Date:
August 26th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4415707
96 A = 6722127
16 meter
Y = 1177666
16 meter E =
0008163
Z = 4922499
90 I = 51
39335
XDOT = -3995
690952 Wp = 52
91572
YDOT = 6248
870548 meter/sec RA = 315
60994 deg
ZDOT = 2091
804073 TA = 16
77253
MA = 16
74555
Ha = 192
359 n
mi
Hp = 182
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14487230
84 X = 4378298
33
Y = 3863734
13 feet Y = 1226836
13 meter
Z = 16149934
07 Z = 4943860
49
XDOT = -13109
222284 XDOT = -4075
431519
YDOT = 20501
543793 feet/sec YDOT = 6203
742573 meter/sec
ZDOT = 6862
874256 ZDOT = 2072
199222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10917541
26 X = -3327666
58
Y = -10143632
76 feet Y = -3091779
27 meter
Z = 16233997
55 Z = 4948122
45
XDOT = 20467
578547 XDOT = 6238
517941
YDOT = -11181
583517 feet/sec YDOT = -3408
146656 meter/sec
ZDOT = 6786
061647 ZDOT = 2068
391590
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 09236
55118355
00020000 00000-0 20000-3 0 9002
2 25544 51
6423 315
9047 0008401 10
3667 349
7668 15
73781612 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55118355 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 315
9047 deg
Eccentricity:
0008401
Arg of perigee: 10
3667 deg
Mean anomaly: 349
7668 deg
Mean motion: 15
73781612 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1672
Checksum: 292
Coasting Arc #2 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2919037
75 A = 6731395
19 meter
Y = -5754706
27 meter E =
0015425
Z = -1891196
17 I = 51
40287
XDOT = 5207
228117 Wp = 24
63748
YDOT = 804
448116 meter/sec RA = 310
42544 deg
ZDOT = 5619
661466 TA = 314
27048
MA = 314
39694
Ha = 192
711 n
mi
Hp = 182
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9576895
50 X = 2992358
00
Y = -18880269
90 feet Y = -5721653
92 meter
Z = -6204711
85 Z = -1876837
37
XDOT = 17084
081749 XDOT = 5170
546327
YDOT = 2639
265472 feet/sec YDOT = 862
473318 meter/sec
ZDOT = 18437
209533 ZDOT = 5644
869076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17111036
66 X = -5215443
97
Y = 12493527
27 feet Y = 3808027
11 meter
Z = -6148509
48 Z = -1874065
69
XDOT = -13037
304980 XDOT = -3973
770558
YDOT = -8782
613233 feet/sec YDOT = -2676
940514 meter/sec
ZDOT = 18536
384638 ZDOT = 5649
890038
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 09237
50367121
00020000 00000-0 20000-3 0 9016
2 25544 51
6416 311
0157 0008645 13
5652 346
5742 15
73736589 16875
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237
50367121 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 311
0157 deg
Eccentricity:
0008645
Arg of perigee: 13
5652 deg
Mean anomaly: 346
5742 deg
Mean motion: 15
73736589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1687
Checksum: 293
Coasting Arc #3 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4621627
45 A = 6722364
69 meter
Y = -242886
01 meter E =
0018737
Z = -4892213
52 I = 51
35358
XDOT = 2696
622057 Wp = 51
38454
YDOT = -6853
084122 meter/sec RA = 305
30791 deg
ZDOT = -2201
404353 TA = 197
07168
MA = 197
13479
Ha = 192
738 n
mi
Hp = 182
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15162819
71 X = -4594802
49
Y = -796870
12 feet Y = -294417
72 meter
Z = -16050569
28 Z = -4914600
22
XDOT = 8847
185226 XDOT = 2783
748021
YDOT = -22483
871792 feet/sec YDOT = -6822
441734 meter/sec
ZDOT = -7222
455227 ZDOT = -2188
092632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13207703
37 X = 4025707
99
Y = 7298509
04 feet Y = 2224585
56 meter
Z = -16138624
95 Z = -4919052
89
XDOT = -17284
180789 XDOT = -5268
218304
YDOT = 15380
749154 feet/sec YDOT = 4688
052342 meter/sec
ZDOT = -7170
422853 ZDOT = -2185
544886
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 09238
51964862
00020000 00000-0 20000-3 0 9024
2 25544 51
6408 305
7998 0008574 18
0388 342
1078 15
73765675 17037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51964862 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 305
7998 deg
Eccentricity:
0008574
Arg of perigee: 18
0388 deg
Mean anomaly: 342
1078 deg
Mean motion: 15
73765675 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1703
Checksum: 323
Coasting Arc #4 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1784130
46 A = 6731031
01 meter
Y = 6186837
82 meter E =
0016566
Z = 1953416
11 I = 51
36751
XDOT = -5298
254128 Wp = 79
95649
YDOT = 247
211375 meter/sec RA = 300
11819 deg
ZDOT = -5579
077846 TA = 78
22698
MA = 78
04119
Ha = 192
830 n
mi
Hp = 182
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5853446
39 X = -1862669
46
Y = 20298024
35 feet Y = 6166447
44 meter
Z = 6408845
50 Z = 1944558
21
XDOT = -17382
723518 XDOT = -5273
522623
YDOT = 811
060943 feet/sec YDOT = 188
101612 meter/sec
ZDOT = -18304
061174 ZDOT = -5604
756623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13892454
25 X = 4234420
06
Y = -15928400
54 feet Y = -4854976
49 meter
Z = 6374299
86 Z = 1942886
60
XDOT = 14848
461371 XDOT = 4525
811026
YDOT = 5528
391095 feet/sec YDOT = 1685
053606 meter/sec
ZDOT = -18405
043713 ZDOT = -5609
857324
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 09239
53561561
00020000 00000-0 20000-3 0 9037
2 25544 51
6413 300
5837 0008830 21
8778 338
2761 15
73828071 17190
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239
53561561 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 300
5837 deg
Eccentricity:
0008830
Arg of perigee: 21
8778 deg
Mean anomaly: 338
2761 deg
Mean motion: 15
73828071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1719
Checksum: 299
Coasting Arc #5 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597899
30 A = 6722305
86 meter
Y = -679900
74 meter E =
0010372
Z = 4846943
24 I = 51
32401
XDOT = -1347
644316 Wp = 64
98786
YDOT = 7234
695364 meter/sec RA = 294
99939 deg
ZDOT = 2293
744494 TA = 2
60940
MA = 2
60399
Ha = 192
751 n
mi
Hp = 182
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15084971
45 X = 4581614
89
Y = -2230645
48 feet Y = -628575
54 meter
Z = 15902044
76 Z = 4869240
14
XDOT = -4421
405236 XDOT = -1439
586299
YDOT = 23735
877177 feet/sec YDOT = 7219
111064 meter/sec
ZDOT = 7525
408445 ZDOT = 2286
974583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14608367
91 X = -4452630
54
Y = -4041282
58 feet Y = -1231782
93 meter
Z = 15989708
97 Z = 4873663
29
XDOT = 13412
920875 XDOT = 4088
258283
YDOT = -18820
333890 feet/sec YDOT = -5736
437770 meter/sec
ZDOT = 7499
128254 ZDOT = 2285
734292
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 09240
55157381
00020000 00000-0 20000-3 0 9043
2 25544 51
6409 295
3678 0008754 25
9266 334
2334 15
73828839 17353
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240
55157381 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 295
3678 deg
Eccentricity:
0008754
Arg of perigee: 25
9266 deg
Mean anomaly: 334
2334 deg
Mean motion: 15
73828839 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 318
Coasting Arc #6 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2009/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 555170
74 A = 6730855
56 meter
Y = -6381058
60 meter E =
0015449
Z = -2049863
13 I = 51
34089
XDOT = 5185
429441 Wp = 34
02637
YDOT = -1318
087893 meter/sec RA = 289
80641 deg
ZDOT = 5540
199096 TA = 302
99822
MA = 303
14660
Ha = 193
002 n
mi
Hp = 181
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1821426
31 X = 636441
35
Y = -20935231
64 feet Y = -6374395
89 meter
Z = -6725272
74 Z = -2046968
93
XDOT = 17012
563782 XDOT = 5172
870081
YDOT = -4324
435346 feet/sec YDOT = -1260
171775 meter/sec
ZDOT = 18176
506219 ZDOT = 5565
359146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9873320
44 X = -3009388
07
Y = 18554456
48 feet Y = 5655398
34 meter
Z = -6714201
31 Z = -2046488
56
XDOT = -15901
688512 XDOT = -4846
834659
YDOT = -1887
390155 feet/sec YDOT = -575
276519 meter/sec
ZDOT = 18275
404163 ZDOT = 5570
343189
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 09241
50402714
00020000 00000-0 20000-3 0 9053
2 25544 51
6406 290
4780 0008905 29
6089 330
5577 15
73822263 17502
Satellite: ISS
Catalog Number: 25544
Epoch time: 09241
50402714 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 290
4780 deg
Eccentricity:
0008905
Arg of perigee: 29
6089 deg
Mean anomaly: 330
5577 deg
Mean motion: 15
73822263 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1750
Checksum: 287
Coasting Arc #7 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2009/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416762
49 A = 6722444
57 meter
Y = 1582025
37 meter E =
0019877
Z = -4832959
33 I = 51
30414
XDOT = -35
525983 Wp = 56
36861
YDOT = -7314
460061 meter/sec RA = 284
68666 deg
ZDOT = -2357
982043 TA = 190
46192
MA = 190
50334
Ha = 193
099 n
mi
Hp = 181
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14490690
57 X = -4410647
33
Y = 5190371
95 feet Y = 1532668
84 meter
Z = -15856165
79 Z = -4854400
82
XDOT = -116
555062 XDOT = 57
722726
YDOT = -23997
572377 feet/sec YDOT = -7314
335896 meter/sec
ZDOT = -7736
161558 ZDOT = -2357
928302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15294340
66 X = 4661715
03
Y = 569219
92 feet Y = 173498
23 meter
Z = -15940426
60 Z = -4858642
03
XDOT = -8864
158384 XDOT = -2701
795475
YDOT = 21168
878219 feet/sec YDOT = 6452
274081 meter/sec
ZDOT = -7736
317912 ZDOT = -2358
029700
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 09242
51996764
00020000 00000-0 20000-3 0 9069
2 25544 51
6411 285
2616 0008926 33
9995 326
1739 15
73828692 17665
Satellite: ISS
Catalog Number: 25544
Epoch time: 09242
51996764 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 285
2616 deg
Eccentricity:
0008926
Arg of perigee: 33
9995 deg
Mean anomaly: 326
1739 deg
Mean motion: 15
73828692 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1766
Checksum: 336
Coasting Arc #8 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2009/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 616007
08 A = 6730651
96 meter
Y = 6370511
56 meter E =
0018855
Z = 2071462
14 I = 51
32525
XDOT = -4860
384471 Wp = 82
93306
YDOT = 2279
448161 meter/sec RA = 279
49128 deg
ZDOT = -5519
516674 TA = 73
83697
MA = 73
62954
Ha = 193
144 n
mi
Hp = 181
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2021020
60 X = 534662
49
Y = 20900628
49 feet Y = 6376945
27 meter
Z = 6796135
62 Z = 2074257
14
XDOT = -15946
143278 XDOT = -4858
699970
YDOT = 7478
504465 feet/sec YDOT = 2225
105959 meter/sec
ZDOT = -18108
650504 ZDOT = -5543
123985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5629332
48 X = 1715820
54
Y = -20225660
65 feet Y = -6164781
37 meter
Z = 6807460
74 Z = 2074914
03
XDOT = 15992
586089 XDOT = 4874
540240
YDOT = -1724
879131 feet/sec YDOT = -525
743159 meter/sec
ZDOT = -18201
396109 ZDOT = -5547
785534
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 09243
53589720
00020000 00000-0 20000-3 0 9073
2 25544 51
6404 280
0454 0009109 37
4699 322
7097 15
73880657 17820
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243
53589720 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 280
0454 deg
Eccentricity:
0009109
Arg of perigee: 37
4699 deg
Mean anomaly: 322
7097 deg
Mean motion: 15
73880657 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1782
Checksum: 315
Coasting Arc #9 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2009/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4040003
01 A = 6722375
60 meter
Y = -2392479
31 meter E =
0012529
Z = 4799258
10 I = 51
29293
XDOT = 1389
351152 Wp = 75
02690
YDOT = 7189
651803 meter/sec RA = 274
37118 deg
ZDOT = 2412
526471 TA = 351
32209
MA = 351
34374
Ha = 193
123 n
mi
Hp = 181
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13254603
06 X = 4043142
28
Y = -7849341
56 feet Y = -2347284
03 meter
Z = 15745597
45 Z = 4818891
80
XDOT = 4558
238688 XDOT = 1297
132521
YDOT = 23588
096468 feet/sec YDOT = 7204
672743 meter/sec
ZDOT = 7915
113093 ZDOT = 2419
051786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15052505
67 X = -4588003
73
Y = 2878294
47 feet Y = 877304
15 meter
Z = 15822705
16 Z = 4822760
53
XDOT = 4030
618720 XDOT = 1228
532586
YDOT = -22612
366960 feet/sec YDOT = -6892
249450 meter/sec
ZDOT = 7941
168327 ZDOT = 2420
468106
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 09244
55181840
00020000 00000-0 20000-3 0 9088
2 25544 51
6396 274
8292 0009169 42
1176 318
0691 15
73878466 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09244
55181840 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 274
8292 deg
Eccentricity:
0009169
Arg of perigee: 42
1176 deg
Mean anomaly: 318
0691 deg
Mean motion: 15
73878466 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1798
Checksum: 330
Coasting Arc #10 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2009/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1798104
97 A = 6730390
49 meter
Y = -6119770
31 meter E =
0015458
Z = -2135668
49 I = 51
32018
XDOT = 4353
727639 Wp = 44
14506
YDOT = -3184
712348 meter/sec RA = 269
17458 deg
ZDOT = 5495
007517 TA = 291
85644
MA = 292
02077
Ha = 193
199 n
mi
Hp = 181
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5899294
53 X = -1719164
46
Y = -20077986
58 feet Y = -6139436
46 meter
Z = -7006786
39 Z = -2144211
64
XDOT = 14283
883331 XDOT = 4362
322677
YDOT = -10448
531326 feet/sec YDOT = -3135
978192 meter/sec
ZDOT = 18028
239886 ZDOT = 5516
178600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -996686
68 X = -303790
10
Y = 20891552
14 feet Y = 6367745
09 meter
Z = -7040734
45 Z = -2146015
86
XDOT = -15284
046290 XDOT = -4658
577309
YDOT = 5336
339245 feet/sec YDOT = 1626
516202 meter/sec
ZDOT = 18111
349689 ZDOT = 5520
339385
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 09245
50423532
00020000 00000-0 20000-3 0 9092
2 25544 51
6405 269
9394 0009164 45
8465 314
3450 15
73921460 18138
Satellite: ISS
Catalog Number: 25544
Epoch time: 09245
50423532 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 269
9394 deg
Eccentricity:
0009164
Arg of perigee: 45
8465 deg
Mean anomaly: 314
3450 deg
Mean motion: 15
73921460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1813
Checksum: 292
Coasting Arc #11 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2009/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3546396
95 A = 6722385
05 meter
Y = 3116737
19 meter E =
0020646
Z = -4804774
15 I = 51
29403
XDOT = -2665
824853 Wp = 62
24880
YDOT = -6784
558242 meter/sec RA = 264
05425 deg
ZDOT = -2431
847772 TA = 183
81880
MA = 183
83458
Ha = 193
317 n
mi
Hp = 181
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11635160
59 X = -3557644
81
Y = 10225515
70 feet Y = 3077016
16 meter
Z = -15763694
72 Z = -4822029
82
XDOT = -8746
144531 XDOT = -2577
947284
YDOT = -22259
049349 feet/sec YDOT = -6813
877832 meter/sec
ZDOT = -7978
503189 ZDOT = -2444
584414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14139183
35 X = 4309623
08
Y = -6154870
73 feet Y = -1876004
60 meter
Z = -15831401
24 Z = -4825411
10
XDOT = 941
483502 XDOT = 286
964172
YDOT = 22827
266961 feet/sec YDOT = 6957
750970 meter/sec
ZDOT = -8028
998425 ZDOT = -2447
238720
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 09246
52013664
00020000 00000-0 20000-3 0 9108
2 25544 51
6399 264
7225 0009172 49
0417 311
1538 15
73899030 18294
Satellite: ISS
Catalog Number: 25544
Epoch time: 09246
52013664 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 264
7225 deg
Eccentricity:
0009172
Arg of perigee: 49
0417 deg
Mean anomaly: 311
1538 deg
Mean motion: 15
73899030 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1829
Checksum: 294
Coasting Arc #12 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2009/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2852714
51 A = 6730394
98 meter
Y = 5710195
23 meter E =
0020669
Z = 2117954
40 I = 51
32435
XDOT = -3714
063354 Wp = 87
45970
YDOT = 3911
809148 meter/sec RA = 258
85637 deg
ZDOT = -5496
969889 TA = 68
75026
MA = 68
52964
Ha = 193
353 n
mi
Hp = 180
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9359299
56 X = 2778361
54
Y = 18734236
32 feet Y = 5741680
37 meter
Z = 6948669
29 Z = 2131631
79
XDOT = -12185
247224 XDOT = -3730
826761
YDOT = 12834
019515 feet/sec YDOT = 3870
182213 meter/sec
ZDOT = -18034
678113 ZDOT = -5515
053643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3424607
82 X = -1043820
46
Y = -20641820
67 feet Y = -6291626
94 meter
Z = 7002814
05 Z = 2134457
72
XDOT = 13803
090774 XDOT = 4207
182068
YDOT = -8484
398180 feet/sec YDOT = -2586
044565 meter/sec
ZDOT = -18105
591629 ZDOT = -5518
584329
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 09247
53602773
00020000 00000-0 20000-3 0 9116
2 25544 51
6385 259
5052 0009339 52
5877 307
6135 15
73932910 18459
Satellite: ISS
Catalog Number: 25544
Epoch time: 09247
53602773 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 259
5052 deg
Eccentricity:
0009339
Arg of perigee: 52
5877 deg
Mean anomaly: 307
6135 deg
Mean motion: 15
73932910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1845
Checksum: 307
Coasting Arc #13 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2009/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2914405
08 A = 6722320
13 meter
Y = -3697965
56 meter E =
0013925
Z = 4785493
81 I = 51
30348
XDOT = 3855
316723 Wp = 83
51896
YDOT = 6212
522494 meter/sec RA = 253
73628 deg
ZDOT = 2448
239462 TA = 342
45119
MA = 342
49925
Ha = 193
313 n
mi
Hp = 180
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9561696
46 X = 2932292
77
Y = -12132432
94 feet Y = -3665274
58 meter
Z = 15700439
00 Z = 4799695
68
XDOT = 12648
676912 XDOT = 3773
667621
YDOT = 20382
291646 feet/sec YDOT = 6255
178580 meter/sec
ZDOT = 8032
281701 ZDOT = 2466
769720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12453673
86 X = -3795879
79
Y = 9043086
60 feet Y = 2756332
79 meter
Z = 15756089
14 Z = 4802455
97
XDOT = -5819
526353 XDOT = -1773
791632
YDOT = -22162
785542 feet/sec YDOT = -6755
217033 meter/sec
ZDOT = 8105
556911 ZDOT = 2470
573746
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 09248
55190896
00020000 00000-0 20000-3 0 9128
2 25544 51
6379 254
2881 0009305 56
1551 304
0496 15
73927273 18611
Satellite: ISS
Catalog Number: 25544
Epoch time: 09248
55190896 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 254
2881 deg
Eccentricity:
0009305
Arg of perigee: 56
1551 deg
Mean anomaly: 304
0496 deg
Mean motion: 15
73927273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 311
Coasting Arc #14 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2009/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3845571
18 A = 6730210
28 meter
Y = -5085429
26 meter E =
0015392
Z = -2148134
44 I = 51
34067
XDOT = 2939
487477 Wp = 53
00197
YDOT = -4526
457042 meter/sec RA = 248
54019 deg
ZDOT = 5489
722553 TA = 282
86319
MA = 283
03510
Ha = 193
353 n
mi
Hp = 180
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12616703
35 X = -3777983
95
Y = -16684479
21 feet Y = -5128054
98 meter
Z = -7047685
16 Z = -2166651
67
XDOT = 9643
987785 XDOT = 2963
216499
YDOT = -14850
580846 feet/sec YDOT = -4493
452847 meter/sec
ZDOT = 18010
900763 ZDOT = 5504
060608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7810015
31 X = 2380492
67
Y = 19378341
27 feet Y = 5906518
42 meter
Z = -7120847
34 Z = -2170434
27
XDOT = -11655
668763 XDOT = -3552
647839
YDOT = 11293
394518 feet/sec YDOT = 3442
226649 meter/sec
ZDOT = 18067
033180 ZDOT = 5506
831713
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 09249
50428735
00020000 00000-0 20000-3 0 9131
2 25544 51
6384 249
3981 0009345 60
0378 300
1712 15
73968457 18761
Satellite: ISS
Catalog Number: 25544
Epoch time: 09249
50428735 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 249
3981 deg
Eccentricity:
0009345
Arg of perigee: 60
0378 deg
Mean anomaly: 300
1712 deg
Mean motion: 15
73968457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1876
Checksum: 314
Coasting Arc #15 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2009/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2227301
98 A = 6722228
97 meter
Y = 4155551
71 meter E =
0021125
Z = -4811429
28 I = 51
32481
XDOT = -4879
537364 Wp = 68
45371
YDOT = -5419
184762 meter/sec RA = 243
42055 deg
ZDOT = -2422
530120 TA = 177
73382
MA = 177
72424
Ha = 193
429 n
mi
Hp = 180
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7307421
20 X = -2250231
33
Y = 13633699
83 feet Y = 4130516
15 meter
Z = -15785529
15 Z = -4822305
58
XDOT = -16008
980854 XDOT = -4806
808157
YDOT = -17779
477567 feet/sec YDOT = -5473
344145 meter/sec
ZDOT = -7947
933464 ZDOT = -2446
058005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10313101
34 X = 3143433
29
Y = -11470460
07 feet Y = -3496196
23 meter
Z = -15828063
45 Z = -4824393
74
XDOT = 10324
928730 XDOT = 3147
038277
YDOT = 20374
617278 feet/sec YDOT = 6210
183346 meter/sec
ZDOT = -8040
834520 ZDOT = -2450
846362
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 09250
52014786
00020000 00000-0 20000-3 0 9143
2 25544 51
6376 244
1800 0009297 63
1065 297
1048 15
73955341 18921
Satellite: ISS
Catalog Number: 25544
Epoch time: 09250
52014786 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 244
1800 deg
Eccentricity:
0009297
Arg of perigee: 63
1065 deg
Mean anomaly: 297
1048 deg
Mean motion: 15
73955341 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1892
Checksum: 296
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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