Date:
August 15th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 3755)
---------------------------------------
Vector Time (GMT): 2008/226/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3755705
22 A = 6729484
69 meter
Y = -2160675
97 meter E =
0018505
Z = -5164009
71 I = 51
94596
XDOT = 2225
053374 Wp = 54
07189
YDOT = 7220
198955 meter/sec RA = 81
18647 deg
ZDOT = -1395
630540 TA = 202
54988
MA = 202
63130
Ha = 196
804 n
mi
Hp = 187
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12321867
52 X = 3804672
52
Y = -7088831
92 feet Y = -2118403
25 meter
Z = -16942289
08 Z = -5145646
05
XDOT = 7300
043879 XDOT = 2150
930194
YDOT = 23688
316783 feet/sec YDOT = 7244
666466 meter/sec
ZDOT = -4578
840355 ZDOT = -1385
000785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14298206
15 X = -4358093
24
Y = -186013
53 feet Y = -56696
92 meter
Z = -16871509
01 Z = -5142435
95
XDOT = 5681
775507 XDOT = 1731
805174
YDOT = -23089
712095 feet/sec YDOT = -7037
744246 meter/sec
ZDOT = -4537
111231 ZDOT = -1382
911503
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 08226
54041081
00020000 00000-0 20000-3 0 9000
2 25544 51
6402 81
7929 0008355 8
4520 351
6781 15
70939455 37566
Satellite: ISS
Catalog Number: 25544
Epoch time: 08226
54041081 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 81
7929 deg
Eccentricity:
0008355
Arg of perigee: 8
4520 deg
Mean anomaly: 351
6781 deg
Mean motion: 15
70939455 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3756
Checksum: 288
Coasting Arc #2 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2008/227/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3119810
12 A = 6738767
47 meter
Y = -5567564
24 meter E =
0015324
Z = 2157552
45 I = 51
97262
XDOT = 3443
894985 Wp = 76
26036
YDOT = -4087
904471 meter/sec RA = 76
06611 deg
ZDOT = -5532
769396 TA = 79
75038
MA = 79
57761
Ha = 196
846 n
mi
Hp = 187
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10235597
51 X = -3067801
65
Y = -18266286
88 feet Y = -5602161
12 meter
Z = 7078584
15 Z = 2142522
61
XDOT = 11298
868061 XDOT = 3516
227300
YDOT = -13411
760074 feet/sec YDOT = -4048
988005 meter/sec
ZDOT = -18152
130565 ZDOT = -5515
863896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -43278
05 X = -13191
15
Y = 20958264
46 feet Y = 6388079
01 meter
Z = 7019994
59 Z = 2139694
35
XDOT = -14997
997266 XDOT = -4571
389567
YDOT = 6067
470243 feet/sec YDOT = 1849
364930 meter/sec
ZDOT = -18087
153899 ZDOT = -5512
964508
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 08227
55822260
00020000 00000-0 20000-3 0 9019
2 25544 51
6408 76
5896 0008507 11
4610 348
6743 15
70993970 37724
Satellite: ISS
Catalog Number: 25544
Epoch time: 08227
55822260 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 76
5896 deg
Eccentricity:
0008507
Arg of perigee: 11
4610 deg
Mean anomaly: 348
6743 deg
Mean motion: 15
70993970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3772
Checksum: 305
Coasting Arc #3 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2008/228/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1960719
53 A = 6732747
15 meter
Y = 4747164
13 meter E =
0012377
Z = 4340490
94 I = 51
94228
XDOT = -4625
515020 Wp = 66
18761
YDOT = -5088
372503 meter/sec RA = 71
01802 deg
ZDOT = 3472
796830 TA = 348
87272
MA = 348
90006
Ha = 197
063 n
mi
Hp = 187
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6432806
85 X = -2034742
23
Y = 15574685
46 feet Y = 4724824
12 meter
Z = 14240455
84 Z = 4330786
42
XDOT = -15175
574214 XDOT = -4585
142114
YDOT = -16694
135507 feet/sec YDOT = -5139
872120 meter/sec
ZDOT = 11393
690387 ZDOT = 3450
424340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13155118
71 X = 4009680
18
Y = -10580622
16 feet Y = -3224973
64 meter
Z = 14203369
32 Z = 4329186
97
XDOT = 4658
935828 XDOT = 1420
043640
YDOT = 20983
261270 feet/sec YDOT = 6395
698035 meter/sec
ZDOT = 11306
759324 ZDOT = 3446
300242
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 08228
57602822
00020000 00000-0 20000-3 0 9023
2 25544 51
6394 71
3851 0008409 15
6534 344
4886 15
70944670 37886
Satellite: ISS
Catalog Number: 25544
Epoch time: 08228
57602822 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 71
3851 deg
Eccentricity:
0008409
Arg of perigee: 15
6534 deg
Mean anomaly: 344
4886 deg
Mean motion: 15
70944670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3788
Checksum: 311
Coasting Arc #4 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2008/229/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4636674
08 A = 6734613
01 meter
Y = 3067572
96 meter E =
0010792
Z = -3802996
89 I = 51
93721
XDOT = -767
805847 Wp = 53
96267
YDOT = 6381
230553 meter/sec RA = 65
87575 deg
ZDOT = 4225
598249 TA = 260
22249
MA = 260
34438
Ha = 197
057 n
mi
Hp = 186
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15212185
30 X = 4620501
27
Y = 10064215
73 feet Y = 3119332
59 meter
Z = -12477023
93 Z = -3780511
59
XDOT = -2519
048055 XDOT = -859
631493
YDOT = 20935
795777 feet/sec YDOT = 6372
130967 meter/sec
ZDOT = 13863
511315 ZDOT = 4221
645459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8907229
26 X = -2714923
48
Y = -15985255
84 feet Y = -4872305
98 meter
Z = -12389834
89 Z = -3776421
67
XDOT = 10808
459928 XDOT = 3294
418586
YDOT = -16719
444362 feet/sec YDOT = -5096
086641 meter/sec
ZDOT = 13848
803438 ZDOT = 4221
115288
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 08229
53021040
00020000 00000-0 20000-3 0 9038
2 25544 51
6386 66
5058 0008276 19
9123 340
2360 15
70976644 38030
Satellite: ISS
Catalog Number: 25544
Epoch time: 08229
53021040 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 66
5058 deg
Eccentricity:
0008276
Arg of perigee: 19
9123 deg
Mean anomaly: 340
2360 deg
Mean motion: 15
70976644 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3803
Checksum: 280
Coasting Arc #5 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2008/230/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -719684
44 A = 6736952
10 meter
Y = -6022971
75 meter E =
0009663
Z = -2945482
82 I = 51
93219
XDOT = 5520
113225 Wp = 51
63002
YDOT = 1799
923243 meter/sec RA = 60
83324 deg
ZDOT = -5034
507687 TA = 162
06933
MA = 162
03522
Ha = 197
079 n
mi
Hp = 186
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2361169
41 X = -637972
75
Y = -19760405
99 feet Y = -6030562
79 meter
Z = -9663657
54 Z = -2948780
52
XDOT = 18110
607694 XDOT = 5524
032215
YDOT = 5905
259984 feet/sec YDOT = 1861
674251 meter/sec
ZDOT = -16517
413670 ZDOT = -5007
681940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6760652
45 X = -2060646
87
Y = 18710568
44 feet Y = 5702981
26 meter
Z = -9676944
26 Z = -2949532
61
XDOT = -12287
672797 XDOT = -3745
282669
YDOT = -12919
955308 feet/sec YDOT = -3938
002378 meter/sec
ZDOT = -16413
559910 ZDOT = -5002
853061
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 08230
54799634
00020000 00000-0 20000-3 0 9043
2 25544 51
6384 61
3021 0008421 23
8639 336
2911 15
71003971 38198
Satellite: ISS
Catalog Number: 25544
Epoch time: 08230
54799634 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 61
3021 deg
Eccentricity:
0008421
Arg of perigee: 23
8639 deg
Mean anomaly: 336
2911 deg
Mean motion: 15
71003971 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3819
Checksum: 283
Coasting Arc #6 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2008/231/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4644070
38 A = 6730605
82 meter
Y = -33974
99 meter E =
0014618
Z = 4867296
89 I = 51
89494
XDOT = -2453
625569 Wp = 41
53723
YDOT = -6900
607947 meter/sec RA = 55
69632 deg
ZDOT = -2374
508626 TA = 71
61761
MA = 71
45871
Ha = 197
245 n
mi
Hp = 186
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15236451
38 X = -4666989
43
Y = -111466
52 feet Y = -86035
73 meter
Z = 15968821
83 Z = 4844680
65
XDOT = -8049
952655 XDOT = -2364
744735
YDOT = -22639
789852 feet/sec YDOT = -6927
548881 meter/sec
ZDOT = -7790
382630 ZDOT = -2386
212170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13782203
89 X = 4200815
74
Y = 6707992
87 feet Y = 2044596
23 meter
Z = 15881398
99 Z = 4840650
41
XDOT = -2047
261333 XDOT = -624
005254
YDOT = 22874
094728 feet/sec YDOT = 6972
024073 meter/sec
ZDOT = -7836
238647 ZDOT = -2388
485540
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 08231
56577348
00020000 00000-0 20000-3 0 9053
2 25544 51
6382 56
0972 0008271 27
6864 332
4737 15
70985456 38355
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
56577348 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 56
0972 deg
Eccentricity:
0008271
Arg of perigee: 27
6864 deg
Mean anomaly: 332
4737 deg
Mean motion: 15
70985456 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3835
Checksum: 320
Coasting Arc #7 (Orbit 3850)
---------------------------------------
Vector Time (GMT): 2008/232/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486582
53 A = 6740130
24 meter
Y = 5642800
25 meter E =
0021604
Z = 1127740
22 I = 51
90998
XDOT = -4635
340485 Wp = 47
64600
YDOT = 1669
000145 meter/sec RA = 50
63063 deg
ZDOT = 5922
452816 TA = 324
65020
MA = 324
79324
Ha = 197
188 n
mi
Hp = 186
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11438919
07 X = 3417746
40
Y = 18513124
17 feet Y = 5681404
37 meter
Z = 3699935
10 Z = 1144510
54
XDOT = -15207
809990 XDOT = -4682
428965
YDOT = 5475
722260 feet/sec YDOT = 1616
901967 meter/sec
ZDOT = 19430
619476 ZDOT = 5899
820105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2693158
26 X = -820874
64
Y = -21583416
68 feet Y = -6578625
40 meter
Z = 3765259
47 Z = 1147651
09
XDOT = 14635
100574 XDOT = 4460
778655
YDOT = 1580
565457 feet/sec YDOT = 481
756351 meter/sec
ZDOT = 19343
286897 ZDOT = 5895
833846
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 08232
58354107
00020000 00000-0 20000-3 0 9063
2 25544 51
6384 50
8927 0008292 32
0020 328
1644 15
71014540 38511
Satellite: ISS
Catalog Number: 25544
Epoch time: 08232
58354107 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 50
8927 deg
Eccentricity:
0008292
Arg of perigee: 32
0020 deg
Mean anomaly: 328
1644 deg
Mean motion: 15
71014540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3851
Checksum: 266
Coasting Arc #8 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2008/233/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3119825
93 A = 6728589
21 meter
Y = -2763487
17 meter E =
0020904
Z = -5299273
63 I = 51
85254
XDOT = 5269
283525 Wp = 72
32920
YDOT = 5585
976293 meter/sec RA = 45
52236 deg
ZDOT = 196
001146 TA = 199
49006
MA = 199
57010
Ha = 197
253 n
mi
Hp = 186
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10235649
38 X = 3176238
65
Y = -9066558
95 feet Y = -2728284
18 meter
Z = -17386068
35 Z = -5283980
48
XDOT = 17287
675606 XDOT = 5205
476483
YDOT = 18326
693874 feet/sec YDOT = 5644
543696 meter/sec
ZDOT = 643
048378 ZDOT = 221
444128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13097823
75 X = -3992216
68
Y = 4178691
35 feet Y = 1273665
12 meter
Z = -17327202
13 Z = -5281331
21
XDOT = -8210
793004 XDOT = -2502
649708
YDOT = -22753
132400 feet/sec YDOT = -6935
154756 meter/sec
ZDOT = 741
882583 ZDOT = 226
125811
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 08233
53768968
00020000 00000-0 20000-3 0 9074
2 25544 51
6392 46
0144 0008331 36
5681 323
6048 15
71035477 38660
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
53768968 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 46
0144 deg
Eccentricity:
0008331
Arg of perigee: 36
5681 deg
Mean anomaly: 323
6048 deg
Mean motion: 15
71035477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 306
Coasting Arc #9 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2008/234/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5468540
13 A = 6740255
76 meter
Y = -3859127
16 meter E =
0015987
Z = 774019
99 I = 51
87075
XDOT = 2181
623612 Wp = 95
11237
YDOT = -4312
759556 meter/sec RA = 40
41849 deg
ZDOT = -5985
182898 TA = 76
49008
MA = 76
31200
Ha = 197
235 n
mi
Hp = 186
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17941404
64 X = -5428740
37
Y = -12661178
36 feet Y = -3920056
99 meter
Z = 2539435
66 Z = 747550
50
XDOT = 7157
557783 XDOT = 2258
762409
YDOT = -14149
473608 feet/sec YDOT = -4287
932130 meter/sec
ZDOT = -19636
426831 ZDOT = -5974
397151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11717845
98 X = 3571599
45
Y = 18585001
96 feet Y = 5664708
60 meter
Z = 2436792
81 Z = 742734
45
XDOT = -10790
219949 XDOT = -3288
859040
YDOT = 9419
116457 feet/sec YDOT = 2870
946696 meter/sec
ZDOT = -19595
115320 ZDOT = -5972
591150
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 08234
55543720
00020000 00000-0 20000-3 0 9085
2 25544 51
6390 40
8095 0008406 38
4613 321
7147 15
71081979 38829
Satellite: ISS
Catalog Number: 25544
Epoch time: 08234
55543720 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 40
8095 deg
Eccentricity:
0008406
Arg of perigee: 38
4613 deg
Mean anomaly: 321
7147 deg
Mean motion: 15
71081979 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 296
Coasting Arc #10 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2008/235/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -489469
61 A = 6729681
92 meter
Y = 4470761
24 meter E =
0010780
Z = 4996389
99 I = 51
81272
XDOT = -6839
003181 Wp = 74
39346
YDOT = -2950
674632 meter/sec RA = 35
34260 deg
ZDOT = 1969
620310 TA = 356
62188
MA = 356
62915
Ha = 197
334 n
mi
Hp = 185
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1605871
43 X = -563697
64
Y = 14667851
83 feet Y = 4464872
60 meter
Z = 16392355
60 Z = 4993831
91
XDOT = -22437
674477 XDOT = -6815
068064
YDOT = -9680
691050 feet/sec YDOT = -3027
018504 meter/sec
ZDOT = 6462
008891 ZDOT = 1936
454418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6978503
51 X = 2127047
87
Y = -13012941
58 feet Y = -3966344
59 meter
Z = 16382852
70 Z = 4993493
50
XDOT = 16385
281048 XDOT = 4994
233663
YDOT = 16763
467657 feet/sec YDOT = 5109
504942 meter/sec
ZDOT = 6333
567909 ZDOT = 1930
471499
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 08235
57317768
00020000 00000-0 20000-3 0 9090
2 25544 51
6396 35
6056 0008320 43
1620 317
0192 15
71072357 38985
Satellite: ISS
Catalog Number: 25544
Epoch time: 08235
57317768 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 35
6056 deg
Eccentricity:
0008320
Arg of perigee: 43
1620 deg
Mean anomaly: 317
0192 deg
Mean motion: 15
71072357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3898
Checksum: 297
Coasting Arc #11 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2008/236/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6097718
69 A = 6737633
08 meter
Y = 1175329
34 meter E =
0013491
Z = -2609070
84 I = 51
81619
XDOT = 1185
332493 Wp = 48
83178
YDOT = 5482
280455 meter/sec RA = 30
20465 deg
ZDOT = 5266
152034 TA = 281
64442
MA = 281
79580
Ha = 197
427 n
mi
Hp = 185
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20005638
75 X = 6096797
20
Y = 3856067
38 feet Y = 1243512
50 meter
Z = -8559943
69 Z = -2579450
23
XDOT = 3888
886133 XDOT = 1098
358581
YDOT = 17986
484432 feet/sec YDOT = 5495
049007 meter/sec
ZDOT = 17277
401687 ZDOT = 5271
699364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17413747
02 X = -5307710
09
Y = -10667934
02 feet Y = -3251586
29 meter
Z = -8445358
01 Z = -2574145
12
XDOT = 2005
485940 XDOT = 611
272115
YDOT = -16899
713162 feet/sec YDOT = -5151
032572 meter/sec
ZDOT = 17299
306710 ZDOT = 5272
828685
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 08236
52729999
00020000 00000-0 20000-3 0 9101
2 25544 51
6410 30
7276 0008369 47
6306 312
5563 15
71075862 39139
Satellite: ISS
Catalog Number: 25544
Epoch time: 08236
52729999 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 30
7276 deg
Eccentricity:
0008369
Arg of perigee: 47
6306 deg
Mean anomaly: 312
5563 deg
Mean motion: 15
71075862 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3913
Checksum: 302
Coasting Arc #12 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2008/237/12:31:53
274
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525462
97 A = 6733215
35 meter
Y = -4737035
84 meter E =
0015720
Z = -4081598
69 I = 51
77593
XDOT = 6644
613739 Wp = 59
78929
YDOT = -229
092967 meter/sec RA = 25
14977 deg
ZDOT = -3848
693295 TA = 170
60351
MA = 170
57406
Ha = 197
390 n
mi
Hp = 185
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8285639
68 X = -2452477
34
Y = -15541456
17 feet Y = -4764868
68 meter
Z = -13391071
81 Z = -4093690
39
XDOT = 21799
913841 XDOT = 6665
377886
YDOT = -751
617347 feet/sec YDOT = -154
672731 meter/sec
ZDOT = -12626
946505 ZDOT = -3816
363372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2512933
22 X = 765942
05
Y = 17395669
04 feet Y = 5302199
92 meter
Z = -13438205
02 Z = -4095964
89
XDOT = -19585
505660 XDOT = -5969
662125
YDOT = -6820
322815 feet/sec YDOT = -2078
834394 meter/sec
ZDOT = -12502
003827 ZDOT = -3810
610767
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 08237
54502016
00020000 00000-0 20000-3 0 9114
2 25544 51
6412 25
5239 0008406 50
7967 309
3940 15
71093514 39296
Satellite: ISS
Catalog Number: 25544
Epoch time: 08237
54502016 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 25
5239 deg
Eccentricity:
0008406
Arg of perigee: 50
7967 deg
Mean anomaly: 309
3940 deg
Mean motion: 15
71093514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 282
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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