 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1429
Checksum: 297
Coasting Arc #5 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2007/191/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 508060
67 A = 6707191
94 meter
Y = -4372296
18 meter E =
0020017
Z = -5077175
17 I = 51
52045
XDOT = 7469
680773 Wp = 82
57411
YDOT = -957
645675 meter/sec RA = 343
09450 deg
ZDOT = 1580
010460 TA = 202
58826
MA = 202
67649
Ha = 185
455 n
mi
Hp = 173
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1666865
71 X = 581578
59
Y = -14344803
74 feet Y = -4366202
72 meter
Z = -16657398
86 Z = -5074529
28
XDOT = 24506
826684 XDOT = 7472
158731
YDOT = -3141
882135 feet/sec YDOT = -874
101961 meter/sec
ZDOT = 5183
761353 ZDOT = 1616
304059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14402916
71 X = -4390009
01
Y = -1194154
55 feet Y = -363978
31 meter
Z = -16647845
43 Z = -5074263
29
XDOT = -4189
999333 XDOT = -1277
111797
YDOT = -23284
491939 feet/sec YDOT = -7097
113143 meter/sec
ZDOT = 5320
940939 ZDOT = 1621
822798
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 07191
47143820
00020000 00000-0 20000-3 0 9040
2 25544 51
6321 343
5334 0008399 50
3623 309
8282 15
78847044 14457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07191
47143820 = yrday
fracday
Element set: 904
Inclination: 51
6321 deg
RA of node: 343
5334 deg
Eccentricity:
0008399
Arg of perigee: 50
3623 deg
Mean anomaly: 309
8282 deg
Mean motion: 15
78847044 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1445
Checksum: 289
Coasting Arc #6 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2007/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6073408
73 A = 6714550
25 meter
Y = -7567
05 meter E =
0011476
Z = -2877161
91 I = 51
51905
XDOT = 2391
464585 Wp = 73
17969
YDOT = -5297
469695 meter/sec RA = 337
95029 deg
ZDOT = -5047
498941 TA = 139
97482
MA = 139
89019
Ha = 185
441 n
mi
Hp = 173
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19925881
66 X = -6058896
04
Y = -24826
29 feet Y = -75401
56 meter
Z = -9439507
57 Z = -2906631
20
XDOT = 7846
012419 XDOT = 2475
043691
YDOT = -17380
149918 feet/sec YDOT = -5270
258598 meter/sec
ZDOT = -16560
035897 ZDOT = -5035
679361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1098907
30 X = 334946
94
Y = 19842299
32 feet Y = 6047932
83 meter
Z = -9550981
11 Z = -2911139
04
XDOT = -16354
250046 XDOT = -4984
775414
YDOT = -7023
361906 feet/sec YDOT = -2140
720709 meter/sec
ZDOT = -16515
874741 ZDOT = -5034
038621
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 07192
48413658
00020000 00000-0 20000-3 0 9052
2 25544 51
6324 338
2938 0008531 53
3113 306
8835 15
78904712 14611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07192
48413658 = yrday
fracday
Element set: 905
Inclination: 51
6324 deg
RA of node: 338
2938 deg
Eccentricity:
0008531
Arg of perigee: 53
3113 deg
Mean anomaly: 306
8835 deg
Mean motion: 15
78904712 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1461
Checksum: 295
Coasting Arc #7 (Orbit 1476)
---------------------------------------
Vector Time (GMT): 2007/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3441088
87 A = 6713586
47 meter
Y = 4722990
19 meter E =
0020274
Z = 3292704
55 I = 51
48860
XDOT = -6021
589388 Wp = 77
92639
YDOT = -1095
886842 meter/sec RA = 332
71677 deg
ZDOT = -4692
621870 TA = 63
21756
MA = 63
01029
Ha = 185
493 n
mi
Hp = 173
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11289661
63 X = -3509641
50
Y = 15495374
65 feet Y = 4684125
98 meter
Z = 10802836
44 Z = 3275822
42
XDOT = -19755
870695 XDOT = -5986
091785
YDOT = -3595
429271 feet/sec YDOT = -1163
024118 meter/sec
ZDOT = -15395
741042 ZDOT = -4721
788515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16289787
84 X = 4965127
33
Y = 10176991
19 feet Y = 3101946
92 meter
Z = 10739461
47 Z = 3273387
86
XDOT = -1393
688690 XDOT = -424
796313
YDOT = 18692
944040 feet/sec YDOT = 5697
609343 meter/sec
ZDOT = -15506
190396 ZDOT = -4726
286833
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 07193
49681426
00020000 00000-0 20000-3 0 9065
2 25544 51
6319 333
0537 0008383 57
5577 302
6398 15
78899635 14770
Satellite: ISS
Catalog Number: 25544
Epoch time: 07193
49681426 = yrday
fracday
Element set: 906
Inclination: 51
6319 deg
RA of node: 333
0537 deg
Eccentricity:
0008383
Arg of perigee: 57
5577 deg
Mean anomaly: 302
6398 deg
Mean motion: 15
78899635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1477
Checksum: 337
Coasting Arc #8 (Orbit 1492)
---------------------------------------
Vector Time (GMT): 2007/194/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4119987
26 A = 6707469
03 meter
Y = 1999819
89 meter E =
0012506
Z = 4889723
70 I = 51
44461
XDOT = -5156
062127 Wp = 86
62897
YDOT = 5319
476007 meter/sec RA = 327
57423 deg
ZDOT = 2164
807892 TA = 342
33042
MA = 342
37388
Ha = 185
256 n
mi
Hp = 173
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13517018
56 X = 4073565
75
Y = 6561088
89 feet Y = 2045631
30 meter
Z = 16042400
59 Z = 4909625
97
XDOT = -16916
214327 XDOT = -5225
678165
YDOT = 17452
349103 feet/sec YDOT = 5261
428315 meter/sec
ZDOT = 7102
388096 ZDOT = 2139
592167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5314041
63 X = 1619719
89
Y = -13967477
60 feet Y = -4257287
17 meter
Z = 16117903
90 Z = 4912737
11
XDOT = 17902
096462 XDOT = 5456
559002
YDOT = 14912
530726 feet/sec YDOT = 4545
339365 meter/sec
ZDOT = 7007
545127 ZDOT = 2135
899755
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 07194
50946886
00020000 00000-0 20000-3 0 9073
2 25544 51
6327 327
8141 0008339 60
6996 299
5002 15
78971853 14939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07194
50946886 = yrday
fracday
Element set: 907
Inclination: 51
6327 deg
RA of node: 327
8141 deg
Eccentricity:
0008339
Arg of perigee: 60
6996 deg
Mean anomaly: 299
5002 deg
Mean motion: 15
78971853 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1493
Checksum: 334
Coasting Arc #9 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2007/195/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5171061
68 A = 6718003
25 meter
Y = -4267364
29 meter E =
0019897
Z = -278768
09 I = 51
45783
XDOT = 3244
525216 Wp = 51
80447
YDOT = 3557
822222 meter/sec RA = 322
36740 deg
ZDOT = 6023
667153 TA = 305
15087
MA = 305
33714
Ha = 185
426 n
mi
Hp = 173
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16965425
47 X = 5219749
83
Y = -14000539
01 feet Y = -4209266
29 meter
Z = -914593
47 Z = -253530
16
XDOT = 10644
767768 XDOT = 3175
238697
YDOT = 11672
645086 feet/sec YDOT = 3593
715735 meter/sec
ZDOT = 19762
687510 ZDOT = 6039
261151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15750958
50 X = -4800892
15
Y = -15359455
43 feet Y = -4681562
01 meter
Z = -819554
83 Z = -249800
31
XDOT = 9346
989516 XDOT = 2848
962404
YDOT = -10583
980507 feet/sec YDOT = -3225
997259 meter/sec
ZDOT = 19822
061740 ZDOT = 6041
764418
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 07195
45881441
00020000 00000-0 20000-3 0 9084
2 25544 51
6341 322
9027 0008466 64
7550 295
4492 15
78983762 15083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07195
45881441 = yrday
fracday
Element set: 908
Inclination: 51
6341 deg
RA of node: 322
9027 deg
Eccentricity:
0008466
Arg of perigee: 64
7550 deg
Mean anomaly: 295
4492 deg
Mean motion: 15
78983762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1508
Checksum: 319
Coasting Arc #10 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2007/196/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1445128
54 A = 6706696
98 meter
Y = -4174018
83 meter E =
0021253
Z = -5064842
27 I = 51
39797
XDOT = 6305
417807 Wp = 89
05361
YDOT = -4109
969376 meter/sec RA = 317
16844 deg
ZDOT = 1594
093104 TA = 196
28677
MA = 196
35517
Ha = 185
380 n
mi
Hp = 173
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4741235
36 X = -1373743
13
Y = -13694287
49 feet Y = -4189779
05 meter
Z = -16616936
57 Z = -5071689
87
XDOT = 20687
066297 XDOT = 6343
163825
YDOT = -13484
151495 feet/sec YDOT = -4039
247878 meter/sec
ZDOT = 5229
964251 ZDOT = 1624
815093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13005476
88 X = -3964069
35
Y = 6324068
04 feet Y = 1927575
94 meter
Z = -16643291
08 Z = -5072875
12
XDOT = -15500
451169 XDOT = -4724
537516
YDOT = -17860
648939 feet/sec YDOT = -5443
925797 meter/sec
ZDOT = 5345
768880 ZDOT = 1629
390355
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 07196
47142783
00020000 00000-0 20000-3 0 9097
2 25544 51
6342 317
6642 0008476 68
1375 292
0692 15
79025282 15240
Satellite: ISS
Catalog Number: 25544
Epoch time: 07196
47142783 = yrday
fracday
Element set: 909
Inclination: 51
6342 deg
RA of node: 317
6642 deg
Eccentricity:
0008476
Arg of perigee: 68
1375 deg
Mean anomaly: 292
0692 deg
Mean motion: 15
79025282 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1524
Checksum: 309
Coasting Arc #11 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2007/197/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5469872
10 A = 6714007
34 meter
Y = 2574267
17 meter E =
0012276
Z = -2932811
19 I = 51
40279
XDOT = -88
206188 Wp = 84
78846
YDOT = -5858
551598 meter/sec RA = 312
01426 deg
ZDOT = -4994
620520 TA = 129
16240
MA = 129
05326
Ha = 185
343 n
mi
Hp = 173
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17945774
61 X = -5484004
68
Y = 8445758
43 feet Y = 2513021
39 meter
Z = -9622083
96 Z = -2959417
16
XDOT = -289
390382 XDOT = 1
573944
YDOT = -19220
969809 feet/sec YDOT = -5859
035251 meter/sec
ZDOT = -16386
550264 ZDOT = -4994
831804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10902507
25 X = 3323084
21
Y = 16509842
99 feet Y = 5032200
14 meter
Z = -9722478
16 Z = -2963411
34
XDOT = -17793
869753 XDOT = -5423
571501
YDOT = 2131
843957 feet/sec YDOT = 649
786038 meter/sec
ZDOT = -16387
983764 ZDOT = -4995
057451
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 07197
48401949
00020000 00000-0 20000-3 0 9103
2 25544 51
6342 312
4234 0008451 71
4109 288
7974 15
79048497 15401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07197
48401949 = yrday
fracday
Element set: 910
Inclination: 51
6342 deg
RA of node: 312
4234 deg
Eccentricity:
0008451
Arg of perigee: 71
4109 deg
Mean anomaly: 288
7974 deg
Mean motion: 15
79048497 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1540
Checksum: 306
Coasting Arc #12 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2007/198/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1145987
18 A = 6713369
58 meter
Y = 5786966
20 meter E =
0021181
Z = 3187757
50 I = 51
38243
XDOT = -5872
893493 Wp = 85
90516
YDOT = 1484
185274 meter/sec RA = 306
77257 deg
ZDOT = -4776
964972 TA = 56
61798
MA = 56
41548
Ha = 185
368 n
mi
Hp = 173
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3759800
47 X = -1226097
93
Y = 18986109
57 feet Y = 5773702
81 meter
Z = 10458521
97 Z = 3181996
53
XDOT = -19268
023270 XDOT = -5865
848264
YDOT = 4869
374257 feet/sec YDOT = 1418
551252 meter/sec
ZDOT = -15672
457257 ZDOT = -4805
477576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19351740
24 X = 5898410
43
Y = 748892
89 feet Y = 228262
55 meter
Z = 10437358
25 Z = 3181306
79
XDOT = 7913
675899 XDOT = 2412
088414
YDOT = 16749
639956 feet/sec YDOT = 5105
290259 meter/sec
ZDOT = -15780
183566 ZDOT = -4809
799951
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 07198
49659008
00020000 00000-0 20000-3 0 9117
2 25544 51
6344 307
1840 0008472 75
1932 285
0172 15
79067387 15561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07198
49659008 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 307
1840 deg
Eccentricity:
0008472
Arg of perigee: 75
1932 deg
Mean anomaly: 285
0172 deg
Mean motion: 15
79067387 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1556
Checksum: 310
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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