Date:
January 26th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8342 03 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 2319)
---------------------------------------
Vector Time (GMT): 2009/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953301
39 A = 6730662
46 meter
Y = 4255055
71 meter E =
0007692
Z = 5131528
05 I = 51
44350
XDOT = -6876
488594 Wp = 332
68670
YDOT = 3172
134079 meter/sec RA = 327
08606 deg
ZDOT = -1346
934733 TA = 130
28711
MA = 130
21985
Ha = 194
907 n
mi
Hp = 191
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3127629
22 X = 880722
30
Y = 13960156
53 feet Y = 4265309
72 meter
Z = 16835721
94 Z = 5135983
25
XDOT = -22560
658116 XDOT = -6904
905821
YDOT = 10407
264038 feet/sec YDOT = 3095
078449 meter/sec
ZDOT = -4419
077208 ZDOT = -1380
408697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10198862
81 X = -3108613
38
Y = 10002915
60 feet Y = 3048888
67 meter
Z = 16853321
48 Z = 5136892
39
XDOT = -20084
544777 XDOT = -6121
769248
YDOT = -12780
564071 feet/sec YDOT = -3895
515929 meter/sec
ZDOT = -4549
210475 ZDOT = -1386
599353
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 09023
54538315
00010596 00000-0 82463-4 0 9008
2 25544 51
6413 327
4020 0008306 301
2044 58
8303 15
70524959 23202
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023
54538315 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 327
4020 deg
Eccentricity:
0008306
Arg of perigee: 301
2044 deg
Mean anomaly: 58
8303 deg
Mean motion: 15
70524959 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2320
Checksum: 270
Coasting Arc #2 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2009/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5333237
41 A = 6742035
83 meter
Y = -4109284
87 meter E =
0013529
Z = 60512
15 I = 51
45778
XDOT = 2884
184743 Wp = 8
58497
YDOT = 3834
264246 meter/sec RA = 321
97534 deg
ZDOT = 6021
649532 TA = 352
07341
MA = 352
09476
Ha = 195
042 n
mi
Hp = 191
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17497498
07 X = 5378497
79
Y = -13481905
75 feet Y = -4049392
46 meter
Z = 198530
68 Z = 86529
92
XDOT = 9462
548371 XDOT = 2811
843653
YDOT = 12579
607105 feet/sec YDOT = 3866
111813 meter/sec
ZDOT = 19756
068019 ZDOT = 6035
485212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20859119
50 X = 6357859
62
Y = 7264366
61 feet Y = 2214178
94 meter
Z = 299578
77 Z = 91311
61
XDOT = -4882
317291 XDOT = -1488
130310
YDOT = 13187
958270 feet/sec YDOT = 4019
689681 meter/sec
ZDOT = 19810
169242 ZDOT = 6038
139585
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 09024
56345741
00010596 00000-0 82463-4 0 9011
2 25544 51
6411 322
2002 0008359 305
0762 54
9615 15
70542617 23361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024
56345741 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 322
2002 deg
Eccentricity:
0008359
Arg of perigee: 305
0762 deg
Mean anomaly: 54
9615 deg
Mean motion: 15
70542617 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2336
Checksum: 282
Coasting Arc #3 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2009/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3799624
99 A = 6730341
84 meter
Y = -2082782
41 meter E =
0010686
Z = -5157852
72 I = 51
39711
XDOT = 4842
883580 Wp = 45
32056
YDOT = -5850
360176 meter/sec RA = 316
86041 deg
ZDOT = -1199
304176 TA = 213
13281
MA = 213
19978
Ha = 195
145 n
mi
Hp = 190
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12465961
25 X = -3750997
35
Y = -6833275
61 feet Y = -2124999
71 meter
Z = -16922088
97 Z = -5176192
84
XDOT = 15888
725655 XDOT = 4913
769183
YDOT = -19194
095067 feet/sec YDOT = -5795
807804 meter/sec
ZDOT = -3934
724987 ZDOT = -1175
606388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1292212
86 X = -393866
48
Y = -14071168
21 feet Y = -4288892
07 meter
Z = -16993626
79 Z = -5179657
45
XDOT = 23791
070671 XDOT = 7251
518341
YDOT = 2479
272095 feet/sec YDOT = 755
682134 meter/sec
ZDOT = -3842
820175 ZDOT = -1171
291589
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 09025
51789048
00010596 00000-0 82463-4 0 9020
2 25544 51
6418 317
3240 0008338 308
9479 51
0939 15
70573554 23519
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025
51789048 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 317
3240 deg
Eccentricity:
0008338
Arg of perigee: 308
9479 deg
Mean anomaly: 51
0939 deg
Mean motion: 15
70573554 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2351
Checksum: 319
Coasting Arc #4 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2009/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2858329
03 A = 6740030
92 meter
Y = 5728890
95 meter E =
0007061
Z = 2102097
89 I = 51
40932
XDOT = -5328
827651 Wp = 83
63482
YDOT = -630
509999 meter/sec RA = 311
70583 deg
ZDOT = -5510
901856 TA = 72
84306
MA = 72
76576
Ha = 195
365 n
mi
Hp = 190
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9377719
91 X = -2932389
31
Y = 18795573
99 feet Y = 5696513
24 meter
Z = 6896646
62 Z = 2088032
98
XDOT = -17483
030352 XDOT = -5294
610945
YDOT = -2068
602359 feet/sec YDOT = -689
908395 meter/sec
ZDOT = -18080
386667 ZDOT = -5536
705483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20789770
33 X = -6336722
00
Y = 3122187
95 feet Y = 951642
89 meter
Z = 6842248
07 Z = 2085517
21
XDOT = -8086
813337 XDOT = -2464
860705
YDOT = -13883
990203 feet/sec YDOT = -4231
840214 meter/sec
ZDOT = -18180
897305 ZDOT = -5541
537498
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 09026
53594052
00010596 00000-0 82463-4 0 9033
2 25544 51
6420 312
1228 0008355 312
7447 47
3010 15
70584519 23676
Satellite: ISS
Catalog Number: 25544
Epoch time: 09026
53594052 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 312
1228 deg
Eccentricity:
0008355
Arg of perigee: 312
7447 deg
Mean anomaly: 47
3010 deg
Mean motion: 15
70584519 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2367
Checksum: 289
Coasting Arc #5 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2009/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5078978
23 A = 6733819
29 meter
Y = -1104599
13 meter E =
0004569
Z = 4276318
62 I = 51
36991
XDOT = -1490
087061 Wp = 49
28624
YDOT = 6692
167357 meter/sec RA = 306
62172 deg
ZDOT = 3498
897122 TA = 5
13288
MA = 5
12820
Ha = 195
369 n
mi
Hp = 190
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16663314
42 X = 5070179
57
Y = -3624012
89 feet Y = -1047852
40 meter
Z = 14029916
72 Z = 4300970
18
XDOT = -4888
737078 XDOT = -1581
805761
YDOT = 21955
929648 feet/sec YDOT = 6674
991382 meter/sec
ZDOT = 11479
321268 ZDOT = 3491
435956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12705841
94 X = 3872740
62
Y = 11254357
81 feet Y = 3430328
26 meter
Z = 14125830
62 Z = 4305553
17
XDOT = -19832
880984 XDOT = -6045
062124
YDOT = 8020
491404 feet/sec YDOT = 2444
645780 meter/sec
ZDOT = 11450
707681 ZDOT = 3490
175701
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 09027
55397777
00010596 00000-0 82463-4 0 9042
2 25544 51
6418 306
9212 0008346 316
5360 43
5142 15
70604586 23832
Satellite: ISS
Catalog Number: 25544
Epoch time: 09027
55397777 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 306
9212 deg
Eccentricity:
0008346
Arg of perigee: 316
5360 deg
Mean anomaly: 43
5142 deg
Mean motion: 15
70604586 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2383
Checksum: 314
Coasting Arc #6 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2009/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -283135
69 A = 6735231
08 meter
Y = -5492099
67 meter E =
0004712
Z = -3885620
34 I = 51
35851
XDOT = 5728
338007 Wp = 11
47209
YDOT = -3158
425962 meter/sec RA = 301
44231 deg
ZDOT = 4052
233170 TA = 300
89905
MA = 300
94537
Ha = 195
592 n
mi
Hp = 190
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -928922
88 X = -202825
94
Y = -18018699
72 feet Y = -5494816
77 meter
Z = -12748098
23 Z = -3886800
79
XDOT = 18793
759866 XDOT = 5743
545812
YDOT = -10362
289900 feet/sec YDOT = -3094
283390 meter/sec
ZDOT = 13294
728247 ZDOT = 4080
097591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13850586
20 X = 4221658
67
Y = -11557295
74 feet Y = -3522663
74 meter
Z = -12753063
27 Z = -3887133
68
XDOT = 18715
750263 XDOT = 5704
560680
YDOT = 7659
240397 feet/sec YDOT = 2334
536473 meter/sec
ZDOT = 13403
012859 ZDOT = 4085
238319
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 09028
50837642
00010596 00000-0 82463-4 0 9059
2 25544 51
6421 302
0447 0008401 320
3171 39
7375 15
70631080 23988
Satellite: ISS
Catalog Number: 25544
Epoch time: 09028
50837642 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 302
0447 deg
Eccentricity:
0008401
Arg of perigee: 320
3171 deg
Mean anomaly: 39
7375 deg
Mean motion: 15
70631080 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2398
Checksum: 287
Coasting Arc #7 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2009/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494424
62 A = 6738606
39 meter
Y = 4251902
19 meter E =
0004225
Z = -2675420
80 I = 51
35597
XDOT = -1968
832326 Wp = 346
52079
YDOT = -5338
500533 meter/sec RA = 296
36087 deg
ZDOT = -5171
071963 TA = 224
02180
MA = 224
05545
Ha = 195
776 n
mi
Hp = 190
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14745487
59 X = -4528639
64
Y = 13949810
32 feet Y = 4201451
61 meter
Z = -8777627
30 Z = -2697337
33
XDOT = -6459
423641 XDOT = -1883
870446
YDOT = -17514
765529 feet/sec YDOT = -5360
042121 meter/sec
ZDOT = -16965
459196 ZDOT = -5180
429955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20045157
50 X = -6109764
00
Y = -2952634
84 feet Y = -899963
10 meter
Z = -8862672
39 Z = -2701342
54
XDOT = 9639
724553 XDOT = 2938
188044
YDOT = -14353
445488 feet/sec YDOT = -4374
930185 meter/sec
ZDOT = -17002
262862 ZDOT = -5182
289720
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 09029
52638953
00010596 00000-0 82463-4 0 9067
2 25544 51
6423 296
8430 0008458 323
6958 36
3628 15
70636552 24145
Satellite: ISS
Catalog Number: 25544
Epoch time: 09029
52638953 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 296
8430 deg
Eccentricity:
0008458
Arg of perigee: 323
6958 deg
Mean anomaly: 36
3628 deg
Mean motion: 15
70636552 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2414
Checksum: 332
Coasting Arc #8 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2009/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2927287
05 A = 6730808
93 meter
Y = 3467114
34 meter E =
0010509
Z = 4974250
90 I = 51
31762
XDOT = -4076
302940 Wp =
88374
YDOT = 6231
054191 meter/sec RA = 291
19056 deg
ZDOT = -1933
852813 TA = 107
95889
MA = 107
84430
Ha = 195
832 n
mi
Hp = 189
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9603960
14 X = 2864136
08
Y = 11375047
05 feet Y = 3499495
92 meter
Z = 16319720
79 Z = 4988317
97
XDOT = -13373
697310 XDOT = -4136
282526
YDOT = 20443
091179 feet/sec YDOT = 6185
135222 meter/sec
ZDOT = -6344
661460 ZDOT = -1953
800872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2831220
78 X = -862956
09
Y = 14553805
27 feet Y = 4435999
85 meter
Z = 16374735
83 Z = 4991019
48
XDOT = -23214
887498 XDOT = -7075
897710
YDOT = 2747
595860 feet/sec YDOT = 837
467218 meter/sec
ZDOT = -6421
897955 ZDOT = -1957
394497
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 09030
54438933
00010596 00000-0 82463-4 0 9078
2 25544 51
6417 291
6409 0008583 327
5640 32
4993 15
70696122 24306
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54438933 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 291
6409 deg
Eccentricity:
0008583
Arg of perigee: 327
5640 deg
Mean anomaly: 32
4993 deg
Mean motion: 15
70696122 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 314
Coasting Arc #9 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2009/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2339454
07 A = 6741488
70 meter
Y = -6278577
91 meter E =
0017010
Z = 636217
66 I = 51
34409
XDOT = 4329
390191 Wp = 21
84737
YDOT = 2221
727724 meter/sec RA = 286
07988 deg
ZDOT = 5970
053468 TA = 345
10531
MA = 345
15535
Ha = 196
023 n
mi
Hp = 189
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7675374
24 X = 2406397
70
Y = -20599008
88 feet Y = -6252042
47 meter
Z = 2087328
29 Z = 647745
22
XDOT = 14204
036060 XDOT = 4275
223660
YDOT = 7289
132954 feet/sec YDOT = 2269
838665 meter/sec
ZDOT = 19586
789592 ZDOT = 5990
953764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20695050
97 X = 6307851
53
Y = -7399858
30 feet Y = -2255476
81 meter
Z = 2131768
91 Z = 649763
16
XDOT = 2955
861355 XDOT = 900
946541
YDOT = 13965
617299 feet/sec YDOT = 4256
720153 meter/sec
ZDOT = 19668
325865 ZDOT = 5994
905724
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 09031
56237912
00010596 00000-0 82463-4 0 9086
2 25544 51
6419 286
4383 0008596 331
7489 28
3206 15
70672262 24460
Satellite: ISS
Catalog Number: 25544
Epoch time: 09031
56237912 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 286
4383 deg
Eccentricity:
0008596
Arg of perigee: 331
7489 deg
Mean anomaly: 28
3206 deg
Mean motion: 15
70672262 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2446
Checksum: 326
Coasting Arc #10 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2009/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4228200
46 A = 6729548
23 meter
Y = -247415
76 meter E =
0014269
Z = -5239827
74 I = 51
29750
XDOT = 1066
078488 Wp = 51
80831
YDOT = -7596
725844 meter/sec RA = 280
94458 deg
ZDOT = -493
773431 TA = 213
42527
MA = 213
51542
Ha = 196
088 n
mi
Hp = 189
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13872048
76 X = -4199665
70
Y = -811731
48 feet Y = -294538
38 meter
Z = -17191035
90 Z = -5260298
82
XDOT = 3497
632834 XDOT = 1153
345736
YDOT = -24923
641219 feet/sec YDOT = -7584
316396 meter/sec
ZDOT = -1619
991572 ZDOT = -488
382536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8435713
55 X = -2571205
49
Y = -10917136
43 feet Y = -3327543
18 meter
Z = -17270762
27 Z = -5264128
34
XDOT = 20298
714557 XDOT = 6187
048197
YDOT = -13114
256336 feet/sec YDOT = -3997
225331 meter/sec
ZDOT = -1599
542615 ZDOT = -487
540589
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 09032
51673154
00010596 00000-0 82463-4 0 9095
2 25544 51
6419 281
5612 0008623 335
0810 24
9935 15
70719874 24616
Satellite: ISS
Catalog Number: 25544
Epoch time: 09032
51673154 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 281
5612 deg
Eccentricity:
0008623
Arg of perigee: 335
0810 deg
Mean anomaly: 24
9935 deg
Mean motion: 15
70719874 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2461
Checksum: 311
Coasting Arc #11 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2009/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 515585
03 A = 6740679
68 meter
Y = 6557677
94 meter E =
0009322
Z = 1467988
14 I = 51
33019
XDOT = -4807
184346 Wp = 82
44372
YDOT = 1675
739736 meter/sec RA = 275
79266 deg
ZDOT = -5764
819327 TA = 81
35734
MA = 81
25175
Ha = 196
298 n
mi
Hp = 189
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1691551
95 X = 435086
51
Y = 21514691
40 feet Y = 6562993
39 meter
Z = 4816234
05 Z = 1470297
45
XDOT = -15771
602185 XDOT = -4797
561252
YDOT = 5497
833780 feet/sec YDOT = 1622
036950 meter/sec
ZDOT = -18913
449237 ZDOT = -5788
149017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14860919
65 X = -4529608
31
Y = 15646249
69 feet Y = 4768976
91 meter
Z = 4825696
05 Z = 1470872
16
XDOT = -13432
000262 XDOT = -4094
073680
YDOT = -6863
587799 feet/sec YDOT = -2092
021561 meter/sec
ZDOT = -19004
171117 ZDOT = -5792
471357
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 09033
53469790
00010596 00000-0 82463-4 0 9109
2 25544 51
6418 276
3589 0008496 338
9429 21
1382 15
70688122 24779
Satellite: ISS
Catalog Number: 25544
Epoch time: 09033
53469790 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 276
3589 deg
Eccentricity:
0008496
Arg of perigee: 338
9429 deg
Mean anomaly: 21
1382 deg
Mean motion: 15
70688122 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2477
Checksum: 338
Coasting Arc #12 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2009/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3758943
65 A = 6732074
18 meter
Y = -3091954
18 meter E =
0006530
Z = 4644863
85 I = 51
29989
XDOT = 2163
094288 Wp = 44
02756
YDOT = 6837
153683 meter/sec RA = 270
69335 deg
ZDOT = 2803
045208 TA = 18
17809
MA = 18
15475
Ha = 196
332 n
mi
Hp = 188
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12332492
30 X = 3770675
32
Y = -10144206
64 feet Y = -3049854
12 meter
Z = 15239054
62 Z = 4663152
98
XDOT = 7096
766038 XDOT = 2072
862777
YDOT = 22431
606571 feet/sec YDOT = 6860
838017 meter/sec
ZDOT = 9196
342545 ZDOT = 2813
334574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15770889
65 X = 4806967
17
Y = 2026193
28 feet Y = 617583
71 meter
Z = 15310050
97 Z = 4666503
54
XDOT = -11440
354369 XDOT = -3487
020012
YDOT = 19307
466194 feet/sec YDOT = 5884
915696 meter/sec
ZDOT = 9236
901611 ZDOT = 2815
407611
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 09034
55265046
00010596 00000-0 82463-4 0 9111
2 25544 51
6418 271
1559 0008704 342
9420 17
1448 15
70720617 24939
Satellite: ISS
Catalog Number: 25544
Epoch time: 09034
55265046 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 271
1559 deg
Eccentricity:
0008704
Arg of perigee: 342
9420 deg
Mean anomaly: 17
1448 deg
Mean motion: 15
70720617 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2493
Checksum: 300
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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