Date:
November 13th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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 1186)
---------------------------------------
Vector Time (GMT): 2008/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2722358
82 A = 6729512
13 meter
Y = -4704987
30 meter E =
0005366
Z = -3970232
18 I = 51
50419
XDOT = 6579
788393 Wp = 71
46388
YDOT = 470
308139 meter/sec RA = 335
56703 deg
ZDOT = 3960
406950 TA = 239
63231
MA = 239
68537
Ha = 192
374 n
mi
Hp = 186
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8931623
43 X = 2794055
83
Y = -15436310
05 feet Y = -4674143
23 meter
Z = -13025696
12 Z = -3956832
54
XDOT = 21587
232260 XDOT = 6554
800626
YDOT = 1543
005707 feet/sec YDOT = 543
747214 meter/sec
ZDOT = 12993
461122 ZDOT = 3992
312108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6396300
39 X = 1949592
36
Y = 16687793
99 feet Y = 5086439
61 meter
Z = -12974097
18 Z = -3954504
82
XDOT = -13456
427523 XDOT = -4101
519109
YDOT = 15340
333343 feet/sec YDOT = 4675
733603 meter/sec
ZDOT = 13117
146319 ZDOT = 3998
106198
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 08317
50856934
00020000 00000-0 20000-3 0 9008
2 25544 51
6430 336
0654 0004034 338
4058 21
6933 15
72552216 11877
Satellite: ISS
Catalog Number: 25544
Epoch time: 08317
50856934 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 336
0654 deg
Eccentricity:
0004034
Arg of perigee: 338
4058 deg
Mean anomaly: 21
6933 deg
Mean motion: 15
72552216 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1187
Checksum: 277
Coasting Arc #2 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2008/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5947425
54 A = 6731937
60 meter
Y = 516188
95 meter E =
0004307
Z = -3117523
09 I = 51
48548
XDOT = 2056
577580 Wp = 47
60644
YDOT = -5602
222235 meter/sec RA = 330
48211 deg
ZDOT = -4852
421117 TA = 168
66431
MA = 168
65461
Ha = 192
404 n
mi
Hp = 186
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19512550
97 X = -5937610
70
Y = 1693533
29 feet Y = 449736
55 meter
Z = -10228094
13 Z = -3146392
85
XDOT = 6747
301773 XDOT = 2142
642730
YDOT = -18379
994210 feet/sec YDOT = -5578
742750 meter/sec
ZDOT = -15920
016787 ZDOT = -4842
221336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10579919
40 X = 3224759
43
Y = -16412567
55 feet Y = -5002550
59 meter
Z = -10339948
83 Z = -3151616
40
XDOT = 9140
178723 XDOT = 2785
926475
YDOT = 15894
074468 feet/sec YDOT = 4844
513898 meter/sec
ZDOT = -15880
875995 ZDOT = -4840
491003
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 08318
52533014
00020000 00000-0 20000-3 0 9013
2 25544 51
6419 330
8544 0004009 341
9086 18
1933 15
72571509 12032
Satellite: ISS
Catalog Number: 25544
Epoch time: 08318
52533014 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 330
8544 deg
Eccentricity:
0004009
Arg of perigee: 341
9086 deg
Mean anomaly: 18
1933 deg
Mean motion: 15
72571509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1203
Checksum: 267
Coasting Arc #3 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -851997
98 A = 6727405
44 meter
Y = 4938703
61 meter E =
0010394
Z = 4485590
06 I = 51
44459
XDOT = -6825
668908 Wp = 44
17789
YDOT = 1683
930813 meter/sec RA = 325
29652 deg
ZDOT = -3138
805798 TA = 77
30146
MA = 77
18528
Ha = 192
479 n
mi
Hp = 186
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2795268
97 X = -928950
91
Y = 16203095
84 feet Y = 4928745
29 meter
Z = 14716502
81 Z = 4481264
57
XDOT = -22393
926864 XDOT = -6828
743367
YDOT = 5524
707391 feet/sec YDOT = 1607
585417 meter/sec
ZDOT = -10297
919286 ZDOT = -3171
973207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11250193
04 X = -3429058
84
Y = -12011250
91 feet Y = -3661029
28 meter
Z = 14700078
45 Z = 4480583
91
XDOT = 8077
864821 XDOT = 2462
133198
YDOT = -20373
469594 feet/sec YDOT = -6209
833532 meter/sec
ZDOT = -10426
356780 ZDOT = -3177
953547
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 08319
54207715
00020000 00000-0 20000-3 0 9023
2 25544 51
6411 325
6434 0004107 346
3692 13
7359 15
72614718 12195
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54207715 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 325
6434 deg
Eccentricity:
0004107
Arg of perigee: 346
3692 deg
Mean anomaly: 13
7359 deg
Mean motion: 15
72614718 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 280
Coasting Arc #4 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5821247
02 A = 6733613
64 meter
Y = -2412546
19 meter E =
0014880
Z = 2349196
38 I = 51
44231
XDOT = 100
666222 Wp = 57
62660
YDOT = 5505
499130 meter/sec RA = 320
20207 deg
ZDOT = 5387
589367 TA = 328
90642
MA = 328
99439
Ha = 192
423 n
mi
Hp = 186
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19098579
46 X = 5836379
61
Y = -7915177
80 feet Y = -2347365
34 meter
Z = 7707337
21 Z = 2377513
13
XDOT = 330
269756 XDOT = 12
922792
YDOT = 18062
661189 feet/sec YDOT = 5506
133545 meter/sec
ZDOT = 17675
818133 ZDOT = 5387
865991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4729866
96 X = -1441663
45
Y = 20083146
13 feet Y = 6121342
94 meter
Z = 7816931
87 Z = 2382600
84
XDOT = -13317
501615 XDOT = -4059
174492
YDOT = -10038
268854 feet/sec YDOT = -3059
664347 meter/sec
ZDOT = 17677
269134 ZDOT = 5388
031632
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 08320
55881113
00020000 00000-0 20000-3 0 9037
2 25544 51
6410 320
4331 0004097 349
4748 10
6328 15
72632859 12353
Satellite: ISS
Catalog Number: 25544
Epoch time: 08320
55881113 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 320
4331 deg
Eccentricity:
0004097
Arg of perigee: 349
4748 deg
Mean anomaly: 10
6328 deg
Mean motion: 15
72632859 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 272
Coasting Arc #5 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2008/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -985609
93 A = 6725768
47 meter
Y = -4528106
90 meter E =
0011370
Z = -4884023
32 I = 51
39363
XDOT = 6311
754176 Wp = 86
36186
YDOT = -3781
439415 meter/sec RA = 315
02214 deg
ZDOT = 2237
330658 TA = 205
46674
MA = 205
52281
Ha = 192
631 n
mi
Hp = 185
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3233628
37 X = -911176
54
Y = -14855993
78 feet Y = -4538711
78 meter
Z = -16023698
56 Z = -4888631
25
XDOT = 20707
854908 XDOT = 6342
701008
YDOT = -12406
297293 feet/sec YDOT = -3710
684976 meter/sec
ZDOT = 7340
323680 ZDOT = 2268
068393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13989454
97 X = 4263985
87
Y = 5905017
70 feet Y = 1799849
40 meter
Z = -16041874
42 Z = -4889563
32
XDOT = -1186
547766 XDOT = -361
659759
YDOT = 23028
921734 feet/sec YDOT = 7019
215345 meter/sec
ZDOT = 7459
215581 ZDOT = 2273
568909
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 08321
51198773
00020000 00000-0 20000-3 0 9048
2 25544 51
6408 315
5478 0004210 353
5005 6
6102 15
72611464 12507
Satellite: ISS
Catalog Number: 25544
Epoch time: 08321
51198773 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 315
5478 deg
Eccentricity:
0004210
Arg of perigee: 353
5005 deg
Mean anomaly: 6
6102 deg
Mean motion: 15
72611464 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1250
Checksum: 257
Coasting Arc #6 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5085119
54 A = 6734893
24 meter
Y = 4127074
90 meter E =
0005232
Z = -1569164
37 I = 51
40452
XDOT = -2045
271532 Wp = 113
75398
YDOT = -4696
165455 meter/sec RA = 309
91222 deg
ZDOT = -5740
578625 TA = 83
59092
MA = 83
53135
Ha = 192
704 n
mi
Hp = 185
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16683463
07 X = -5123268
42
Y = 13540271
98 feet Y = 4069997
02 meter
Z = -5148177
08 Z = -1593960
42
XDOT = -6710
208439 XDOT = -1964
719205
YDOT = -15407
366979 feet/sec YDOT = -4718
585874 meter/sec
ZDOT = -18833
919372 ZDOT = -5750
319501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1972671
17 X = -601270
17
Y = -21372634
60 feet Y = -6514379
03 meter
Z = -5244014
83 Z = -1598375
72
XDOT = 14915
403750 XDOT = 4546
215063
YDOT = 3240
217864 feet/sec YDOT = 987
618405 meter/sec
ZDOT = -18872
011209 ZDOT = -5752
189017
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 08322
52869593
00020000 00000-0 20000-3 0 9056
2 25544 51
6403 310
3365 0004250 358
8035 1
3117 15
72655735 12669
Satellite: ISS
Catalog Number: 25544
Epoch time: 08322
52869593 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 310
3365 deg
Eccentricity:
0004250
Arg of perigee: 358
8035 deg
Mean anomaly: 1
3117 deg
Mean motion: 15
72655735 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 277
Coasting Arc #7 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2008/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2515818
12 A = 6724487
44 meter
Y = 3557338
05 meter E =
0007730
Z = 5120238
13 I = 51
35119
XDOT = -5152
763946 Wp = 27
59286
YDOT = 5566
415222 meter/sec RA = 304
74204 deg
ZDOT = -1327
969403 TA = 75
20654
MA = 75
12092
Ha = 192
670 n
mi
Hp = 185
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8253996
46 X = 2450978
97
Y = 11671056
59 feet Y = 3585108
44 meter
Z = 16798681
53 Z = 5132302
88
XDOT = -16905
393522 XDOT = -5208
174441
YDOT = 18262
517134 feet/sec YDOT = 5508
484327 meter/sec
ZDOT = -4356
854996 ZDOT = -1353
135933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14229837
84 X = -4337254
57
Y = 521074
08 feet Y = 158823
38 meter
Z = 16845709
16 Z = 5134572
15
XDOT = -6146
123752 XDOT = -1873
338520
YDOT = -23049
941224 feet/sec YDOT = -7025
622085 meter/sec
ZDOT = -4454
025866 ZDOT = -1357
587084
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 08323
54538980
00020000 00000-0 20000-3 0 9063
2 25544 51
6398 305
1256 0004303
6412 359
4755 15
72676208 12824
Satellite: ISS
Catalog Number: 25544
Epoch time: 08323
54538980 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 305
1256 deg
Eccentricity:
0004303
Arg of perigee:
6412 deg
Mean anomaly: 359
4755 deg
Mean motion: 15
72676208 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1282
Checksum: 289
Coasting Arc #8 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2008/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3808115
79 A = 6735508
46 meter
Y = -5494166
66 meter E =
0016532
Z = 745207
98 I = 51
37314
XDOT = 3594
360963 Wp = 42
30674
YDOT = 3307
972567 meter/sec RA = 299
61613 deg
ZDOT = 5956
436316 TA = 325
84618
MA = 325
95243
Ha = 192
656 n
mi
Hp = 185
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12493818
22 X = 3865649
31
Y = -18025481
16 feet Y = -5451260
46 meter
Z = 2444908
07 Z = 763847
44
XDOT = 11792
522846 XDOT = 3528
167942
YDOT = 10852
928371 feet/sec YDOT = 3347
796350 meter/sec
ZDOT = 19542
113898 ZDOT = 5973
737307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8719584
47 X = 2657729
35
Y = 20115310
94 feet Y = 6131146
77 meter
Z = 2516774
30 Z = 767112
81
XDOT = -13917
021280 XDOT = -4241
908086
YDOT = 3553
570994 feet/sec YDOT = 1083
128439 meter/sec
ZDOT = 19609
430180 ZDOT = 5976
954319
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 08324
56206840
00020000 00000-0 20000-3 0 9074
2 25544 51
6397 299
9152 0004120 5
7535 354
3674 15
72744656 12981
Satellite: ISS
Catalog Number: 25544
Epoch time: 08324
56206840 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 299
9152 deg
Eccentricity:
0004120
Arg of perigee: 5
7535 deg
Mean anomaly: 354
3674 deg
Mean motion: 15
72744656 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1298
Checksum: 307
Coasting Arc #9 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2008/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3637551
58 A = 6723856
96 meter
Y = -2145338
83 meter E =
0015977
Z = -5245431
80 I = 51
32010
XDOT = 3467
940478 Wp = 77
24613
YDOT = -6849
302589 meter/sec RA = 294
45806 deg
ZDOT = 400
895639 TA = 196
55799
MA = 196
61023
Ha = 192
854 n
mi
Hp = 185
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11934224
34 X = -3587810
01
Y = -7038513
21 feet Y = -2185737
70 meter
Z = -17209421
90 Z = -5262982
51
XDOT = 11377
757473 XDOT = 3542
325245
YDOT = -22471
465186 feet/sec YDOT = -6810
106182 meter/sec
ZDOT = 1315
274406 ZDOT = 417
923523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12115491
18 X = 3692801
71
Y = -6544395
93 feet Y = -1994731
88 meter
Z = -17277625
31 Z = -5266220
19
XDOT = 12972
236906 XDOT = 3953
937809
YDOT = 20408
670024 feet/sec YDOT = 6220
562623 meter/sec
ZDOT = 1380
787117 ZDOT = 420
863913
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 08325
51519536
00020000 00000-0 20000-3 0 9080
2 25544 51
6397 295
0293 0004378 8
8175 351
3063 15
72704910 13139
Satellite: ISS
Catalog Number: 25544
Epoch time: 08325
51519536 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 295
0293 deg
Eccentricity:
0004378
Arg of perigee: 8
8175 deg
Mean anomaly: 351
3063 deg
Mean motion: 15
72704910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1313
Checksum: 291
Coasting Arc #10 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2008/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2202922
95 A = 6735738
30 meter
Y = 6362206
92 meter E =
0010555
Z = 31591
33 I = 51
34984
XDOT = -4553
739696 Wp = 113
38929
YDOT = -1539
029147 meter/sec RA = 289
31348 deg
ZDOT = -6010
177634 TA = 66
26647
MA = 66
15578
Ha = 192
893 n
mi
Hp = 185
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7227437
50 X = -2274055
93
Y = 20873382
27 feet Y = 6337174
83 meter
Z = 103646
10 Z = 20716
77
XDOT = -14940
090867 XDOT = -4506
994724
YDOT = -5049
308225 feet/sec YDOT = -1589
690140 meter/sec
ZDOT = -19718
430559 ZDOT = -6032
186581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14492918
65 X = -4417441
60
Y = -16670217
54 feet Y = -5081082
31 meter
Z = 61959
55 Z = 18885
27
XDOT = 10552
086949 XDOT = 3216
276102
YDOT = -9279
799163 feet/sec YDOT = -2828
482785 meter/sec
ZDOT = -19803
875653 ZDOT = -6036
221299
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 08326
53184812
00020000 00000-0 20000-3 0 9099
2 25544 51
6400 289
8178 0004492 11
8279 348
2989 15
72749047 13292
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
53184812 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 289
8178 deg
Eccentricity:
0004492
Arg of perigee: 11
8279 deg
Mean anomaly: 348
2989 deg
Mean motion: 15
72749047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1329
Checksum: 323
Coasting Arc #11 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2008/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4194363
86 A = 6723684
04 meter
Y = 496761
58 meter E =
0004956
Z = 5228113
44 I = 51
30104
XDOT = -1499
177724 Wp = 47
30992
YDOT = 7539
385979 meter/sec RA = 284
16992 deg
ZDOT = 489
397152 TA = 38
03786
MA = 38
00288
Ha = 192
788 n
mi
Hp = 185
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13761036
28 X = 4163099
48
Y = 1629795
21 feet Y = 543490
40 meter
Z = 17152603
15 Z = 5248414
17
XDOT = -4918
562086 XDOT = -1585
750397
YDOT = 24735
518304 feet/sec YDOT = 7522
137237 meter/sec
ZDOT = 1605
633702 ZDOT = 481
903958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8031914
20 X = -2448127
45
Y = 11171532
58 feet Y = 3405083
13 meter
Z = 17231348
20 Z = 5252114
93
XDOT = -18455
737628 XDOT = -5625
308829
YDOT = -15686
405058 feet/sec YDOT = -4781
216262 meter/sec
ZDOT = 1577
148766 ZDOT = 480
714944
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 08327
54848702
00020000 00000-0 20000-3 0 9108
2 25544 51
6401 284
6069 0004467 14
7704 345
3588 15
72768189 13451
Satellite: ISS
Catalog Number: 25544
Epoch time: 08327
54848702 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 284
6069 deg
Eccentricity:
0004467
Arg of perigee: 14
7704 deg
Mean anomaly: 345
3588 deg
Mean motion: 15
72768189 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1345
Checksum: 311
Coasting Arc #12 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2008/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 393658
66 A = 6735343
00 meter
Y = -6666439
98 meter E =
0014609
Z = -818595
54 I = 51
33437
XDOT = 4881
592683 Wp = 33
14936
YDOT = -433
601852 meter/sec RA = 279
00831 deg
ZDOT = 5940
624098 TA = 317
88597
MA = 317
99815
Ha = 192
942 n
mi
Hp = 184
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1291531
05 X = 472151
31
Y = -21871522
24 feet Y = -6661598
95 meter
Z = -2685680
92 Z = -816492
74
XDOT = 16015
724027 XDOT = 4857
219274
YDOT = -1422
578253 feet/sec YDOT = -379
149603 meter/sec
ZDOT = 19490
236541 ZDOT = 5964
280247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18712642
85 X = 5703613
54
Y = 11397787
86 feet Y = 3474045
74 meter
Z = -2678030
81 Z = -816263
79
XDOT = -5360
125658 XDOT = -1633
766300
YDOT = 13353
232141 feet/sec YDOT = 4070
065157 meter/sec
ZDOT = 19581
921784 ZDOT = 5968
569760
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 08328
50157299
00020000 00000-0 20000-3 0 9110
2 25544 51
6399 279
7210 0004454 19
2038 340
9292 15
72785983 13607
Satellite: ISS
Catalog Number: 25544
Epoch time: 08328
50157299 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 279
7210 deg
Eccentricity:
0004454
Arg of perigee: 19
2038 deg
Mean anomaly: 340
9292 deg
Mean motion: 15
72785983 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1360
Checksum: 309
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/plugins/scheduled_mailings pl/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list