Date:
April 28th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 3797)
---------------------------------------
Vector Time (GMT): 2009/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6142773
21 A = 6733374
23 meter
Y = 591615
32 meter E =
0005149
Z = 2689974
23 I = 51
50476
XDOT = 1749
419137 Wp = 82
88093
YDOT = 5418
073641 meter/sec RA = 205
78469 deg
ZDOT = -5177
468923 TA = 66
41910
MA = 66
36503
Ha = 191
582 n
mi
Hp = 189
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20153455
41 X = 6122633
46
Y = 1940995
14 feet Y = 660194
58 meter
Z = 8825374
77 Z = 2719767
52
XDOT = 5739
564097 XDOT = 1713
854996
YDOT = 17775
832154 feet/sec YDOT = 5437
438209 meter/sec
ZDOT = -16986
446598 ZDOT = -5169
056056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17606970
76 X = 5366604
69
Y = -9892133
80 feet Y = -3015122
38 meter
Z = 8941853
08 Z = 2725476
82
XDOT = 14225
810240 XDOT = 4336
026961
YDOT = 9969
297320 feet/sec YDOT = 3038
641823 meter/sec
ZDOT = -16953
164495 ZDOT = -5167
324538
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 09117
53727279
00010596 00000-0 82463-4 0 9000
2 25544 51
6408 206
6130 0008882 291
7304 68
2913 15
72447891 37980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09117
53727279 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 206
6130 deg
Eccentricity:
0008882
Arg of perigee: 291
7304 deg
Mean anomaly: 68
2913 deg
Mean motion: 15
72447891 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3798
Checksum: 330
Coasting Arc #2 (Orbit 3813)
---------------------------------------
Vector Time (GMT): 2009/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2502465
26 A = 6728634
19 meter
Y = -4565955
78 meter E =
0001690
Z = 4260158
68 I = 51
51610
XDOT = 6820
846903 Wp = 56
63332
YDOT = -433
156829 meter/sec RA = 200
69867 deg
ZDOT = 3542
298759 TA = 357
36180
MA = 357
36269
Ha = 191
760 n
mi
Hp = 188
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8210187
86 X = -2471917
35
Y = -14980169
89 feet Y = -4593769
39 meter
Z = 13976898
55 Z = 4248075
32
XDOT = 22378
106637 XDOT = 6807
975512
YDOT = -1421
118207 feet/sec YDOT = -356
954432 meter/sec
ZDOT = 11621
715089 ZDOT = 3575
403582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15490945
63 X = -4721640
23
Y = -7291825
89 feet Y = -2222548
53 meter
Z = 13929330
44 Z = 4245659
92
XDOT = 16724
892176 XDOT = 5097
747135
YDOT = -13082
515746 feet/sec YDOT = -3987
550799 meter/sec
ZDOT = 11751
076952 ZDOT = 3581
728255
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 09118
55409624
00010596 00000-0 82463-4 0 9015
2 25544 51
6407 201
4024 0009011 295
6797 64
3434 15
72495225 38146
Satellite: ISS
Catalog Number: 25544
Epoch time: 09118
55409624 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 201
4024 deg
Eccentricity:
0009011
Arg of perigee: 295
6797 deg
Mean anomaly: 64
3434 deg
Mean motion: 15
72495225 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3814
Checksum: 301
Coasting Arc #3 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2009/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5610346
96 A = 6731071
45 meter
Y = 1306336
00 meter E =
0004807
Z = -3475879
68 I = 51
55201
XDOT = -3930
670109 Wp = 327
13854
YDOT = -4825
598116 meter/sec RA = 195
51775 deg
ZDOT = 4531
863350 TA = 351
58644
MA = 351
59449
Ha = 191
835 n
mi
Hp = 188
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18406650
13 X = -5607652
33
Y = 4285879
27 feet Y = 1243613
21 meter
Z = -11403804
72 Z = -3503128
29
XDOT = -12895
899307 XDOT = -3898
432461
YDOT = -15832
014815 feet/sec YDOT = -4869
373325 meter/sec
ZDOT = 14868
318077 ZDOT = 4512
845872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12114550
50 X = -3692514
99
Y = 14421255
84 feet Y = 4395598
78 meter
Z = -11510227
55 Z = -3508317
36
XDOT = -18828
236415 XDOT = -5738
846459
YDOT = -4011
919604 feet/sec YDOT = -1222
833095 meter/sec
ZDOT = 14793
616750 ZDOT = 4509
094385
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 09119
50735746
00010596 00000-0 82463-4 0 9029
2 25544 51
6398 196
5188 0009009 299
9999 60
0269 15
72509991 38299
Satellite: ISS
Catalog Number: 25544
Epoch time: 09119
50735746 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 196
5188 deg
Eccentricity:
0009009
Arg of perigee: 299
9999 deg
Mean anomaly: 60
0269 deg
Mean motion: 15
72509991 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3829
Checksum: 368
Coasting Arc #4 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2009/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4274996
64 A = 6730777
23 meter
Y = 3719896
00 meter E =
0006275
Z = -3635520
97 I = 51
57884
XDOT = -5844
879701 Wp = 341
80206
YDOT = 2443
512527 meter/sec RA = 190
43994 deg
ZDOT = -4364
872395 TA = 241
76580
MA = 241
82917
Ha = 192
174 n
mi
Hp = 188
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14025579
52 X = 4250743
16
Y = 12204383
21 feet Y = 3767566
18 meter
Z = -11927562
23 Z = -3614811
59
XDOT = -19176
114506 XDOT = -5850
565243
YDOT = 8016
773384 feet/sec YDOT = 2378
120224 meter/sec
ZDOT = -14320
447491 ZDOT = -4393
280524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18616837
57 X = 5674412
09
Y = 1004357
95 feet Y = 306128
30 meter
Z = -11846316
51 Z = -3610757
27
XDOT = -10099
366365 XDOT = -3078
286868
YDOT = 16679
122782 feet/sec YDOT = 5083
796624 meter/sec
ZDOT = -14431
332942 ZDOT = -4398
670281
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 09120
52415573
00010596 00000-0 82463-4 0 9037
2 25544 51
6391 191
3085 0009004 304
4763 55
5548 15
72506139 38455
Satellite: ISS
Catalog Number: 25544
Epoch time: 09120
52415573 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 191
3085 deg
Eccentricity:
0009004
Arg of perigee: 304
4763 deg
Mean anomaly: 55
5548 deg
Mean motion: 15
72506139 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3845
Checksum: 302
Coasting Arc #5 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2009/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4482070
04 A = 6728780
36 meter
Y = -2867747
53 meter E =
0008914
Z = 4121948
96 I = 51
60323
XDOT = 5717
865396 Wp = 19
09552
YDOT = 3518
218958 meter/sec RA = 185
26098 deg
ZDOT = -3759
140122 TA = 109
51584
MA = 109
41954
Ha = 192
288 n
mi
Hp = 187
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14704954
21 X = 4493780
87
Y = -9408620
51 feet Y = -2817561
16 meter
Z = 13523454
58 Z = 4143751
15
XDOT = 18759
400906 XDOT = 5696
360344
YDOT = 11542
713118 feet/sec YDOT = 3582
039430 meter/sec
ZDOT = -12333
136882 ZDOT = -3731
414763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5507405
56 X = 1678657
21
Y = -16496033
88 feet Y = -5027991
13 meter
Z = 13608489
72 Z = 4147867
67
XDOT = 20705
675890 XDOT = 6311
090011
YDOT = -3200
187242 feet/sec YDOT = -975
417071 meter/sec
ZDOT = -12224
460421 ZDOT = -3726
015536
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 09121
54093834
00010596 00000-0 82463-4 0 9043
2 25544 51
6399 186
0978 0009202 309
0424 50
9919 15
72572576 38617
Satellite: ISS
Catalog Number: 25544
Epoch time: 09121
54093834 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 186
0978 deg
Eccentricity:
0009202
Arg of perigee: 309
0424 deg
Mean anomaly: 50
9919 deg
Mean motion: 15
72572576 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3861
Checksum: 330
Coasting Arc #6 (Orbit 3876)
---------------------------------------
Vector Time (GMT): 2009/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5598110
74 A = 6732681
76 meter
Y = -2324114
74 meter E =
0010619
Z = 2914275
73 I = 51
64510
XDOT = 4269
691095 Wp = 39
79343
YDOT = -3969
675614 meter/sec RA = 180
18432 deg
ZDOT = 5033
922905 TA = 353
74981
MA = 353
76305
Ha = 192
598 n
mi
Hp = 187
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18366505
06 X = -5585863
07
Y = -7625048
36 feet Y = -2386647
69 meter
Z = 9561272
07 Z = 2887109
77
XDOT = 14008
172884 XDOT = 4289
309439
YDOT = -13023
870125 feet/sec YDOT = -3921
819895 meter/sec
ZDOT = 16515
495096 ZDOT = 5054
712613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19036647
84 X = -5802370
26
Y = 5924477
83 feet Y = 1805780
84 meter
Z = 9454860
95 Z = 2881841
62
XDOT = 2793
219665 XDOT = 851
373354
YDOT = -17521
949785 feet/sec YDOT = -5340
690294 meter/sec
ZDOT = 16596
494257 ZDOT = 5058
611449
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 09122
55771013
00010596 00000-0 82463-4 0 9058
2 25544 51
6395 180
8872 0009028 313
8661 46
1755 15
72556031 38770
Satellite: ISS
Catalog Number: 25544
Epoch time: 09122
55771013 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 180
8872 deg
Eccentricity:
0009028
Arg of perigee: 313
8661 deg
Mean anomaly: 46
1755 deg
Mean motion: 15
72556031 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3877
Checksum: 318
Coasting Arc #7 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2009/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2882685
96 A = 6726817
90 meter
Y = 3932634
37 meter E =
0005226
Z = -4636177
02 I = 51
65550
XDOT = -6932
571450 Wp = 52
97133
YDOT = -1686
382235 meter/sec RA = 175
01526 deg
ZDOT = 2885
381868 TA = 245
55812
MA = 245
61264
Ha = 192
667 n
mi
Hp = 187
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9457631
10 X = -2903925
30
Y = 12902343
72 feet Y = 3900279
78 meter
Z = -15210554
52 Z = -4650232
70
XDOT = -22744
656988 XDOT = -6927
215507
YDOT = -5532
750115 feet/sec YDOT = -1763
876380 meter/sec
ZDOT = 9466
475946 ZDOT = 2851
716310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1326246
92 X = 404240
06
Y = 15890002
44 feet Y = 4843272
74 meter
Z = -15265225
84 Z = -4652840
83
XDOT = -19723
096698 XDOT = -6011
599873
YDOT = 10597
138088 feet/sec YDOT = 3230
007689 meter/sec
ZDOT = 9334
684750 ZDOT = 2845
211912
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 09123
51092052
00010596 00000-0 82463-4 0 9065
2 25544 51
6395 176
0024 0009101 318
3091 41
7377 15
72580292 38929
Satellite: ISS
Catalog Number: 25544
Epoch time: 09123
51092052 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 176
0024 deg
Eccentricity:
0009101
Arg of perigee: 318
3091 deg
Mean anomaly: 41
7377 deg
Mean motion: 15
72580292 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3892
Checksum: 294
Coasting Arc #8 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2009/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6364428
70 A = 6734225
42 meter
Y = 576152
20 meter E =
0002660
Z = -2127626
35 I = 51
71061
XDOT = -2287
102949 Wp = 331
89869
YDOT = 4837
110210 meter/sec RA = 169
93415 deg
ZDOT = -5526
513144 TA = 231
83361
MA = 231
85757
Ha = 192
849 n
mi
Hp = 187
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20880671
58 X = 6367848
75
Y = 1890263
14 feet Y = 647342
09 meter
Z = -6980401
41 Z = -2096699
39
XDOT = -7503
618598 XDOT = -2314
175325
YDOT = 15869
784154 feet/sec YDOT = 4811
383132 meter/sec
ZDOT = -18131
604803 ZDOT = -5537
689729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16868143
48 X = 5141410
13
Y = -12518624
11 feet Y = -3815676
63 meter
Z = -6859397
19 Z = -2090744
26
XDOT = 4132
745137 XDOT = 1259
660718
YDOT = 15536
658867 feet/sec YDOT = 4735
573623 meter/sec
ZDOT = -18174
950803 ZDOT = -5539
725005
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 09124
52766529
00010596 00000-0 82463-4 0 9075
2 25544 51
6401 170
7918 0009087 322
8368 37
2164 15
72613486 39084
Satellite: ISS
Catalog Number: 25544
Epoch time: 09124
52766529 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 170
7918 deg
Eccentricity:
0009087
Arg of perigee: 322
8368 deg
Mean anomaly: 37
2164 deg
Mean motion: 15
72613486 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3908
Checksum: 329
Coasting Arc #9 (Orbit 3923)
---------------------------------------
Vector Time (GMT): 2009/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1084787
22 A = 6725200
47 meter
Y = -4378891
36 meter E =
0010867
Z = 4991096
49 I = 51
70867
XDOT = 7428
952918 Wp = 358
65571
YDOT = -412
591371 meter/sec RA = 164
77969 deg
ZDOT = -1966
054502 TA = 110
39829
MA = 110
28153
Ha = 192
944 n
mi
Hp = 186
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3559013
20 X = 1109425
93
Y = -14366441
48 feet Y = -4366622
91 meter
Z = 16374988
49 Z = 4996426
28
XDOT = 24373
205111 XDOT = 7442
565308
YDOT = -1353
646230 feet/sec YDOT = -329
440360 meter/sec
ZDOT = -6450
310045 ZDOT = -1929
931107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7203300
59 X = -2195566
02
Y = -12903539
30 feet Y = -3932998
78 meter
Z = 16395505
43 Z = 4997350
05
XDOT = 16071
492950 XDOT = 4898
591051
YDOT = -17032
203813 feet/sec YDOT = -5191
415722 meter/sec
ZDOT = -6309
048033 ZDOT = -1922
997841
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 09125
54439567
00010596 00000-0 82463-4 0 9088
2 25544 51
6392 165
5812 0009146 326
5251 33
5332 15
72643583 39241
Satellite: ISS
Catalog Number: 25544
Epoch time: 09125
54439567 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 165
5812 deg
Eccentricity:
0009146
Arg of perigee: 326
5251 deg
Mean anomaly: 33
5332 deg
Mean motion: 15
72643583 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3924
Checksum: 319
Coasting Arc #10 (Orbit 3939)
---------------------------------------
Vector Time (GMT): 2009/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6467750
21 A = 6735468
81 meter
Y = 1305599
20 meter E =
0017126
Z = 1295580
23 I = 51
77080
XDOT = 170
654183 Wp = 26
62509
YDOT = -4991
866977 meter/sec RA = 159
68941 deg
ZDOT = 5867
689618 TA = 347
57303
MA = 347
61521
Ha = 193
328 n
mi
Hp = 186
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21219652
91 X = -6488162
74
Y = 4283461
94 feet Y = 1233158
88 meter
Z = 4250591
31 Z = 1264109
79
XDOT = 559
889052 XDOT = 197
956715
YDOT = -16377
516329 feet/sec YDOT = -4989
806084 meter/sec
ZDOT = 19250
950189 ZDOT = 5868
584889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12394698
00 X = -3777903
95
Y = 17777056
23 feet Y = 5418446
74 meter
Z = 4127587
16 Z = 1258088
57
XDOT = -9697
369880 XDOT = -2955
758339
YDOT = -11243
372582 feet/sec YDOT = -3426
979963 meter/sec
ZDOT = 19254
081127 ZDOT = 5868
643928
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 09126
56111601
00010596 00000-0 82463-4 0 9098
2 25544 51
6390 160
3700 0009238 332
1946 27
8721 15
72605293 39406
Satellite: ISS
Catalog Number: 25544
Epoch time: 09126
56111601 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 160
3700 deg
Eccentricity:
0009238
Arg of perigee: 332
1946 deg
Mean anomaly: 27
8721 deg
Mean motion: 15
72605293 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3940
Checksum: 294
Coasting Arc #11 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2009/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 764360
81 A = 6724262
70 meter
Y = 4186620
40 meter E =
0012313
Z = -5214230
65 I = 51
76150
XDOT = -7188
547101 Wp = 58
88821
YDOT = 2547
960335 meter/sec RA = 154
55279 deg
ZDOT = 999
996972 TA = 220
59315
MA = 220
68502
Ha = 193
335 n
mi
Hp = 186
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2507745
45 X = 742818
83
Y = 13735631
24 feet Y = 4195047
70 meter
Z = -17107055
95 Z = -5210569
47
XDOT = -23584
472117 XDOT = -7221
362454
YDOT = 8359
449918 feet/sec YDOT = 2467
390284 meter/sec
ZDOT = 3280
829960 ZDOT = 964
994679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11514338
11 X = 3509570
26
Y = 7929478
20 feet Y = 2416904
96 meter
Z = -17092428
42 Z = -5209772
18
XDOT = -10318
699944 XDOT = -3145
139743
YDOT = 21704
612463 feet/sec YDOT = 6615
565879 meter/sec
ZDOT = 3144
089475 ZDOT = 958
318472
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 09127
51427509
00010596 00000-0 82463-4 0 9103
2 25544 51
6395 155
4848 0009191 334
5969 25
4739 15
72645585 39555
Satellite: ISS
Catalog Number: 25544
Epoch time: 09127
51427509 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 155
4848 deg
Eccentricity:
0009191
Arg of perigee: 334
5969 deg
Mean anomaly: 25
4739 deg
Mean motion: 15
72645585 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3955
Checksum: 348
Coasting Arc #12 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2009/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5965006
65 A = 6735841
63 meter
Y = -3094607
79 meter E =
0004280
Z = -466638
11 I = 51
82577
XDOT = 1826
249962 Wp = 88
98594
YDOT = 4421
399175 meter/sec RA = 149
45045 deg
ZDOT = -6023
850638 TA = 96
06949
MA = 96
02071
Ha = 193
417 n
mi
Hp = 186
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19570231
79 X = 6001434
63
Y = -10152912
70 feet Y = -3027699
90 meter
Z = -1530964
92 Z = -437571
18
XDOT = 5991
633733 XDOT = 1805
936816
YDOT = 14505
902805 feet/sec YDOT = 4441
708180 meter/sec
ZDOT = -19763
289494 ZDOT = -6015
027577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6412933
14 X = 1954662
02
Y = -21101766
13 feet Y = -6431818
32 meter
Z = -1417468
46 Z = -432044
39
XDOT = 13105
905833 XDOT = 3994
680098
YDOT = 5296
919824 feet/sec YDOT = 1614
501162 meter/sec
ZDOT = -19728
456200 ZDOT = -6013
233450
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 09128
53096670
00010596 00000-0 82463-4 0 9118
2 25544 51
6383 150
2733 0009144 339
2835 20
7955 15
72682015 39715
Satellite: ISS
Catalog Number: 25544
Epoch time: 09128
53096670 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 150
2733 deg
Eccentricity:
0009144
Arg of perigee: 339
2835 deg
Mean anomaly: 20
7955 deg
Mean motion: 15
72682015 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3971
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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