Date:
July 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13723 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 2855)
---------------------------------------
Vector Time (GMT): 2010/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3906144
67 A = 6739025
12 meter
Y = -5229640
10 meter E =
0021784
Z = 1631575
89 I = 51
96936
XDOT = 3049
067042 Wp = 119
29510
YDOT = -4092
261644 meter/sec RA = 64
51720 deg
ZDOT = -5770
131660 TA = 42
77449
MA = 42
60517
Ha = 197
077 n
mi
Hp = 185
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12815435
27 X = -3855301
44
Y = -17157611
89 feet Y = -5273036
87 meter
Z = 5352939
29 Z = 1612722
77
XDOT = 10003
500793 XDOT = 3122
630988
YDOT = -13426
055262 feet/sec YDOT = -4057
753127 meter/sec
ZDOT = -18930
878150 ZDOT = -5755
141165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9656461
64 X = -2943289
51
Y = 19135642
40 feet Y = 5832543
80 meter
Z = 5277586
96 Z = 1608608
50
XDOT = -15128
587201 XDOT = -4611
193379
YDOT = -2386
735670 feet/sec YDOT = -727
477032 meter/sec
ZDOT = -18870
918721 ZDOT = -5751
856026
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 10200
53499775
00016717 00000-0 10270-3 0 9009
2 25544 51
6460 65
0153 0007755 124
4991 235
6904 15
71206104 28565
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
53499775 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 65
0153 deg
Eccentricity:
0007755
Arg of perigee: 124
4991 deg
Mean anomaly: 235
6904 deg
Mean motion: 15
71206104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2856
Checksum: 298
Coasting Arc #2 (Orbit 2871)
---------------------------------------
Vector Time (GMT): 2010/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1547622
82 A = 6730675
38 meter
Y = 4581786
07 meter E =
0015525
Z = 4673691
34 I = 51
92687
XDOT = -5374
048220 Wp = 121
86821
YDOT = -4728
700991 meter/sec RA = 59
46022 deg
ZDOT = 2841
305502 TA = 300
10875
MA = 300
26257
Ha = 196
990 n
mi
Hp = 185
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5077502
68 X = -1621445
99
Y = 15032106
54 feet Y = 4564066
20 meter
Z = 15333633
02 Z = 4665994
36
XDOT = -17631
391798 XDOT = -5334
574086
YDOT = -15514
110862 feet/sec YDOT = -4788
576495 meter/sec
ZDOT = 9321
868445 ZDOT = 2815
293724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15725210
09 X = 4793044
04
Y = -2325275
14 feet Y = -708743
86 meter
Z = 15302824
08 Z = 4664300
78
XDOT = -5810
107524 XDOT = -1770
920773
YDOT = 21693
297298 feet/sec YDOT = 6612
117016 meter/sec
ZDOT = 9217
895154 ZDOT = 2809
614443
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 10201
55262302
00016717 00000-0 10270-3 0 9017
2 25544 51
6455 59
8107 0007602 127
7416 232
4435 15
71212389 28722
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
55262302 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 59
8107 deg
Eccentricity:
0007602
Arg of perigee: 127
7416 deg
Mean anomaly: 232
4435 deg
Mean motion: 15
71212389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2872
Checksum: 283
Coasting Arc #3 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2010/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176592
60 A = 6735502
43 meter
Y = 2849948
83 meter E =
0010952
Z = -3245697
28 I = 51
92631
XDOT = -307
728151 Wp = 113
23643
YDOT = 6003
146808 meter/sec RA = 54
31915 deg
ZDOT = 4788
884844 TA = 209
06237
MA = 209
12338
Ha = 196
763 n
mi
Hp = 185
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16983571
52 X = 5160106
09
Y = 9350225
80 feet Y = 2907744
89 meter
Z = -10648613
11 Z = -3220589
21
XDOT = -1009
606793 XDOT = -398
096898
YDOT = 19695
363543 feet/sec YDOT = 5999
199596 meter/sec
ZDOT = 15711
564448 ZDOT = 4787
171328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 127269
00 X = 38791
59
Y = -19441703
30 feet Y = -5925831
17 meter
Z = -10548239
70 Z = -3215103
46
XDOT = 16436
592555 XDOT = 5009
873411
YDOT = -8397
806181 feet/sec YDOT = -2559
651324 meter/sec
ZDOT = 15704
661014 ZDOT = 4786
780677
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 10202
50663340
00016717 00000-0 10270-3 0 9021
2 25544 51
6447 54
9311 0007466 132
6133 227
5660 15
71262324 28870
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
50663340 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 54
9311 deg
Eccentricity:
0007466
Arg of perigee: 132
6133 deg
Mean anomaly: 227
5660 deg
Mean motion: 15
71262324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 285
Coasting Arc #4 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2010/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1078242
79 A = 6734289
50 meter
Y = -5586869
96 meter E =
0011485
Z = -3607002
37 I = 51
90304
XDOT = 6047
768122 Wp = 112
86725
YDOT = 1689
372810 meter/sec RA = 49
27440 deg
ZDOT = -4440
031425 TA = 110
00317
MA = 109
87947
Ha = 196
674 n
mi
Hp = 185
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3537541
97 X = -998167
32
Y = -18329625
84 feet Y = -5598479
22 meter
Z = -11833997
29 Z = -3612046
79
XDOT = 19841
758931 XDOT = 6049
996358
YDOT = 5542
561711 feet/sec YDOT = 1757
015720 meter/sec
ZDOT = -14567
032233 ZDOT = -4410
646055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14276558
67 X = -4351495
08
Y = 12008027
00 feet Y = 3660046
63 meter
Z = -11854114
83 Z = -3613134
20
XDOT = -4062
891288 XDOT = -1238
369265
YDOT = -19044
640077 feet/sec YDOT = -5804
806295 meter/sec
ZDOT = -14449
541893 ZDOT = -4404
220369
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 10203
52423336
00016717 00000-0 10270-3 0 9034
2 25544 51
6438 49
7268 0007433 136
4507 223
7243 15
71273361 29031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
52423336 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 49
7268 deg
Eccentricity:
0007433
Arg of perigee: 136
4507 deg
Mean anomaly: 223
7243 deg
Mean motion: 15
71273361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2903
Checksum: 289
Coasting Arc #5 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2010/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5059879
86 A = 6731424
31 meter
Y = -68250
72 meter E =
0013589
Z = 4426285
91 I = 51
87330
XDOT = -2819
081898 Wp = 99
83911
YDOT = -6358
508863 meter/sec RA = 44
12742 deg
ZDOT = -3314
366431 TA = 23
34242
MA = 23
28078
Ha = 196
648 n
mi
Hp = 185
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16600655
71 X = -5080242
34
Y = -223919
68 feet Y = -124947
84 meter
Z = 14521935
41 Z = 4401655
96
XDOT = -9248
956358 XDOT = -2731
670053
YDOT = -20861
249552 feet/sec YDOT = -6389
544270 meter/sec
ZDOT = -10873
905614 ZDOT = -3327
849951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8236148
79 X = 2510378
15
Y = 14513742
23 feet Y = 4423788
63 meter
Z = 14423441
27 Z = 4396264
90
XDOT = -12306
484550 XDOT = -3751
016491
YDOT = 17864
019267 feet/sec YDOT = 5444
953073 meter/sec
ZDOT = -10927
759929 ZDOT = -3330
781226
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 10204
54181932
00016717 00000-0 10270-3 0 9041
2 25544 51
6442 44
5218 0007331 140
8207 219
3487 15
71315825 29197
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
54181932 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 44
5218 deg
Eccentricity:
0007331
Arg of perigee: 140
8207 deg
Mean anomaly: 219
3487 deg
Mean motion: 15
71315825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 292
Coasting Arc #6 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2010/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3752823
45 A = 6737802
16 meter
Y = 5178335
32 meter E =
0017563
Z = 2108511
80 I = 51
87128
XDOT = -5132
874595 Wp = 94
01379
YDOT = 1443
634766 meter/sec RA = 39
07052 deg
ZDOT = 5549
586146 TA = 289
44295
MA = 289
63265
Ha = 196
440 n
mi
Hp = 185
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12312412
90 X = 3684396
89
Y = 16989289
09 feet Y = 5219918
74 meter
Z = 6917689
63 Z = 2126577
17
XDOT = -16840
139747 XDOT = -5175
594430
YDOT = 4736
334535 feet/sec YDOT = 1385
996261 meter/sec
ZDOT = 18207
303628 ZDOT = 5524
547583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8132758
98 X = 2478864
94
Y = -19315426
40 feet Y = -5887341
97 meter
Z = 6989879
79 Z = 2130515
36
XDOT = 11449
178780 XDOT = 3489
709692
YDOT = 11421
108241 feet/sec YDOT = 3481
153792 meter/sec
ZDOT = 18107
155792 ZDOT = 5519
061085
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 10205
55939296
00016717 00000-0 10270-3 0 9058
2 25544 51
6428 39
3164 0007448 145
0451 215
1201 15
71337832 29358
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
55939296 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 39
3164 deg
Eccentricity:
0007448
Arg of perigee: 145
0451 deg
Mean anomaly: 215
1201 deg
Mean motion: 15
71337832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 300
Coasting Arc #7 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2010/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3630423
08 A = 6728463
66 meter
Y = -2426164
57 meter E =
0019778
Z = -5136222
08 I = 51
81471
XDOT = 5527
664220 Wp = 117
00661
YDOT = 5124
591597 meter/sec RA = 33
93716 deg
ZDOT = 1482
016714 TA = 167
22644
MA = 167
17626
Ha = 196
420 n
mi
Hp = 186
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11910836
89 X = 3682233
35
Y = -7959857
52 feet Y = -2385276
70 meter
Z = -16851122
31 Z = -5118460
34
XDOT = 18135
381300 XDOT = 5462
750070
YDOT = 16812
964558 feet/sec YDOT = 5186
042105 meter/sec
ZDOT = 4862
259561 ZDOT = 1508
712456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147648
85 X = -4007403
37
Y = -5895463
70 feet Y = -1796937
34 meter
Z = -16780063
40 Z = -5114563
32
XDOT = 4101
317460 XDOT = 1250
081562
YDOT = -23330
902307 feet/sec YDOT = -7111
259023 meter/sec
ZDOT = 4968
966348 ZDOT = 1514
540943
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 10206
51335732
00016717 00000-0 10270-3 0 9061
2 25544 51
6421 34
4356 0007498 147
6282 212
5341 15
71339989 29503
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
51335732 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 34
4356 deg
Eccentricity:
0007498
Arg of perigee: 147
6282 deg
Mean anomaly: 212
5341 deg
Mean motion: 15
71339989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 308
Coasting Arc #8 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2010/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5698422
64 A = 6739511
60 meter
Y = -3551635
90 meter E =
0018328
Z = -459201
69 I = 51
82723
XDOT = 2865
449783 Wp = 143
09763
YDOT = -3835
413368 meter/sec RA = 28
85199 deg
ZDOT = -6031
953187 TA = 41
88126
MA = 41
74119
Ha = 196
176 n
mi
Hp = 186
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18695612
35 X = -5656053
42
Y = -11652348
75 feet Y = -3615122
12 meter
Z = -1506567
22 Z = -486781
43
XDOT = 9401
081964 XDOT = 2937
426556
YDOT = -12583
377193 feet/sec YDOT = -3802
967134 meter/sec
ZDOT = -19789
872661 ZDOT = -6017
858724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 519208
27 X = 158254
68
Y = 22015657
82 feet Y = 6710372
50 meter
Z = -1616827
42 Z = -492809
00
XDOT = -14138
003593 XDOT = -4309
263495
YDOT = -1084
834739 feet/sec YDOT = -330
657629 meter/sec
ZDOT = -19733
465214 ZDOT = -6014
760197
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 10207
53090448
00016717 00000-0 10270-3 0 9077
2 25544 51
6426 29
2310 0007264 150
9558 209
2009 15
71390343 29666
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
53090448 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 29
2310 deg
Eccentricity:
0007264
Arg of perigee: 150
9558 deg
Mean anomaly: 209
2009 deg
Mean motion: 15
71390343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 297
Coasting Arc #9 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2010/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1183680
86 A = 6727772
32 meter
Y = 4012056
60 meter E =
0009535
Z = 5264823
45 I = 51
75946
XDOT = -7177
913965 Wp = 142
62158
YDOT = -2749
813064 meter/sec RA = 23
74595 deg
ZDOT = 473
820313 TA = 302
83969
MA = 302
93146
Ha = 196
322 n
mi
Hp = 186
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3883467
39 X = -1254031
41
Y = 13162915
34 feet Y = 3998426
18 meter
Z = 17273042
81 Z = 5258902
71
XDOT = -23549
586498 XDOT = -7148
933257
YDOT = -9021
696404 feet/sec YDOT = -2829
918787 meter/sec
ZDOT = 1554
528585 ZDOT = 439
020963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13121541
19 X = 3999445
76
Y = -4121608
69 feet Y = -1256266
33 meter
Z = 17249323
62 Z = 5257593
84
XDOT = 5515
301826 XDOT = 1681
063997
YDOT = 23590
322951 feet/sec YDOT = 7190
330435 meter/sec
ZDOT = 1415
387898 ZDOT = 431
410231
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 10208
54844158
00016717 00000-0 10270-3 0 9085
2 25544 51
6419 24
0252 0007475 154
5327 205
6205 15
71330897 29828
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
54844158 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 24
0252 deg
Eccentricity:
0007475
Arg of perigee: 154
5327 deg
Mean anomaly: 205
6205 deg
Mean motion: 15
71330897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 307
Coasting Arc #10 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2010/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6520641
10 A = 6738927
33 meter
Y = 1150234
27 meter E =
0008342
Z = -1259615
39 I = 51
77003
XDOT = 251
615605 Wp = 87
92447
YDOT = 4962
943458 meter/sec RA = 18
62296 deg
ZDOT = 5868
129882 TA = 258
31242
MA = 258
40603
Ha = 196
129 n
mi
Hp = 186
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21393179
47 X = 6513413
20
Y = 3773734
49 feet Y = 1223111
65 meter
Z = -4132596
44 Z = -1227956
25
XDOT = 825
510514 XDOT = 167
594639
YDOT = 16282
622895 feet/sec YDOT = 4965
287010 meter/sec
ZDOT = 19252
394625 ZDOT = 5869
148442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9285698
81 X = -2830281
00
Y = -19665078
43 feet Y = -5993915
90 meter
Z = -4006000
66 Z = -1221029
00
XDOT = 11449
618644 XDOT = 3489
843763
YDOT = -9305
996351 feet/sec YDOT = -2836
467688 meter/sec
ZDOT = 19256
418469 ZDOT = 5869
356349
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 10209
50236677
00016717 00000-0 10270-3 0 9094
2 25544 51
6425 19
1448 0007553 158
7768 201
3708 15
71401039 29973
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
50236677 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 19
1448 deg
Eccentricity:
0007553
Arg of perigee: 158
7768 deg
Mean anomaly: 201
3708 deg
Mean motion: 15
71401039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 321
Coasting Arc #11 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2010/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1622851
10 A = 6729152
66 meter
Y = -4353112
88 meter E =
0014639
Z = -4879027
34 I = 51
70915
XDOT = 7324
347414 Wp = 103
76210
YDOT = -128
391612 meter/sec RA = 13
54482 deg
ZDOT = -2330
896019 TA = 143
56221
MA = 143
46249
Ha = 195
990 n
mi
Hp = 186
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5324314
65 X = -1550352
17
Y = -14281866
41 feet Y = -4370854
96 meter
Z = -16007307
53 Z = -4886735
13
XDOT = 24030
011200 XDOT = 7336
561625
YDOT = -421
232323 feet/sec YDOT = -46
417970 meter/sec
ZDOT = -7647
296650 ZDOT = -2295
285295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8424710
65 X = -2567851
81
Y = 12663250
46 feet Y = 3859758
74 meter
Z = -16038088
01 Z = -4888409
23
XDOT = -13653
703809 XDOT = -4161
648921
YDOT = -18550
318750 feet/sec YDOT = -5654
137155 meter/sec
ZDOT = -7504
890910 ZDOT = -2287
490749
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 10210
51987555
00016717 00000-0 10270-3 0 9107
2 25544 51
6431 13
9402 0007509 161
4222 198
7215 15
71432856 30132
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
51987555 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 13
9402 deg
Eccentricity:
0007509
Arg of perigee: 161
4222 deg
Mean anomaly: 198
7215 deg
Mean motion: 15
71432856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 283
Coasting Arc #12 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2010/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5976516
79 A = 6736246
44 meter
Y = 1336797
95 meter E =
0017997
Z = 2779228
58 I = 51
70253
XDOT = -3426
549583 Wp = 122
54072
YDOT = -4606
873775 meter/sec RA = 8
39176 deg
ZDOT = -5138
122740 TA = 25
68575
MA = 25
59647
Ha = 195
964 n
mi
Hp = 186
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19607994
72 X = -6004521
73
Y = 4385820
06 feet Y = 1269808
27 meter
Z = 9118204
02 Z = 2750127
09
XDOT = -11241
960573 XDOT = -3349
820278
YDOT = -15114
415273 feet/sec YDOT = -4644
762268 meter/sec
ZDOT = -16857
358071 ZDOT = -5154
582514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15390192
27 X = 4690930
61
Y = 12998450
11 feet Y = 3961927
59 meter
Z = 9001821
78 Z = 2743755
28
XDOT = -4342
596705 XDOT = -1323
623476
YDOT = 16894
843671 feet/sec YDOT = 5149
548351 meter/sec
ZDOT = -16923
131814 ZDOT = -5158
170577
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 10211
53737039
00016717 00000-0 10270-3 0 9111
2 25544 51
6426 8
7342 0007487 166
6029 193
5333 15
71426252 30292
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53737039 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 8
7342 deg
Eccentricity:
0007487
Arg of perigee: 166
6029 deg
Mean anomaly: 193
5333 deg
Mean motion: 15
71426252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 297
Coasting Arc #13 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2010/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222689
56 A = 6732382
87 meter
Y = 3403121
55 meter E =
0015302
Z = 3985926
69 I = 51
66111
XDOT = -5990
445218 Wp = 128
72026
YDOT = 2782
027823 meter/sec RA = 3
32743 deg
ZDOT = 3951
463185 TA = 280
30823
MA = 280
48072
Ha = 195
662 n
mi
Hp = 186
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13853968
38 X = 4164958
67
Y = 11165096
94 feet Y = 3450019
23 meter
Z = 13077187
30 Z = 4006300
23
XDOT = -19653
691659 XDOT = -6040
304443
YDOT = 9127
387870 feet/sec YDOT = 2714
760141 meter/sec
ZDOT = 12964
118061 ZDOT = 3922
240893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 247133
82 X = 75326
39
Y = -17731168
43 feet Y = -5404460
14 meter
Z = 13158618
77 Z = 4010747
00
XDOT = 18085
862707 XDOT = 5512
570953
YDOT = 9833
580107 feet/sec YDOT = 2997
275217 meter/sec
ZDOT = 12847
243885 ZDOT = 3915
839936
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 10212
55485113
00016717 00000-0 10270-3 0 9128
2 25544 51
6435 3
5290 0007510 170
5632 189
5672 15
71481545 30453
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55485113 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 3
5290 deg
Eccentricity:
0007510
Arg of perigee: 170
5632 deg
Mean anomaly: 189
5672 deg
Mean motion: 15
71481545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 285
Coasting Arc #14 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2010/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4253795
07 A = 6732427
94 meter
Y = -3329832
99 meter E =
0012283
Z = -4031435
41 I = 51
63177
XDOT = 5959
609306 Wp = 141
05956
YDOT = 2893
950319 meter/sec RA = 358
16139 deg
ZDOT = 3895
058453 TA = 169
22618
MA = 169
19985
Ha = 195
627 n
mi
Hp = 186
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13956020
58 X = 4310297
58
Y = -10924648
92 feet Y = -3281948
40 meter
Z = -13226494
14 Z = -4010633
52
XDOT = 19552
523970 XDOT = 5907
884324
YDOT = 9494
587662 feet/sec YDOT = 2960
304838 meter/sec
ZDOT = 12779
063166 ZDOT = 3923
884550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17337064
75 X = -5284337
34
Y = -3967216
97 feet Y = -1209207
73 meter
Z = -13143286
76 Z = -4006073
80
XDOT = -5245
129061 XDOT = -1598
715338
YDOT = -19829
119874 feet/sec YDOT = -6043
915737 meter/sec
ZDOT = 12894
291995 ZDOT = 3930
180200
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 10213
50872836
00016717 00000-0 10270-3 0 9137
2 25544 51
6446 358
6497 0007439 173
2185 186
9078 15
71476292 30602
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50872836 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 358
6497 deg
Eccentricity:
0007439
Arg of perigee: 173
2185 deg
Mean anomaly: 186
9078 deg
Mean motion: 15
71476292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 333
Coasting Arc #15 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5956396
82 A = 6735887
74 meter
Y = -1483899
69 meter E =
0010632
Z = -2763808
71 I = 51
61365
XDOT = 3506
473893 Wp = 154
81451
YDOT = -4528
347274 meter/sec RA = 353
09240 deg
ZDOT = -5142
320711 TA = 56
77079
MA = 56
66892
Ha = 195
370 n
mi
Hp = 186
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19541984
32 X = -5925934
86
Y = -4868437
32 feet Y = -1550337
20 meter
Z = -9067613
89 Z = -2792670
87
XDOT = 11504
179439 XDOT = 3581
830449
YDOT = -14856
782396 feet/sec YDOT = -4488
714136 meter/sec
ZDOT = -16871
130943 ZDOT = -5125
103564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8858994
82 X = 2700221
62
Y = 18027846
07 feet Y = 5494887
48 meter
Z = -9182996
88 Z = -2798977
45
XDOT = -17523
194881 XDOT = -5341
069800
YDOT = 79
801418 feet/sec YDOT = 24
323472 meter/sec
ZDOT = -16802
245269 ZDOT = -5121
324358
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 10214
52618292
00016717 00000-0 10270-3 0 9145
2 25544 51
6445 353
4442 0007355 177
3530 182
7672 15
71503929 30769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52618292 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 353
4442 deg
Eccentricity:
0007355
Arg of perigee: 177
3530 deg
Mean anomaly: 182
7672 deg
Mean motion: 15
71503929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 308
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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