Date:
November 8th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2837)
---------------------------------------
Vector Time (GMT): 2009/310/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3203973
17 A = 6726568
47 meter
Y = 5889051
52 meter E =
0005615
Z = -504591
16 I = 51
35950
XDOT = -4021
960151 Wp = 159
71451
YDOT = -2699
094210 meter/sec RA = 295
09907 deg
ZDOT = -5988
015121 TA = 25
79945
MA = 25
77146
Ha = 186
145 n
mi
Hp = 182
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10511723
01 X = -3267136
17
Y = 19321035
18 feet Y = 5852869
69 meter
Z = -1655482
82 Z = -520309
37
XDOT = -13195
407321 XDOT = -3962
390134
YDOT = -8855
295966 feet/sec YDOT = -2743
736580 meter/sec
ZDOT = -19645
718900 ZDOT = -6007
409767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8966042
96 X = -2732849
89
Y = -20079850
82 feet Y = -6120338
53 meter
Z = -1717267
96 Z = -523423
28
XDOT = 13516
643658 XDOT = 4119
872987
YDOT = -4355
534570 feet/sec YDOT = -1327
566937 meter/sec
ZDOT = -19722
289092 ZDOT = -6011
353715
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 09310
55155124
00016717 00000-0 10270-3 0 9008
2 25544 51
6424 295
5889 0006201 300
2651 59
7899 15
75929877 28384
Satellite: ISS
Catalog Number: 25544
Epoch time: 09310
55155124 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 295
5889 deg
Eccentricity:
0006201
Arg of perigee: 300
2651 deg
Mean anomaly: 59
7899 deg
Mean motion: 15
75929877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 336
Coasting Arc #2 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2009/311/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3342909
67 A = 6715131
67 meter
Y = 2793986
80 meter E =
0006198
Z = 5112568
51 I = 51
30920
XDOT = -3558
894124 Wp = 344
16259
YDOT = 6700
096711 meter/sec RA = 289
91071 deg
ZDOT = -1329
032138 TA = 118
64056
MA = 118
57821
Ha = 186
194 n
mi
Hp = 182
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10967551
42 X = 3286582
01
Y = 9166623
34 feet Y = 2831053
87 meter
Z = 16773518
75 Z = 5128672
03
XDOT = -11676
161824 XDOT = -3627
094955
YDOT = 21981
944591 feet/sec YDOT = 6659
917824 meter/sec
ZDOT = -4360
341660 ZDOT = -1346
486730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13830056
52 X = -4215401
23
Y = 3302421
04 feet Y = 1006577
93 meter
Z = 16837121
21 Z = 5131954
55
XDOT = -10528
234915 XDOT = -3209
006002
YDOT = -21418
337455 feet/sec YDOT = -6528
309256 meter/sec
ZDOT = -4428
945191 ZDOT = -1349
942494
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 09311
56612955
00016717 00000-0 10270-3 0 9011
2 25544 51
6421 290
3640 0006263 303
4865 56
5700 15
75956171 28540
Satellite: ISS
Catalog Number: 25544
Epoch time: 09311
56612955 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 290
3640 deg
Eccentricity:
0006263
Arg of perigee: 303
4865 deg
Mean anomaly: 56
5700 deg
Mean motion: 15
75956171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2854
Checksum: 305
Coasting Arc #3 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2009/312/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3004364
68 A = 6724931
17 meter
Y = -5730149
29 meter E =
0012270
Z = 1805453
85 I = 51
33417
XDOT = 3694
265958 Wp = 40
17497
YDOT = 3720
778863 meter/sec RA = 284
76615 deg
ZDOT = 5649
522677 TA = 339
96028
MA = 340
00842
Ha = 186
145 n
mi
Hp = 182
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9856839
49 X = 3059446
22
Y = -18799702
39 feet Y = -5696244
83 meter
Z = 5923405
03 Z = 1820182
76
XDOT = 12120
295137 XDOT = 3624
940248
YDOT = 12207
279735 feet/sec YDOT = 3761
702408 meter/sec
ZDOT = 18535
179385 ZDOT = 5667
301473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9620824
02 X = 2932427
16
Y = 18903352
88 feet Y = 5761741
96 meter
Z = 5981288
90 Z = 1823096
86
XDOT = -15532
493047 XDOT = -4734
303881
YDOT = 2005
828603 feet/sec YDOT = 611
376558 meter/sec
ZDOT = 18605
429510 ZDOT = 5670
934915
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 09312
58067935
00016717 00000-0 10270-3 0 9027
2 25544 51
6422 285
1390 0006160 306
1709 53
8885 15
76040732 28708
Satellite: ISS
Catalog Number: 25544
Epoch time: 09312
58067935 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 285
1390 deg
Eccentricity:
0006160
Arg of perigee: 306
1709 deg
Mean anomaly: 53
8885 deg
Mean motion: 15
76040732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 309
Coasting Arc #4 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2009/313/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3150908
65 A = 6716936
70 meter
Y = -3696253
37 meter E =
0005621
Z = -4644264
55 I = 51
30065
XDOT = 3338
310027 Wp = 84
53434
YDOT = -6351
328045 meter/sec RA = 279
55352 deg
ZDOT = 2793
406721 TA = 213
14885
MA = 213
18408
Ha = 186
400 n
mi
Hp = 182
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10337626
80 X = -3086781
02
Y = -12126815
50 feet Y = -3731130
00 meter
Z = -15237088
41 Z = -4659416
20
XDOT = 10952
460718 XDOT = 3395
513528
YDOT = -20837
690435 feet/sec YDOT = -6313
677329 meter/sec
ZDOT = 9164
720212 ZDOT = 2809
763218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15797817
28 X = 4815174
71
Y = -1589424
38 feet Y = -484456
55 meter
Z = -15296984
83 Z = -4662520
98
XDOT = 10899
930202 XDOT = 3322
298725
YDOT = 19623
830442 feet/sec YDOT = 5981
343519 meter/sec
ZDOT = 9228
994397 ZDOT = 2812
997492
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 09313
53179811
00016717 00000-0 10270-3 0 9031
2 25544 51
6422 280
2401 0006298 311
3968 48
6655 15
76027563 28854
Satellite: ISS
Catalog Number: 25544
Epoch time: 09313
53179811 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 280
2401 deg
Eccentricity:
0006298
Arg of perigee: 311
3968 deg
Mean anomaly: 48
6655 deg
Mean motion: 15
76027563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 319
Coasting Arc #5 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/314/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2853038
23 A = 6722133
30 meter
Y = 5272734
13 meter E =
0003250
Z = -3044489
45 I = 51
31557
XDOT = -3562
724283 Wp = 358
23696
YDOT = -4755
767549 meter/sec RA = 274
42483 deg
ZDOT = -4894
459467 TA = 217
21718
MA = 217
23971
Ha = 186
553 n
mi
Hp = 181
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9360361
64 X = -2896997
01
Y = 17298996
49 feet Y = 5240584
00 meter
Z = -9988482
46 Z = -3058456
47
XDOT = -11688
727963 XDOT = -3485
502916
YDOT = -15602
911905 feet/sec YDOT = -4795
176238 meter/sec
ZDOT = -16057
937884 ZDOT = -4911
579892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9300339
50 X = -2834743
48
Y = -17299592
44 feet Y = -5272915
78 meter
Z = -10043366
85 Z = -3061218
22
XDOT = 18148
795162 XDOT = 5531
752765
YDOT = -388
714223 feet/sec YDOT = -118
480095 meter/sec
ZDOT = -16125
647387 ZDOT = -4915
097324
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 09314
54629678
00016717 00000-0 10270-3 0 9045
2 25544 51
6427 275
0143 0006329 315
6262 44
4394 15
76096503 29016
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54629678 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 275
0143 deg
Eccentricity:
0006329
Arg of perigee: 315
6262 deg
Mean anomaly: 44
4394 deg
Mean motion: 15
76096503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 315
Coasting Arc #6 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/315/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3115581
76 A = 6719710
36 meter
Y = 4574704
75 meter E =
0009632
Z = 3809601
85 I = 51
30681
XDOT = -3227
262622 Wp = 47
75474
YDOT = 5645
894861 meter/sec RA = 269
19899 deg
ZDOT = -4127
412715 TA = 85
65846
MA = 85
54841
Ha = 186
604 n
mi
Hp = 181
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10221724
92 X = 3045688
35
Y = 15008873
84 feet Y = 4609154
25 meter
Z = 12498693
72 Z = 3824567
82
XDOT = -10588
131962 XDOT = -3270
105541
YDOT = 18523
277102 feet/sec YDOT = 5609
566130 meter/sec
ZDOT = -13541
380300 ZDOT = -4143
195158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18111226
41 X = -5520301
81
Y = 499795
40 feet Y = 152337
64 meter
Z = 12557905
14 Z = 3827649
49
XDOT = -9944
532415 XDOT = -3031
093480
YDOT = -17491
983892 feet/sec YDOT = -5331
556690 meter/sec
ZDOT = -13603
405287 ZDOT = -4146
317932
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 09315
56076820
00016717 00000-0 10270-3 0 9054
2 25544 51
6428 269
7887 0006361 319
1174 40
9513 15
76139401 29175
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56076820 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 269
7887 deg
Eccentricity:
0006361
Arg of perigee: 319
1174 deg
Mean anomaly: 40
9513 deg
Mean motion: 15
76139401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 323
Coasting Arc #7 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2009/316/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2827590
52 A = 6718562
82 meter
Y = -4509808
30 meter E =
0006692
Z = 4092447
46 I = 51
30557
XDOT = 3614
184235 Wp = 69
71111
YDOT = 5677
221804 meter/sec RA = 264
07502 deg
ZDOT = 3756
394029 TA = 341
63511
MA = 341
65926
Ha = 186
522 n
mi
Hp = 181
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9276871
78 X = 2857928
98
Y = -14795959
00 feet Y = -4478018
86 meter
Z = 13426664
88 Z = 4106257
94
XDOT = 11857
559825 XDOT = 3532
183617
YDOT = 18626
055788 feet/sec YDOT = 5717
179281 meter/sec
ZDOT = 12324
127393 ZDOT = 3773
752929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7809733
19 X = 2380406
68
Y = 15573310
83 feet Y = 4746745
14 meter
Z = 13480954
72 Z = 4108995
00
XDOT = -20903
730888 XDOT = -6371
457175
YDOT = -252
479140 feet/sec YDOT = -76
955642 meter/sec
ZDOT = 12392
826277 ZDOT = 3777
333449
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 09316
57521141
00016717 00000-0 10270-3 0 9068
2 25544 51
6432 264
5627 0006272 321
8911 38
1809 15
76196044 29336
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
57521141 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 264
5627 deg
Eccentricity:
0006272
Arg of perigee: 321
8911 deg
Mean anomaly: 38
1809 deg
Mean motion: 15
76196044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 308
Coasting Arc #8 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2009/317/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3212476
67 A = 6722777
20 meter
Y = -5263836
13 meter E =
0008083
Z = -2665945
40 I = 51
32403
XDOT = 3312
782445 Wp = 3
55943
YDOT = -4641
689465 meter/sec RA = 258
85062 deg
ZDOT = 5181
765728 TA = 325
89043
MA = 325
94235
Ha = 186
732 n
mi
Hp = 181
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10539621
62 X = -3140425
73
Y = -17269803
56 feet Y = -5299357
06 meter
Z = -8746540
02 Z = -2681377
06
XDOT = 10868
708808 XDOT = 3339
267616
YDOT = -15228
639976 feet/sec YDOT = -4604
495917 meter/sec
ZDOT = 17000
543726 ZDOT = 5197
923990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20203613
53 X = 6158061
40
Y = -267330
64 feet Y = -81482
38 meter
Z = -8807623
75 Z = -2684563
72
XDOT = 7632
052356 XDOT = 2326
249558
YDOT = 15536
418312 feet/sec YDOT = 4735
500302 meter/sec
ZDOT = 17064
088277 ZDOT = 5201
134107
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 09317
52622860
00016717 00000-0 10270-3 0 9075
2 25544 51
6430 259
6629 0006406 326
2728 33
8028 15
76199133 29488
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52622860 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 259
6629 deg
Eccentricity:
0006406
Arg of perigee: 326
2728 deg
Mean anomaly: 33
8028 deg
Mean motion: 15
76199133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 327
Coasting Arc #9 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/318/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3023086
68 A = 6715378
89 meter
Y = 3529183
21 meter E =
0012557
Z = -4858574
02 I = 51
30764
XDOT = -3740
675125 Wp = 43
94484
YDOT = -6331
763055 meter/sec RA = 253
71602 deg
ZDOT = -2266
356098 TA = 203
85810
MA = 203
91635
Ha = 186
830 n
mi
Hp = 181
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9918263
39 X = -3038723
12
Y = 11578685
07 feet Y = 3495289
96 meter
Z = -15940203
47 Z = -4873298
53
XDOT = -12272
556184 XDOT = -3658
584333
YDOT = -20773
500836 feet/sec YDOT = -6373
134440 meter/sec
ZDOT = -7435
551504 ZDOT = -2284
329622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5232469
56 X = -1594856
72
Y = -14255130
63 feet Y = -4344963
81 meter
Z = -15998140
41 Z = -4876233
20
XDOT = 23062
961309 XDOT = 7029
590607
YDOT = -21
024407 feet/sec YDOT = -6
408239 meter/sec
ZDOT = -7506
707596 ZDOT = -2288
044475
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 09318
54061949
00016717 00000-0 10270-3 0 9084
2 25544 51
6440 254
4362 0006334 330
6659 29
4149 15
76269028 29642
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
54061949 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 254
4362 deg
Eccentricity:
0006334
Arg of perigee: 330
6659 deg
Mean anomaly: 29
4149 deg
Mean motion: 15
76269028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 330
Coasting Arc #10 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/319/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3311806
53 A = 6724973
93 meter
Y = 5718491
96 meter E =
0009300
Z = 1233880
53 I = 51
35042
XDOT = -3684
081532 Wp = 99
90513
YDOT = 3402
532700 meter/sec RA = 248
51065 deg
ZDOT = -5845
175417 TA = 66
50210
MA = 66
40439
Ha = 186
914 n
mi
Hp = 180
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10865507
00 X = 3241621
05
Y = 18761456
57 feet Y = 5755134
05 meter
Z = 4048164
46 Z = 1249799
59
XDOT = -12086
881668 XDOT = -3693
459705
YDOT = 11163
165026 feet/sec YDOT = 3361
282972 meter/sec
ZDOT = -19177
084700 ZDOT = -5863
095884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21661573
58 X = -6602447
63
Y = 559860
25 feet Y = 170645
40 meter
Z = 4111194
09 Z = 1253091
96
XDOT = -4043
887103 XDOT = -1232
576789
YDOT = -14273
270760 feet/sec YDOT = -4350
492928 meter/sec
ZDOT = -19247
637921 ZDOT = -5866
680038
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 09319
55498327
00016717 00000-0 10270-3 0 9091
2 25544 51
6445 249
2099 0006299 334
1504 25
9345 15
76293016 29805
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
55498327 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 249
2099 deg
Eccentricity:
0006299
Arg of perigee: 334
1504 deg
Mean anomaly: 25
9345 deg
Mean motion: 15
76293016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 340
Coasting Arc #11 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2009/320/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3472982
34 A = 6713422
01 meter
Y = -2397038
58 meter E =
0004707
Z = 5220979
70 I = 51
32430
XDOT = 3819
670820 Wp =
39294
YDOT = 6671
691487 meter/sec RA = 243
35289 deg
ZDOT = 526
892177 TA = 84
60929
MA = 84
55559
Ha = 186
762 n
mi
Hp = 180
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11394299
00 X = 3474164
94
Y = -7864299
82 feet Y = -2358195
40 meter
Z = 17129198
49 Z = 5237854
69
XDOT = 12531
728413 XDOT = 3742
223284
YDOT = 21888
751599 feet/sec YDOT = 6713
972230 meter/sec
ZDOT = 1728
648876 ZDOT = 545
261068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1747054
18 X = 532502
11
Y = 13650761
50 feet Y = 4160752
11 meter
Z = 17195674
30 Z = 5241241
53
XDOT = -24202
874931 XDOT = -7377
036279
YDOT = 847
470801 feet/sec YDOT = 258
309100 meter/sec
ZDOT = 1801
385426 ZDOT = 549
062278
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 09320
56931781
00016717 00000-0 10270-3 0 9102
2 25544 51
6443 243
9835 0006345 336
5187 23
5687 15
76377235 29963
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
56931781 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 243
9835 deg
Eccentricity:
0006345
Arg of perigee: 336
5187 deg
Mean anomaly: 23
5687 deg
Mean motion: 15
76377235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 339
Coasting Arc #12 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2009/321/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3307452
13 A = 6725409
95 meter
Y = -5834788
80 meter E =
0016453
Z = 333392
99 I = 51
37935
XDOT = 4341
607805 Wp = 27
56530
YDOT = -2111
642013 meter/sec RA = 238
17739 deg
ZDOT = 6011
477356 TA = 336
07797
MA = 336
15433
Ha = 187
025 n
mi
Hp = 180
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10851220
90 X = -3243580
29
Y = -19143007
88 feet Y = -5871417
58 meter
Z = 1093809
04 Z = 317479
56
XDOT = 14244
120095 XDOT = 4335
694361
YDOT = -6927
959360 feet/sec YDOT = -2063
125193 meter/sec
ZDOT = 19722
694736 ZDOT = 6032
554945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21977703
78 X = 6698804
11
Y = -1148118
82 feet Y = -349946
62 meter
Z = 1030787
82 Z = 314184
13
XDOT = -207
532533 XDOT = -63
255916
YDOT = 14132
430161 feet/sec YDOT = 4307
564713 meter/sec
ZDOT = 19805
769883 ZDOT = 6036
798660
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 09321
58362876
00016717 00000-0 10270-3 0 9119
2 25544 51
6445 238
7566 0006399 341
6214 18
4718 15
76368835 30129
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
58362876 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 238
7566 deg
Eccentricity:
0006399
Arg of perigee: 341
6214 deg
Mean anomaly: 18
4718 deg
Mean motion: 15
76368835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 332
Coasting Arc #13 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4151013
27 A = 6713728
48 meter
Y = 1299126
39 meter E =
0012889
Z = -5124172
78 I = 51
35797
XDOT = -3684
752913 Wp = 73
55170
YDOT = -6628
882829 meter/sec RA = 232
99025 deg
ZDOT = 1310
663824 TA = 209
00555
MA = 209
07722
Ha = 187
015 n
mi
Hp = 180
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13618809
94 X = -4140338
89
Y = 4262225
68 feet Y = 1252767
51 meter
Z = -16811590
48 Z = -5144312
85
XDOT = -12089
084360 XDOT = -3616
720853
YDOT = -21748
303246 feet/sec YDOT = -6669
707655 meter/sec
ZDOT = 4300
078162 ZDOT = 1292
927423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1994735
43 X = 607995
36
Y = -14035063
03 feet Y = -4277887
21 meter
Z = -16891008
34 Z = -5148379
34
XDOT = 23823
675744 XDOT = 7261
456367
YDOT = -1679
769774 feet/sec YDOT = -511
993827 meter/sec
ZDOT = 4229
823974 ZDOT = 1289
250347
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 09322
53451801
00016717 00000-0 10270-3 0 9123
2 25544 51
6449 233
8566 0006356 344
8982 15
1991 15
76429128 30275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53451801 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 233
8566 deg
Eccentricity:
0006356
Arg of perigee: 344
8982 deg
Mean anomaly: 15
1991 deg
Mean motion: 15
76429128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 322
Coasting Arc #14 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/323/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3039476
91 A = 6723600
69 meter
Y = 5673666
39 meter E =
0003123
Z = -1947808
37 I = 51
41039
XDOT = -5219
902539 Wp = 77
07011
YDOT = 879
858038 meter/sec RA = 227
84700 deg
ZDOT = -5589
384258 TA = 124
68033
MA = 124
65090
Ha = 187
106 n
mi
Hp = 180
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9972037
11 X = 2985269
38
Y = 18614391
03 feet Y = 5707352
73 meter
Z = -6390447
40 Z = -1933173
34
XDOT = -17125
664499 XDOT = -5202
200526
YDOT = 2886
673354 feet/sec YDOT = 821
585587 meter/sec
ZDOT = -18337
874862 ZDOT = -5614
699981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21091375
99 X = -6428651
40
Y = 1352292
99 feet Y = 412178
90 meter
Z = -6332460
65 Z = -1930134
01
XDOT = 4558
421794 XDOT = 1389
406963
YDOT = -15137
082077 feet/sec YDOT = -4613
782617 meter/sec
ZDOT = -18437
743836 ZDOT = -5619
824321
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
54877483
00016717 00000-0 10270-3 0 9134
2 25544 51
6449 228
6295 0006282 347
6229 12
4780 15
76444361 30439
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
54877483 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 228
6295 deg
Eccentricity:
0006282
Arg of perigee: 347
6229 deg
Mean anomaly: 12
4780 deg
Mean motion: 15
76444361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 327
Coasting Arc #15 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4978280
65 A = 6716032
80 meter
Y = -295482
76 meter E =
0012139
Z = 4497285
10 I = 51
40642
XDOT = 3185
296698 Wp = 35
64702
YDOT = 6294
080615 meter/sec RA = 222
63521 deg
ZDOT = -3098
516140 TA = 85
38900
MA = 85
25036
Ha = 187
052 n
mi
Hp = 179
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16332941
77 X = 4959367
43
Y = -969431
61 feet Y = -239918
91 meter
Z = 14754872
38 Z = 4521424
03
XDOT = 10450
448485 XDOT = 3129
730734
YDOT = 20649
870784 feet/sec YDOT = 6329
390119 meter/sec
ZDOT = -10165
735366 ZDOT = -3083
176018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5619806
31 X = -1712916
96
Y = 15274239
14 feet Y = 4655588
09 meter
Z = 14850132
63 Z = 4526320
43
XDOT = -22016
619959 XDOT = -6710
665764
YDOT = 1767
957512 feet/sec YDOT = 538
873450 meter/sec
ZDOT = -10104
929579 ZDOT = -3079
982536
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
56300389
00016717 00000-0 10270-3 0 9144
2 25544 51
6443 223
4023 0006462 351
7319 8
3738 15
76534950 30599
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
56300389 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 223
4023 deg
Eccentricity:
0006462
Arg of perigee: 351
7319 deg
Mean anomaly: 8
3738 deg
Mean motion: 15
76534950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 307
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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