Date:
March 29th 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 3309)
---------------------------------------
Vector Time (GMT): 2009/086/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5840376
81 A = 6735270
99 meter
Y = 1733096
83 meter E =
0019462
Z = 2843637
45 I = 51
68009
XDOT = -3783
916535 Wp = 125
69382
YDOT = -4378
033295 meter/sec RA = 5
11986 deg
ZDOT = -5090
224577 TA = 21
68299
MA = 21
60070
Ha = 196
224 n
mi
Hp = 185
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19161341
23 X = -5873136
48
Y = 5686013
22 feet Y = 1667603
44 meter
Z = 9329519
21 Z = 2815184
98
XDOT = -12414
424327 XDOT = -3709
951845
YDOT = -14363
626296 feet/sec YDOT = -4419
934192 meter/sec
ZDOT = -16700
211867 ZDOT = -5108
426878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19504839
28 X = -5945075
01
Y = 4594282
61 feet Y = 1400337
34 meter
Z = 9218540
26 Z = 2809811
07
XDOT = -11153
669957 XDOT = -3399
638603
YDOT = -13612
745040 feet/sec YDOT = -4149
164688 meter/sec
ZDOT = -16771
574819 ZDOT = -5111
976005
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 09086
51668157
00010596 00000-0 82463-4 0 9002
2 25544 51
6419 5
4491 0009525 165
4871 194
6566 15
71711249 33106
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
51668157 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 5
4491 deg
Eccentricity:
0009525
Arg of perigee: 165
4871 deg
Mean anomaly: 194
6566 deg
Mean motion: 15
71711249 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3310
Checksum: 318
Coasting Arc #2 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2009/087/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398300
37 A = 6731634
72 meter
Y = 3164125
34 meter E =
0016967
Z = 3992616
07 I = 51
63875
XDOT = -5834
113802 Wp = 132
83979
YDOT = 3112
121325 meter/sec RA =
05223 deg
ZDOT = 3938
697126 TA = 276
32165
MA = 276
51486
Ha = 195
959 n
mi
Hp = 185
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14430119
32 X = 4343196
09
Y = 10380988
65 feet Y = 3213001
90 meter
Z = 13099134
07 Z = 4013849
14
XDOT = -19140
793314 XDOT = -5887
614137
YDOT = 10210
371800 feet/sec YDOT = 3046
582025 meter/sec
ZDOT = 12922
234666 ZDOT = 3910
224519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13936523
72 X = 4247852
43
Y = 10935370
99 feet Y = 3333101
08 meter
Z = 13182243
75 Z = 4017947
89
XDOT = -18802
942164 XDOT = -5731
136772
YDOT = 8433
757560 feet/sec YDOT = 2570
609304 meter/sec
ZDOT = 12811
270349 ZDOT = 3904
875202
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 09087
53398445
00010596 00000-0 82463-4 0 9016
2 25544 51
6419
2426 0009515 169
4513 190
6850 15
71734596 33262
Satellite: ISS
Catalog Number: 25544
Epoch time: 09087
53398445 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node:
2426 deg
Eccentricity:
0009515
Arg of perigee: 169
4513 deg
Mean anomaly: 190
6850 deg
Mean motion: 15
71734596 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3326
Checksum: 318
Coasting Arc #3 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2009/088/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4164841
16 A = 6731835
60 meter
Y = -3523009
81 meter E =
0013701
Z = -3959858
44 I = 51
61032
XDOT = 6020
054224 Wp = 145
80861
YDOT = 2631
515063 meter/sec RA = 354
88140 deg
ZDOT = 3986
025881 TA = 165
64575
MA = 165
60679
Ha = 195
834 n
mi
Hp = 186
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13664177
04 X = 4223163
01
Y = -11558431
13 feet Y = -3476110
23 meter
Z = -12991661
56 Z = -3939483
57
XDOT = 19750
834068 XDOT = 5970
817133
YDOT = 8633
579602 feet/sec YDOT = 2698
559715 meter/sec
ZDOT = 13077
512732 ZDOT = 4015
151919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13989733
34 X = 4264070
72
Y = -11253852
58 feet Y = -3430174
27 meter
Z = -12912338
98 Z = -3935680
92
XDOT = 18659
782721 XDOT = 5687
501773
YDOT = 8043
816440 feet/sec YDOT = 2451
755251 meter/sec
ZDOT = 13191
399465 ZDOT = 4020
738557
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 09088
48769174
00010596 00000-0 82463-4 0 9023
2 25544 51
6423 355
3611 0009459 173
1777 186
9515 15
71768462 33410
Satellite: ISS
Catalog Number: 25544
Epoch time: 09088
48769174 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 355
3611 deg
Eccentricity:
0009459
Arg of perigee: 173
1777 deg
Mean anomaly: 186
9515 deg
Mean motion: 15
71768462 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3341
Checksum: 343
Coasting Arc #4 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2009/089/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5917787
80 A = 6734682
48 meter
Y = -1297540
95 meter E =
0011998
Z = -2931296
60 I = 51
59144
XDOT = 3501
183914 Wp = 156
94052
YDOT = -4671
647397 meter/sec RA = 349
80976 deg
ZDOT = -5018
123017 TA = 56
82664
MA = 56
71162
Ha = 195
589 n
mi
Hp = 186
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19415314
30 X = -5888598
80
Y = -4257024
12 feet Y = -1363553
96 meter
Z = -9617114
84 Z = -2959974
58
XDOT = 11486
823866 XDOT = 3577
540228
YDOT = -15326
927156 feet/sec YDOT = -4632
068295 meter/sec
ZDOT = -16463
658193 ZDOT = -5000
928518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19338842
95 X = -5894479
33
Y = -4349492
15 feet Y = -1325725
21 meter
Z = -9729165
07 Z = -2965449
51
XDOT = 11337
688800 XDOT = 3455
727546
YDOT = -13861
408181 feet/sec YDOT = -4224
957213 meter/sec
ZDOT = -16396
822359 ZDOT = -4997
751455
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 09089
50496457
00010596 00000-0 82463-4 0 9039
2 25544 51
6427 350
1542 0009427 177
7386 182
3821 15
71779468 33576
Satellite: ISS
Catalog Number: 25544
Epoch time: 09089
50496457 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 350
1542 deg
Eccentricity:
0009427
Arg of perigee: 177
7386 deg
Mean anomaly: 182
3821 deg
Mean motion: 15
71779468 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3357
Checksum: 345
Coasting Arc #5 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2009/090/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1831931
04 A = 6728640
33 meter
Y = 4404924
11 meter E =
0008576
Z = 4737124
85 I = 51
54189
XDOT = -7236
903045 Wp = 131
03090
YDOT = -180
894019 meter/sec RA = 344
64180 deg
ZDOT = -2632
881954 TA = 344
83612
MA = 344
86180
Ha = 195
458 n
mi
Hp = 186
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6010272
44 X = -1904063
73
Y = 14451850
75 feet Y = 4384035
07 meter
Z = 15541748
18 Z = 4728050
06
XDOT = -23743
120228 XDOT = -7221
552245
YDOT = -593
484313 feet/sec YDOT = -261
735455 meter/sec
ZDOT = -8638
064155 ZDOT = -2668
001772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5919956
89 X = -1804402
86
Y = 14526698
12 feet Y = 4427737
59 meter
Z = 15506593
89 Z = 4726409
82
XDOT = -22639
021399 XDOT = -6900
373722
YDOT = 132
613870 feet/sec YDOT = 40
420708 meter/sec
ZDOT = -8775
196978 ZDOT = -2674
680039
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 09090
52222167
00010596 00000-0 82463-4 0 9049
2 25544 51
6422 344
9475 0009313 181
8315 178
2814 15
71831153 33733
Satellite: ISS
Catalog Number: 25544
Epoch time: 09090
52222167 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 344
9475 deg
Eccentricity:
0009313
Arg of perigee: 181
8315 deg
Mean anomaly: 178
2814 deg
Mean motion: 15
71831153 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3373
Checksum: 302
Coasting Arc #6 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2009/091/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6453952
48 A = 6737161
56 meter
Y = -1013259
94 meter E =
0012193
Z = 1643646
22 I = 51
54288
XDOT = -666
483312 Wp = 104
29972
YDOT = 5098
332427 meter/sec RA = 339
55121 deg
ZDOT = 5721
639468 TA = 273
85456
MA = 273
99395
Ha = 195
319 n
mi
Hp = 186
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21174384
77 X = 6456818
70
Y = -3324343
62 feet Y = -941072
07 meter
Z = 5392540
10 Z = 1675006
51
XDOT = -2186
625038 XDOT = -751
238908
YDOT = 16726
812426 feet/sec YDOT = 5090
405474 meter/sec
ZDOT = 18771
783030 ZDOT = 5718
195866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21035082
82 X = 6411493
24
Y = -3949206
44 feet Y = -1203718
12 meter
Z = 5514923
29 Z = 1680948
62
XDOT = -2086
555286 XDOT = -635
982051
YDOT = 15253
751353 feet/sec YDOT = 4649
343412 meter/sec
ZDOT = 18758
657467 ZDOT = 5717
638796
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 09091
53946473
00010596 00000-0 82463-4 0 9055
2 25544 51
6426 339
7397 0009285 185
7147 174
3910 15
71820711 33895
Satellite: ISS
Catalog Number: 25544
Epoch time: 09091
53946473 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 339
7397 deg
Eccentricity:
0009285
Arg of perigee: 185
7147 deg
Mean anomaly: 174
3910 deg
Mean motion: 15
71820711 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3389
Checksum: 340
Coasting Arc #7 (Orbit 3403)
---------------------------------------
Vector Time (GMT): 2009/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -639400
13 A = 6726645
23 meter
Y = -4262828
67 meter E =
0016931
Z = -5176727
72 I = 51
48086
XDOT = 7196
524212 Wp = 131
87468
YDOT = -2455
754169 meter/sec RA = 334
39757 deg
ZDOT = 1124
594555 TA = 148
95282
MA = 148
85264
Ha = 195
104 n
mi
Hp = 186
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2097769
47 X = -566537
45
Y = -13985658
36 feet Y = -4269571
39 meter
Z = -16984014
82 Z = -5179656
95
XDOT = 23610
643740 XDOT = 7217
986949
YDOT = -8056
936250 feet/sec YDOT = -2375
158442 meter/sec
ZDOT = 3689
614682 ZDOT = 1159
607246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2652076
70 X = -808352
98
Y = -13876886
12 feet Y = -4229674
89 meter
Z = -16995721
72 Z = -5180295
98
XDOT = 22173
943314 XDOT = 6758
617922
YDOT = -8958
994927 feet/sec YDOT = -2730
701654 meter/sec
ZDOT = 3826
171974 ZDOT = 1166
217218
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 09092
49311455
00010596 00000-0 82463-4 0 9068
2 25544 51
6429 334
8577 0009292 190
0450 170
0528 15
71867015 34042
Satellite: ISS
Catalog Number: 25544
Epoch time: 09092
49311455 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 334
8577 deg
Eccentricity:
0009292
Arg of perigee: 190
0450 deg
Mean anomaly: 170
0528 deg
Mean motion: 15
71867015 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3404
Checksum: 310
Coasting Arc #8 (Orbit 3419)
---------------------------------------
Vector Time (GMT): 2009/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5898072
30 A = 6738301
49 meter
Y = 3219553
01 meter E =
0018526
Z = -308120
16 I = 51
49384
XDOT = -2062
944310 Wp = 162
37743
YDOT = -4344
594697 meter/sec RA = 329
28068 deg
ZDOT = -6018
994023 TA = 20
97829
MA = 20
90238
Ha = 195
025 n
mi
Hp = 186
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19350630
91 X = -5932138
74
Y = 10562837
96 feet Y = 3153406
85 meter
Z = -1010892
92 Z = -336855
56
XDOT = -6768
189995 XDOT = -1984
970055
YDOT = -14253
919610 feet/sec YDOT = -4367
227852 meter/sec
ZDOT = -19747
355720 ZDOT = -6028
826265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18628889
31 X = -5678085
46
Y = 11779047
67 feet Y = 3590253
73 meter
Z = -1122891
60 Z = -342257
36
XDOT = -6693
426707 XDOT = -2040
156460
YDOT = -12440
674872 feet/sec YDOT = -3791
917701 meter/sec
ZDOT = -19786
026288 ZDOT = -6030
780813
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 09093
51032821
00010596 00000-0 82463-4 0 9070
2 25544 51
6430 329
6507 0009467 194
0244 166
0656 15
71834670 34204
Satellite: ISS
Catalog Number: 25544
Epoch time: 09093
51032821 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 329
6507 deg
Eccentricity:
0009467
Arg of perigee: 194
0244 deg
Mean anomaly: 166
0656 deg
Mean motion: 15
71834670 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3420
Checksum: 304
Coasting Arc #9 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2009/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2849193
85 A = 6726115
04 meter
Y = 3101754
89 meter E =
0009615
Z = 5245124
53 I = 51
42876
XDOT = -6019
483441 Wp = 182
12058
YDOT = 4777
626226 meter/sec RA = 324
14897 deg
ZDOT = 435
101535 TA = 263
67859
MA = 263
78811
Ha = 194
659 n
mi
Hp = 187
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9347748
86 X = 2788818
13
Y = 10176361
18 feet Y = 3133278
87 meter
Z = 17208413
82 Z = 5258819
01
XDOT = -19748
961422 XDOT = -6074
573901
YDOT = 15674
626725 feet/sec YDOT = 4710
004843 meter/sec
ZDOT = 1427
498473 ZDOT = 405
725163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10043366
70 X = 3061218
17
Y = 9392511
43 feet Y = 2862837
48 meter
Z = 17262090
15 Z = 5261485
08
XDOT = -17734
860222 XDOT = -5405
585396
YDOT = 16493
794658 feet/sec YDOT = 5027
308612 meter/sec
ZDOT = 1313
100868 ZDOT = 400
233145
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 09094
52752433
00010596 00000-0 82463-4 0 9081
2 25544 51
6430 324
4433 0009253 198
4360 161
6468 15
71909214 34361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09094
52752433 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 324
4433 deg
Eccentricity:
0009253
Arg of perigee: 198
4360 deg
Mean anomaly: 161
6468 deg
Mean motion: 15
71909214 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3436
Checksum: 312
Coasting Arc #10 (Orbit 3450)
---------------------------------------
Vector Time (GMT): 2009/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4439824
34 A = 6737604
25 meter
Y = -4960580
88 meter E =
0002603
Z = -1042732
75 I = 51
44389
XDOT = 4229
940441 Wp = 107
39029
YDOT = 2549
033006 meter/sec RA = 319
00073 deg
ZDOT = 5895
404302 TA = 241
19655
MA = 241
22269
Ha = 194
511 n
mi
Hp = 187
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14566352
81 X = 4500029
77
Y = -16274871
64 feet Y = -4910595
61 meter
Z = -3421039
19 Z = -1021017
70
XDOT = 13877
757353 XDOT = 4172
483775
YDOT = 8362
969181 feet/sec YDOT = 2596
013796 meter/sec
ZDOT = 19341
877630 ZDOT = 5915
813452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12915783
08 X = 3936730
68
Y = -17629617
04 feet Y = -5373507
27 meter
Z = -3336576
21 Z = -1016988
43
XDOT = 13235
373020 XDOT = 4034
141696
YDOT = 6027
944510 feet/sec YDOT = 1837
317487 meter/sec
ZDOT = 19421
739883 ZDOT = 5919
746316
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 09095
48113293
00010596 00000-0 82463-4 0 9093
2 25544 51
6424 319
5608 0009199 202
8733 157
2020 15
71934330 34515
Satellite: ISS
Catalog Number: 25544
Epoch time: 09095
48113293 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 319
5608 deg
Eccentricity:
0009199
Arg of perigee: 202
8733 deg
Mean anomaly: 157
2020 deg
Mean motion: 15
71934330 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3451
Checksum: 308
Coasting Arc #11 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2009/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350595
82 A = 6727096
61 meter
Y = -1224564
15 meter E =
0009870
Z = -4988609
66 I = 51
38623
XDOT = 3957
796895 Wp = 119
61265
YDOT = -6313
885838 meter/sec RA = 313
88989 deg
ZDOT = -1909
365348 TA = 131
90797
MA = 131
82376
Ha = 194
206 n
mi
Hp = 187
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14273608
34 X = -4312345
54
Y = -4017598
93 feet Y = -1273001
60 meter
Z = -16366829
60 Z = -5009651
75
XDOT = 12984
897950 XDOT = 4037
380983
YDOT = -20714
848551 feet/sec YDOT = -6269
182625 meter/sec
ZDOT = -6264
322008 ZDOT = -1889
944624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14547589
01 X = -4434105
13
Y = -2354930
62 feet Y = -717782
85 meter
Z = -16449074
84 Z = -5013678
01
XDOT = 10372
061008 XDOT = 3161
404195
YDOT = -21018
125974 feet/sec YDOT = -6406
324797 meter/sec
ZDOT = -6188
916383 ZDOT = -1886
381714
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 09096
49830028
00010596 00000-0 82463-4 0 9109
2 25544 51
6413 314
3527 0009167 207
5903 152
4773 15
71957595 34679
Satellite: ISS
Catalog Number: 25544
Epoch time: 09096
49830028 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 314
3527 deg
Eccentricity:
0009167
Arg of perigee: 207
5903 deg
Mean anomaly: 152
4773 deg
Mean motion: 15
71957595 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3467
Checksum: 328
Coasting Arc #12 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2009/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 669292
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2372538
28 A = 6735687
12 meter
Y = 5866932
23 meter E =
0014803
Z = 2277603
55 I = 51
39589
XDOT = -5468
755076 Wp = 144
27107
YDOT = -103
140355 meter/sec RA = 308
71700 deg
ZDOT = -5425
152777 TA = 10
05014
MA = 10
02057
Ha = 194
053 n
mi
Hp = 187
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7783918
23 X = -2449031
16
Y = 19248465
32 feet Y = 5839973
63 meter
Z = 7472452
58 Z = 2265891
42
XDOT = -17942
109828 XDOT = -5440
840850
YDOT = -338
386993 feet/sec YDOT = -164
139575 meter/sec
ZDOT = -17799
057668 ZDOT = -5451
652200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5208520
45 X = -1587557
03
Y = 20115653
41 feet Y = 6131251
16 meter
Z = 7427122
62 Z = 2263786
97
XDOT = -16259
674168 XDOT = -4955
948687
YDOT = 2407
047478 feet/sec YDOT = 733
668071 meter/sec
ZDOT = -17902
532916 ZDOT = -5456
692033
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 09097
51545297
00010596 00000-0 82463-4 0 9115
2 25544 51
6415 309
1454 0009088 211
4683 148
5937 15
71987523 34833
Satellite: ISS
Catalog Number: 25544
Epoch time: 09097
51545297 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 309
1454 deg
Eccentricity:
0009088
Arg of perigee: 211
4683 deg
Mean anomaly: 148
5937 deg
Mean motion: 15
71987523 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3483
Checksum: 338
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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