Date:
June 16th 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 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
171/06:52:31
170 9
6 11
4 11
4
N/A -3
1 0
1 186
8
000/00:19:02
341 -5
2 0
2 186
3
Coasting Arc #1 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2008/165/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -647600
36 A = 6714771
97 meter
Y = -4856190
94 meter E =
0010671
Z = -4601472
61 I = 51
81512
XDOT = 6840
246055 Wp = 35
75483
YDOT = 1906
918667 meter/sec RA = 34
78313 deg
ZDOT = -2970
116898 TA = 204
81868
MA = 204
87005
Ha = 185
644 n
mi
Hp = 180
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2124673
09 X = -570896
20
Y = -15932384
99 feet Y = -4863003
24 meter
Z = -15096694
92 Z = -4604433
07
XDOT = 22441
752149 XDOT = 6832
842630
YDOT = 6256
294838 feet/sec YDOT = 1983
369248 meter/sec
ZDOT = -9744
478012 ZDOT = -2936
904373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15967443
57 X = -4866876
80
Y = 1743509
63 feet Y = 531421
73 meter
Z = -15108482
54 Z = -4605065
48
XDOT = 6798
509416 XDOT = 2072
185670
YDOT = -21212
963183 feet/sec YDOT = -6465
711178 meter/sec
ZDOT = -9616
461982 ZDOT = -2931
097612
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 08165
54180422
00020000 00000-0 20000-3 0 9005
2 25544 51
6398 35
1898 0006215 324
0244 36
0501 15
76874514 27957
Satellite: ISS
Catalog Number: 25544
Epoch time: 08165
54180422 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 35
1898 deg
Eccentricity:
0006215
Arg of perigee: 324
0244 deg
Mean anomaly: 36
0501 deg
Mean motion: 15
76874514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2795
Checksum: 284
Coasting Arc #2 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2008/166/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6192514
04 A = 6722725
65 meter
Y = -1985783
13 meter E =
0009513
Z = 1693955
91 I = 51
81768
XDOT = 73
829778 Wp = 95
26065
YDOT = -5143
812627 meter/sec RA = 29
60047 deg
ZDOT = -5733
514797 TA = 66
03511
MA = 65
93553
Ha = 185
776 n
mi
Hp = 180
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20316647
12 X = -6178077
48
Y = -6515036
53 feet Y = -2054950
93 meter
Z = 5557598
12 Z = 1663907
09
XDOT = 242
223682 XDOT = 159
195889
YDOT = -16876
025678 feet/sec YDOT = -5142
508776 meter/sec
ZDOT = -18810
744085 ZDOT = -5732
949613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6541432
59 X = -1993828
65
Y = 20339510
38 feet Y = 6199482
76 meter
Z = 5441757
55 Z = 1658647
70
XDOT = -15392
469975 XDOT = -4691
624848
YDOT = 105
669749 feet/sec YDOT = 32
208140 meter/sec
ZDOT = -18808
974874 ZDOT = -5732
975542
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 08166
55577769
00020000 00000-0 20000-3 0 9012
2 25544 51
6402 29
9604 0006195 328
8821 31
1976 15
76904998 28110
Satellite: ISS
Catalog Number: 25544
Epoch time: 08166
55577769 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 29
9604 deg
Eccentricity:
0006195
Arg of perigee: 328
8821 deg
Mean anomaly: 31
1976 deg
Mean motion: 15
76904998 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2811
Checksum: 324
Coasting Arc #3 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2008/167/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -847896
92 A = 6712076
42 meter
Y = 4133951
16 meter E =
0003870
Z = 5219170
34 I = 51
75476
XDOT = -7222
212933 Wp = 358
09052
YDOT = -2550
727346 meter/sec RA = 24
47530 deg
ZDOT = 850
862008 TA = 83
85005
MA = 83
80595
Ha = 185
951 n
mi
Hp = 180
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2781814
03 X = -919414
44
Y = 13562831
90 feet Y = 4124068
66 meter
Z = 17123262
28 Z = 5214878
26
XDOT = -23694
924322 XDOT = -7197
286901
YDOT = -8368
528039 feet/sec YDOT = -2631
351053 meter/sec
ZDOT = 2791
542020 ZDOT = 815
836204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13606994
89 X = 4147412
04
Y = 2663307
38 feet Y = 811776
09 meter
Z = 17107059
75 Z = 5214231
81
XDOT = -7796
184762 XDOT = -2376
277115
YDOT = 22848
294955 feet/sec YDOT = 6964
160302 meter/sec
ZDOT = 2656
497045 ZDOT = 809
700299
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 08167
56973861
00020000 00000-0 20000-3 0 9028
2 25544 51
6394 24
7299 0006194 332
2799 27
8034 15
76893864 28278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08167
56973861 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 24
7299 deg
Eccentricity:
0006194
Arg of perigee: 332
2799 deg
Mean anomaly: 27
8034 deg
Mean motion: 15
76893864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2827
Checksum: 338
Coasting Arc #4 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2008/168/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6267704
04 A = 6723823
05 meter
Y = 2395325
32 meter E =
0015817
Z = 236987
27 I = 51
76635
XDOT = -1908
582481 Wp = 25
20925
YDOT = 4382
322461 meter/sec RA = 19
32074 deg
ZDOT = 6050
437222 TA = 337
36629
MA = 337
43597
Ha = 185
970 n
mi
Hp = 179
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20563333
48 X = 6239302
06
Y = 7858678
88 feet Y = 2465255
53 meter
Z = 777517
30 Z = 267367
54
XDOT = -6261
753546 XDOT = -1986
836628
YDOT = 14377
698362 feet/sec YDOT = 4360
540849 meter/sec
ZDOT = 19850
515821 ZDOT = 6040
976041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7173899
53 X = 2186604
58
Y = -20807421
49 feet Y = -6342102
07 meter
Z = 894665
96 Z = 272694
18
XDOT = 13063
628290 XDOT = 3981
793903
YDOT = 5372
272664 feet/sec YDOT = 1637
468708 meter/sec
ZDOT = 19814
426113 ZDOT = 6039
437079
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 08168
58368556
00020000 00000-0 20000-3 0 9031
2 25544 51
6383 19
4991 0006274 335
2252 24
8611 15
76933677 28435
Satellite: ISS
Catalog Number: 25544
Epoch time: 08168
58368556 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 19
4991 deg
Eccentricity:
0006274
Arg of perigee: 335
2252 deg
Mean anomaly: 24
8611 deg
Mean motion: 15
76933677 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2843
Checksum: 318
Coasting Arc #5 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2008/169/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2499617
66 A = 6712357
76 meter
Y = -3547894
40 meter E =
0011934
Z = -5129733
28 I = 51
69865
XDOT = 6989
512464 Wp = 74
37086
YDOT = 2905
002668 meter/sec RA = 14
15395 deg
ZDOT = 1402
498758 TA = 209
02017
MA = 209
08657
Ha = 186
048 n
mi
Hp = 179
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8200845
33 X = 2564024
44
Y = -11640073
48 feet Y = -3519581
04 meter
Z = -16829833
59 Z = -5117434
37
XDOT = 22931
471338 XDOT = 6949
695667
YDOT = 9530
848648 feet/sec YDOT = 2982
940473 meter/sec
ZDOT = 4601
373877 ZDOT = 1436
357900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12042649
09 X = -3670599
44
Y = -7700804
08 feet Y = -2347205
08 meter
Z = -16782749
87 Z = -5115382
16
XDOT = 7805
459550 XDOT = 2379
104071
YDOT = -22477
002498 feet/sec YDOT = -6850
990361 meter/sec
ZDOT = 4731
958024 ZDOT = 1442
300806
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 08169
53425008
00020000 00000-0 20000-3 0 9044
2 25544 51
6372 14
5950 0006207 339
0569 21
0340 15
76961044 28586
Satellite: ISS
Catalog Number: 25544
Epoch time: 08169
53425008 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 14
5950 deg
Eccentricity:
0006207
Arg of perigee: 339
0569 deg
Mean anomaly: 21
0340 deg
Mean motion: 15
76961044 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2858
Checksum: 282
Coasting Arc #6 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2008/170/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5776502
39 A = 6721578
34 meter
Y = -2661191
99 meter E =
0002739
Z = -2179663
19 I = 51
70122
XDOT = 3822
310726 Wp = 55
29147
YDOT = -3792
565173 meter/sec RA = 9
03243 deg
ZDOT = -5502
741630 TA = 149
10871
MA = 149
09260
Ha = 186
150 n
mi
Hp = 179
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18951779
49 X = -5735726
77
Y = -8730944
84 feet Y = -2725559
68 meter
Z = -7151125
97 Z = -2207627
03
XDOT = 12540
389521 XDOT = 3891
167062
YDOT = -12442
799125 feet/sec YDOT = -3749
435711 meter/sec
ZDOT = -18053
614272 ZDOT = -5484
006389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7435406
97 X = -2266312
05
Y = 19456608
90 feet Y = 5930374
39 meter
Z = -7258997
16 Z = -2212542
33
XDOT = -11848
644482 XDOT = -3611
466838
YDOT = -11232
722795 feet/sec YDOT = -3423
733908 meter/sec
ZDOT = -17981
762956 ZDOT = -5480
841349
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 08170
54817326
00020000 00000-0 20000-3 0 9056
2 25544 51
6371 9
3653 0006310 342
8862 17
2089 15
76978047 28746
Satellite: ISS
Catalog Number: 25544
Epoch time: 08170
54817326 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 9
3653 deg
Eccentricity:
0006310
Arg of perigee: 342
8862 deg
Mean anomaly: 17
2089 deg
Mean motion: 15
76978047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2874
Checksum: 304
Coasting Arc #7 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2008/171/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 531205
48 A = 6718599
47 meter
Y = -4139291
60 meter E =
0005750
Z = -5270248
14 I = 51
64821
XDOT = 7655
661204 Wp = 88
32135
YDOT = 792
713655 meter/sec RA = 5
03202 deg
ZDOT = 149
340873 TA = 183
09439
MA = 183
09795
Ha = 186
827 n
mi
Hp = 186
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1742800
14 X = 603054
07
Y = -13580353
02 feet Y = -4132948
48 meter
Z = -17290840
34 Z = -5267493
93
XDOT = 25116
998701 XDOT = 7645
502499
YDOT = 2600
766584 feet/sec YDOT = 878
266808 meter/sec
ZDOT = 489
963493 ZDOT = 186
507513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1174758
68 X = -358066
45
Y = -13654271
84 feet Y = -4161822
06 meter
Z = -17280546
94 Z = -5267110
71
XDOT = 24078
627605 XDOT = 7339
165694
YDOT = -2871
640388 feet/sec YDOT = -875
275990 meter/sec
ZDOT = 633
132833 ZDOT = 192
978888
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 08171
30862780
00020000 00000-0 20000-3 0 9066
2 25544 51
6403 5
4450 0009304 273
2494 86
7605 15
74529680 28869
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
30862780 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 5
4450 deg
Eccentricity:
0009304
Arg of perigee: 273
2494 deg
Mean anomaly: 86
7605 deg
Mean motion: 15
74529680 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2886
Checksum: 297
Coasting Arc #8 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2008/172/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6713287
24 A = 6730670
99 meter
Y = -244996
84 meter E =
0007603
Z = -324838
21 I = 51
65968
XDOT = 466
602490 Wp = 191
67768
YDOT = -4769
123219 meter/sec RA = 359
89829 deg
ZDOT = -6028
970432 TA = 351
85276
MA = 351
86510
Ha = 187
409 n
mi
Hp = 186
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22025220
61 X = -6708470
71
Y = -803795
40 feet Y = -320041
66 meter
Z = -1065742
16 Z = -357439
53
XDOT = 1530
848063 XDOT = 549
184374
YDOT = -15646
729722 feet/sec YDOT = -4763
442384 meter/sec
ZDOT = -19780
086719 ZDOT = -6026
504112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21588524
59 X = -6580182
29
Y = 4405525
34 feet Y = 1342804
12 meter
Z = -1191297
08 Z = -363107
35
XDOT = -1767
138854 XDOT = -538
623923
YDOT = -14019
444880 feet/sec YDOT = -4273
126799 meter/sec
ZDOT = -19770
949656 ZDOT = -6026
185455
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 08172
32412140
00020000 00000-0 20000-3 0 9071
2 25544 51
6405
2256 0009370 276
6913 83
3184 15
74509871 29028
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
32412140 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node:
2256 deg
Eccentricity:
0009370
Arg of perigee: 276
6913 deg
Mean anomaly: 83
3184 deg
Mean motion: 15
74509871 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2902
Checksum: 271
Coasting Arc #9 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2008/173/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -289640
47 A = 6718567
34 meter
Y = 4200195
78 meter E =
0007400
Z = 5241825
16 I = 51
59035
XDOT = -7670
195099 Wp = 294
90290
YDOT = 225
544672 meter/sec RA = 354
74862 deg
ZDOT = -602
147934 TA = 160
84076
MA = 160
81291
Ha = 187
742 n
mi
Hp = 186
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -950264
00 X = -362049
81
Y = 13780169
87 feet Y = 4196550
95 meter
Z = 17197589
12 Z = 5240243
05
XDOT = -25164
682084 XDOT = -7669
222011
YDOT = 739
975958 feet/sec YDOT = 139
777719 meter/sec
ZDOT = -1975
550965 ZDOT = -639
407018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2461533
47 X = 750275
40
Y = 13599098
20 feet Y = 4145005
13 meter
Z = 17191815
96 Z = 5240065
51
XDOT = -23161
362426 XDOT = -7059
583268
YDOT = 6881
153650 feet/sec YDOT = 2097
375633 meter/sec
ZDOT = -2119
010776 ZDOT = -645
874485
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 08173
33960208
00020000 00000-0 20000-3 0 9087
2 25544 51
6406 355
0060 0009523 281
5054 78
5040 15
74587604 29188
Satellite: ISS
Catalog Number: 25544
Epoch time: 08173
33960208 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 355
0060 deg
Eccentricity:
0009523
Arg of perigee: 281
5054 deg
Mean anomaly: 78
5040 deg
Mean motion: 15
74587604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2918
Checksum: 287
Coasting Arc #10 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2008/174/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6653433
90 A = 6730322
40 meter
Y = -630291
57 meter E =
0010822
Z = 730618
89 I = 51
60120
XDOT = -196
822150 Wp = 8
25950
YDOT = 4853
954503 meter/sec RA = 349
61789 deg
ZDOT = 5979
406827 TA = 359
71119
MA = 359
71182
Ha = 188
049 n
mi
Hp = 186
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21828851
37 X = 6656438
24
Y = -2067885
74 feet Y = -555872
40 meter
Z = 2397043
59 Z = 762948
13
XDOT = -645
741961 XDOT = -280
131785
YDOT = 15925
047582 feet/sec YDOT = 4851
286652 meter/sec
ZDOT = 19617
476468 ZDOT = 5978
249182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20455714
81 X = 6234901
87
Y = -7856623
61 feet Y = -2394698
87 meter
Z = 2521491
32 Z = 768550
55
XDOT = 2978
835722 XDOT = 907
949128
YDOT = 14050
850956 feet/sec YDOT = 4282
699371 meter/sec
ZDOT = 19613
391110 ZDOT = 5978
161610
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 08174
35507513
00020000 00000-0 20000-3 0 9097
2 25544 51
6410 349
7862 0009517 286
1162 73
8953 15
74564932 29345
Satellite: ISS
Catalog Number: 25544
Epoch time: 08174
35507513 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 349
7862 deg
Eccentricity:
0009517
Arg of perigee: 286
1162 deg
Mean anomaly: 73
8953 deg
Mean motion: 15
74564932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2934
Checksum: 314
Coasting Arc #11 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2008/175/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 48595
17 A = 6718791
93 meter
Y = -4284585
16 meter E =
0005340
Z = -5179449
78 I = 51
53431
XDOT = 7526
968393 Wp = 77
78800
YDOT = -1208
982012 meter/sec RA = 344
45627 deg
ZDOT = 1072
762632 TA = 202
45177
MA = 202
47515
Ha = 188
244 n
mi
Hp = 185
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 159432
97 X = 121663
05
Y = -14057037
91 feet Y = -4283632
38 meter
Z = -16992945
47 Z = -5179036
90
XDOT = 24694
778192 XDOT = 7534
716766
YDOT = -3966
476416 feet/sec YDOT = -1124
767983 meter/sec
ZDOT = 3519
562440 ZDOT = 1109
346923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3765901
41 X = -1147846
75
Y = -13545716
87 feet Y = -4128734
50 meter
Z = -16991688
28 Z = -5179066
59
XDOT = 21528
530225 XDOT = 6561
896013
YDOT = -10568
374995 feet/sec YDOT = -3221
240699 meter/sec
ZDOT = 3660
351672 ZDOT = 1115
675190
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
30706971
00020000 00000-0 20000-3 0 9104
2 25544 51
6412 344
8930 0009589 289
7800 70
2329 15
74601649 29497
Satellite: ISS
Catalog Number: 25544
Epoch time: 08175
30706971 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 344
8930 deg
Eccentricity:
0009589
Arg of perigee: 289
7800 deg
Mean anomaly: 70
2329 deg
Mean motion: 15
74601649 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2949
Checksum: 313
Coasting Arc #12 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2008/176/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6464635
11 A = 6729951
51 meter
Y = 1461748
16 meter E =
0004871
Z = -1151194
10 I = 51
54395
XDOT = -73
395709 Wp = 221
08248
YDOT = -4966
065440 meter/sec RA = 339
33004 deg
ZDOT = -5883
147110 TA = 331
54030
MA = 331
56689
Ha = 188
500 n
mi
Hp = 185
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21209432
77 X = -6474907
89
Y = 4795761
68 feet Y = 1389399
62 meter
Z = -3776883
54 Z = -1182623
82
XDOT = -240
799569 XDOT = 10
720122
YDOT = -16292
865616 feet/sec YDOT = -4966
415069 meter/sec
ZDOT = -19301
663748 ZDOT = -5883
300030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18752007
79 X = -5715611
97
Y = 10966930
51 feet Y = 3342720
42 meter
Z = -3897801
51 Z = -1188049
90
XDOT = -4242
453884 XDOT = -1293
099944
YDOT = -14126
262563 feet/sec YDOT = -4305
684829 meter/sec
ZDOT = -19302
642588 ZDOT = -5883
445461
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
32252157
00020000 00000-0 20000-3 0 9110
2 25544 51
6413 339
6740 0009634 292
8115 67
2030 15
74566443 29659
Satellite: ISS
Catalog Number: 25544
Epoch time: 08176
32252157 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 339
6740 deg
Eccentricity:
0009634
Arg of perigee: 292
8115 deg
Mean anomaly: 67
2030 deg
Mean motion: 15
74566443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2965
Checksum: 291
Coasting Arc #13 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2008/177/07:02:02
341
Vector Time (MET): N/A
Weight (LBS) : 661039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 182904
51 A = 6719109
34 meter
Y = 4402681
24 meter E =
0008758
Z = 5078144
55 I = 51
48112
XDOT = -7232
518120 Wp = 327
74711
YDOT = 2116
241553 meter/sec RA = 334
15586 deg
ZDOT = -1568
204096 TA = 137
38060
MA = 137
31262
Ha = 188
677 n
mi
Hp = 185
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 600080
40 X = 108990
82
Y = 14444492
26 feet Y = 4404312
67 meter
Z = 16660579
23 Z = 5078854
11
XDOT = -23728
733989 XDOT = -7248
026707
YDOT = 6943
049714 feet/sec YDOT = 2035
276874 meter/sec
ZDOT = -5145
026561 ZDOT = -1603
376951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5074710
37 X = 1546771
72
Y = 13533221
60 feet Y = 4124925
94 meter
Z = 16663660
50 Z = 5079083
72
XDOT = -19271
459272 XDOT = -5873
940786
YDOT = 13752
588383 feet/sec YDOT = 4191
788939 meter/sec
ZDOT = -5280
304106 ZDOT = -1609
436692
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
33796017
00020000 00000-0 20000-3 0 9121
2 25544 51
6413 334
4540 0009788 297
8354 62
1817 15
74651117 29818
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
33796017 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 334
4540 deg
Eccentricity:
0009788
Arg of perigee: 297
8354 deg
Mean anomaly: 62
1817 deg
Mean motion: 15
74651117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2981
Checksum: 311
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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