Date:
September 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2112)
---------------------------------------
Vector Time (GMT): 2009/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2297990
96 A = 6720134
64 meter
Y = -3723243
83 meter E =
0013621
Z = 5091879
37 I = 51
67068
XDOT = 7189
083305 Wp = 118
44233
YDOT = -2319
904816 meter/sec RA = 171
38182 deg
ZDOT = 1538
652669 TA = 316
76478
MA = 316
87162
Ha = 192
855 n
mi
Hp = 180
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7539340
43 X = -2280922
03
Y = -12215366
91 feet Y = -3748845
54 meter
Z = 16705640
98 Z = 5080757
27
XDOT = 23586
231314 XDOT = 7207
015956
YDOT = -7611
236274 feet/sec YDOT = -2239
411883 meter/sec
ZDOT = 5048
073060 ZDOT = 1573
621485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7578803
65 X = 2310019
35
Y = 12251066
29 feet Y = 3734125
01 meter
Z = 16661584
35 Z = 5078450
91
XDOT = -22698
746496 XDOT = -6918
577932
YDOT = 6947
058199 feet/sec YDOT = 2117
463339 meter/sec
ZDOT = 5185
652392 ZDOT = 1580
586849
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 09264
55031164
00020000 00000-0 20000-3 0 9005
2 25544 51
6398 172
1370 0008788 113
9736 246
2355 15
74277084 21135
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
55031164 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 172
1370 deg
Eccentricity:
0008788
Arg of perigee: 113
9736 deg
Mean anomaly: 246
2355 deg
Mean motion: 15
74277084 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2113
Checksum: 292
Coasting Arc #2 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2009/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6116416
70 A = 6730640
32 meter
Y = 2515475
96 meter E =
0013629
Z = -1250855
54 I = 51
73593
XDOT = -2862
143907 Wp = 76
98662
YDOT = -4067
245340 meter/sec RA = 166
22364 deg
ZDOT = 5872
457590 TA = 269
32200
MA = 269
47817
Ha = 192
707 n
mi
Hp = 180
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20066983
91 X = -6138014
07
Y = 8252873
89 feet Y = 2446957
77 meter
Z = -4103856
75 Z = -1280622
13
XDOT = -9390
235916 XDOT = -2844
978331
YDOT = -13343
980773 feet/sec YDOT = -4099
155258 meter/sec
ZDOT = 19266
593144 ZDOT = 5858
594969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19938199
69 X = 6077163
27
Y = -8502189
32 feet Y = -2591467
30 meter
Z = -4220945
48 Z = -1286544
18
XDOT = 9048
162830 XDOT = 2757
880031
YDOT = 11770
177211 feet/sec YDOT = 3587
550014 meter/sec
ZDOT = 19211
718889 ZDOT = 5855
731917
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 09265
50249405
00020000 00000-0 20000-3 0 9011
2 25544 51
6400 167
2450 0008753 117
1369 243
0688 15
74283601 21285
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
50249405 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 167
2450 deg
Eccentricity:
0008753
Arg of perigee: 117
1369 deg
Mean anomaly: 243
0688 deg
Mean motion: 15
74283601 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2128
Checksum: 278
Coasting Arc #3 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2009/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2663143
02 A = 6719757
00 meter
Y = 3397796
67 meter E =
0021509
Z = -5167482
02 I = 51
72844
XDOT = -6781
798832 Wp = 95
63816
YDOT = 3384
260456 meter/sec RA = 161
11517 deg
ZDOT = -1276
442674 TA = 162
18730
MA = 162
11178
Ha = 192
618 n
mi
Hp = 180
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8737345
87 X = 2650053
39
Y = 11147626
87 feet Y = 3427504
16 meter
Z = -16953681
18 Z = -5154576
19
XDOT = -22249
996167 XDOT = -6812
937359
YDOT = 11103
216720 feet/sec YDOT = 3308
248247 meter/sec
ZDOT = -4187
804049 ZDOT = -1309
464855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9162953
51 X = -2792868
23
Y = -10880251
44 feet Y = -3316300
64 meter
Z = -16902618
57 Z = -5151918
14
XDOT = 21092
546194 XDOT = 6429
008080
YDOT = -11089
567429 feet/sec YDOT = -3380
100152 meter/sec
ZDOT = -4317
676432 ZDOT = -1316
027777
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 09266
51813764
00020000 00000-0 20000-3 0 9029
2 25544 51
6403 162
0265 0008702 120
7187 239
4835 15
74323399 21447
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
51813764 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 162
0265 deg
Eccentricity:
0008702
Arg of perigee: 120
7187 deg
Mean anomaly: 239
4835 deg
Mean motion: 15
74323399 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2144
Checksum: 288
Coasting Arc #4 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2009/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5714666
38 A = 6730892
89 meter
Y = -3396175
74 meter E =
0022516
Z = 983590
00 I = 51
79346
XDOT = 3229
230106 Wp = 124
93699
YDOT = 3686
878743 meter/sec RA = 155
96523 deg
ZDOT = -5948
944778 TA = 44
32795
MA = 44
14788
Ha = 192
625 n
mi
Hp = 180
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18748905
46 X = 5747440
12
Y = -11142308
85 feet Y = -3332087
71 meter
Z = 3227001
30 Z = 1011431
83
XDOT = 10594
586961 XDOT = 3216
662014
YDOT = 12096
058867 feet/sec YDOT = 3722
919514 meter/sec
ZDOT = -19517
535362 ZDOT = -5933
287595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18187038
48 X = -5543409
33
Y = 12007729
68 feet Y = 3659956
01 meter
Z = 3336480
06 Z = 1016959
12
XDOT = -10387
689925 XDOT = -3166
167889
YDOT = -10254
418217 feet/sec YDOT = -3125
546673 meter/sec
ZDOT = -19455
611772 ZDOT = -5930
070468
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 09267
53376562
00020000 00000-0 20000-3 0 9033
2 25544 51
6400 156
8081 0008769 125
4505 234
7478 15
74296896 21600
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
53376562 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 156
8081 deg
Eccentricity:
0008769
Arg of perigee: 125
4505 deg
Mean anomaly: 234
7478 deg
Mean motion: 15
74296896 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2160
Checksum: 315
Coasting Arc #5 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2009/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2968092
77 A = 6719399
52 meter
Y = -3034542
98 meter E =
0012245
Z = 5201614
23 I = 51
78246
XDOT = 6256
656709 Wp = 127
39885
YDOT = -4390
268829 meter/sec RA = 150
85595 deg
ZDOT = 999
998428 TA = 313
04586
MA = 313
14833
Ha = 192
516 n
mi
Hp = 180
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9737837
17 X = -2959208
10
Y = -9955849
68 feet Y = -3067684
19 meter
Z = 17065663
49 Z = 5187216
74
XDOT = 20527
088939 XDOT = 6300
426591
YDOT = -14403
769125 feet/sec YDOT = -4320
058468 meter/sec
ZDOT = 3280
834736 ZDOT = 1030
499892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10454550
18 X = 3186546
89
Y = 9305181
82 feet Y = 2836219
42 meter
Z = 17008740
63 Z = 5184264
15
XDOT = -18864
587000 XDOT = -5749
926118
YDOT = 14925
049821 feet/sec YDOT = 4549
155185 meter/sec
ZDOT = 3400
745682 ZDOT = 1036
547284
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 09268
54937389
00020000 00000-0 20000-3 0 9046
2 25544 51
6402 151
5897 0008577 128
8354 231
3576 15
74369118 21762
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
54937389 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 151
5897 deg
Eccentricity:
0008577
Arg of perigee: 128
8354 deg
Mean anomaly: 231
3576 deg
Mean motion: 15
74369118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2176
Checksum: 330
Coasting Arc #6 (Orbit 2190)
---------------------------------------
Vector Time (GMT): 2009/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5176471
31 A = 6730766
82 meter
Y = 4236710
71 meter E =
0013089
Z = -743944
56 I = 51
84680
XDOT = -3537
654490 Wp = 79
96692
YDOT = -3286
050670 meter/sec RA = 145
71359 deg
ZDOT = 5992
749322 TA = 271
95261
MA = 272
10250
Ha = 192
259 n
mi
Hp = 180
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16983173
58 X = -5219848
24
Y = 13899969
52 feet Y = 4178581
81 meter
Z = -2440762
98 Z = -769197
42
XDOT = -11606
477986 XDOT = -3529
758220
YDOT = -10781
006134 feet/sec YDOT = -3325
566549 meter/sec
ZDOT = 19661
251055 ZDOT = 5975
582546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15784028
73 X = 4810971
96
Y = -15231789
80 feet Y = -4642649
53 meter
Z = -2540015
29 Z = -774196
66
XDOT = 11446
875053 XDOT = 3489
007516
YDOT = 8642
422507 feet/sec YDOT = 2634
210380 meter/sec
ZDOT = 19593
394629 ZDOT = 5972
066683
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 09269
50149243
00020000 00000-0 20000-3 0 9058
2 25544 51
6403 146
6970 0008459 132
6076 227
5802 15
74400608 21919
Satellite: ISS
Catalog Number: 25544
Epoch time: 09269
50149243 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 146
6970 deg
Eccentricity:
0008459
Arg of perigee: 132
6076 deg
Mean anomaly: 227
5802 deg
Mean motion: 15
74400608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2191
Checksum: 289
Coasting Arc #7 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2009/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3187995
12 A = 6719041
05 meter
Y = 2733880
80 meter E =
0021002
Z = -5261861
75 I = 51
83107
XDOT = -5576
538277 Wp = 103
10461
YDOT = 5249
638013 meter/sec RA = 140
60162 deg
ZDOT = -657
963788 TA = 160
68495
MA = 160
60522
Ha = 192
130 n
mi
Hp = 180
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10459301
59 X = 3182748
71
Y = 8969425
18 feet Y = 2769501
35 meter
Z = -17263325
94 Z = -5246387
24
XDOT = -18295
729254 XDOT = -5631
629896
YDOT = 17223
221826 feet/sec YDOT = 5186
969827 meter/sec
ZDOT = -2158
673845 ZDOT = -685
188652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11390561
71 X = -3471843
21
Y = -7887364
86 feet Y = -2404068
81 meter
Z = -17202167
88 Z = -5243220
77
XDOT = 15925
575461 XDOT = 4854
115400
YDOT = -18106
801570 feet/sec YDOT = -5518
953118 meter/sec
ZDOT = -2265
646962 ZDOT = -690
569194
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 09270
51706833
00020000 00000-0 20000-3 0 9066
2 25544 51
6399 141
4778 0008319 136
4531 223
7291 15
74429096 22075
Satellite: ISS
Catalog Number: 25544
Epoch time: 09270
51706833 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 141
4778 deg
Eccentricity:
0008319
Arg of perigee: 136
4531 deg
Mean anomaly: 223
7291 deg
Mean motion: 15
74429096 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2207
Checksum: 303
Coasting Arc #8 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2009/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4552100
35 A = 6730972
46 meter
Y = -4926573
66 meter E =
0021406
Z = 407610
69 I = 51
89357
XDOT = 3756
766662 Wp = 134
87354
YDOT = 2956
297547 meter/sec RA = 135
46930 deg
ZDOT = -6046
373054 TA = 40
70539
MA = 40
54561
Ha = 192
166 n
mi
Hp = 180
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14934712
42 X = 4604871
72
Y = -16163299
42 feet Y = -4875374
32 meter
Z = 1337305
40 Z = 429853
22
XDOT = 12325
349942 XDOT = 3752
801864
YDOT = 9699
138933 feet/sec YDOT = 2998
285498 meter/sec
ZDOT = -19837
181936 ZDOT = -6028
132405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12961151
76 X = -3950559
06
Y = 17778220
56 feet Y = 5418801
63 meter
Z = 1424671
19 Z = 434239
78
XDOT = -12180
830049 XDOT = -3712
716999
YDOT = -7252
790835 feet/sec YDOT = -2210
650646 meter/sec
ZDOT = -19765
102477 ZDOT = -6024
403235
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 09271
53262879
00020000 00000-0 20000-3 0 9077
2 25544 51
6401 136
2595 0008461 141
0251 219
1524 15
74398023 22238
Satellite: ISS
Catalog Number: 25544
Epoch time: 09271
53262879 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 136
2595 deg
Eccentricity:
0008461
Arg of perigee: 141
0251 deg
Mean anomaly: 219
1524 deg
Mean motion: 15
74398023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2223
Checksum: 277
Coasting Arc #9 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2009/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3371166
39 A = 6718817
89 meter
Y = -2426582
83 meter E =
0010341
Z = 5275195
26 I = 51
87326
XDOT = 4807
364577 Wp = 135
76246
YDOT = -6017
351835 meter/sec RA = 130
35405 deg
ZDOT = 296
614976 TA = 311
38905
MA = 311
47790
Ha = 192
045 n
mi
Hp = 180
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11060257
19 X = -3369407
37
Y = -7961229
74 feet Y = -2464271
04 meter
Z = 17307071
06 Z = 5258822
52
XDOT = 15772
193493 XDOT = 4872
853445
YDOT = -19741
967964 feet/sec YDOT = -5963
226868 meter/sec
ZDOT = 973
146246 ZDOT = 320
128636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12117450
28 X = 3693398
84
Y = 6411927
18 feet Y = 1954355
40 meter
Z = 17242382
82 Z = 5255478
28
XDOT = -12543
875958 XDOT = -3823
373392
YDOT = 20773
287864 feet/sec YDOT = 6331
698141 meter/sec
ZDOT = 1065
463026 ZDOT = 324
753130
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 09272
54816931
00020000 00000-0 20000-3 0 9084
2 25544 51
6397 131
0403 0008252 144
5377 215
6336 15
74459901 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 09272
54816931 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 131
0403 deg
Eccentricity:
0008252
Arg of perigee: 144
5377 deg
Mean anomaly: 215
6336 deg
Mean motion: 15
74459901 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2239
Checksum: 296
Coasting Arc #10 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2009/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3822292
00 A = 6730753
24 meter
Y = 5538220
19 meter E =
0012753
Z = -92477
75 I = 51
93125
XDOT = -3947
957399 Wp = 82
76799
YDOT = -2635
436187 meter/sec RA = 125
22885 deg
ZDOT = 6058
506842 TA = 276
23189
MA = 276
37715
Ha = 191
751 n
mi
Hp = 181
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12540328
07 X = -3883488
01
Y = 18170013
75 feet Y = 5495134
90 meter
Z = -303404
69 Z = -111195
59
XDOT = -12952
616139 XDOT = -3947
625326
YDOT = -8646
444182 feet/sec YDOT = -2679
582242 meter/sec
ZDOT = 19876
990953 ZDOT = 6039
328603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9680427
32 X = 2950594
25
Y = -19840579
42 feet Y = -6047408
61 meter
Z = -376852
53 Z = -114864
65
XDOT = 12767
485447 XDOT = 3891
529564
YDOT = 5888
905553 feet/sec YDOT = 1794
938413 meter/sec
ZDOT = 19801
227629 ZDOT = 6035
414181
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 09273
50022314
00020000 00000-0 20000-3 0 9096
2 25544 51
6387 126
1466 0008143 148
6482 211
5168 15
74495445 22542
Satellite: ISS
Catalog Number: 25544
Epoch time: 09273
50022314 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 126
1466 deg
Eccentricity:
0008143
Arg of perigee: 148
6482 deg
Mean anomaly: 211
5168 deg
Mean motion: 15
74495445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2254
Checksum: 290
Coasting Arc #11 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2009/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3519277
86 A = 6718610
67 meter
Y = 2207876
12 meter E =
0020205
Z = -5296289
39 I = 51
90549
XDOT = -3940
894003 Wp = 111
71832
YDOT = 6599
795267 meter/sec RA = 120
10788 deg
ZDOT = 125
703981 TA = 159
51276
MA = 159
43161
Ha = 191
633 n
mi
Hp = 181
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11546187
19 X = 3520056
05
Y = 7243688
06 feet Y = 2247234
61 meter
Z = -17376277
54 Z = -5279190
94
XDOT = -12929
442266 XDOT = -4015
011810
YDOT = 21652
871610 feet/sec YDOT = 6555
311466 meter/sec
ZDOT = 412
414636 ZDOT = 106
378327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12690892
32 X = -3868183
98
Y = -5202819
38 feet Y = -1585819
35 meter
Z = -17308737
66 Z = -5275703
24
XDOT = 8766
156987 XDOT = 2671
924650
YDOT = -22578
457985 feet/sec YDOT = -6881
913994 meter/sec
ZDOT = 336
629330 ZDOT = 102
604620
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 09274
51573018
00020000 00000-0 20000-3 0 9102
2 25544 51
6374 120
9261 0008112 152
5248 207
6346 15
74526878 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 09274
51573018 = yrday
fracday
Element set: 910
Inclination: 51
6374 deg
RA of node: 120
9261 deg
Eccentricity:
0008112
Arg of perigee: 152
5248 deg
Mean anomaly: 207
6346 deg
Mean motion: 15
74526878 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2270
Checksum: 284
Coasting Arc #12 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2009/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3056495
90 A = 6730611
95 meter
Y = -5976808
08 meter E =
0019448
Z = -313109
12 I = 51
96007
XDOT = 4108
631812 Wp = 145
29928
YDOT = 2408
209271 meter/sec RA = 114
99350 deg
ZDOT = -6059
988440 TA = 38
09219
MA = 37
95487
Ha = 191
536 n
mi
Hp = 181
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10027873
67 X = 3124623
48
Y = -19608950
40 feet Y = -5942247
66 meter
Z = -1027260
90 Z = -298094
39
XDOT = 13479
763163 XDOT = 4110
836116
YDOT = 7900
949053 feet/sec YDOT = 2454
166109 meter/sec
ZDOT = -19881
851837 ZDOT = -6040
023369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6266110
00 X = -1909910
33
Y = 21116876
38 feet Y = 6436423
92 meter
Z = -968425
97 Z = -295176
24
XDOT = -13274
309833 XDOT = -4046
009637
YDOT = -4815
491138 feet/sec YDOT = -1467
761699 meter/sec
ZDOT = -19802
998878 ZDOT = -6035
954058
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 09275
53121958
00020000 00000-0 20000-3 0 9118
2 25544 51
6374 115
7072 0008072 156
6443 203
5089 15
74539465 22861
Satellite: ISS
Catalog Number: 25544
Epoch time: 09275
53121958 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 115
7072 deg
Eccentricity:
0008072
Arg of perigee: 156
6443 deg
Mean anomaly: 203
5089 deg
Mean motion: 15
74539465 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2286
Checksum: 301
Coasting Arc #13 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2009/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3662835
09 A = 6718624
50 meter
Y = -1993085
11 meter E =
0008374
Z = 5262930
38 I = 51
93040
XDOT = 3029
183804 Wp = 141
17154
YDOT = -7063
511550 meter/sec RA = 109
86644 deg
ZDOT = -572
650880 TA = 314
20982
MA = 314
27857
Ha = 191
534 n
mi
Hp = 181
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12017175
51 X = -3665842
64
Y = -6538993
15 feet Y = -2034061
36 meter
Z = 17266831
96 Z = 5245128
93
XDOT = 9938
267074 XDOT = 3110
725958
YDOT = -23174
250492 feet/sec YDOT = -7029
181565 meter/sec
ZDOT = -1878
775852 ZDOT = -557
736048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13181979
64 X = 4017867
39
Y = 3978571
05 feet Y = 1212668
46 meter
Z = 17196534
82 Z = 5241503
81
XDOT = -4814
647036 XDOT = -1467
504417
YDOT = 23736
373144 feet/sec YDOT = 7234
846534 meter/sec
ZDOT = -1820
390533 ZDOT = -554
855035
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 09276
54669064
00020000 00000-0 20000-3 0 9126
2 25544 51
6365 110
4866 0008082 160
6907 199
4564 15
74550768 23024
Satellite: ISS
Catalog Number: 25544
Epoch time: 09276
54669064 = yrday
fracday
Element set: 912
Inclination: 51
6365 deg
RA of node: 110
4866 deg
Eccentricity:
0008082
Arg of perigee: 160
6907 deg
Mean anomaly: 199
4564 deg
Mean motion: 15
74550768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2302
Checksum: 312
Coasting Arc #14 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2009/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2230353
62 A = 6730275
40 meter
Y = 6309451
55 meter E =
0012746
Z = 702702
22 I = 51
97802
XDOT = -4281
273109 Wp = 88
13729
YDOT = -2192
994863 meter/sec RA = 104
75868 deg
ZDOT = 6009
288304 TA = 279
48054
MA = 279
62458
Ha = 191
237 n
mi
Hp = 181
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7317433
14 X = -2304154
91
Y = 20700300
37 feet Y = 6284097
85 meter
Z = 2305453
48 Z = 691687
06
XDOT = -14046
171618 XDOT = -4285
625141
YDOT = -7194
865036 feet/sec YDOT = -2240
894342 meter/sec
ZDOT = 19715
512807 ZDOT = 5988
479066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2660597
35 X = 810950
07
Y = -21798284
42 feet Y = -6644117
09 meter
Z = 2262387
40 Z = 689575
68
XDOT = 13795
816976 XDOT = 4204
965014
YDOT = 3753
694568 feet/sec YDOT = 1144
126104 meter/sec
ZDOT = 19633
348214 ZDOT = 5984
244536
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 09277
56214232
00020000 00000-0 20000-3 0 9133
2 25544 51
6354 105
2654 0008050 164
7590 195
3817 15
74597316 23180
Satellite: ISS
Catalog Number: 25544
Epoch time: 09277
56214232 = yrday
fracday
Element set: 913
Inclination: 51
6354 deg
RA of node: 105
2654 deg
Eccentricity:
0008050
Arg of perigee: 164
7590 deg
Mean anomaly: 195
3817 deg
Mean motion: 15
74597316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2318
Checksum: 295
Coasting Arc #15 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2009/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 726328
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3825383
76 A = 6718686
84 meter
Y = 1861490
47 meter E =
0018898
Z = -5215424
33 I = 51
94533
XDOT = -2092
135859 Wp = 121
94325
YDOT = 7320
805307 meter/sec RA = 99
62414 deg
ZDOT = 1071
465638 TA = 158
29034
MA = 158
21013
Ha = 191
135 n
mi
Hp = 181
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12550471
64 X = 3829620
17
Y = 6107252
18 feet Y = 1904291
45 meter
Z = -17110972
22 Z = -5196830
00
XDOT = -6863
962791 XDOT = -2179
047998
YDOT = 24018
390116 feet/sec YDOT = 7296
923943 meter/sec
ZDOT = 3515
307212 ZDOT = 1061
090106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13727649
43 X = -4184187
55
Y = -2978489
43 feet Y = -907843
58 meter
Z = -17037560
86 Z = -5193048
55
XDOT = 857
871449 XDOT = 261
479218
YDOT = -23961
423610 feet/sec YDOT = -7303
441916 meter/sec
ZDOT = 3474
805924 ZDOT = 1059
120845
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 09278
51411151
00020000 00000-0 20000-3 0 9149
2 25544 51
6351 100
3706 0008111 167
7125 192
4238 15
74630428 23330
Satellite: ISS
Catalog Number: 25544
Epoch time: 09278
51411151 = yrday
fracday
Element set: 914
Inclination: 51
6351 deg
RA of node: 100
3706 deg
Eccentricity:
0008111
Arg of perigee: 167
7125 deg
Mean anomaly: 192
4238 deg
Mean motion: 15
74630428 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2333
Checksum: 261
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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