Date:
November 6th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 1077)
---------------------------------------
Vector Time (GMT): 2008/310/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 878275
15 A = 6725411
05 meter
Y = 4289082
27 meter E =
0000854
Z = 5104807
25 I = 51
68881
XDOT = -7540
357514 Wp = 129
69655
YDOT = -277
366572 meter/sec RA = 11
32319 deg
ZDOT = 1529
648656 TA = 305
63191
MA = 305
63986
Ha = 191
721 n
mi
Hp = 187
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2881480
16 X = 805450
01
Y = 14071792
21 feet Y = 4298496
27 meter
Z = 16748055
28 Z = 5108897
25
XDOT = -24738
705756 XDOT = -7544
126420
YDOT = -909
995314 feet/sec YDOT = -361
708336 meter/sec
ZDOT = 5018
532337 ZDOT = 1493
007805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13185915
04 X = -4019066
90
Y = -5648732
21 feet Y = -1721733
58 meter
Z = 16764220
49 Z = 5109734
41
XDOT = 14326
628918 XDOT = 4366
756494
YDOT = -18963
643543 feet/sec YDOT = -5780
118552 meter/sec
ZDOT = 4876
485003 ZDOT = 1486
352629
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
58144808
00020000 00000-0 20000-3 0 9009
2 25544 51
6424 11
5523 0003822 304
8068 55
2734 15
72393907 10783
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
58144808 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 11
5523 deg
Eccentricity:
0003822
Arg of perigee: 304
8068 deg
Mean anomaly: 55
2734 deg
Mean motion: 15
72393907 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1078
Checksum: 274
Coasting Arc #2 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/311/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6430855
95 A = 6735338
13 meter
Y = -761450
45 meter E =
0008488
Z = -1833904
45 I = 51
69304
XDOT = 2173
154752 Wp = 10
89057
YDOT = 4737
086700 meter/sec RA = 6
17428 deg
ZDOT = 5666
031456 TA = 328
79090
MA = 328
84127
Ha = 191
933 n
mi
Hp = 187
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21098608
75 X = 6447801
58
Y = -2498197
01 feet Y = -689442
11 meter
Z = -6016746
90 Z = -1802621
67
XDOT = 7129
772807 XDOT = 2092
497335
YDOT = 15541
623033 feet/sec YDOT = 4760
937080 meter/sec
ZDOT = 18589
342048 ZDOT = 5676
392998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9547669
95 X = -2910129
80
Y = 19017835
75 feet Y = 5796636
34 meter
Z = -5895544
48 Z = -1796961
96
XDOT = -15454
184554 XDOT = -4710
435452
YDOT = -1996
202841 feet/sec YDOT = -608
442626 meter/sec
ZDOT = 18629
850277 ZDOT = 5678
378364
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 08311
53476665
00020000 00000-0 20000-3 0 9015
2 25544 51
6424 6
6683 0003841 310
7726 49
3103 15
72396750 10933
Satellite: ISS
Catalog Number: 25544
Epoch time: 08311
53476665 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 6
6683 deg
Eccentricity:
0003841
Arg of perigee: 310
7726 deg
Mean anomaly: 49
3103 deg
Mean motion: 15
72396750 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 280
Coasting Arc #3 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2008/312/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2854389
89 A = 6726830
06 meter
Y = -3818925
83 meter E =
0010446
Z = -4755113
68 I = 51
63619
XDOT = 6964
561532 Wp = 52
47941
YDOT = -1941
267016 meter/sec RA = 1
08936 deg
ZDOT = -2619
281756 TA = 191
76067
MA = 191
78508
Ha = 191
959 n
mi
Hp = 187
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9364796
24 X = -2788373
98
Y = -12529284
22 feet Y = -3850476
14 meter
Z = -15600766
65 Z = -4768820
22
XDOT = 22849
611326 XDOT = 6998
475707
YDOT = -6368
986272 feet/sec YDOT = -1863
195629 meter/sec
ZDOT = -8593
444081 ZDOT = -2585
364908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15549049
18 X = 4739350
19
Y = -1113643
70 feet Y = -339438
60 meter
Z = -15654173
86 Z = -4771392
19
XDOT = -6979
165422 XDOT = -2127
249621
YDOT = 21610
962728 feet/sec YDOT = 6587
021440 meter/sec
ZDOT = -8462
120124 ZDOT = -2579
254214
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 08312
55162592
00020000 00000-0 20000-3 0 9020
2 25544 51
6431 1
4585 0003755 315
3936 44
6924 15
72414888 11093
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
55162592 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 1
4585 deg
Eccentricity:
0003755
Arg of perigee: 315
3936 deg
Mean anomaly: 44
6924 deg
Mean motion: 15
72414888 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 285
Coasting Arc #4 (Orbit 1124)
---------------------------------------
Vector Time (GMT): 2008/313/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5595759
22 A = 6733407
29 meter
Y = 2560991
22 meter E =
0010992
Z = 2723770
31 I = 51
62847
XDOT = -4261
158612 Wp = 88
09068
YDOT = -3796
922687 meter/sec RA = 355
92263 deg
ZDOT = -5165
940801 TA = 60
82896
MA = 60
71902
Ha = 192
077 n
mi
Hp = 186
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18358790
09 X = -5637212
62
Y = 8402202
16 feet Y = 2498184
45 meter
Z = 8936254
29 Z = 2696484
79
XDOT = -13980
179173 XDOT = -4193
288340
YDOT = -12457
095431 feet/sec YDOT = -3844
193991 meter/sec
ZDOT = -16948
624674 ZDOT = -5186
477073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2430134
07 X = 740704
86
Y = -20090104
61 feet Y = -6123463
89 meter
Z = 8830682
90 Z = 2691592
15
XDOT = 16403
596811 XDOT = 4999
816308
YDOT = -5527
361706 feet/sec YDOT = -1684
739848 meter/sec
ZDOT = -17028
501106 ZDOT = -5190
287137
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 08313
56847029
00020000 00000-0 20000-3 0 9038
2 25544 51
6424 356
2489 0003841 321
7244 38
3645 15
72465717 11253
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
56847029 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 356
2489 deg
Eccentricity:
0003841
Arg of perigee: 321
7244 deg
Mean anomaly: 38
3645 deg
Mean motion: 15
72465717 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1125
Checksum: 293
Coasting Arc #5 (Orbit 1140)
---------------------------------------
Vector Time (GMT): 2008/314/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4486672
28 A = 6728682
86 meter
Y = 2677449
77 meter E =
0007456
Z = 4233273
55 I = 51
58315
XDOT = -5657
810237 Wp = 88
01360
YDOT = 3796
083592 meter/sec RA = 350
84386 deg
ZDOT = 3590
373317 TA = 325
44888
MA = 325
49731
Ha = 192
110 n
mi
Hp = 186
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14720053
43 X = 4435834
11
Y = 8784284
02 feet Y = 2727338
14 meter
Z = 13888692
76 Z = 4254946
87
XDOT = -18562
369543 XDOT = -5717
280009
YDOT = 12454
342492 feet/sec YDOT = 3732
482219 meter/sec
ZDOT = 11779
440016 ZDOT = 3562
742434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14991241
19 X = -4569330
32
Y = 8170704
30 feet Y = 2490430
67 meter
Z = 13972891
04 Z = 4258937
19
XDOT = -702
050768 XDOT = -213
985074
YDOT = -21278
518057 feet/sec YDOT = -6485
692304 meter/sec
ZDOT = 11672
623780 ZDOT = 3557
815728
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 08314
58530254
00020000 00000-0 20000-3 0 9041
2 25544 51
6420 351
0388 0003761 327
8928 32
2005 15
72460449 11415
Satellite: ISS
Catalog Number: 25544
Epoch time: 08314
58530254 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 351
0388 deg
Eccentricity:
0003761
Arg of perigee: 327
8928 deg
Mean anomaly: 32
2005 deg
Mean motion: 15
72460449 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1141
Checksum: 268
Coasting Arc #6 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2008/315/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4167109
18 A = 6731151
86 meter
Y = -3946026
60 meter E =
0004425
Z = -3517406
80 I = 51
56390
XDOT = 5854
064500 Wp = 47
70845
YDOT = 2183
656369 meter/sec RA = 345
66551 deg
ZDOT = 4492
138140 TA = 270
44619
MA = 270
49689
Ha = 192
283 n
mi
Hp = 186
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13671618
04 X = 4228012
05
Y = -12946281
49 feet Y = -3899087
06 meter
Z = -11540048
57 Z = -3497014
39
XDOT = 19206
248360 XDOT = 5807
388714
YDOT = 7164
226934 feet/sec YDOT = 2248
858943 meter/sec
ZDOT = 14737
986022 ZDOT = 4520
464706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4516669
13 X = 1376680
75
Y = 18328403
54 feet Y = 5586497
40 meter
Z = -11461299
61 Z = -3493404
12
XDOT = -14305
149580 XDOT = -4360
209592
YDOT = 12796
614949 feet/sec YDOT = 3900
408236 meter/sec
ZDOT = 14847
930223 ZDOT = 4525
649132
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 08315
53856907
00020000 00000-0 20000-3 0 9054
2 25544 51
6431 346
1552 0003838 331
5093 28
5859 15
72499028 11561
Satellite: ISS
Catalog Number: 25544
Epoch time: 08315
53856907 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 346
1552 deg
Eccentricity:
0003838
Arg of perigee: 331
5093 deg
Mean anomaly: 28
5859 deg
Mean motion: 15
72499028 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 307
Coasting Arc #7 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2008/316/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5591344
13 A = 6730704
51 meter
Y = -1062447
47 meter E =
0005872
Z = -3600501
99 I = 51
53358
XDOT = 3791
319690 Wp = 40
26250
YDOT = -5042
105219 meter/sec RA = 340
58634 deg
ZDOT = -4399
418161 TA = 182
80128
MA = 182
80457
Ha = 192
312 n
mi
Hp = 186
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18344304
90 X = -5561556
88
Y = -3485720
05 feet Y = -1124806
49 meter
Z = -11812670
58 Z = -3627593
39
XDOT = 12438
712894 XDOT = 3868
791902
YDOT = -16542
339958 feet/sec YDOT = -4999
275234 meter/sec
ZDOT = -14433
786619 ZDOT = -4380
811174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11777074
67 X = 3589652
36
Y = -14403849
15 feet Y = -4390293
22 meter
Z = -11917742
85 Z = -3632528
02
XDOT = 7521
895613 XDOT = 2292
673783
YDOT = 18034
413469 feet/sec YDOT = 5496
889225 meter/sec
ZDOT = -14362
034621 ZDOT = -4377
548152
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 08316
55537368
00020000 00000-0 20000-3 0 9065
2 25544 51
6421 340
9448 0003885 334
8027 25
2945 15
72508769 11722
Satellite: ISS
Catalog Number: 25544
Epoch time: 08316
55537368 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 340
9448 deg
Eccentricity:
0003885
Arg of perigee: 334
8027 deg
Mean anomaly: 25
2945 deg
Mean motion: 15
72508769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1172
Checksum: 309
Coasting Arc #8 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2008/317/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2395886
05 A = 6728884
66 meter
Y = 4724317
36 meter E =
0010746
Z = 4146414
27 I = 51
49920
XDOT = -6745
438832 Wp = 53
28951
YDOT = -155
511714 meter/sec RA = 335
40198 deg
ZDOT = -3707
526426 TA = 74
74742
MA = 74
62864
Ha = 192
406 n
mi
Hp = 186
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7860518
55 X = -2468679
37
Y = 15499728
87 feet Y = 4697117
94 meter
Z = 13603721
35 Z = 4134598
04
XDOT = -22130
704831 XDOT = -6725
187354
YDOT = -510
209037 feet/sec YDOT = -230
829679 meter/sec
ZDOT = -12163
800609 ZDOT = -3740
247833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10086235
71 X = -3074284
64
Y = -14196196
98 feet Y = -4327000
84 meter
Z = 13558260
28 Z = 4132557
73
XDOT = 9599
365379 XDOT = 2925
886568
YDOT = -18599
258846 feet/sec YDOT = -5669
054096 meter/sec
ZDOT = -12290
627037 ZDOT = -3746
183121
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
57216410
00020000 00000-0 20000-3 0 9071
2 25544 51
6410 335
7342 0003996 339
3958 20
7043 15
72553537 11880
Satellite: ISS
Catalog Number: 25544
Epoch time: 08317
57216410 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 335
7342 deg
Eccentricity:
0003996
Arg of perigee: 339
3958 deg
Mean anomaly: 20
7043 deg
Mean motion: 15
72553537 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1188
Checksum: 293
Coasting Arc #9 (Orbit 1203)
---------------------------------------
Vector Time (GMT): 2008/318/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6033000
84 A = 6732659
01 meter
Y = -823816
59 meter E =
0013368
Z = 2854707
76 I = 51
48559
XDOT = -1639
999176 Wp = 64
12466
YDOT = 5571
008625 meter/sec RA = 330
31623 deg
ZDOT = 5061
009039 TA = 328
73057
MA = 328
81001
Ha = 192
344 n
mi
Hp = 186
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19793309
86 X = 6027896
35
Y = -2702810
33 feet Y = -756380
88 meter
Z = 9365839
11 Z = 2884004
67
XDOT = -5380
574723 XDOT = -1726
759568
YDOT = 18277
587354 feet/sec YDOT = 5552
183650 meter/sec
ZDOT = 16604
360364 ZDOT = 5052
831386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6389183
20 X = -1947423
04
Y = 18871139
85 feet Y = 5751923
43 meter
Z = 9479328
03 Z = 2889299
18
XDOT = -12537
716420 XDOT = -3821
495965
YDOT = -12590
318064 feet/sec YDOT = -3837
528946 meter/sec
ZDOT = 16573
054370 ZDOT = 5051
466972
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
58894152
00020000 00000-0 20000-3 0 9089
2 25544 51
6405 330
5240 0003995 342
7374 17
3652 15
72559899 12047
Satellite: ISS
Catalog Number: 25544
Epoch time: 08318
58894152 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 330
5240 deg
Eccentricity:
0003995
Arg of perigee: 342
7374 deg
Mean anomaly: 17
3652 deg
Mean motion: 15
72559899 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1204
Checksum: 308
Coasting Arc #10 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 464208
26 A = 6726942
17 meter
Y = -4843614
95 meter E =
0009237
Z = -4652705
35 I = 51
44102
XDOT = 6859
558661 Wp = 87
35518
YDOT = -2043
041511 meter/sec RA = 325
13364 deg
ZDOT = 2816
489424 TA = 210
54057
MA = 210
59439
Ha = 192
566 n
mi
Hp = 186
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1522992
97 X = 540938
55
Y = -15891125
16 feet Y = -4837994
34 meter
Z = -15264781
32 Z = -4650264
34
XDOT = 22505
113716 XDOT = 6868
212041
YDOT = -6702
892096 feet/sec YDOT = -1966
285911 meter/sec
ZDOT = 9240
450865 ZDOT = 2849
834975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13647587
95 X = 4159784
81
Y = 8298751
02 feet Y = 2529459
31 meter
Z = -15255654
36 Z = -4649923
45
XDOT = -3016
938153 XDOT = -919
562749
YDOT = 22154
029690 feet/sec YDOT = 6752
548249 meter/sec
ZDOT = 9369
554328 ZDOT = 2855
840159
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
54215785
00020000 00000-0 20000-3 0 9096
2 25544 51
6404 325
6389 0004089 346
7900 13
3154 15
72546027 12197
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54215785 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 325
6389 deg
Eccentricity:
0004089
Arg of perigee: 346
7900 deg
Mean anomaly: 13
3154 deg
Mean motion: 15
72546027 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 295
Coasting Arc #11 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/320/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806207
66 A = 6734274
64 meter
Y = 2712125
34 meter E =
0003733
Z = -2071085
57 I = 51
44233
XDOT = -515
536241 Wp = 101
87703
YDOT = -5321
052933 meter/sec RA = 320
03449 deg
ZDOT = -5531
892070 TA = 101
28044
MA = 101
23848
Ha = 192
628 n
mi
Hp = 185
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19049237
71 X = -5826042
35
Y = 8898049
01 feet Y = 2647086
33 meter
Z = -6794900
17 Z = -2099340
63
XDOT = -1691
391868 XDOT = -429
123477
YDOT = -17457
522747 feet/sec YDOT = -5326
334085 meter/sec
ZDOT = -18149
252198 ZDOT = -5534
187390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -202607
41 X = -61754
74
Y = -20988327
38 feet Y = -6397242
19 meter
Z = -6904235
36 Z = -2104410
94
XDOT = 15010
479620 XDOT = 4575
194188
YDOT = 5818
721876 feet/sec YDOT = 1773
546428 meter/sec
ZDOT = -18158
515367 ZDOT = -5534
715484
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
55890849
00020000 00000-0 20000-3 0 9101
2 25544 51
6398 320
4276 0004099 352
0912 8
0185 15
72587866 12350
Satellite: ISS
Catalog Number: 25544
Epoch time: 08320
55890849 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 320
4276 deg
Eccentricity:
0004099
Arg of perigee: 352
0912 deg
Mean anomaly: 8
0185 deg
Mean motion: 15
72587866 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 303
Coasting Arc #12 (Orbit 1250)
---------------------------------------
Vector Time (GMT): 2008/321/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1325715
37 A = 6725290
45 meter
Y = 4312474
24 meter E =
0008569
Z = 4985905
49 I = 51
39017
XDOT = -6227
221868 Wp = 29
74696
YDOT = 4113
920052 meter/sec RA = 314
85909 deg
ZDOT = -1893
769905 TA = 78
64661
MA = 78
55034
Ha = 192
628 n
mi
Hp = 185
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4349459
86 X = 1253173
01
Y = 14148537
54 feet Y = 4326892
94 meter
Z = 16357957
66 Z = 4992170
25
XDOT = -20430
517939 XDOT = -6263
561821
YDOT = 13497
113032 feet/sec YDOT = 4044
080705 meter/sec
ZDOT = -6213
155856 ZDOT = -1924
110030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14670700
94 X = -4471629
65
Y = -1750590
47 feet Y = -533579
98 meter
Z = 16382541
36 Z = 4993398
61
XDOT = -4354
378421 XDOT = -1327
214543
YDOT = -23018
392213 feet/sec YDOT = -7016
005946 meter/sec
ZDOT = -6330
483597 ZDOT = -1929
531400
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
57564438
00020000 00000-0 20000-3 0 9117
2 25544 51
6395 315
2167 0004190 353
9851 6
1261 15
72614044 12513
Satellite: ISS
Catalog Number: 25544
Epoch time: 08321
57564438 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 315
2167 deg
Eccentricity:
0004190
Arg of perigee: 353
9851 deg
Mean anomaly: 6
1261 deg
Mean motion: 15
72614044 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1251
Checksum: 272
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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