Date:
June 29th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3015)
---------------------------------------
Vector Time (GMT): 2008/179/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5917694
75 A = 6727204
12 meter
Y = -2050028
82 meter E =
0009675
Z = 2438648
70 I = 51
45201
XDOT = -278
421843 Wp = 36
27577
YDOT = 5549
508643 meter/sec RA = 322
81730 deg
ZDOT = 5337
691650 TA = 351
36682
MA = 351
38345
Ha = 188
193 n
mi
Hp = 185
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19415009
01 X = 5928332
09
Y = -6725816
34 feet Y = -1983794
63 meter
Z = 8000815
96 Z = 2467422
60
XDOT = -913
457489 XDOT = -366
386332
YDOT = 18207
049355 feet/sec YDOT = 5545
902602 meter/sec
ZDOT = 17512
111712 ZDOT = 5336
126164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8459447
59 X = -2578439
63
Y = -18677106
76 feet Y = -5692782
14 meter
Z = 8111452
76 Z = 2472370
80
XDOT = 16861
884892 XDOT = 5139
502515
YDOT = -29
876298 feet/sec YDOT = -9
106296 meter/sec
ZDOT = 17506
525686 ZDOT = 5335
989029
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 08179
55853120
00020000 00000-0 20000-3 0 9003
2 25544 51
6384 323
0373 0008732 299
1474 60
8815 15
74814860 30168
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
55853120 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 323
0373 deg
Eccentricity:
0008732
Arg of perigee: 299
1474 deg
Mean anomaly: 60
8815 deg
Mean motion: 15
74814860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3016
Checksum: 293
Coasting Arc #2 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2008/180/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 107798
35 A = 6721006
41 meter
Y = -4977494
33 meter E =
0002483
Z = -4516020
65 I = 51
40863
XDOT = 6543
593896 Wp = 56
03973
YDOT = -2647
457526 meter/sec RA = 317
61684 deg
ZDOT = 3076
760299 TA = 244
69155
MA = 244
71728
Ha = 188
511 n
mi
Hp = 184
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 353669
13 X = 185387
67
Y = -16330361
98 feet Y = -4975854
32 meter
Z = -14816340
70 Z = -4515309
29
XDOT = 21468
483911 XDOT = 6557
765375
YDOT = -8685
884271 feet/sec YDOT = -2574
204567 meter/sec
ZDOT = 10094
357935 ZDOT = 3108
583358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16282159
72 X = -4962802
28
Y = 1329108
85 feet Y = 405112
38 meter
Z = -14813996
78 Z = -4515306
22
XDOT = -10851
734236 XDOT = -3307
608595
YDOT = -19159
250028 feet/sec YDOT = -5839
739409 meter/sec
ZDOT = 10216
690036 ZDOT = 3114
047123
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 08180
51039074
00020000 00000-0 20000-3 0 9016
2 25544 51
6387 318
1438 0008786 303
6382 56
3943 15
74805365 30315
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
51039074 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 318
1438 deg
Eccentricity:
0008786
Arg of perigee: 303
6382 deg
Mean anomaly: 56
3943 deg
Mean motion: 15
74805365 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3031
Checksum: 293
Coasting Arc #3 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2008/181/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5498025
11 A = 6725966
72 meter
Y = 2528636
44 meter E =
0004660
Z = -2937770
49 I = 51
40509
XDOT = -27
018058 Wp = 323
60283
YDOT = -5862
360262 meter/sec RA = 312
50496 deg
ZDOT = -4987
626913 TA = 250
36715
MA = 250
41745
Ha = 188
694 n
mi
Hp = 184
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18038140
12 X = -5511620
82
Y = 8296051
31 feet Y = 2467078
92 meter
Z = -9638354
61 Z = -2964512
67
XDOT = -88
641923 XDOT = 62
766986
YDOT = -19233
465427 feet/sec YDOT = -5862
159430 meter/sec
ZDOT = -16363
605359 ZDOT = -4987
541195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10481287
10 X = 3194696
31
Y = 16803266
05 feet Y = 5121635
49 meter
Z = -9741135
29 Z = -2969098
04
XDOT = -17857
618972 XDOT = -5443
002263
YDOT = 1638
061960 feet/sec YDOT = 499
281285 meter/sec
ZDOT = -16363
738536 ZDOT = -4987
667506
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 08181
52569184
00020000 00000-0 20000-3 0 9029
2 25544 51
6388 312
9225 0008821 307
8582 52
1783 15
74835534 30474
Satellite: ISS
Catalog Number: 25544
Epoch time: 08181
52569184 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 312
9225 deg
Eccentricity:
0008821
Arg of perigee: 307
8582 deg
Mean anomaly: 52
1783 deg
Mean motion: 15
74835534 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3047
Checksum: 305
Coasting Arc #4 (Orbit 3062)
---------------------------------------
Vector Time (GMT): 2008/182/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 179194
45 A = 6722235
87 meter
Y = 5268690
13 meter E =
0009235
Z = 4173798
67 I = 51
37400
XDOT = -6027
419106 Wp = 21
09403
YDOT = 3103
298369 meter/sec RA = 307
29568 deg
ZDOT = -3647
598872 TA = 106
29296
MA = 106
19136
Ha = 188
883 n
mi
Hp = 184
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 587908
29 X = 99990
14
Y = 17285728
76 feet Y = 5270250
21 meter
Z = 13693565
18 Z = 4174477
96
XDOT = -19774
997068 XDOT = -6043
953238
YDOT = 10181
425094 feet/sec YDOT = 3035
804667 meter/sec
ZDOT = -11967
187901 ZDOT = -3676
919724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17037672
21 X = 5193082
49
Y = -2962559
45 feet Y = -902988
12 meter
Z = 13696596
26 Z = 4174722
54
XDOT = 12664
020423 XDOT = 3859
993425
YDOT = 16816
017751 feet/sec YDOT = 5125
522211 meter/sec
ZDOT = -12079
860799 ZDOT = -3681
941571
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 08182
54097893
00020000 00000-0 20000-3 0 9036
2 25544 51
6393 307
7018 0008754 312
0258 48
0160 15
74831116 30638
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
54097893 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 307
7018 deg
Eccentricity:
0008754
Arg of perigee: 312
0258 deg
Mean anomaly: 48
0160 deg
Mean motion: 15
74831116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3063
Checksum: 286
Coasting Arc #5 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2008/183/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5028214
67 A = 6724383
34 meter
Y = -2852506
80 meter E =
0008653
Z = 3423393
29 I = 51
36653
XDOT = 408
476666 Wp = 45
30007
YDOT = 6196
623807 meter/sec RA = 302
18507 deg
ZDOT = 4562
264197 TA = 355
41449
MA = 355
42241
Ha = 188
835 n
mi
Hp = 183
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16496767
29 X = 5043107
93
Y = -9358618
10 feet Y = -2796195
96 meter
Z = 11231605
29 Z = 3447855
85
XDOT = 1340
146542 XDOT = 316
992044
YDOT = 20330
130601 feet/sec YDOT = 6200
679029 meter/sec
ZDOT = 14968
058388 ZDOT = 4564
027828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11855245
55 X = -3613478
84
Y = -14732958
07 feet Y = -4490605
62 meter
Z = 11325595
82 Z = 3452041
61
XDOT = 18796
835292 XDOT = 5729
275397
YDOT = -3610
811435 feet/sec YDOT = -1100
575325 meter/sec
ZDOT = 14975
339793 ZDOT = 4564
483569
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 08183
55624785
00020000 00000-0 20000-3 0 9045
2 25544 51
6404 302
4808 0008890 315
7837 44
2615 15
74915840 30791
Satellite: ISS
Catalog Number: 25544
Epoch time: 08183
55624785 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 302
4808 deg
Eccentricity:
0008890
Arg of perigee: 315
7837 deg
Mean anomaly: 44
2615 deg
Mean motion: 15
74915840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3079
Checksum: 308
Coasting Arc #6 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2008/184/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -564682
52 A = 6723449
54 meter
Y = -5536076
33 meter E =
0005489
Z = -3768793
44 I = 51
34854
XDOT = 5492
913049 Wp =
93730
YDOT = -3407
942396 meter/sec RA = 296
97148 deg
ZDOT = 4188
500891 TA = 313
17034
MA = 313
21621
Ha = 189
192 n
mi
Hp = 183
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1852632
94 X = -484427
31
Y = -18162980
07 feet Y = -5541941
30 meter
Z = -12364807
87 Z = -3771343
03
XDOT = 18021
368270 XDOT = 5510
266147
YDOT = -11180
913372 feet/sec YDOT = -3346
421469 meter/sec
ZDOT = 13741
800825 ZDOT = 4215
226588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17565090
80 X = -5353839
67
Y = 4953768
15 feet Y = 1509908
53 meter
Z = -12375069
05 Z = -3771921
05
XDOT = -13805
509582 XDOT = -4207
919321
YDOT = -14411
602885 feet/sec YDOT = -4392
656559 meter/sec
ZDOT = 13844
471489 ZDOT = 4219
794910
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 08184
50805239
00020000 00000-0 20000-3 0 9057
2 25544 51
6404 297
5874 0009090 320
0420 40
0074 15
74887832 30947
Satellite: ISS
Catalog Number: 25544
Epoch time: 08184
50805239 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 297
5874 deg
Eccentricity:
0009090
Arg of perigee: 320
0420 deg
Mean anomaly: 40
0074 deg
Mean motion: 15
74887832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3094
Checksum: 286
Coasting Arc #7 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2008/185/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4570978
58 A = 6722920
37 meter
Y = 3045905
37 meter E =
0009296
Z = -3884550
84 I = 51
33524
XDOT = -881
616533 Wp = 6
73982
YDOT = -6487
970448 meter/sec RA = 291
86007 deg
ZDOT = -4041
736801 TA = 220
94785
MA = 221
01770
Ha = 189
327 n
mi
Hp = 183
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14996648
87 X = -4585828
49
Y = 9993127
87 feet Y = 2994707
91 meter
Z = -12744589
38 Z = -3906791
72
XDOT = -2892
442694 XDOT = -789
367769
YDOT = -21285
992282 feet/sec YDOT = -6497
312497 meter/sec
ZDOT = -13260
291341 ZDOT = -4045
797010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12686286
62 X = 3866780
16
Y = 12713590
87 feet Y = 3875102
50 meter
Z = -12830018
69 Z = -3910589
70
XDOT = -19414
690408 XDOT = -5917
597636
YDOT = 5948
234036 feet/sec YDOT = 1813
021734 meter/sec
ZDOT = -13276
456581 ZDOT = -4046
663966
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 08185
52329511
00020000 00000-0 20000-3 0 9065
2 25544 51
6407 292
3668 0009011 324
0077 36
0479 15
74918072 31103
Satellite: ISS
Catalog Number: 25544
Epoch time: 08185
52329511 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 292
3668 deg
Eccentricity:
0009011
Arg of perigee: 324
0077 deg
Mean anomaly: 36
0479 deg
Mean motion: 15
74918072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3110
Checksum: 280
Coasting Arc #8 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2008/186/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1000152
45 A = 6724858
62 meter
Y = 5790928
36 meter E =
0010903
Z = 3270230
49 I = 51
33175
XDOT = -4977
689579 Wp = 48
02271
YDOT = 3522
832705 meter/sec RA = 286
64469 deg
ZDOT = -4698
650784 TA = 93
45726
MA = 93
33254
Ha = 189
512 n
mi
Hp = 183
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3281340
06 X = 919437
16
Y = 18999108
79 feet Y = 5801660
69 meter
Z = 10729102
65 Z = 3274894
22
XDOT = -16331
002557 XDOT = -4993
887748
YDOT = 11557
850083 feet/sec YDOT = 3467
079681 meter/sec
ZDOT = -15415
520944 ZDOT = -4722
870594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17899927
29 X = 5455897
84
Y = -7136511
21 feet Y = -2175208
62 meter
Z = 10747547
72 Z = 3275852
54
XDOT = 14189
439929 XDOT = 4324
941290
YDOT = 12149
442834 feet/sec YDOT = 3703
150176 meter/sec
ZDOT = -15508
536546 ZDOT = -4727
001939
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 08186
53852360
00020000 00000-0 20000-3 0 9071
2 25544 51
6403 287
1465 0008993 328
9915 31
0716 15
74933487 31261
Satellite: ISS
Catalog Number: 25544
Epoch time: 08186
53852360 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 287
1465 deg
Eccentricity:
0008993
Arg of perigee: 328
9915 deg
Mean anomaly: 31
0716 deg
Mean motion: 15
74933487 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3126
Checksum: 314
Coasting Arc #9 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2008/187/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142623
83 A = 6721179
82 meter
Y = -3073362
68 meter E =
0006943
Z = 4301827
10 I = 51
31298
XDOT = 1434
734340 Wp = 44
59866
YDOT = 6745
424164 meter/sec RA = 281
52859 deg
ZDOT = 3439
036054 TA = 10
53857
MA = 10
52402
Ha = 189
477 n
mi
Hp = 182
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13591285
54 X = 4155785
70
Y = -10083210
89 feet Y = -3026964
61 meter
Z = 14113605
96 Z = 4321983
02
XDOT = 4707
133663 XDOT = 1342
493429
YDOT = 22130
656707 feet/sec YDOT = 6760
951871 meter/sec
ZDOT = 11282
926686 ZDOT = 3445
782923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12883465
74 X = -3926880
36
Y = -10872894
68 feet Y = -3314058
30 meter
Z = 14191001
72 Z = 4325417
32
XDOT = 19709
166856 XDOT = 6007
354058
YDOT = -8599
373695 feet/sec YDOT = -2621
089102 meter/sec
ZDOT = 11309
489973 ZDOT = 3447
132544
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 08187
55373516
00020000 00000-0 20000-3 0 9086
2 25544 51
6404 281
9249 0009122 332
6327 27
4355 15
74998683 31423
Satellite: ISS
Catalog Number: 25544
Epoch time: 08187
55373516 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 281
9249 deg
Eccentricity:
0009122
Arg of perigee: 332
6327 deg
Mean anomaly: 27
4355 deg
Mean motion: 15
74998683 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3142
Checksum: 311
Coasting Arc #10 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2008/188/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1528743
48 A = 6726181
85 meter
Y = -5953187
28 meter E =
0011161
Z = -2716440
72 I = 51
32450
XDOT = 4534
350838 Wp = 1
51244
YDOT = -3508
286978 meter/sec RA = 276
31587 deg
ZDOT = 5148
214018 TA = 327
30317
MA = 327
37221
Ha = 189
796 n
mi
Hp = 182
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5015562
61 X = -1448864
64
Y = -19531454
32 feet Y = -5969835
56 meter
Z = -8912207
07 Z = -2723674
02
XDOT = 14876
479127 XDOT = 4548
235421
YDOT = -11510
127879 feet/sec YDOT = -3457
504349 meter/sec
ZDOT = 16890
465939 ZDOT = 5170
274736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17735512
13 X = -5405784
10
Y = 9569664
67 feet Y = 2916833
79 meter
Z = -8940589
39 Z = -2725091
65
XDOT = -14063
721923 XDOT = -4286
622442
YDOT = -10240
178379 feet/sec YDOT = -3121
206370 meter/sec
ZDOT = 16975
160870 ZDOT = 5174
029033
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 08188
50548548
00020000 00000-0 20000-3 0 9092
2 25544 51
6400 277
0311 0009360 336
3284 23
7448 15
74968562 31573
Satellite: ISS
Catalog Number: 25544
Epoch time: 08188
50548548 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 277
0311 deg
Eccentricity:
0009360
Arg of perigee: 336
3284 deg
Mean anomaly: 23
7448 deg
Mean motion: 15
74968562 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3157
Checksum: 307
Coasting Arc #11 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2008/189/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3802067
45 A = 6719789
64 meter
Y = 3005398
65 meter E =
0014368
Z = -4666619
90 I = 51
30034
XDOT = -2058
368767 Wp = 30
59003
YDOT = -6883
762873 meter/sec RA = 271
19390 deg
ZDOT = -2747
770433 TA = 212
12733
MA = 212
21497
Ha = 189
918 n
mi
Hp = 182
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12473974
58 X = -3812722
46
Y = 9860231
80 feet Y = 2962822
74 meter
Z = -15310432
73 Z = -4685115
59
XDOT = -6753
178370 XDOT = -1967
892481
YDOT = -22584
523862 feet/sec YDOT = -6906
274523 meter/sec
ZDOT = -9014
994859 ZDOT = -2757
550912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12742184
30 X = 3883817
77
Y = 9395840
72 feet Y = 2863852
25 meter
Z = -15381432
96 Z = -4688260
77
XDOT = -19379
393929 XDOT = -5906
839270
YDOT = 11415
386596 feet/sec YDOT = 3479
409835 meter/sec
ZDOT = -9053
282767 ZDOT = -2759
440587
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 08189
52067132
00020000 00000-0 20000-3 0 9102
2 25544 51
6390 271
8100 0009275 340
3408 19
7397 15
74999291 31736
Satellite: ISS
Catalog Number: 25544
Epoch time: 08189
52067132 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 271
8100 deg
Eccentricity:
0009275
Arg of perigee: 340
3408 deg
Mean anomaly: 19
7397 deg
Mean motion: 15
74999291 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3173
Checksum: 300
Coasting Arc #12 (Orbit 3188)
---------------------------------------
Vector Time (GMT): 2008/190/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2080644
69 A = 6727334
78 meter
Y = 6055157
77 meter E =
0011568
Z = 2063707
34 I = 51
32664
XDOT = -4197
993080 Wp = 69
05522
YDOT = 3334
955610 meter/sec RA = 265
98681 deg
ZDOT = -5523
697051 TA = 87
80706
MA = 87
67461
Ha = 190
082 n
mi
Hp = 182
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6826262
10 X = 2002755
30
Y = 19866003
17 feet Y = 6077988
99 meter
Z = 6770693
37 Z = 2073626
50
XDOT = -13772
943176 XDOT = -4208
140239
YDOT = 10941
455412 feet/sec YDOT = 3287
955129 meter/sec
ZDOT = -18122
365653 ZDOT = -5544
114964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17213039
19 X = 5246534
34
Y = -12018356
23 feet Y = -3663194
98 meter
Z = 6809450
81 Z = 2075520
61
XDOT = 13419
442809 XDOT = 4090
246168
YDOT = 8853
794455 feet/sec YDOT = 2698
636550 meter/sec
ZDOT = -18200
741277 ZDOT = -5547
585941
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 08190
53584295
00020000 00000-0 20000-3 0 9110
2 25544 51
6388 266
5884 0009399 345
3707 14
7183 15
75044616 31895
Satellite: ISS
Catalog Number: 25544
Epoch time: 08190
53584295 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 266
5884 deg
Eccentricity:
0009399
Arg of perigee: 345
3707 deg
Mean anomaly: 14
7183 deg
Mean motion: 15
75044616 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3189
Checksum: 327
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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