Date:
June 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10548 63 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 2952)
---------------------------------------
Vector Time (GMT): 2008/175/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6521478
80 A = 6729244
90 meter
Y = -734564
97 meter E =
0009608
Z = 1458505
08 I = 51
56015
XDOT = -732
231806 Wp = 23
60314
YDOT = 5019
686971 meter/sec RA = 343
41340 deg
ZDOT = 5797
725143 TA = 352
47692
MA = 352
49133
Ha = 187
661 n
mi
Hp = 186
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21395927
83 X = 6522123
05
Y = -2409990
07 feet Y = -661634
68 meter
Z = 4785121
65 Z = 1490187
58
XDOT = -2402
335322 XDOT = -816
472348
YDOT = 16468
789276 feet/sec YDOT = 5011
026842 meter/sec
ZDOT = 19021
407948 ZDOT = 5793
964137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2885060
57 X = -879366
46
Y = -21309346
46 feet Y = -6495088
80 meter
Z = 4907071
24 Z = 1495675
31
XDOT = 14966
795910 XDOT = 4561
879393
YDOT = 2353
905999 feet/sec YDOT = 717
470549 meter/sec
ZDOT = 19007
315383 ZDOT = 5793
429729
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 08175
56055979
00020000 00000-0 20000-3 0 9006
2 25544 51
6367 343
5889 0008741 284
2843 75
7349 15
74691371 29539
Satellite: ISS
Catalog Number: 25544
Epoch time: 08175
56055979 = yrday
fracday
Element set: 900
Inclination: 51
6367 deg
RA of node: 343
5889 deg
Eccentricity:
0008741
Arg of perigee: 284
2843 deg
Mean anomaly: 75
7349 deg
Mean motion: 15
74691371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2953
Checksum: 337
Coasting Arc #2 (Orbit 2967)
---------------------------------------
Vector Time (GMT): 2008/176/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 546258
35 A = 6719363
39 meter
Y = -4482911
39 meter E =
0004407
Z = -4979362
79 I = 51
49989
XDOT = 7340
743166 Wp = 98
09250
YDOT = -1264
986935 meter/sec RA = 338
23491 deg
ZDOT = 1945
031380 TA = 190
73660
MA = 190
74601
Ha = 187
853 n
mi
Hp = 185
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1792186
19 X = 620535
05
Y = -14707714
54 feet Y = -4476386
85 meter
Z = -16336492
08 Z = -4976529
27
XDOT = 24083
803038 XDOT = 7344
894325
YDOT = -4150
219603 feet/sec YDOT = -1182
875589 meter/sec
ZDOT = 6381
336549 ZDOT = 1980
702386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14770728
53 X = -4502118
06
Y = -1303553
69 feet Y = -397323
17 meter
Z = -16325933
31 Z = -4976144
47
XDOT = -5190
796967 XDOT = -1582
154915
YDOT = -22787
448465 feet/sec YDOT = -6945
614292 meter/sec
ZDOT = 6518
602211 ZDOT = 1986
869954
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 08176
51247762
00020000 00000-0 20000-3 0 9016
2 25544 51
6374 338
6952 0008629 288
0012 72
0211 15
74715628 29684
Satellite: ISS
Catalog Number: 25544
Epoch time: 08176
51247762 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 338
6952 deg
Eccentricity:
0008629
Arg of perigee: 288
0012 deg
Mean anomaly: 72
0211 deg
Mean motion: 15
74715628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2968
Checksum: 302
Coasting Arc #3 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2008/177/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6274157
14 A = 6728285
62 meter
Y = 1444727
49 meter E =
0004116
Z = -1946715
11 I = 51
50386
XDOT = 528
133149 Wp = 243
37158
YDOT = -5259
427729 meter/sec RA = 333
11805 deg
ZDOT = -5598
077777 TA = 318
33155
MA = 318
36290
Ha = 188
073 n
mi
Hp = 185
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20584505
05 X = -6280389
24
Y = 4739919
59 feet Y = 1374531
67 meter
Z = -6386860
59 Z = -1977209
84
XDOT = 1732
720305 XDOT = 614
100024
YDOT = -17255
340318 feet/sec YDOT = -5253
040480 meter/sec
ZDOT = -18366
396905 ZDOT = -5595
303953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5896052
26 X = 1797116
73
Y = 20246306
73 feet Y = 6171074
29 meter
Z = -6504176
04 Z = -1982472
86
XDOT = -15855
414904 XDOT = -4832
730463
YDOT = -1287
131652 feet/sec YDOT = -392
317727 meter/sec
ZDOT = -18356
132641 ZDOT = -5594
949229
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 08177
52783973
00020000 00000-0 20000-3 0 9028
2 25544 51
6373 333
4748 0008727 293
2309 66
7935 15
74766897 29840
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
52783973 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 333
4748 deg
Eccentricity:
0008727
Arg of perigee: 293
2309 deg
Mean anomaly: 66
7935 deg
Mean motion: 15
74766897 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2984
Checksum: 350
Coasting Arc #4 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2008/178/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -362570
54 A = 6720189
81 meter
Y = 4718211
08 meter E =
0007530
Z = 4775710
21 I = 51
45020
XDOT = -6990
940709 Wp = 349
26943
YDOT = 2015
471554 meter/sec RA = 327
92694 deg
ZDOT = -2515
306193 TA = 125
46089
MA = 125
39058
Ha = 188
261 n
mi
Hp = 185
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1189535
89 X = -438502
96
Y = 15479695
13 feet Y = 4713731
45 meter
Z = 15668340
60 Z = 4773764
99
XDOT = -22936
157181 XDOT = -7000
739522
YDOT = 6612
439480 feet/sec YDOT = 1937
240374 meter/sec
ZDOT = -8252
316905 ZDOT = -2549
291805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15531940
67 X = 4734135
52
Y = 132939
24 feet Y = 40519
88 meter
Z = 15661226
02 Z = 4773541
69
XDOT = 8293
311810 XDOT = 2527
801440
YDOT = 21205
677106 feet/sec YDOT = 6463
490382 meter/sec
ZDOT = -8383
026724 ZDOT = -2555
146545
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 08178
54318773
00020000 00000-0 20000-3 0 9034
2 25544 51
6371 328
2541 0008610 296
1934 63
8344 15
74730560 30008
Satellite: ISS
Catalog Number: 25544
Epoch time: 08178
54318773 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 328
2541 deg
Eccentricity:
0008610
Arg of perigee: 296
1934 deg
Mean anomaly: 63
8344 deg
Mean motion: 15
74730560 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3000
Checksum: 284
Coasting Arc #5 (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 = 5917125
57 A = 6727183
55 meter
Y = -2042922
94 meter E =
0009745
Z = 2445800
50 I = 51
45171
XDOT = -288
519372 Wp = 36
41777
YDOT = 5553
221326 meter/sec RA = 322
81343 deg
ZDOT = 5333
384553 TA = 351
31328
MA = 351
33013
Ha = 188
214 n
mi
Hp = 185
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19413141
63 X = 5927648
75
Y = -6702503
08 feet Y = -1976695
75 meter
Z = 8024279
85 Z = 2474571
36
XDOT = -946
585866 XDOT = -376
503703
YDOT = 18219
230072 feet/sec YDOT = 5549
502258 meter/sec
ZDOT = 17497
980816 ZDOT = 5331
769965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8436048
83 X = -2571307
68
Y = -18677234
14 feet Y = -5692820
97 meter
Z = 8134905
50 Z = 2479519
20
XDOT = 16877
011294 XDOT = 5144
113043
YDOT =
219941 feet/sec YDOT =
067038 meter/sec
ZDOT = 17492
206011 ZDOT = 5331
624392
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
55851565
00020000 00000-0 20000-3 0 9048
2 25544 51
6381 323
0334 0008713 299
7298 60
2998 15
74816672 30160
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
55851565 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 323
0334 deg
Eccentricity:
0008713
Arg of perigee: 299
7298 deg
Mean anomaly: 60
2998 deg
Mean motion: 15
74816672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3016
Checksum: 320
Coasting Arc #6 (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 = 117221
44 A = 6721013
87 meter
Y = -4981464
90 meter E =
0002553
Z = -4511405
40 I = 51
40845
XDOT = 6543
194722 Wp = 55
12136
YDOT = -2638
093626 meter/sec RA = 317
61283 deg
ZDOT = 3085
650328 TA = 245
70804
MA = 245
73471
Ha = 188
530 n
mi
Hp = 184
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 384584
79 X = 194832
04
Y = -16343388
79 feet Y = -4979719
40 meter
Z = -14801198
83 Z = -4510648
22
XDOT = 21467
174284 XDOT = 6557
218336
YDOT = -8655
162814 feet/sec YDOT = -2564
845959 meter/sec
ZDOT = 10123
524697 ZDOT = 3117
471090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16298441
61 X = -4967765
00
Y = 1299868
30 feet Y = 396199
86 meter
Z = -14798678
75 Z = -4510637
28
XDOT = -10823
165288 XDOT = -3298
900780
YDOT = -19159
915278 feet/sec YDOT = -5839
942177 meter/sec
ZDOT = 10245
848692 ZDOT = 3122
934681
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
51037340
00020000 00000-0 20000-3 0 9054
2 25544 51
6384 318
1399 0008771 304
2274 55
8058 15
74809168 30315
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
51037340 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 318
1399 deg
Eccentricity:
0008771
Arg of perigee: 304
2274 deg
Mean anomaly: 55
8058 deg
Mean motion: 15
74809168 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3031
Checksum: 291
Coasting Arc #7 (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 = -5497934
01 A = 6725927
02 meter
Y = 2518559
67 meter E =
0004696
Z = -2946669
94 I = 51
40477
XDOT = -14
605967 Wp = 325
05719
YDOT = -5868
215752 meter/sec RA = 312
50097 deg
ZDOT = -4980
686369 TA = 249
02977
MA = 249
08003
Ha = 188
709 n
mi
Hp = 184
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18037841
24 X = -5511373
81
Y = 8262991
05 feet Y = 2457004
04 meter
Z = -9667552
31 Z = -2973411
31
XDOT = -47
919838 XDOT = 75
209916
YDOT = -19252
676351 feet/sec YDOT = -5867
875949 meter/sec
ZDOT = -16340
834545 ZDOT = -4980
540279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10448428
34 X = 3184680
96
Y = 16806941
71 feet Y = 5122755
83 meter
Z = -9770330
63 Z = -2977996
78
XDOT = -17881
490633 XDOT = -5450
278345
YDOT = 1602
589832 feet/sec YDOT = 488
469381 meter/sec
ZDOT = -16340
735703 ZDOT = -4980
656242
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
52567130
00020000 00000-0 20000-3 0 9062
2 25544 51
6385 312
9185 0008807 308
4501 51
5872 15
74841423 30474
Satellite: ISS
Catalog Number: 25544
Epoch time: 08181
52567130 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 312
9185 deg
Eccentricity:
0008807
Arg of perigee: 308
4501 deg
Mean anomaly: 51
5872 deg
Mean motion: 15
74841423 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3047
Checksum: 288
Coasting Arc #8 (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 = 166438
00 A = 6722242
06 meter
Y = 5275408
13 meter E =
0009310
Z = 4165800
86 I = 51
37386
XDOT = -6027
728451 Wp = 21
62360
YDOT = 3088
729745 meter/sec RA = 307
29153 deg
ZDOT = -3659
490303 TA = 105
90645
MA = 105
80383
Ha = 188
895 n
mi
Hp = 184
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 546056
42 X = 87198
37
Y = 17307769
45 feet Y = 5276825
37 meter
Z = 13667325
66 Z = 4166418
10
XDOT = -19776
011979 XDOT = -6044
041885
YDOT = 10133
627773 feet/sec YDOT = 3021
233821 meter/sec
ZDOT = -12006
201783 ZDOT = -3688
812125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17065418
54 X = 5201539
57
Y = -2924415
75 feet Y = -891361
92 meter
Z = 13670118
30 Z = 4166652
06
XDOT = 12619
602713 XDOT = 3846
454907
YDOT = 16821
575319 feet/sec YDOT = 5127
216157 meter/sec
ZDOT = -12118
879559 ZDOT = -3693
834490
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
54095384
00020000 00000-0 20000-3 0 9073
2 25544 51
6390 307
6978 0008744 312
6264 47
4162 15
74839213 30632
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
54095384 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 307
6978 deg
Eccentricity:
0008744
Arg of perigee: 312
6264 deg
Mean anomaly: 47
4162 deg
Mean motion: 15
74839213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3063
Checksum: 307
Coasting Arc #9 (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 = 5029019
49 A = 6724318
42 meter
Y = -2836351
29 meter E =
0008693
Z = 3435433
03 I = 51
36617
XDOT = 391
385607 Wp = 45
45264
YDOT = 6206
602580 meter/sec RA = 302
18088 deg
ZDOT = 4550
297284 TA = 355
43648
MA = 355
44440
Ha = 188
844 n
mi
Hp = 183
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16499407
77 X = 5043673
55
Y = -9305614
46 feet Y = -2780032
79 meter
Z = 11271105
74 Z = 3459898
92
XDOT = 1284
073513 XDOT = 299
848803
YDOT = 20362
869357 feet/sec YDOT = 6210
466391 meter/sec
ZDOT = 14928
796862 ZDOT = 4551
977762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11803302
15 X = -3597646
50
Y = -14743780
59 feet Y = -4493904
32 meter
Z = 11365110
37 Z = 3464085
64
XDOT = 18837
258138 XDOT = 5741
596280
YDOT = -3564
675352 feet/sec YDOT = -1086
513047 meter/sec
ZDOT = 14935
758803 ZDOT = 4552
419283
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
55621690
00020000 00000-0 20000-3 0 9081
2 25544 51
6401 302
4767 0008881 316
3844 43
6617 15
74925853 30797
Satellite: ISS
Catalog Number: 25544
Epoch time: 08183
55621690 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 302
4767 deg
Eccentricity:
0008881
Arg of perigee: 316
3844 deg
Mean anomaly: 43
6617 deg
Mean motion: 15
74925853 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3079
Checksum: 310
Coasting Arc #10 (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 = -547251
00 A = 6723461
28 meter
Y = -5547054
18 meter E =
0005595
Z = -3755139
42 I = 51
34846
XDOT = 5495
063315 Wp = 1
23393
YDOT = -3384
664464 meter/sec RA = 296
96715 deg
ZDOT = 4204
606893 TA = 313
08710
MA = 313
13391
Ha = 189
199 n
mi
Hp = 183
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1795442
90 X = -466940
65
Y = -18198996
67 feet Y = -5552723
92 meter
Z = -12320011
21 Z = -3757604
19
XDOT = 18028
422948 XDOT = 5512
077716
YDOT = -11104
542204 feet/sec YDOT = -3323
121389 meter/sec
ZDOT = 13794
642037 ZDOT = 4231
342219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17610573
24 X = -5367702
72
Y = 4904069
59 feet Y = 1494760
41 meter
Z = -12329946
59 Z = -3758167
72
XDOT = -13735
146105 XDOT = -4186
472533
YDOT = -14428
387230 feet/sec YDOT = -4397
772428 meter/sec
ZDOT = 13897
351638 ZDOT = 4235
912779
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
50801472
00020000 00000-0 20000-3 0 9096
2 25544 51
6401 297
5832 0009085 320
6407 39
4096 15
74899517 30942
Satellite: ISS
Catalog Number: 25544
Epoch time: 08184
50801472 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 297
5832 deg
Eccentricity:
0009085
Arg of perigee: 320
6407 deg
Mean anomaly: 39
4096 deg
Mean motion: 15
74899517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3094
Checksum: 310
Coasting Arc #11 (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 = -4574250
59 A = 6722826
19 meter
Y = 3020374
77 meter E =
0009419
Z = -3900608
68 I = 51
33483
XDOT = -858
295421 Wp = 7
51152
YDOT = -6503
663346 meter/sec RA = 291
85559 deg
ZDOT = -4021
371299 TA = 220
43731
MA = 220
50735
Ha = 189
330 n
mi
Hp = 183
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15007383
82 X = -4588736
77
Y = 9909366
03 feet Y = 2969142
75 meter
Z = -12797272
57 Z = -3922864
57
XDOT = -2815
929859 XDOT = -765
971840
YDOT = -21337
478169 feet/sec YDOT = -6512
744192 meter/sec
ZDOT = -13193
475391 ZDOT = -4025
318037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12606114
84 X = 3842343
80
Y = 12740000
26 feet Y = 3883152
08 meter
Z = -12882761
80 Z = -3926665
80
XDOT = -19477
979564 XDOT = -5936
888171
YDOT = 5889
322333 feet/sec YDOT = 1795
065447 meter/sec
ZDOT = -13209
204797 ZDOT = -4026
165622
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
52324901
00020000 00000-0 20000-3 0 9108
2 25544 51
6404 292
3625 0009006 324
6081 35
4484 15
74931970 31109
Satellite: ISS
Catalog Number: 25544
Epoch time: 08185
52324901 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 292
3625 deg
Eccentricity:
0009006
Arg of perigee: 324
6081 deg
Mean anomaly: 35
4484 deg
Mean motion: 15
74931970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3110
Checksum: 269
Coasting Arc #12 (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 = 976573
97 A = 6724877
90 meter
Y = 5807711
33 meter E =
0010967
Z = 3247484
64 I = 51
33174
XDOT = -4983
702332 Wp = 48
62390
YDOT = 3486
642567 meter/sec RA = 286
64016 deg
ZDOT = -4719
272101 TA = 93
17250
MA = 93
04702
Ha = 189
511 n
mi
Hp = 183
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3203982
84 X = 895783
25
Y = 19054171
02 feet Y = 5818179
57 meter
Z = 10654477
18 Z = 3252033
65
XDOT = -16350
729435 XDOT = -4999
395197
YDOT = 11439
116032 feet/sec YDOT = 3430
825133 meter/sec
ZDOT = -15483
176183 ZDOT = -4743
519900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17969911
04 X = 5477228
88
Y = -7072853
42 feet Y = -2155805
72 meter
Z = 10672481
67 Z = 3252972
41
XDOT = 14082
052765 XDOT = 4292
209683
YDOT = 12188
173144 feet/sec YDOT = 3714
955174 meter/sec
ZDOT = -15576
302597 ZDOT = -4747
657032
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
53846776
00020000 00000-0 20000-3 0 9110
2 25544 51
6400 287
1421 0008991 329
5935 30
4707 15
74949532 31268
Satellite: ISS
Catalog Number: 25544
Epoch time: 08186
53846776 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 287
1421 deg
Eccentricity:
0008991
Arg of perigee: 329
5935 deg
Mean anomaly: 30
4707 deg
Mean motion: 15
74949532 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3126
Checksum: 310
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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