Date:
February 20th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 2697)
---------------------------------------
Vector Time (GMT): 2009/047/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3195758
48 A = 6735001
61 meter
Y = 4629514
92 meter E =
0013348
Z = -3719613
74 I = 51
50548
XDOT = -6320
120763 Wp = 50
54962
YDOT = 936
016235 meter/sec RA = 203
65705 deg
ZDOT = -4266
897132 TA = 174
25596
MA = 174
24064
Ha = 197
444 n
mi
Hp = 186
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10484771
92 X = 3161821
93
Y = 15188697
24 feet Y = 4665062
01 meter
Z = -12203457
17 Z = -3704171
37
XDOT = -20735
304342 XDOT = -6309
390188
YDOT = 3070
919407 feet/sec YDOT = 865
400982 meter/sec
ZDOT = -13999
006337 ZDOT = -4297
573802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8107069
07 X = 2471034
65
Y = 16624603
44 feet Y = 5067179
13 meter
Z = -12142871
34 Z = -3701147
18
XDOT = -19668
512905 XDOT = -5994
962733
YDOT = -716
442918 feet/sec YDOT = -218
371801 meter/sec
ZDOT = -14118
503761 ZDOT = -4303
319946
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 09047
59421421
00010596 00000-0 82463-4 0 9008
2 25544 51
6390 204
5060 0008681 31
9070 328
2616 15
70932188 26983
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047
59421421 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 204
5060 deg
Eccentricity:
0008681
Arg of perigee: 31
9070 deg
Mean anomaly: 328
2616 deg
Mean motion: 15
70932188 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2698
Checksum: 301
Coasting Arc #2 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2009/048/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4681588
67 A = 6732606
75 meter
Y = -2087338
49 meter E =
0017383
Z = 4358898
91 I = 51
52536
XDOT = 5197
888047 Wp = 54
01163
YDOT = 4566
996406 meter/sec RA = 198
48655 deg
ZDOT = -3376
279126 TA = 70
14833
MA = 69
96106
Ha = 197
485 n
mi
Hp = 186
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15359542
90 X = 4683407
28
Y = -6848223
38 feet Y = -2034976
14 meter
Z = 14300849
44 Z = 4381646
10
XDOT = 17053
438476 XDOT = 5162
833918
YDOT = 14983
584009 feet/sec YDOT = 4624
926266 meter/sec
ZDOT = -11077
031253 ZDOT = -3351
113253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16065982
60 X = 4896911
50
Y = -4707315
90 feet Y = -1434789
89 meter
Z = 14389350
09 Z = 4385873
91
XDOT = 14577
576074 XDOT = 4443
245187
YDOT = 16000
183681 feet/sec YDOT = 4876
855986 meter/sec
ZDOT = -10978
538314 ZDOT = -3346
258478
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 09048
61202544
00010596 00000-0 82463-4 0 9016
2 25544 51
6392 199
3028 0008767 36
4258 323
7497 15
70922763 27147
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048
61202544 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 199
3028 deg
Eccentricity:
0008767
Arg of perigee: 36
4258 deg
Mean anomaly: 323
7497 deg
Mean motion: 15
70922763 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2714
Checksum: 323
Coasting Arc #3 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2009/049/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5636084
78 A = 6738992
77 meter
Y = -3032435
23 meter E =
0022185
Z = 2070677
35 I = 51
57620
XDOT = 3974
240338 Wp = 58
06296
YDOT = -3576
625433 meter/sec RA = 193
41046 deg
ZDOT = 5547
730962 TA = 325
07343
MA = 325
21878
Ha = 197
585 n
mi
Hp = 186
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18491091
79 X = -5611815
49
Y = -9948934
49 feet Y = -3095325
56 meter
Z = 6793560
86 Z = 2043356
64
XDOT = 13038
846253 XDOT = 3986
990008
YDOT = -11734
335410 feet/sec YDOT = -3532
111993 meter/sec
ZDOT = 18201
217068 ZDOT = 5567
068360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17215541
54 X = -5247297
06
Y = -12081650
66 feet Y = -3682487
12 meter
Z = 6686784
64 Z = 2038131
96
XDOT = 13356
060663 XDOT = 4070
927290
YDOT = -8857
630251 feet/sec YDOT = -2699
805701 meter/sec
ZDOT = 18276
307157 ZDOT = 5570
618422
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 09049
62982512
00010596 00000-0 82463-4 0 9029
2 25544 51
6399 194
0994 0008825 39
6772 320
5034 15
70979633 27307
Satellite: ISS
Catalog Number: 25544
Epoch time: 09049
62982512 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 194
0994 deg
Eccentricity:
0008825
Arg of perigee: 39
6772 deg
Mean anomaly: 320
5034 deg
Mean motion: 15
70979633 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2730
Checksum: 336
Coasting Arc #4 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2009/050/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2029632
37 A = 6729188
92 meter
Y = 3839305
62 meter E =
0020470
Z = -5156739
15 I = 51
57260
XDOT = -7272
438317 Wp = 78
62931
YDOT = -2102
744686 meter/sec RA = 188
26520 deg
ZDOT = 1305
134941 TA = 203
84842
MA = 203
94340
Ha = 197
593 n
mi
Hp = 185
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6658898
86 X = -2047363
32
Y = 12596147
06 feet Y = 3816510
05 meter
Z = -16918435
54 Z = -5166641
89
XDOT = -23859
705764 XDOT = -7254
724547
YDOT = -6898
768656 feet/sec YDOT = -2183
970300 meter/sec
ZDOT = 4281
938782 ZDOT = 1269
849194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7809419
59 X = -2380311
09
Y = 11862539
44 feet Y = 3615702
02 meter
Z = -16956722
55 Z = -5168409
03
XDOT = -22192
527322 XDOT = -6764
282328
YDOT = -8725
068176 feet/sec YDOT = -2659
400780 meter/sec
ZDOT = 4144
169626 ZDOT = 1263
142902
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 09050
58400607
00010596 00000-0 82463-4 0 9037
2 25544 51
6400 189
2222 0008920 42
6850 317
5003 15
71002325 27451
Satellite: ISS
Catalog Number: 25544
Epoch time: 09050
58400607 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 189
2222 deg
Eccentricity:
0008920
Arg of perigee: 42
6850 deg
Mean anomaly: 317
5003 deg
Mean motion: 15
71002325 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2745
Checksum: 268
Coasting Arc #5 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2009/051/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6716015
22 A = 6740734
78 meter
Y = 525612
44 meter E =
0014903
Z = -194997
21 I = 51
64075
XDOT = -535
186222 Wp = 99
81925
YDOT = 4747
893271 meter/sec RA = 183
16229 deg
ZDOT = -6027
278913 TA = 82
29540
MA = 82
12620
Ha = 197
672 n
mi
Hp = 185
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22034170
67 X = 6710585
83
Y = 1724450
26 feet Y = 600684
47 meter
Z = -639754
63 Z = -162384
80
XDOT = -1755
860310 XDOT = -558
959472
YDOT = 15577
077660 feet/sec YDOT = 4741
775637 meter/sec
ZDOT = -19774
537116 ZDOT = -6029
936485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21812302
52 X = 6648389
81
Y = 3584475
55 feet Y = 1092548
15 meter
Z = -512528
44 Z = -156218
67
XDOT = -2693
479991 XDOT = -820
972701
YDOT = 13791
335771 feet/sec YDOT = 4203
599143 meter/sec
ZDOT = -19784
494242 ZDOT = -6030
313845
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 09051
60179007
00010596 00000-0 82463-4 0 9049
2 25544 51
6400 184
0181 0008887 46
3797 313
8100 15
70991824 27616
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051
60179007 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 184
0181 deg
Eccentricity:
0008887
Arg of perigee: 46
3797 deg
Mean anomaly: 313
8100 deg
Mean motion: 15
70991824 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2761
Checksum: 305
Coasting Arc #6 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2009/052/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1146066
03 A = 6728822
77 meter
Y = -4088840
13 meter E =
0010498
Z = 5210799
06 I = 51
63144
XDOT = 7588
596865 Wp = 68
28136
YDOT = -975
373355 meter/sec RA = 178
05543 deg
ZDOT = 906
042063 TA = 13
10577
MA = 13
07851
Ha = 197
660 n
mi
Hp = 185
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3760059
17 X = -1125571
20
Y = -13414829
81 feet Y = -4101541
48 meter
Z = 17095797
43 Z = 5205281
43
XDOT = 24896
971342 XDOT = 7594
538385
YDOT = -3200
043815 feet/sec YDOT = -890
480025 meter/sec
ZDOT = 2972
578948 ZDOT = 942
920901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2943990
22 X = -897328
22
Y = -13644633
46 feet Y = -4158884
28 meter
Z = 17073924
36 Z = 5204132
14
XDOT = 24043
714693 XDOT = 7328
524239
YDOT = -1297
875760 feet/sec YDOT = -395
592532 meter/sec
ZDOT = 3116
330271 ZDOT = 949
857467
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 09052
61956352
00010596 00000-0 82463-4 0 9058
2 25544 51
6408 178
8144 0008915 49
5306 310
6631 15
71043806 27777
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052
61956352 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 178
8144 deg
Eccentricity:
0008915
Arg of perigee: 49
5306 deg
Mean anomaly: 310
6631 deg
Mean motion: 15
71043806 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2777
Checksum: 315
Coasting Arc #7 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2009/053/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6134118
59 A = 6739374
35 meter
Y = 2157491
87 meter E =
0016382
Z = -1753626
63 I = 51
69625
XDOT = -3078
170220 Wp = 46
16892
YDOT = -4154
543450 meter/sec RA = 172
92124 deg
ZDOT = 5700
019126 TA = 294
45240
MA = 294
62320
Ha = 197
762 n
mi
Hp = 185
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20125060
98 X = -6149269
56
Y = 7078385
40 feet Y = 2088811
83 meter
Z = -5753368
20 Z = -1783462
18
XDOT = -10098
983663 XDOT = -3059
173530
YDOT = -13630
391895 feet/sec YDOT = -4188
858981 meter/sec
ZDOT = 18700
850150 ZDOT = 5685
112045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20422470
99 X = -6224769
16
Y = 6057544
08 feet Y = 1846339
44 meter
Z = -5869557
33 Z = -1789041
08
XDOT = -9065
720088 XDOT = -2763
231483
YDOT = -12637
711735 feet/sec YDOT = -3851
974537 meter/sec
ZDOT = 18642
341301 ZDOT = 5682
185628
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 09053
57372045
00010596 00000-0 82463-4 0 9066
2 25544 51
6411 173
9370 0009075 51
9420 308
2559 15
70986040 27924
Satellite: ISS
Catalog Number: 25544
Epoch time: 09053
57372045 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 173
9370 deg
Eccentricity:
0009075
Arg of perigee: 51
9420 deg
Mean anomaly: 308
2559 deg
Mean motion: 15
70986040 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2792
Checksum: 310
Coasting Arc #8 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2009/054/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4027300
01 A = 6731640
71 meter
Y = 2848700
83 meter E =
0019123
Z = -4599332
21 I = 51
69913
XDOT = -6028
203630 Wp = 64
03478
YDOT = 3707
829012 meter/sec RA = 167
85130 deg
ZDOT = -2983
321281 TA = 176
30447
MA = 176
29033
Ha = 197
785 n
mi
Hp = 185
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13212926
53 X = 4017488
15
Y = 9346131
34 feet Y = 2893681
37 meter
Z = -15089672
62 Z = -4579792
10
XDOT = -19777
570963 XDOT = -6054
725130
YDOT = 12164
793347 feet/sec YDOT = 3640
269703 meter/sec
ZDOT = -9787
799477 ZDOT = -3012
670066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12982496
70 X = 3957064
99
Y = 9782050
36 feet Y = 2981568
95 meter
Z = -15013197
14 Z = -4576022
49
XDOT = -19400
082537 XDOT = -5913
145157
YDOT = 10557
117258 feet/sec YDOT = 3217
809340 meter/sec
ZDOT = -9901
962089 ZDOT = -3018
118045
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 09054
59147802
00010596 00000-0 82463-4 0 9071
2 25544 51
6409 168
7336 0008987 56
5761 303
6259 15
71017752 28085
Satellite: ISS
Catalog Number: 25544
Epoch time: 09054
59147802 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 168
7336 deg
Eccentricity:
0008987
Arg of perigee: 56
5761 deg
Mean anomaly: 303
6259 deg
Mean motion: 15
71017752 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2808
Checksum: 336
Coasting Arc #9 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2009/055/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4128472
86 A = 6735498
81 meter
Y = -4088995
28 meter E =
0020956
Z = 3393468
66 I = 51
74160
XDOT = 5817
367671 Wp = 77
22644
YDOT = 2009
687128 meter/sec RA = 162
69659 deg
ZDOT = -4627
344070 TA = 62
81456
MA = 62
60110
Ha = 197
784 n
mi
Hp = 185
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13544858
45 X = 4157405
41
Y = -13415338
86 feet Y = -4042666
30 meter
Z = 11133427
35 Z = 3413594
82
XDOT = 19085
851939 XDOT = 5816
940887
YDOT = 6593
461707 feet/sec YDOT = 2074
737620 meter/sec
ZDOT = -15181
575032 ZDOT = -4599
085196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13692938
06 X = 4173607
52
Y = -13198165
52 feet Y = -4022800
85 meter
Z = 11211582
67 Z = 3417290
40
XDOT = 18103
002618 XDOT = 5517
795198
YDOT = 5900
300559 feet/sec YDOT = 1798
411611 meter/sec
ZDOT = -15071
152574 ZDOT = -4593
687304
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 09055
60922628
00010596 00000-0 82463-4 0 9082
2 25544 51
6411 163
5300 0009201 59
7818 300
4253 15
71059166 28242
Satellite: ISS
Catalog Number: 25544
Epoch time: 09055
60922628 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 163
5300 deg
Eccentricity:
0009201
Arg of perigee: 59
7818 deg
Mean anomaly: 300
4253 deg
Mean motion: 15
71059166 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2824
Checksum: 294
Coasting Arc #10 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2009/056/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5814709
78 A = 6735752
35 meter
Y = -458962
72 meter E =
0021302
Z = 3346513
99 I = 51
77007
XDOT = 3120
159622 Wp = 78
57068
YDOT = -5268
100103 meter/sec RA = 157
64259 deg
ZDOT = 4678
068925 TA = 320
73952
MA = 320
89381
Ha = 197
912 n
mi
Hp = 185
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19077131
83 X = -5825401
83
Y = -1505783
21 feet Y = -524045
69 meter
Z = 10979376
61 Z = 3318240
82
XDOT = 10236
744167 XDOT = 3156
111773
YDOT = -17283
792990 feet/sec YDOT = -5233
007249 meter/sec
ZDOT = 15347
995160 ZDOT = 4693
314100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19142053
99 X = -5834498
06
Y = -1482237
73 feet Y = -451786
06 meter
Z = 10869029
08 Z = 3312880
06
XDOT = 10018
661622 XDOT = 3053
688062
YDOT = -15900
223426 feet/sec YDOT = -4846
388100 meter/sec
ZDOT = 15407
006078 ZDOT = 4696
055453
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 09056
62696493
00010596 00000-0 82463-4 0 9094
2 25544 51
6411 158
3265 0009139 63
6256 296
5843 15
71075057 28409
Satellite: ISS
Catalog Number: 25544
Epoch time: 09056
62696493 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 158
3265 deg
Eccentricity:
0009139
Arg of perigee: 63
6256 deg
Mean anomaly: 296
5843 deg
Mean motion: 15
71075057 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2840
Checksum: 333
Coasting Arc #11 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2009/057/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1209544
72 A = 6731162
80 meter
Y = 4744709
91 meter E =
0018620
Z = -4634759
57 I = 51
78094
XDOT = -7023
941593 Wp = 90
02471
YDOT = 1058
817425 meter/sec RA = 152
49280 deg
ZDOT = 2927
074626 TA = 208
93210
MA = 209
03544
Ha = 197
882 n
mi
Hp = 185
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3968322
58 X = -1239996
51
Y = 15566633
58 feet Y = 4731013
39 meter
Z = -15205904
09 Z = -4640709
84
XDOT = -23044
427797 XDOT = -7049
478396
YDOT = 3473
810450 feet/sec YDOT = 980
129110 meter/sec
ZDOT = 9603
263209 ZDOT = 2892
890765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3592942
42 X = -1095128
85
Y = 15635365
85 feet Y = 4765659
51 meter
Z = -15228699
34 Z = -4641707
56
XDOT = -21891
423853 XDOT = -6672
505990
YDOT = 4160
942951 feet/sec YDOT = 1268
255412 meter/sec
ZDOT = 9469
983565 ZDOT = 2886
450991
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 09057
58108798
00010596 00000-0 82463-4 0 9108
2 25544 51
6402 153
4486 0009328 66
5921 293
6221 15
71089922 28551
Satellite: ISS
Catalog Number: 25544
Epoch time: 09057
58108798 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 153
4486 deg
Eccentricity:
0009328
Arg of perigee: 66
5921 deg
Mean anomaly: 293
6221 deg
Mean motion: 15
71089922 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2855
Checksum: 329
Coasting Arc #12 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2009/058/13:41:07
008
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6100385
85 A = 6739232
13 meter
Y = -2293551
02 meter E =
0013886
Z = -1719315
11 I = 51
83327
XDOT = 326
934703 Wp = 102
53590
YDOT = 5127
226951 meter/sec RA = 147
42831 deg
ZDOT = -5721
266216 TA = 96
39586
MA = 96
23772
Ha = 197
960 n
mi
Hp = 185
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20014389
26 X = 6133931
35
Y = -7524773
68 feet Y = -2225145
54 meter
Z = -5640797
60 Z = -1689598
08
XDOT = 1072
620417 XDOT = 297
369464
YDOT = 16821
610730 feet/sec YDOT = 5130
717092 meter/sec
ZDOT = -18770
558451 ZDOT = -5719
750269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19765860
36 X = 6024634
24
Y = -8234147
82 feet Y = -2509768
25 meter
Z = -5525049
13 Z = -1684034
97
XDOT = 1179
032927 XDOT = 359
369236
YDOT = 15327
357932 feet/sec YDOT = 4671
778698 meter/sec
ZDOT = -18764
191644 ZDOT = -5719
325613
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 09058
59881026
00010596 00000-0 82463-4 0 9113
2 25544 51
6399 148
2443 0009394 70
1290 290
0883 15
71090689 28719
Satellite: ISS
Catalog Number: 25544
Epoch time: 09058
59881026 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 148
2443 deg
Eccentricity:
0009394
Arg of perigee: 70
1290 deg
Mean anomaly: 290
0883 deg
Mean motion: 15
71090689 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2871
Checksum: 332
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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