Date:
October 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5543 41 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
303/01:34:51
818 1
4 1
9 1
9
N/A 1
3 -0
3 191
4
000/00:03:43
636 0
2 -0
0 188
5
Coasting Arc #1 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2008/298/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3437872
29 A = 6724884
99 meter
Y = 2568571
39 meter E =
0002599
Z = 5178478
65 I = 51
93715
XDOT = -3227
218677 Wp = 190
70039
YDOT = -6873
620778 meter/sec RA = 72
34213 deg
ZDOT = 1264
504694 TA = 247
24376
MA = 247
27122
Ha = 191
114 n
mi
Hp = 187
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11279108
56 X = -3491495
48
Y = 8427071
50 feet Y = 2529827
56 meter
Z = 16989759
35 Z = 5161646
82
XDOT = -10587
987784 XDOT = -3156
259712
YDOT = -22551
249273 feet/sec YDOT = -6909
312587 meter/sec
ZDOT = 4148
637449 ZDOT = 1248
999326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2243426
70 X = -683796
46
Y = -13978762
75 feet Y = -4260726
89 meter
Z = 16924744
47 Z = 5158662
11
XDOT = 23885
240279 XDOT = 7280
221237
YDOT = 1125
727829 feet/sec YDOT = 343
121842 meter/sec
ZDOT = 4087
949068 ZDOT = 1246
006876
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 08298
63311119
00020000 00000-0 20000-3 0 9001
2 25544 51
6425 72
7516 0003878 267
3608 92
7110 15
72502774 8908
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
63311119 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 72
7516 deg
Eccentricity:
0003878
Arg of perigee: 267
3608 deg
Mean anomaly: 92
7110 deg
Mean motion: 15
72502774 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 890
Checksum: 291
Coasting Arc #2 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2008/299/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3630690
61 A = 6735504
92 meter
Y = 5442269
43 meter E =
0006853
Z = -1584661
83 I = 51
96257
XDOT = -3283
245725 Wp = 9
06105
YDOT = 3872
196371 meter/sec RA = 67
21522 deg
ZDOT = 5786
026054 TA = 333
54753
MA = 333
58250
Ha = 191
119 n
mi
Hp = 187
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11911714
61 X = 3577262
59
Y = 17855214
66 feet Y = 5482571
09 meter
Z = -5199021
75 Z = -1567153
65
XDOT = -10771
803559 XDOT = -3354
409292
YDOT = 12704
056335 feet/sec YDOT = 3835
083641 meter/sec
ZDOT = 18983
025111 ZDOT = 5769
902641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21303909
91 X = -6493431
74
Y = 2747143
51 feet Y = 837329
34 meter
Z = -5130700
52 Z = -1563837
52
XDOT = -6333
984578 XDOT = -1930
598499
YDOT = -13844
016922 feet/sec YDOT = -4219
656358 meter/sec
ZDOT = 18920
865218 ZDOT = 5767
079719
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 08299
58637925
00020000 00000-0 20000-3 0 9013
2 25544 51
6427 67
8677 0003849 274
4005 85
6717 15
72457468 9051
Satellite: ISS
Catalog Number: 25544
Epoch time: 08299
58637925 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 67
8677 deg
Eccentricity:
0003849
Arg of perigee: 274
4005 deg
Mean anomaly: 85
6717 deg
Mean motion: 15
72457468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 905
Checksum: 336
Coasting Arc #3 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2008/300/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2182154
56 A = 6726162
72 meter
Y = -4076504
59 meter E =
0008837
Z = -4892988
62 I = 51
91897
XDOT = 4928
303050 Wp = 63
04503
YDOT = 5428
428687 meter/sec RA = 62
14556 deg
ZDOT = -2323
978345 TA = 184
37785
MA = 184
38558
Ha = 191
039 n
mi
Hp = 187
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7159299
74 X = 2251346
39
Y = -13374358
89 feet Y = -4051715
85 meter
Z = -16053112
27 Z = -4882219
17
XDOT = 16168
973262 XDOT = 4878
524954
YDOT = 17809
805402 feet/sec YDOT = 5483
261381 meter/sec
ZDOT = -7624
600869 ZDOT = -2300
157214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8962537
70 X = 2731781
49
Y = 12293467
30 feet Y = 3747048
83 meter
Z = -16011715
77 Z = -4880370
97
XDOT = -22150
802598 XDOT = -6751
564632
YDOT = 6336
078729 feet/sec YDOT = 1931
236797 meter/sec
ZDOT = -7531
822263 ZDOT = -2295
699426
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 08300
60318616
00020000 00000-0 20000-3 0 9023
2 25544 51
6428 62
6581 0003898 276
6015 83
4704 15
72487043 9210
Satellite: ISS
Catalog Number: 25544
Epoch time: 08300
60318616 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 62
6581 deg
Eccentricity:
0003898
Arg of perigee: 276
6015 deg
Mean anomaly: 83
4704 deg
Mean motion: 15
72487043 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 921
Checksum: 285
Coasting Arc #4 (Orbit 936)
---------------------------------------
Vector Time (GMT): 2008/301/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4862244
70 A = 6733845
50 meter
Y = -3946687
28 meter E =
0010177
Z = 2462255
27 I = 51
93005
XDOT = 1572
535473 Wp = 106
36357
YDOT = -5293
843682 meter/sec RA = 57
00259 deg
ZDOT = -5364
687654 TA = 45
93956
MA = 45
85580
Ha = 191
158 n
mi
Hp = 187
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15952246
39 X = -4829712
38
Y = -12948449
09 feet Y = -4000877
73 meter
Z = 8078265
33 Z = 2438712
95
XDOT = 5159
237117 XDOT = 1657
676682
YDOT = -17368
253550 feet/sec YDOT = -5275
782824 meter/sec
ZDOT = -17600
681278 ZDOT = -5356
841045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18409747
42 X = 5611291
01
Y = -9202646
35 feet Y = -2804966
61 meter
Z = 7986699
54 Z = 2434346
02
XDOT = 12961
502347 XDOT = 3950
665915
YDOT = 10635
905378 feet/sec YDOT = 3241
823959 meter/sec
ZDOT = -17570
706910 ZDOT = -5355
551466
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 08301
61998194
00020000 00000-0 20000-3 0 9031
2 25544 51
6427 57
4485 0003716 282
2909 77
7838 15
72512425 9372
Satellite: ISS
Catalog Number: 25544
Epoch time: 08301
61998194 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 57
4485 deg
Eccentricity:
0003716
Arg of perigee: 282
2909 deg
Mean anomaly: 77
7838 deg
Mean motion: 15
72512425 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 937
Checksum: 315
Coasting Arc #5 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2008/302/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -491780
65 A = 6727715
73 meter
Y = 5024961
88 meter E =
0005307
Z = 4443473
68 I = 51
89362
XDOT = -6017
092342 Wp = 114
90673
YDOT = -3501
545250 meter/sec RA = 51
94163 deg
ZDOT = 3288
595991 TA = 302
19209
MA = 302
24355
Ha = 191
109 n
mi
Hp = 187
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1613453
59 X = -569520
34
Y = 16486095
40 feet Y = 5019027
91 meter
Z = 14578325
73 Z = 4440895
61
XDOT = -19741
116608 XDOT = -5993
466212
YDOT = -11488
009352 feet/sec YDOT = -3568
699699 meter/sec
ZDOT = 10789
356925 ZDOT = 3259
421454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14446436
80 X = -4403273
94
Y = -8122466
25 feet Y = -2475727
71 meter
Z = 14568739
16 Z = 4440551
70
XDOT = 17831
920431 XDOT = 5435
169347
YDOT = -12535
782520 feet/sec YDOT = -3820
906512 meter/sec
ZDOT = 10676
006783 ZDOT = 3254
046867
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 08302
63676398
00020000 00000-0 20000-3 0 9044
2 25544 51
6434 52
2380 0003857 286
8361 73
2379 15
72560154 9536
Satellite: ISS
Catalog Number: 25544
Epoch time: 08302
63676398 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 52
2380 deg
Eccentricity:
0003857
Arg of perigee: 286
8361 deg
Mean anomaly: 73
2379 deg
Mean motion: 15
72560154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 953
Checksum: 302
Coasting Arc #6 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2008/303/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3737162
59 A = 6725466
89 meter
Y = -1962928
20 meter E =
0009611
Z = -5243897
31 I = 51
87374
XDOT = 4448
511930 Wp = 89
51666
YDOT = 6217
102739 meter/sec RA = 49
44144 deg
ZDOT = 844
495357 TA = 188
49867
MA = 188
51496
Ha = 191
425 n
mi
Hp = 188
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12261032
12 X = 3784309
37
Y = -6440053
15 feet Y = -1920873
51 meter
Z = -17204387
51 Z = -5225627
04
XDOT = 14594
855413 XDOT = 4374
558108
YDOT = 20397
318698 feet/sec YDOT = 6266
435079 meter/sec
ZDOT = 2770
654057 ZDOT = 865
927263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 313334
46 X = 95504
34
Y = -13933235
32 feet Y = -4246850
13 meter
Z = -17133736
25 Z = -5222362
81
XDOT = 23882
204515 XDOT = 7279
295936
YDOT = -2967
073800 feet/sec YDOT = -904
364094 meter/sec
ZDOT = 2854
210311 ZDOT = 869
963303
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 08303
08160549
00020000 00000-0 20000-3 0 9051
2 25544 51
6436 49
9598 0005236 289
5266 70
5331 15
72206364 9605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08303
08160549 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 49
9598 deg
Eccentricity:
0005236
Arg of perigee: 289
5266 deg
Mean anomaly: 70
5331 deg
Mean motion: 15
72206364 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 960
Checksum: 298
Coasting Arc #7 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2008/304/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4720995
83 A = 6737323
10 meter
Y = -4797631
77 meter E =
0007371
Z = -167044
77 I = 51
89382
XDOT = 3490
035962 Wp = 152
85537
YDOT = -3227
371832 meter/sec RA = 44
34602 deg
ZDOT = -6053
359506 TA = 28
95147
MA = 28
91060
Ha = 191
529 n
mi
Hp = 188
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15488831
46 X = -4666185
55
Y = -15740261
73 feet Y = -4850118
21 meter
Z = -548047
14 Z = -189847
06
XDOT = 11450
249218 XDOT = 3555
272674
YDOT = -10588
490261 feet/sec YDOT = -3187
979391 meter/sec
ZDOT = -19860
103366 ZDOT = -6036
245926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21148536
75 X = -6446074
00
Y = 6347754
13 feet Y = 1934795
46 meter
Z = -636793
34 Z = -194094
61
XDOT = -3503
626548 XDOT = -1067
905372
YDOT = -13627
241774 feet/sec YDOT = -4153
583293 meter/sec
ZDOT = -19794
029294 ZDOT = -6033
220129
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 08304
09859950
00020000 00000-0 20000-3 0 9065
2 25544 51
6439 44
7514 0005241 292
5240 67
5367 15
72187901 9768
Satellite: ISS
Catalog Number: 25544
Epoch time: 08304
09859950 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 44
7514 deg
Eccentricity:
0005241
Arg of perigee: 292
5240 deg
Mean anomaly: 67
5367 deg
Mean motion: 15
72187901 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 976
Checksum: 305
Coasting Arc #8 (Orbit 991)
---------------------------------------
Vector Time (GMT): 2008/305/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2220272
22 A = 6725133
69 meter
Y = 3537766
59 meter E =
0002773
Z = 5272697
57 I = 51
83177
XDOT = -6175
865737 Wp = 305
20482
YDOT = -4570
027727 meter/sec RA = 39
24196 deg
ZDOT = 467
454457 TA = 140
37499
MA = 140
35472
Ha = 191
706 n
mi
Hp = 188
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7284357
69 X = -2285281
72
Y = 11606845
76 feet Y = 3512574
56 meter
Z = 17298876
55 Z = 5261753
35
XDOT = -20262
026695 XDOT = -6126
574817
YDOT = -14993
529287 feet/sec YDOT = -4638
814241 meter/sec
ZDOT = 1533
643231 ZDOT = 437
570725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7022980
44 X = 2140604
44
Y = 11828562
06 feet Y = 3605345
72 meter
Z = 17256730
01 Z = 5259851
31
XDOT = -21667
793244 XDOT = -6604
343381
YDOT = 10805
207945 feet/sec YDOT = 3293
427382 meter/sec
ZDOT = 1417
475301 ZDOT = 432
046472
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 08305
11557998
00020000 00000-0 20000-3 0 9077
2 25544 51
6441 39
5428 0005364 297
7910 62
2708 15
72256669 9921
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
11557998 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 39
5428 deg
Eccentricity:
0005364
Arg of perigee: 297
7910 deg
Mean anomaly: 62
2708 deg
Mean motion: 15
72256669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 992
Checksum: 320
Coasting Arc #9 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2008/306/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5906006
57 A = 6736736
89 meter
Y = 3075074
72 meter E =
0010829
Z = -976606
27 I = 51
84766
XDOT = -1448
445111 Wp = 8
42332
YDOT = 4666
041824 meter/sec RA = 34
12086 deg
ZDOT = 5951
430566 TA = 340
94245
MA = 340
98293
Ha = 191
855 n
mi
Hp = 188
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19376661
97 X = 5875925
95
Y = 10088827
83 feet Y = 3140950
96 meter
Z = -3204088
80 Z = -947986
97
XDOT = -4752
116505 XDOT = -1529
425715
YDOT = 15308
536167 feet/sec YDOT = 4649
391403 meter/sec
ZDOT = 19525
690833 ZDOT = 5944
197329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17536644
58 X = 5345169
27
Y = -13053945
81 feet Y = -3978842
68 meter
Z = -3092936
64 Z = -942727
09
XDOT = 10703
364477 XDOT = 3262
385493
YDOT = 9774
210932 feet/sec YDOT = 2979
179492 meter/sec
ZDOT = 19498
005497 ZDOT = 5942
992075
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 08306
06899075
00020000 00000-0 20000-3 0 9088
2 25544 51
6445 34
6596 0005412 302
2544 57
8094 15
72263234 10078
Satellite: ISS
Catalog Number: 25544
Epoch time: 08306
06899075 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 34
6596 deg
Eccentricity:
0005412
Arg of perigee: 302
2544 deg
Mean anomaly: 57
8094 deg
Mean motion: 15
72263234 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1007
Checksum: 288
Coasting Arc #10 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2008/307/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 245429
48 A = 6725932
20 meter
Y = -4426571
81 meter E =
0010823
Z = -5067129
18 I = 51
78638
XDOT = 7103
670635 Wp = 53
92735
YDOT = 2382
328531 meter/sec RA = 29
03454 deg
ZDOT = -1733
423887 TA = 199
38107
MA = 199
42226
Ha = 191
943 n
mi
Hp = 188
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 805214
82 X = 319525
72
Y = -14522873
39 feet Y = -4423412
69 meter
Z = -16624439
57 Z = -5065757
12
XDOT = 23306
006021 XDOT = 7084
923964
YDOT = 7816
038488 feet/sec YDOT = 2461
661160 meter/sec
ZDOT = -5687
086242 ZDOT = -1698
958755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12797629
46 X = -3900717
46
Y = -6924510
02 feet Y = -2110590
65 meter
Z = -16619448
09 Z = -5065607
78
XDOT = 16400
891726 XDOT = 4998
991798
YDOT = -16954
113570 feet/sec YDOT = -5167
613816 meter/sec
ZDOT = -5553
327104 ZDOT = -1692
654101
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 08307
08595011
00020000 00000-0 20000-3 0 9095
2 25544 51
6442 29
4508 0005523 307
0145 53
0511 15
72289699 10236
Satellite: ISS
Catalog Number: 25544
Epoch time: 08307
08595011 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 29
4508 deg
Eccentricity:
0005523
Arg of perigee: 307
0145 deg
Mean anomaly: 53
0511 deg
Mean motion: 15
72289699 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1023
Checksum: 273
Coasting Arc #11 (Orbit 1038)
---------------------------------------
Vector Time (GMT): 2008/308/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6330588
90 A = 6735378
40 meter
Y = -1053671
04 meter E =
0009169
Z = 2033201
93 I = 51
79151
XDOT = -930
523017 Wp = 99
97041
YDOT = -5217
351893 meter/sec RA = 23
89076 deg
ZDOT = -5581
400949 TA = 57
42546
MA = 57
33695
Ha = 192
133 n
mi
Hp = 187
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20769648
62 X = -6328213
22
Y = -3456925
98 feet Y = -1124450
18 meter
Z = 6670610
01 Z = 2002452
94
XDOT = -3052
897036 XDOT = -844
998529
YDOT = -17117
296237 feet/sec YDOT = -5227
279016 meter/sec
ZDOT = -18311
682904 ZDOT = -5585
714099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11585190
30 X = -3531166
00
Y = 17626368
50 feet Y = 5372517
12 meter
Z = 6551349
33 Z = 1996851
28
XDOT = -15559
874577 XDOT = -4742
649771
YDOT = -3390
098552 feet/sec YDOT = -1033
302039 meter/sec
ZDOT = -18328
781773 ZDOT = -5586
612685
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 08308
10289987
00020000 00000-0 20000-3 0 9103
2 25544 51
6442 24
2421 0005405 311
1905 48
8791 15
72269948 10396
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
10289987 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 24
2421 deg
Eccentricity:
0005405
Arg of perigee: 311
1905 deg
Mean anomaly: 48
8791 deg
Mean motion: 15
72269948 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1039
Checksum: 291
Coasting Arc #12 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2008/309/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1869982
53 A = 6727693
25 meter
Y = 4499629
98 meter E =
0003398
Z = 4635711
62 I = 51
73835
XDOT = -7134
672303 Wp = 83
30775
YDOT = -18
974511 meter/sec RA = 18
81622 deg
ZDOT = 2895
029708 TA = 338
07427
MA = 338
08881
Ha = 192
284 n
mi
Hp = 187
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6135113
29 X = 1797008
06
Y = 14762565
54 feet Y = 4520132
93 meter
Z = 15209027
61 Z = 4644619
16
XDOT = -23407
717528 XDOT = -7147
993666
YDOT = -62
252333 feet/sec YDOT = -98
833180 meter/sec
ZDOT = 9498
128963 ZDOT = 2860
336423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15952484
35 X = 4862317
23
Y = 172634
61 feet Y = 52619
03 meter
Z = 15243881
32 Z = 4646335
03
XDOT = -9173
196885 XDOT = -2795
990410
YDOT = 20425
680344 feet/sec YDOT = 6225
747369 meter/sec
ZDOT = 9363
652208 ZDOT = 2854
041193
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 08309
11983700
00020000 00000-0 20000-3 0 9110
2 25544 51
6439 19
0323 0005554 316
0429 44
0291 15
72282666 10558
Satellite: ISS
Catalog Number: 25544
Epoch time: 08309
11983700 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 19
0323 deg
Eccentricity:
0005554
Arg of perigee: 316
0429 deg
Mean anomaly: 44
0291 deg
Mean motion: 15
72282666 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1055
Checksum: 270
Coasting Arc #13 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2008/310/01:36:43
636
Vector Time (MET): N/A
Weight (LBS) : 626550
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5943521
26 A = 6733163
60 meter
Y = -990140
35 meter E =
0005963
Z = -2997843
62 I = 51
72798
XDOT = 3314
876671 Wp = 3
44239
YDOT = 4846
640214 meter/sec RA = 13
65405 deg
ZDOT = 4977
644920 TA = 321
98928
MA = 322
03134
Ha = 192
456 n
mi
Hp = 187
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19499741
66 X = 5968714
67
Y = -3248491
96 feet Y = -923535
47 meter
Z = -9835444
95 Z = -2968908
33
XDOT = 10875
579629 XDOT = 3236
253455
YDOT = 15901
050570 feet/sec YDOT = 4883
269259 meter/sec
ZDOT = 16330
856038 ZDOT = 4993
558108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4283875
11 X = 1305725
13
Y = -19355446
76 feet Y = -5899540
17 meter
Z = -9723358
33 Z = -2963679
62
XDOT = 17364
511045 XDOT = 5292
702966
YDOT = -4381
292433 feet/sec YDOT = -1335
417934 meter/sec
ZDOT = 16392
890288 ZDOT = 4996
552960
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 08310
07320450
00020000 00000-0 20000-3 0 9125
2 25544 51
6432 14
1483 0005747 318
2578 41
8145 15
72313666 10702
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
07320450 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 14
1483 deg
Eccentricity:
0005747
Arg of perigee: 318
2578 deg
Mean anomaly: 41
8145 deg
Mean motion: 15
72313666 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1070
Checksum: 259
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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