Date:
September 3rd 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 1776)
---------------------------------------
Vector Time (GMT): 2009/243/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251951
70 A = 6720731
65 meter
Y = -29406
97 meter E =
0009917
Z = 5196962
76 I = 51
29087
XDOT = -882
775797 Wp = 55
74679
YDOT = 7618
541549 meter/sec RA = 281
22348 deg
ZDOT = 769
830353 TA = 26
92554
MA = 26
87411
Ha = 193
022 n
mi
Hp = 181
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13949972
77 X = 4226718
95
Y = -96479
55 feet Y = 17999
69 meter
Z = 17050402
76 Z = 5217557
18
XDOT = -2896
246053 XDOT = -971
641677
YDOT = 24995
215057 feet/sec YDOT = 7608
172945 meter/sec
ZDOT = 2525
690136 ZDOT = 765
326147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10591018
73 X = 3228142
51
Y = -8925935
33 feet Y = -2720625
09 meter
Z = 17131412
19 Z = 5221654
44
XDOT = 13085
068382 XDOT = 3988
328843
YDOT = 20312
275210 feet/sec YDOT = 6191
181484 meter/sec
ZDOT = 2508
363210 ZDOT = 764
549107
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
21844157
00020000 00000-0 20000-3 0 9009
2 25544 51
6380 281
6777 0008941 37
7731 322
4058 15
73842617 17773
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243
21844157 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 281
6777 deg
Eccentricity:
0008941
Arg of perigee: 37
7731 deg
Mean anomaly: 322
4058 deg
Mean motion: 15
73842617 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1777
Checksum: 304
Coasting Arc #2 (Orbit 1791)
---------------------------------------
Vector Time (GMT): 2009/244/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 139613
81 A = 6732293
97 meter
Y = -6684836
29 meter E =
0019499
Z = -707111
84 I = 51
32663
XDOT = 4853
159365 Wp = 40
75356
YDOT = -517
936561 meter/sec RA = 276
05209 deg
ZDOT = 5961
484655 TA = 311
50473
MA = 311
67190
Ha = 193
103 n
mi
Hp = 181
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 458050
54 X = 217789
39
Y = -21931877
58 feet Y = -6682837
94 meter
Z = -2319920
75 Z = -706243
71
XDOT = 15922
438863 XDOT = 4829
630924
YDOT = -1699
266933 feet/sec YDOT = -463
797224 meter/sec
ZDOT = 19558
676690 ZDOT = 5985
003815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13947594
66 X = -4251226
85
Y = -16932095
51 feet Y = -5160902
71 meter
Z = -2316860
26 Z = -706179
01
XDOT = 9639
846449 XDOT = 2938
225198
YDOT = -10581
590397 feet/sec YDOT = -3225
268753 meter/sec
ZDOT = 19651
168867 ZDOT = 5989
676271
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
17085959
00020000 00000-0 20000-3 0 9013
2 25544 51
6390 276
7878 0008858 41
9620 318
2221 15
73882500 17929
Satellite: ISS
Catalog Number: 25544
Epoch time: 09244
17085959 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 276
7878 deg
Eccentricity:
0008858
Arg of perigee: 41
9620 deg
Mean anomaly: 318
2221 deg
Mean motion: 15
73882500 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1792
Checksum: 314
Coasting Arc #3 (Orbit 1807)
---------------------------------------
Vector Time (GMT): 2009/245/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187924
37 A = 6720574
98 meter
Y = 841896
21 meter E =
0022450
Z = -5207365
52 I = 51
28549
XDOT = -524
906377 Wp = 69
54458
YDOT = -7624
097432 meter/sec RA = 270
90835 deg
ZDOT = -805
554541 TA = 192
70609
MA = 192
76277
Ha = 193
165 n
mi
Hp = 181
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13739909
34 X = -4171731
26
Y = 2762126
67 feet Y = 795154
80 meter
Z = -17084532
54 Z = -5227670
85
XDOT = -1722
133782 XDOT = -435
700212
YDOT = -25013
443017 feet/sec YDOT = -7629
468483 meter/sec
ZDOT = -2642
895477 ZDOT = -807
887656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8347553
42 X = -2544334
28
Y = 11135465
25 feet Y = 3394089
81 meter
Z = -17164366
29 Z = -5231698
85
XDOT = -17101
058059 XDOT = -5212
402496
YDOT = -16932
929166 feet/sec YDOT = -5161
156810 meter/sec
ZDOT = -2652
492113 ZDOT = -808
479596
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
18676352
00020000 00000-0 20000-3 0 9029
2 25544 51
6390 271
5723 0008949 45
9080 314
2818 15
73913829 18081
Satellite: ISS
Catalog Number: 25544
Epoch time: 09245
18676352 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 271
5723 deg
Eccentricity:
0008949
Arg of perigee: 45
9080 deg
Mean anomaly: 314
2818 deg
Mean motion: 15
73913829 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1808
Checksum: 312
Coasting Arc #4 (Orbit 1823)
---------------------------------------
Vector Time (GMT): 2009/246/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1049692
61 A = 6732181
88 meter
Y = 6610408
50 meter E =
0017461
Z = 693457
86 I = 51
32467
XDOT = -4677
769448 Wp = 97
72346
YDOT = 1380
810003 meter/sec RA = 265
73416 deg
ZDOT = -5956
091612 TA = 74
69122
MA = 74
49830
Ha = 193
174 n
mi
Hp = 181
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3443873
40 X = 972327
22
Y = 21687691
94 feet Y = 6621714
24 meter
Z = 2275124
22 Z = 698369
01
XDOT = -15347
012625 XDOT = -4663
928984
YDOT = 4530
216544 feet/sec YDOT = 1328
577568 meter/sec
ZDOT = -19540
982979 ZDOT = -5978
782371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17224751
74 X = 5250104
33
Y = 13617421
44 feet Y = 4150590
05 meter
Z = 2294819
55 Z = 699461
00
XDOT = -7134
017812 XDOT = -2174
448629
YDOT = 12400
878933 feet/sec YDOT = 3779
787899 meter/sec
ZDOT = -19630
171018 ZDOT = -5983
276126
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
20265693
00020000 00000-0 20000-3 0 9036
2 25544 51
6381 266
3541 0008887 49
0099 311
1832 15
73924204 18246
Satellite: ISS
Catalog Number: 25544
Epoch time: 09246
20265693 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 266
3541 deg
Eccentricity:
0008887
Arg of perigee: 49
0099 deg
Mean anomaly: 311
1832 deg
Mean motion: 15
73924204 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1824
Checksum: 294
Coasting Arc #5 (Orbit 1839)
---------------------------------------
Vector Time (GMT): 2009/247/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3955865
58 A = 6720456
91 meter
Y = -1574546
75 meter E =
0010541
Z = 5190743
72 I = 51
28985
XDOT = 1892
349739 Wp = 69
03191
YDOT = 7429
013586 meter/sec RA = 260
58931 deg
ZDOT = 813
736955 TA = 13
20773
MA = 13
18016
Ha = 193
048 n
mi
Hp = 181
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12978561
60 X = 3947962
95
Y = -5165835
80 feet Y = -1530353
80 meter
Z = 17029999
08 Z = 5209942
04
XDOT = 6208
496519 XDOT = 1805
183635
YDOT = 24373
404153 feet/sec YDOT = 7449
687632 meter/sec
ZDOT = 2669
740665 ZDOT = 822
717724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5749376
50 X = 1752409
96
Y = -12629272
93 feet Y = -3849402
39 meter
Z = 17105435
52 Z = 5213736
75
XDOT = 20388
030997 XDOT = 6214
271848
YDOT = 12935
288191 feet/sec YDOT = 3942
675841 meter/sec
ZDOT = 2705
505542 ZDOT = 824
638089
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
21854050
00020000 00000-0 20000-3 0 9040
2 25544 51
6391 261
1375 0008868 52
5730 307
6238 15
73949812 18405
Satellite: ISS
Catalog Number: 25544
Epoch time: 09247
21854050 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 261
1375 deg
Eccentricity:
0008868
Arg of perigee: 52
5730 deg
Mean anomaly: 307
6238 deg
Mean motion: 15
73949812 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1840
Checksum: 297
Coasting Arc #6 (Orbit 1854)
---------------------------------------
Vector Time (GMT): 2009/248/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2238887
53 A = 6732113
93 meter
Y = -6299416
20 meter E =
0019310
Z = -725724
88 I = 51
33592
XDOT = 4348
843831 Wp = 47
51277
YDOT = -2219
003667 meter/sec RA = 255
41692 deg
ZDOT = 5958
398737 TA = 304
54285
MA = 304
72496
Ha = 193
239 n
mi
Hp = 180
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7345431
54 X = -2164754
55
Y = -20667376
00 feet Y = -6324038
32 meter
Z = -2380987
13 Z = -736420
80
XDOT = 14267
860338 XDOT = 4344
389208
YDOT = -7280
195759 feet/sec YDOT = -2170
396798 meter/sec
ZDOT = 19548
552286 ZDOT = 5979
514663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19740820
88 X = -6017002
21
Y = -9549440
22 feet Y = -2910669
38 meter
Z = -2423443
23 Z = -738665
50
XDOT = 4255
645890 XDOT = 1297
120867
YDOT = -13686
650677 feet/sec YDOT = -4171
691126 meter/sec
ZDOT = 19631
493042 ZDOT = 5983
679079
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
17092259
00020000 00000-0 20000-3 0 9052
2 25544 51
6398 256
2473 0008961 56
5720 303
6299 15
73937999 18555
Satellite: ISS
Catalog Number: 25544
Epoch time: 09248
17092259 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 256
2473 deg
Eccentricity:
0008961
Arg of perigee: 56
5720 deg
Mean anomaly: 303
6299 deg
Mean motion: 15
73937999 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1855
Checksum: 339
Coasting Arc #7 (Orbit 1870)
---------------------------------------
Vector Time (GMT): 2009/249/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3623951
74 A = 6720428
28 meter
Y = 2257181
54 meter E =
0023171
Z = -5209993
18 I = 51
30565
XDOT = -3174
108524 Wp = 74
86585
YDOT = -6951
514011 meter/sec RA = 250
27342 deg
ZDOT = -800
853764 TA = 187
44270
MA = 187
47716
Ha = 193
255 n
mi
Hp = 180
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11889605
46 X = -3623613
38
Y = 7405451
25 feet Y = 2216657
85 meter
Z = -17093153
48 Z = -5227597
70
XDOT = -10413
741878 XDOT = -3092
249186
YDOT = -22806
804498 feet/sec YDOT = -6986
551125 meter/sec
ZDOT = -2627
472979 ZDOT = -816
074188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2948723
89 X = -898771
04
Y = 13606639
22 feet Y = 4147303
63 meter
Z = -17162276
03 Z = -5231061
73
XDOT = -22583
782408 XDOT = -6883
536878
YDOT = -8296
633543 feet/sec YDOT = -2528
813904 meter/sec
ZDOT = -2687
776545 ZDOT = -819
234291
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
18678591
00020000 00000-0 20000-3 0 9064
2 25544 51
6400 251
0310 0008947 60
0380 300
1670 15
73967232 18714
Satellite: ISS
Catalog Number: 25544
Epoch time: 09249
18678591 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 251
0310 deg
Eccentricity:
0008947
Arg of perigee: 60
0380 deg
Mean anomaly: 300
1670 deg
Mean motion: 15
73967232 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1871
Checksum: 280
Coasting Arc #8 (Orbit 1886)
---------------------------------------
Vector Time (GMT): 2009/250/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3294408
90 A = 6732042
81 meter
Y = 5827421
42 meter E =
0019112
Z = 668889
57 I = 51
35648
XDOT = -3906
590037 Wp = 103
21426
YDOT = 2908
941243 meter/sec RA = 245
10154 deg
ZDOT = -5963
713182 TA = 69
47223
MA = 69
26723
Ha = 193
272 n
mi
Hp = 180
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10808428
16 X = 3225751
46
Y = 19118836
67 feet Y = 5863877
60 meter
Z = 2194519
59 Z = 684726
67
XDOT = -12816
896447 XDOT = -3909
857185
YDOT = 9543
770481 feet/sec YDOT = 2865
236732 meter/sec
ZDOT = -19565
988129 ZDOT = -5982
699645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21311012
93 X = 6495596
74
Y = 5283350
17 feet Y = 1610365
13 meter
Z = 2257186
31 Z = 687990
39
XDOT = -1401
634179 XDOT = -427
218098
YDOT = 14233
368200 feet/sec YDOT = 4338
330627 meter/sec
ZDOT = -19640
507167 ZDOT = -5986
426585
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
20263881
00020000 00000-0 20000-3 0 9072
2 25544 51
6403 245
8134 0008929 64
3374 295
8711 15
73976075 18870
Satellite: ISS
Catalog Number: 25544
Epoch time: 09250
20263881 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 245
8134 deg
Eccentricity:
0008929
Arg of perigee: 64
3374 deg
Mean anomaly: 295
8711 deg
Mean motion: 15
73976075 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1887
Checksum: 314
Coasting Arc #9 (Orbit 1902)
---------------------------------------
Vector Time (GMT): 2009/251/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3174736
73 A = 6720193
71 meter
Y = -2820419
00 meter E =
0011143
Z = 5198727
32 I = 51
33178
XDOT = 4358
243342 Wp = 80
54401
YDOT = 6314
065583 meter/sec RA = 239
95830 deg
ZDOT = 764
458136 TA = 2
16278
MA = 2
15797
Ha = 193
094 n
mi
Hp = 180
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10415802
92 X = 3180784
49
Y = -9253343
17 feet Y = -2784883
08 meter
Z = 17056192
01 Z = 5214165
20
XDOT = 14298
698630 XDOT = 4283
600824
YDOT = 20715
438264 feet/sec YDOT = 6362
384723 meter/sec
ZDOT = 2508
064750 ZDOT = 785
448961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 120703
64 X = 36790
47
Y = -13857455
77 feet Y = -4223752
52 meter
Z = 17116756
31 Z = 5217187
32
XDOT = 23919
210454 XDOT = 7290
575346
YDOT = 3407
117683 feet/sec YDOT = 1038
489470 meter/sec
ZDOT = 2591
042819 ZDOT = 789
749851
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 09251
21847913
00020000 00000-0 20000-3 0 9089
2 25544 51
6412 240
5966 0008900 67
4662 292
7442 15
74035415 19039
Satellite: ISS
Catalog Number: 25544
Epoch time: 09251
21847913 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 240
5966 deg
Eccentricity:
0008900
Arg of perigee: 67
4662 deg
Mean anomaly: 292
7442 deg
Mean motion: 15
74035415 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1903
Checksum: 290
Coasting Arc #10 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2009/252/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4278805
46 A = 6731987
06 meter
Y = -5146928
00 meter E =
0019055
Z = -661608
45 I = 51
38756
XDOT = 3344
893405 Wp = 54
17213
YDOT = -3531
494011 meter/sec RA = 234
79005 deg
ZDOT = 5971
484129 TA = 298
59573
MA = 298
78732
Ha = 193
303 n
mi
Hp = 180
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14038075
66 X = -4217719
60
Y = -16886246
73 feet Y = -5194434
60 meter
Z = -2170631
41 Z = -682246
52
XDOT = 10974
059727 XDOT = 3355
125871
YDOT = -11586
266439 feet/sec YDOT = -3494
031980 meter/sec
ZDOT = 19591
483362 ZDOT = 5987
758800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21941565
35 X = -6687789
12
Y = -648112
22 feet Y = -197544
61 meter
Z = -2252154
15 Z = -686456
59
XDOT = -1555
329928 XDOT = -474
064562
YDOT = -14207
991832 feet/sec YDOT = -4330
595910 meter/sec
ZDOT = 19655
298693 ZDOT = 5990
935042
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 09252
17082188
00020000 00000-0 20000-3 0 9091
2 25544 51
6415 235
7066 0009050 70
4985 289
7155 15
73993486 19181
Satellite: ISS
Catalog Number: 25544
Epoch time: 09252
17082188 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 235
7066 deg
Eccentricity:
0009050
Arg of perigee: 70
4985 deg
Mean anomaly: 289
7155 deg
Mean motion: 15
73993486 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1918
Checksum: 324
Coasting Arc #11 (Orbit 1933)
---------------------------------------
Vector Time (GMT): 2009/253/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2673381
31 A = 6720236
16 meter
Y = 3304287
14 meter E =
0023615
Z = -5225864
12 I = 51
36631
XDOT = -5367
604525 Wp = 80
87311
YDOT = -5452
697273 meter/sec RA = 229
64887 deg
ZDOT = -700
833454 TA = 182
41552
MA = 182
42695
Ha = 193
276 n
mi
Hp = 180
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8770936
04 X = -2684745
14
Y = 10840837
06 feet Y = 3274328
17 meter
Z = -17145223
49 Z = -5238879
21
XDOT = -17610
251066 XDOT = -5302
828030
YDOT = -17889
426750 feet/sec YDOT = -5512
358813 meter/sec
ZDOT = -2299
322355 ZDOT = -726
752104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2631426
08 X = 802058
67
Y = 13630002
75 feet Y = 4154424
84 meter
Z = -17196231
49 Z = -5241411
36
XDOT = -24034
843453 XDOT = -7325
820284
YDOT = 1606
090862 feet/sec YDOT = 489
536495 meter/sec
ZDOT = -2401
648985 ZDOT = -732
022611
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 09253
18664150
00020000 00000-0 20000-3 0 9100
2 25544 51
6415 230
4902 0008928 74
5093 285
7055 15
74018564 19349
Satellite: ISS
Catalog Number: 25544
Epoch time: 09253
18664150 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 230
4902 deg
Eccentricity:
0008928
Arg of perigee: 74
5093 deg
Mean anomaly: 285
7055 deg
Mean motion: 15
74018564 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1934
Checksum: 291
Coasting Arc #12 (Orbit 1949)
---------------------------------------
Vector Time (GMT): 2009/254/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5084199
01 A = 6731926
72 meter
Y = 4367802
76 meter E =
0020297
Z = 559680
00 I = 51
42554
XDOT = -2750
310352 Wp = 109
16404
YDOT = 3990
146544 meter/sec RA = 224
48418 deg
ZDOT = -5985
659241 TA = 64
72613
MA = 64
51594
Ha = 193
310 n
mi
Hp = 180
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16680442
96 X = 5032260
77
Y = 14330061
55 feet Y = 4424366
86 meter
Z = 1836220
47 Z = 584253
08
XDOT = -9023
327926 XDOT = -2765
646957
YDOT = 13091
031968 feet/sec YDOT = 3959
305208 meter/sec
ZDOT = -19637
989635 ZDOT = -5999
057609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21656105
26 X = 6600780
88
Y = -3772984
17 feet Y = -1150005
58 meter
Z = 1933194
81 Z = 589237
78
XDOT = 4177
240080 XDOT = 1273
222776
YDOT = 13616
471703 feet/sec YDOT = 4150
300575 meter/sec
ZDOT = -19690
467782 ZDOT = -6001
654580
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 09254
20245002
00020000 00000-0 20000-3 0 9116
2 25544 51
6407 225
2735 0009053 78
9933 281
2248 15
74036566 19502
Satellite: ISS
Catalog Number: 25544
Epoch time: 09254
20245002 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 225
2735 deg
Eccentricity:
0009053
Arg of perigee: 78
9933 deg
Mean anomaly: 281
2248 deg
Mean motion: 15
74036566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1950
Checksum: 280
Coasting Arc #13 (Orbit 1965)
---------------------------------------
Vector Time (GMT): 2009/255/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2109604
53 A = 6719938
61 meter
Y = -3656134
40 meter E =
0011497
Z = 5218881
06 I = 51
40837
XDOT = 6243
215939 Wp = 90
66180
YDOT = 4482
768658 meter/sec RA = 219
34331 deg
ZDOT = 615
482100 TA = 353
46903
MA = 353
48401
Ha = 193
115 n
mi
Hp = 180
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6921274
71 X = 2124978
78
Y = -11995191
61 feet Y = -3632457
67 meter
Z = 17122313
19 Z = 5229166
86
XDOT = 20482
991927 XDOT = 6189
634923
YDOT = 14707
246252 feet/sec YDOT = 4552
284374 meter/sec
ZDOT = 2019
298227 ZDOT = 645
681668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5152782
83 X = -1570568
21
Y = -12800679
92 feet Y = -3901647
24 meter
Z = 17162566
74 Z = 5231150
34
XDOT = 23313
651263 XDOT = 7106
000905
YDOT = -6511
869129 feet/sec YDOT = -1984
817711 meter/sec
ZDOT = 2138
436752 ZDOT = 651
795522
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 09255
21824409
00020000 00000-0 20000-3 0 9123
2 25544 51
6411 220
0563 0008936 82
2136 278
0042 15
74101959 19663
Satellite: ISS
Catalog Number: 25544
Epoch time: 09255
21824409 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 220
0563 deg
Eccentricity:
0008936
Arg of perigee: 82
2136 deg
Mean anomaly: 278
0042 deg
Mean motion: 15
74101959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1966
Checksum: 278
Coasting Arc #14 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2009/256/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5766015
93 A = 6731907
08 meter
Y = -3427116
55 meter E =
0018690
Z = -508031
20 I = 51
47165
XDOT = 2078
715040 Wp = 60
73100
YDOT = -4360
528001 meter/sec RA = 214
18320 deg
ZDOT = 5997
072430 TA = 293
72904
MA = 293
92500
Ha = 193
275 n
mi
Hp = 180
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18917375
08 X = -5724796
85
Y = -11243820
69 feet Y = -3491365
05 meter
Z = -1666769
04 Z = -535942
39
XDOT = 6819
931234 XDOT = 2098
188059
YDOT = -14306
194230 feet/sec YDOT = -4337
173771 meter/sec
ZDOT = 19675
434482 ZDOT = 6007
218071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20424898
28 X = -6225509
00
Y = 8169151
33 feet Y = 2489957
32 meter
Z = -1776850
99 Z = -541584
18
XDOT = -6681
559327 XDOT = -2036
539283
YDOT = -12534
068726 feet/sec YDOT = -3820
384148 meter/sec
ZDOT = 19715
094288 ZDOT = 6009
160739
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 09256
17054268
00020000 00000-0 20000-3 0 9138
2 25544 51
6406 215
1661 0009042 84
4196 275
7998 15
74048457 19814
Satellite: ISS
Catalog Number: 25544
Epoch time: 09256
17054268 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 215
1661 deg
Eccentricity:
0009042
Arg of perigee: 84
4196 deg
Mean anomaly: 275
7998 deg
Mean motion: 15
74048457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1981
Checksum: 314
Coasting Arc #15 (Orbit 1996)
---------------------------------------
Vector Time (GMT): 2009/257/04:04:04
831
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1544020
02 A = 6719983
13 meter
Y = 3927187
58 meter E =
0023837
Z = -5250407
51 I = 51
45617
XDOT = -6886
412392 Wp = 87
33105
YDOT = -3371
041669 meter/sec RA = 209
04400 deg
ZDOT = -497
185270 TA = 177
92812
MA = 177
91822
Ha = 193
228 n
mi
Hp = 180
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5065682
47 X = -1562314
36
Y = 12884473
67 feet Y = 3909819
12 meter
Z = -17225746
43 Z = -5257952
78
XDOT = -22593
216508 XDOT = -6845
789785
YDOT = -11059
847995 feet/sec YDOT = -3447
822452 meter/sec
ZDOT = -1631
185270 ZDOT = -530
540581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7408591
38 X = 2258138
65
Y = 11651955
51 feet Y = 3551516
04 meter
Z = -17255197
70 Z = -5259384
26
XDOT = -21469
056911 XDOT = -6543
768546
YDOT = 11044
295350 feet/sec YDOT = 3366
301223 meter/sec
ZDOT = -1762
712710 ZDOT = -537
274834
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 09257
18631463
00020000 00000-0 20000-3 0 9149
2 25544 51
6397 209
9488 0008945 88
9224 271
2964 15
74078605 19972
Satellite: ISS
Catalog Number: 25544
Epoch time: 09257
18631463 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 209
9488 deg
Eccentricity:
0008945
Arg of perigee: 88
9224 deg
Mean anomaly: 271
2964 deg
Mean motion: 15
74078605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1997
Checksum: 343
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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