Date:
November 21st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19913 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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
326/16:15:32
303 0
2 0
4 0
4
N/A 0
3 -0
0 187
2
000/00:00:04
605 -0
2 -0
0 179
3
326/17:31:04
865 0
1 0
1 0
1
N/A -0
0 0
0 187
2
000/00:34:09
730 0
0 -0
0 179
3
326/18:20:02
638 -0
4 0
4 0
4
N/A -0
2 -0
0 187
3
000/00:00:05
277 -0
0 -0
0 179
4
326/18:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 187
2
000/00:00:00
000 0
0 0
0 179
4
328/09:45:33
979 -0
5 0
6 0
6
N/A 0
0 -0
0 187
4
000/00:00:07
958 -0
3 -0
0 179
5
328/10:20:08
398 0
8 2
0 2
0
N/A -1
2 0
3 188
7
000/00:30:16
797 1
4 0
0 179
9
328/10:45:32
231 0
3 0
3 0
3
N/A 0
2 0
0 188
7
000/00:00:04
462 -0
1 -0
0 179
9
Coasting Arc #1 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2009/323/10:50:28
866
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4931586
87 A = 6724788
10 meter
Y = 4487198
53 meter E =
0010543
Z = 857253
54 I = 51
41398
XDOT = -2688
872021 Wp = 100
41537
YDOT = 4101
132610 meter/sec RA = 228
18685 deg
ZDOT = -5938
560043 TA = 70
19541
MA = 70
08177
Ha = 187
174 n
mi
Hp = 179
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16179746
94 X = 4876879
23
Y = 14721779
94 feet Y = 4542040
46 meter
Z = 2812511
60 Z = 881079
29
XDOT = -8821
758600 XDOT = -2705
682700
YDOT = 13455
159480 feet/sec YDOT = 4070
970700 meter/sec
ZDOT = -19483
464708 ZDOT = -5951
663255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21850957
12 X = -6660171
73
Y = -715468
69 feet Y = -218074
86 meter
Z = 2906718
88 Z = 885967
91
XDOT = -2155
880294 XDOT = -657
112313
YDOT = -14294
587806 feet/sec YDOT = -4356
990363 meter/sec
ZDOT = -19535
006872 ZDOT = -5954
270095
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 09323
48515883
00016717 00000-0 10270-3 0 9006
2 25544 51
6457 228
9667 0006118 353
4457 6
6626 15
76478796 30422
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
48515883 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 228
9667 deg
Eccentricity:
0006118
Arg of perigee: 353
4457 deg
Mean anomaly: 6
6626 deg
Mean motion: 15
76478796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 342
Coasting Arc #2 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2009/324/10:50:28
866
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2847238
90 A = 6712765
31 meter
Y = -3070762
66 meter E =
0006317
Z = 5244760
08 I = 51
39477
XDOT = 5643
148720 Wp = 17
60234
YDOT = 5249
475807 meter/sec RA = 223
02479 deg
ZDOT = 15
943524 TA = 72
28045
MA = 72
21151
Ha = 186
998 n
mi
Hp = 179
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9341334
97 X = 2855886
56
Y = -10074680
64 feet Y = -3038875
36 meter
Z = 17207218
11 Z = 5258612
89
XDOT = 18514
267453 XDOT = 5583
951298
YDOT = 17222
689656 feet/sec YDOT = 5312
249831 meter/sec
ZDOT = 52
308151 ZDOT = 43
215173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -260005
51 X = -79249
68
Y = 13667916
30 feet Y = 4165980
89 meter
Z = 17261765
42 Z = 5261386
10
XDOT = -24280
630649 XDOT = -7400
736222
YDOT = -639
659373 feet/sec YDOT = -194
968177 meter/sec
ZDOT = 160
161293 ZDOT = 48
817162
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 09324
49936961
00016717 00000-0 10270-3 0 9013
2 25544 51
6452 223
7398 0006147 355
6154 4
4956 15
76573258 30589
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
49936961 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 223
7398 deg
Eccentricity:
0006147
Arg of perigee: 355
6154 deg
Mean anomaly: 4
4956 deg
Mean motion: 15
76573258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 336
Coasting Arc #3 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/10:50:28
866
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821639
99 A = 6724589
83 meter
Y = -4596050
63 meter E =
0017979
Z = 839973
35 I = 51
45738
XDOT = 3889
619759 Wp = 37
84813
YDOT = -2982
912452 meter/sec RA = 217
86233 deg
ZDOT = 5952
782625 TA = 331
35617
MA = 331
45481
Ha = 187
229 n
mi
Hp = 179
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15819028
83 X = -4773968
28
Y = -15078906
27 feet Y = -4649702
59 meter
Z = 2755818
08 Z = 816664
84
XDOT = 12761
219681 XDOT = 3893
768170
YDOT = -9786
458177 feet/sec YDOT = -2939
393809 meter/sec
ZDOT = 19530
126724 ZDOT = 5971
688457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21861238
55 X = 6663305
51
Y = 448332
24 feet Y = 136651
67 meter
Z = 2663619
35 Z = 811871
18
XDOT = -2701
026328 XDOT = -823
272825
YDOT = 14161
319148 feet/sec YDOT = 4316
370076 meter/sec
ZDOT = 19604
627431 ZDOT = 5975
490441
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 09325
51355199
00016717 00000-0 10270-3 0 9026
2 25544 51
6451 218
5119 0006216
5635 359
5535 15
76571878 30749
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51355199 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 218
5119 deg
Eccentricity:
0006216
Arg of perigee:
5635 deg
Mean anomaly: 359
5535 deg
Mean motion: 15
76571878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 319
Coasting Arc #4 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2009/326/10:50:28
866
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3968813
14 A = 6713809
76 meter
Y = 2164327
33 meter E =
0013460
Z = -4974279
75 I = 51
44679
XDOT = -5290
875608 Wp = 77
84400
YDOT = -5238
307926 meter/sec RA = 212
66967 deg
ZDOT = 1949
428244 TA = 211
01468
MA = 211
09422
Ha = 187
181 n
mi
Hp = 179
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13021040
47 X = -3968555
60
Y = 7100811
45 feet Y = 2119947
58 meter
Z = -16319815
45 Z = -4993559
68
XDOT = -17358
515775 XDOT = -5241
376790
YDOT = -17186
049627 feet/sec YDOT = -5297
197017 meter/sec
ZDOT = 6395
761954 ZDOT = 1923
844645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4510234
48 X = 1374719
47
Y = -14040648
41 feet Y = -4279589
64 meter
Z = -16395833
98 Z = -4997450
20
XDOT = 23423
667981 XDOT = 7139
534001
YDOT = 201
459206 feet/sec YDOT = 61
404766 meter/sec
ZDOT = 6294
540034 ZDOT = 1918
575802
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 09326
46431656
00016717 00000-0 10270-3 0 9035
2 25544 51
6456 213
6109 0006181 3
6353 356
4856 15
76634896 30899
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
46431656 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 213
6109 deg
Eccentricity:
0006181
Arg of perigee: 3
6353 deg
Mean anomaly: 356
4856 deg
Mean motion: 15
76634896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 328
Coasting Arc #5 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2009/326/16:15:34
605
Vector Time (MET): N/A
Weight (LBS) : 731767
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5424560
66 A = 6717957
88 meter
Y = -360044
50 meter E =
0013751
Z = 3942880
96 I = 51
46266
XDOT = 3283
137629 Wp = 54
87197
YDOT = 5725
390609 meter/sec RA = 211
48959 deg
ZDOT = -3976
539154 TA = 76
48729
MA = 76
33412
Ha = 187
155 n
mi
Hp = 179
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17797115
01 X = 5409029
53
Y = -1181248
37 feet Y = -299471
02 meter
Z = 12935961
16 Z = 3969196
05
XDOT = 10771
448913 XDOT = 3238
188845
YDOT = 18784
089923 feet/sec YDOT = 5761
853585 meter/sec
ZDOT = -13046
388302 ZDOT = -3960
698199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11109163
18 X = 3386072
94
Y = 13857164
39 feet Y = 4223663
71 meter
Z = 13039832
43 Z = 3974540
93
XDOT = -8186
568586 XDOT = -2495
266105
YDOT = 18834
619107 feet/sec YDOT = 5740
791904 meter/sec
ZDOT = -12983
603940 ZDOT = -3957
402481
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 09326
71784943
00016717 00000-0 10270-3 0 9044
2 25544 51
6422 212
3005 0005823 4
5950 355
5267 15
76578342 30932
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
71784943 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 212
3005 deg
Eccentricity:
0005823
Arg of perigee: 4
5950 deg
Mean anomaly: 355
5267 deg
Mean motion: 15
76578342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 310
Coasting Arc #6 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/17:48:09
730
Vector Time (MET): N/A
Weight (LBS) : 731763
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5660361
12 A = 6719126
95 meter
Y = 58099
79 meter E =
0014254
Z = 3614798
90 I = 51
46738
XDOT = 2743
494146 Wp = 63
08078
YDOT = 5723
780773 meter/sec RA = 211
15507 deg
ZDOT = -4368
441346 TA = 73
44565
MA = 73
28913
Ha = 187
214 n
mi
Hp = 179
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18570738
59 X = 5641730
49
Y = 190616
10 feet Y = 121292
83 meter
Z = 11859576
45 Z = 3642252
03
XDOT = 9000
965046 XDOT = 2700
507284
YDOT = 18778
808309 feet/sec YDOT = 5754
220134 meter/sec
ZDOT = -14332
156646 ZDOT = -4355
217251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15608783
54 X = 4757557
22
Y = 9934387
11 feet Y = 3028001
19 meter
Z = 11967959
26 Z = 3647833
98
XDOT = -1480
487005 XDOT = -451
252439
YDOT = 19605
467540 feet/sec YDOT = 5975
746506 meter/sec
ZDOT = -14279
702537 ZDOT = -4352
453333
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 09326
78123722
00016717 00000-0 10270-3 0 9054
2 25544 51
6416 211
9717 0005556 8
2319 351
8936 15
76549810 30944
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
78123722 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 211
9717 deg
Eccentricity:
0005556
Arg of perigee: 8
2319 deg
Mean anomaly: 351
8936 deg
Mean motion: 15
76549810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 322
Coasting Arc #7 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/18:20:05
277
Vector Time (MET): N/A
Weight (LBS) : 731729
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1367401
48 A = 6713200
02 meter
Y = 4023953
91 meter E =
0016807
Z = -5210578
49 I = 51
44881
XDOT = -6861
715680 Wp = 65
39067
YDOT = -3383
733232 meter/sec RA = 211
07473 deg
ZDOT = -807
587786 TA = 196
86726
MA = 196
92321
Ha = 187
273 n
mi
Hp = 179
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4486225
34 X = -1386984
05
Y = 13201948
53 feet Y = 4008553
74 meter
Z = -17095073
77 Z = -5217268
65
XDOT = -22512
190550 XDOT = -6819
445039
YDOT = -11101
486980 feet/sec YDOT = -3460
228572 meter/sec
ZDOT = -2649
566228 ZDOT = -840
820002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9355132
46 X = -2851444
37
Y = 10295698
30 feet Y = 3138128
84 meter
Z = -17121311
37 Z = -5218575
71
XDOT = -15325
341189 XDOT = -4671
163994
YDOT = -18576
239764 feet/sec YDOT = -5662
037880 meter/sec
ZDOT = -2780
908101 ZDOT = -847
620789
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 09326
78123765
00016717 00000-0 10270-3 0 9062
2 25544 51
6430 211
9728 0005450 6
7285 353
3952 15
76508990 30949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
78123765 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 211
9728 deg
Eccentricity:
0005450
Arg of perigee: 6
7285 deg
Mean anomaly: 353
3952 deg
Mean motion: 15
76508990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 325
Coasting Arc #8 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4836446
38 A = 6716202
40 meter
Y = 1267864
73 meter E =
0010144
Z = -4491896
16 I = 51
45927
XDOT = -4349
932231 Wp = 79
73357
YDOT = -5525
311971 meter/sec RA = 211
00831 deg
ZDOT = 3131
799370 TA = 221
56927
MA = 221
64644
Ha = 187
219 n
mi
Hp = 179
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15867606
25 X = -4828443
32
Y = 4159661
17 feet Y = 1213825
83 meter
Z = -14737192
12 Z = -4515372
37
XDOT = -14271
431205 XDOT = -4303
037830
YDOT = -18127
663946 feet/sec YDOT = -5573
693524 meter/sec
ZDOT = 10274
932317 ZDOT = 3110
780613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16210917
02 X = -4941087
51
Y = -1884467
89 feet Y = -574385
81 meter
Z = -14829817
63 Z = -4520128
41
XDOT = -6867
910719 XDOT = -2093
339187
YDOT = -20924
206203 feet/sec YDOT = -6377
698051 meter/sec
ZDOT = 10191
714409 ZDOT = 3106
434552
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 09326
78123769
00016717 00000-0 10270-3 0 9077
2 25544 51
6432 211
9721 0005401 5
8524 354
2703 15
76487117 30947
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
78123769 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 211
9721 deg
Eccentricity:
0005401
Arg of perigee: 5
8524 deg
Mean anomaly: 354
2703 deg
Mean motion: 15
76487117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 308
Coasting Arc #9 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2009/327/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3389956
67 A = 6719859
77 meter
Y = 4683307
01 meter E =
0008016
Z = -3435599
08 I = 51
49838
XDOT = -6103
685327 Wp = 46
97467
YDOT = 1071
905157 meter/sec RA = 205
89110 deg
ZDOT = -4562
717788 TA = 173
77628
MA = 173
76632
Ha = 187
278 n
mi
Hp = 179
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11121905
09 X = 3354024
89
Y = 15365180
47 feet Y = 4721014
82 meter
Z = -11271650
53 Z = -3419217
45
XDOT = -20025
214328 XDOT = -6093
052779
YDOT = 3516
749204 feet/sec YDOT = 1003
709887 meter/sec
ZDOT = -14969
546550 ZDOT = -4592
343971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5126874
79 X = 1562671
44
Y = 18301890
87 feet Y = 5578416
34 meter
Z = -11206765
58 Z = -3415822
15
XDOT = -18577
372984 XDOT = -5662
383285
YDOT = -4031
180143 feet/sec YDOT = -1228
703708 meter/sec
ZDOT = -15086
470178 ZDOT = -4598
356110
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 09327
79544712
00016717 00000-0 10270-3 0 9085
2 25544 51
6432 206
7442 0005445 9
3193 350
8071 15
76545212 31108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
79544712 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 206
7442 deg
Eccentricity:
0005445
Arg of perigee: 9
3193 deg
Mean anomaly: 350
8071 deg
Mean motion: 15
76545212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3110
Checksum: 297
Coasting Arc #10 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2009/328/09:45:37
958
Vector Time (MET): N/A
Weight (LBS) : 731746
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550284
29 A = 6717709
31 meter
Y = 4637058
06 meter E =
0011535
Z = -4150265
16 I = 51
51026
XDOT = -6732
870822 Wp = 44
82233
YDOT = 386
177717 meter/sec RA = 202
61192 deg
ZDOT = -3703
980542 TA = 187
21477
MA = 187
23139
Ha = 187
397 n
mi
Hp = 179
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8367074
43 X = 2518403
86
Y = 15213445
07 feet Y = 4665398
81 meter
Z = -13616355
52 Z = -4137952
90
XDOT = -22089
471200 XDOT = -6718
695213
YDOT = 1266
987262 feet/sec YDOT = 310
966246 meter/sec
ZDOT = -12152
167133 ZDOT = -3736
654816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14782986
28 X = -4505854
22
Y = -9178633
02 feet Y = -2797647
34 meter
Z = -13567534
62 Z = -4135384
55
XDOT = 17948
320218 XDOT = 5470
648003
YDOT = -10744
943197 feet/sec YDOT = -3275
058686 meter/sec
ZDOT = -12281
162746 ZDOT = -3743
298405
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 09328
42931367
00016717 00000-0 10270-3 0 9093
2 25544 51
6457 203
4820 0005626 7
2520 352
8725 15
76471643 31206
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
42931367 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 203
4820 deg
Eccentricity:
0005626
Arg of perigee: 7
2520 deg
Mean anomaly: 352
8725 deg
Mean motion: 15
76471643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 303
Coasting Arc #11 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:35:16
797
Vector Time (MET): N/A
Weight (LBS) : 731742
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -863784
56 A = 6716265
40 meter
Y = -4542201
01 meter E =
0007661
Z = 4864351
47 I = 51
50106
XDOT = 7290
698848 Wp = 60
95363
YDOT = 1050
247564 meter/sec RA = 202
42667 deg
ZDOT = 2276
311350 TA = 6
88731
MA = 6
87679
Ha = 188
715 n
mi
Hp = 179
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2833938
85 X = -836559
14
Y = -14902234
28 feet Y = -4551708
39 meter
Z = 15959158
37 Z = 4860221
03
XDOT = 23919
615644 XDOT = 7267
354873
YDOT = 3445
694109 feet/sec YDOT = 1131
645814 meter/sec
ZDOT = 7468
213090 ZDOT = 2311
673399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12077949
12 X = 3681358
89
Y = 9206393
44 feet Y = 2806108
72 meter
Z = 15942647
11 Z = 4859318
84
XDOT = -19477
407501 XDOT = -5936
713806
YDOT = 12383
614423 feet/sec YDOT = 3774
525676 meter/sec
ZDOT = 7607
885688 ZDOT = 2318
883558
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 09328
49272412
00016717 00000-0 10270-3 0 9101
2 25544 51
6452 203
1551 0007385 7
7513 352
3764 15
75966246 31216
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
49272412 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 203
1551 deg
Eccentricity:
0007385
Arg of perigee: 7
7513 deg
Mean anomaly: 352
3764 deg
Mean motion: 15
75966246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 301
Coasting Arc #12 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3480105
43 A = 6715739
95 meter
Y = -2854116
51 meter E =
0011976
Z = 4982431
64 I = 51
49938
XDOT = 6182
509332 Wp = 28
81391
YDOT = 4184
626020 meter/sec RA = 202
35606 deg
ZDOT = -1908
991931 TA = 79
70825
MA = 79
57324
Ha = 188
702 n
mi
Hp = 179
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11417668
73 X = 3487557
93
Y = -9363899
31 feet Y = -2815158
52 meter
Z = 16346560
49 Z = 4999356
17
XDOT = 20283
823267 XDOT = 6144
530274
YDOT = 13729
087993 feet/sec YDOT = 4253
550238 meter/sec
ZDOT = -6263
096885 ZDOT = -1879
048918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1601343
60 X = -488089
53
Y = 14604671
44 feet Y = 4451503
86 meter
Z = 16413259
28 Z = 5002761
43
XDOT = -23077
742247 XDOT = -7034
095837
YDOT = 4420
156853 feet/sec YDOT = 1347
263809 meter/sec
ZDOT = -6144
681367 ZDOT = -1872
898881
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 09328
49272525
00016717 00000-0 10270-3 0 9117
2 25544 51
6451 203
1552 0007408 8
6176 351
5115 15
75939196 31212
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
49272525 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 203
1552 deg
Eccentricity:
0007408
Arg of perigee: 8
6176 deg
Mean anomaly: 351
5115 deg
Mean motion: 15
75939196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 303
Coasting Arc #13 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/329/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5256091
82 A = 6724531
72 meter
Y = -3510407
06 meter E =
0019013
Z = 2262005
33 I = 51
55735
XDOT = 4456
454164 Wp = 52
44387
YDOT = -3147
701245 meter/sec RA = 197
23367 deg
ZDOT = 5450
589368 TA = 333
03691
MA = 333
13557
Ha = 188
972 n
mi
Hp = 179
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17244395
75 X = -5227435
78
Y = -11517083
52 feet Y = -3569023
65 meter
Z = 7421277
33 Z = 2236540
28
XDOT = 14620
912611 XDOT = 4464
842692
YDOT = -10327
103823 feet/sec YDOT = -3097
819876 meter/sec
ZDOT = 17882
511050 ZDOT = 5472
259410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20358014
73 X = 6205122
89
Y = -4128964
52 feet Y = -1258508
38 meter
Z = 7320563
03 Z = 2231307
61
XDOT = -3221
541798 XDOT = -981
925940
YDOT = 16088
985926 feet/sec YDOT = 4903
922910 meter/sec
ZDOT = 17967
939708 ZDOT = 5476
628023
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 09329
50732050
00016717 00000-0 10270-3 0 9125
2 25544 51
6455 197
9301 0007476 13
0491 347
0865 15
75927591 31378
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
50732050 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 197
9301 deg
Eccentricity:
0007476
Arg of perigee: 13
0491 deg
Mean anomaly: 347
0865 deg
Mean motion: 15
75927591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 317
Coasting Arc #14 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2009/330/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4290183
98 A = 6717873
37 meter
Y = 2678914
69 meter E =
0011599
Z = -4428665
85 I = 51
56507
XDOT = -5786
867176 Wp = 71
53333
YDOT = -3884
375536 meter/sec RA = 192
03405 deg
ZDOT = 3266
817026 TA = 231
22207
MA = 231
32574
Ha = 188
824 n
mi
Hp = 179
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14075406
76 X = -4298307
14
Y = 8789090
19 feet Y = 2630894
07 meter
Z = -14529743
61 Z = -4449527
60
XDOT = -18985
784697 XDOT = -5758
871227
YDOT = -12744
014227 feet/sec YDOT = -3948
931288 meter/sec
ZDOT = 10717
903630 ZDOT = 3238
771739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3361802
79 X = 1024677
49
Y = -16176098
05 feet Y = -4930474
69 meter
Z = -14612007
56 Z = -4453739
91
XDOT = 21209
080611 XDOT = 6464
527770
YDOT = -5142
427183 feet/sec YDOT = -1567
411805 meter/sec
ZDOT = 10606
974558 ZDOT = 3233
005845
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 09330
45847457
00016717 00000-0 10270-3 0 9130
2 25544 51
6457 193
0319 0007414 15
2905 344
8482 15
75991455 31529
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
45847457 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 193
0319 deg
Eccentricity:
0007414
Arg of perigee: 15
2905 deg
Mean anomaly: 344
8482 deg
Mean motion: 15
75991455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 323
Coasting Arc #15 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2009/331/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760827
18 A = 6721455
50 meter
Y = 3305872
19 meter E =
0010000
Z = -3416671
64 I = 51
60656
XDOT = -5386
668852 Wp = 46
13134
YDOT = 3011
826494 meter/sec RA = 186
92901 deg
ZDOT = -4593
205153 TA = 174
25373
MA = 174
24225
Ha = 188
875 n
mi
Hp = 179
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15619511
76 X = 4740104
46
Y = 10846037
36 feet Y = 3358994
83 meter
Z = -11209552
62 Z = -3393593
21
XDOT = -17672
798071 XDOT = -5397
633790
YDOT = 9881
320519 feet/sec YDOT = 2951
528456 meter/sec
ZDOT = -15069
570713 ZDOT = -4619
400716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18621414
42 X = -5675807
11
Y = 4109379
80 feet Y = 1252538
96 meter
Z = -11118258
25 Z = -3388845
11
XDOT = 5028
786671 XDOT = 1532
774177
YDOT = -18250
240321 feet/sec YDOT = -5562
673250 meter/sec
ZDOT = -15172
891811 ZDOT = -4624
697424
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 09331
47301225
00016717 00000-0 10270-3 0 9142
2 25544 51
6455 187
8066 0007321 18
1581 341
9844 15
76013029 31686
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
47301225 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 187
8066 deg
Eccentricity:
0007321
Arg of perigee: 18
1581 deg
Mean anomaly: 341
9844 deg
Mean motion: 15
76013029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 302
Coasting Arc #16 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2009/332/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5084590
87 A = 6720706
71 meter
Y = -2630541
34 meter E =
0016820
Z = 3514944
55 I = 51
63516
XDOT = 5041
477270 Wp = 63
41082
YDOT = 3709
744409 meter/sec RA = 181
72492 deg
ZDOT = -4492
607986 TA = 74
72796
MA = 74
54208
Ha = 188
830 n
mi
Hp = 179
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16681728
57 X = 5096552
72
Y = -8630384
97 feet Y = -2573615
74 meter
Z = 11531970
30 Z = 3539675
08
XDOT = 16540
279757 XDOT = 5021
444424
YDOT = 12171
077457 feet/sec YDOT = 3766
009405 meter/sec
ZDOT = -14739
527512 ZDOT = -4468
164301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4673948
23 X = -1424619
42
Y = 18128931
04 feet Y = 5525698
18 meter
Z = 11629532
19 Z = 3544681
41
XDOT = -18840
846830 XDOT = -5742
690114
YDOT = 4585
574094 feet/sec YDOT = 1397
682984 meter/sec
ZDOT = -14642
817673 ZDOT = -4463
130827
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 09332
48752080
00016717 00000-0 10270-3 0 9154
2 25544 51
6454 182
5811 0007541 22
0154 338
1333 15
76108850 31845
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
48752080 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 182
5811 deg
Eccentricity:
0007541
Arg of perigee: 22
0154 deg
Mean anomaly: 338
1333 deg
Mean motion: 15
76108850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 293
Coasting Arc #17 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2009/333/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3974190
89 A = 6718045
74 meter
Y = -3211634
85 meter E =
0012894
Z = 4348897
65 I = 51
65497
XDOT = 6205
528518 Wp = 74
04962
YDOT = -3063
286021 meter/sec RA = 176
62384 deg
ZDOT = 3403
817320 TA = 341
68141
MA = 341
72780
Ha = 189
077 n
mi
Hp = 178
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13038684
02 X = -3959109
23
Y = -10536859
75 feet Y = -3255992
60 meter
Z = 14268036
89 Z = 4329626
86
XDOT = 20359
345531 XDOT = 6222
785890
YDOT = -10050
150989 feet/sec YDOT = -2993
795901 meter/sec
ZDOT = 11167
379660 ZDOT = 3434
006355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16556627
62 X = 5046460
10
Y = -3013489
79 feet Y = -918511
69 meter
Z = 14191776
92 Z = 4325653
61
XDOT = -5918
619626 XDOT = -1803
995262
YDOT = 20709
713277 feet/sec YDOT = 6312
320607 meter/sec
ZDOT = 11286
496027 ZDOT = 3440
123989
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 09333
50200297
00016717 00000-0 10270-3 0 9167
2 25544 51
6445 177
3549 0007550 26
0059 334
1483 15
76092974 32003
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333
50200297 = yrday
fracday
Element set: 916
Inclination: 51
6445 deg
RA of node: 177
3549 deg
Eccentricity:
0007550
Arg of perigee: 26
0059 deg
Mean anomaly: 334
1483 deg
Mean motion: 15
76092974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 304
Coasting Arc #18 (Orbit 3214)
---------------------------------------
Vector Time (GMT): 2009/334/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5671925
97 A = 6723578
75 meter
Y = 2731344
54 meter E =
0012894
Z = -2349840
77 I = 51
70341
XDOT = -4024
092138 Wp = 36
12783
YDOT = -3718
609327 meter/sec RA = 171
42938 deg
ZDOT = 5416
013933 TA = 297
41143
MA = 297
54253
Ha = 188
847 n
mi
Hp = 178
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18608681
02 X = -5690631
35
Y = 8961104
14 feet Y = 2667813
38 meter
Z = -7709451
34 Z = -2377440
96
XDOT = -13202
402028 XDOT = -4008
521711
YDOT = -12200
161834 feet/sec YDOT = -3763
522601 meter/sec
ZDOT = 17769
074582 ZDOT = 5396
501747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5045224
24 X = 1537784
35
Y = -19985965
46 feet Y = -6091722
27 meter
Z = -7818371
55 Z = -2383039
65
XDOT = 16438
485397 XDOT = 5010
450349
YDOT = -2739
324725 feet/sec YDOT = -834
946176 meter/sec
ZDOT = 17691
835431 ZDOT = 5392
471440
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 09334
45305143
00016717 00000-0 10270-3 0 9179
2 25544 51
6435 172
4553 0007454 27
7674 332
3886 15
76151057 32158
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
45305143 = yrday
fracday
Element set: 917
Inclination: 51
6435 deg
RA of node: 172
4553 deg
Eccentricity:
0007454
Arg of perigee: 27
7674 deg
Mean anomaly: 332
3886 deg
Mean motion: 15
76151057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3215
Checksum: 311
Coasting Arc #19 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2009/335/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984170
35 A = 6715061
55 meter
Y = 3348719
80 meter E =
0019167
Z = -5014225
39 I = 51
70312
XDOT = -6743
956890 Wp = 60
35745
YDOT = 3176
454994 meter/sec RA = 166
31788 deg
ZDOT = -1888
315969 TA = 191
38776
MA = 191
43119
Ha = 188
889 n
mi
Hp = 178
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9790585
12 X = 2970861
45
Y = 10986613
51 feet Y = 3382016
80 meter
Z = -16450870
70 Z = -4999759
77
XDOT = -22125
842816 XDOT = -6769
801986
YDOT = 10421
440270 feet/sec YDOT = 3100
895835 meter/sec
ZDOT = -6195
262366 ZDOT = -1921
141370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14759086
75 X = -4498569
64
Y = 782462
54 feet Y = 238494
58 meter
Z = -16393580
79 Z = -4996763
42
XDOT = 5838
575232 XDOT = 1779
597731
YDOT = -22653
715203 feet/sec YDOT = -6904
852394 meter/sec
ZDOT = -6324
827517 ZDOT = -1927
807427
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 09335
46747692
00016717 00000-0 10270-3 0 9181
2 25544 51
6421 167
2284 0007431 31
5929 328
5680 15
76205387 32310
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335
46747692 = yrday
fracday
Element set: 918
Inclination: 51
6421 deg
RA of node: 167
2284 deg
Eccentricity:
0007431
Arg of perigee: 31
5929 deg
Mean anomaly: 328
5680 deg
Mean motion: 15
76205387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 325
Coasting Arc #20 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2009/336/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6039096
68 A = 6725368
22 meter
Y = -2812065
04 meter E =
0015626
Z = 900984
83 I = 51
76789
XDOT = 2771
582583 Wp = 96
70334
YDOT = 4015
086356 meter/sec RA = 161
14790 deg
ZDOT = -5959
749843 TA = 73
47248
MA = 73
30088
Ha = 188
888 n
mi
Hp = 178
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19813309
30 X = 6065715
92
Y = -9225935
18 feet Y = -2744383
61 meter
Z = 2955986
99 Z = 930387
65
XDOT = 9093
118710 XDOT = 2755
431224
YDOT = 13172
855500 feet/sec YDOT = 4045
990444 meter/sec
ZDOT = -19552
985049 ZDOT = -5946
323801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4904029
53 X = -1494748
20
Y = 21282290
16 feet Y = 6486842
04 meter
Z = 3072065
19 Z = 936365
47
XDOT = -14497
194614 XDOT = -4418
744918
YDOT = -486
583218 feet/sec YDOT = -148
310565 meter/sec
ZDOT = -19499
772413 ZDOT = -5943
530632
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 09336
48187423
00016717 00000-0 10270-3 0 9195
2 25544 51
6424 162
0021 0007502 35
2711 324
8948 15
76260878 32473
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336
48187423 = yrday
fracday
Element set: 919
Inclination: 51
6424 deg
RA of node: 162
0021 deg
Eccentricity:
0007502
Arg of perigee: 35
2711 deg
Mean anomaly: 324
8948 deg
Mean motion: 15
76260878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 312
Coasting Arc #21 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2009/337/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1851765
90 A = 6713649
82 meter
Y = -3719807
93 meter E =
0008879
Z = 5267028
08 I = 51
75562
XDOT = 6989
421151 Wp = 53
38635
YDOT = -3252
495537 meter/sec RA = 156
01349 deg
ZDOT = 165
271728 TA = 35
07903
MA = 35
02059
Ha = 188
974 n
mi
Hp = 178
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6075347
45 X = -1835619
40
Y = -12204094
25 feet Y = -3740426
05 meter
Z = 17280275
87 Z = 5258070
68
XDOT = 22931
171754 XDOT = 7024
468778
YDOT = -10670
917116 feet/sec YDOT = -3174
139774 meter/sec
ZDOT = 542
230080 ZDOT = 199
311475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13464209
92 X = 4103891
18
Y = 2406657
81 feet Y = 733549
30 meter
Z = 17244730
98 Z = 5256194
00
XDOT = -5091
241350 XDOT = -1551
810363
YDOT = 23752
861653 feet/sec YDOT = 7239
872232 meter/sec
ZDOT = 676
639143 ZDOT = 206
239611
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 09337
49624395
00016717 00000-0 10270-3 0 9203
2 25544 51
6416 156
7745 0007434 39
3739 320
7964 15
76265642 32631
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337
49624395 = yrday
fracday
Element set: 920
Inclination: 51
6416 deg
RA of node: 156
7745 deg
Eccentricity:
0007434
Arg of perigee: 39
3739 deg
Mean anomaly: 320
7964 deg
Mean motion: 15
76265642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
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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