Date:
January 20th 2011
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) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 1749)
---------------------------------------
Vector Time (GMT): 2011/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6433817
97 A = 6736862
22 meter
Y = -1410465
26 meter E =
0004084
Z = -1410024
65 I = 51
52455
XDOT = -162
554489 Wp = 52
79224
YDOT = -5046
868250 meter/sec RA = 202
16069 deg
ZDOT = 5804
109696 TA = 291
69884
MA = 291
74232
Ha = 193
187 n
mi
Hp = 187
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21108326
67 X = -6410718
25
Y = -4627510
70 feet Y = -1482282
81 meter
Z = -4626065
13 Z = -1441223
29
XDOT = -533
315252 XDOT = -134
301907
YDOT = -16557
966701 feet/sec YDOT = -5048
528589 meter/sec
ZDOT = 19042
354647 ZDOT = 5803
388195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5720255
74 X = -1743533
95
Y = -20810463
01 feet Y = -6343029
13 meter
Z = -4751746
22 Z = -1448332
25
XDOT = 12833
997756 XDOT = 3911
802516
YDOT = -7864
941838 feet/sec YDOT = -2397
234272 meter/sec
ZDOT = 19039
515128 ZDOT = 5803
244211
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 11019
50281657
00016717 00000-0 10270-3 0 9003
2 25544 51
6391 203
1923 0004680 204
0934 156
0010 15
72033607 17507
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
50281657 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 203
1923 deg
Eccentricity:
0004680
Arg of perigee: 204
0934 deg
Mean anomaly: 156
0010 deg
Mean motion: 15
72033607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 264
Coasting Arc #2 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2011/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293361
49 A = 6727386
96 meter
Y = 4454743
63 meter E =
0009707
Z = -4880507
39 I = 51
52165
XDOT = -7337
190139 Wp = 93
57633
YDOT = -359
205427 meter/sec RA = 197
06377 deg
ZDOT = -2276
747179 TA = 154
22821
MA = 154
17982
Ha = 193
054 n
mi
Hp = 187
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4243311
98 X = 1267159
49
Y = 14615300
62 feet Y = 4469060
58 meter
Z = -16012163
34 Z = -4874287
79
XDOT = -24072
146124 XDOT = -7321
568432
YDOT = -1178
495496 feet/sec YDOT = -441
166828 meter/sec
ZDOT = -7469
642975 ZDOT = -2312
352247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10728653
47 X = -3270093
58
Y = 10830926
38 feet Y = 3301266
36 meter
Z = -15987154
60 Z = -4872884
72
XDOT = -9728
477044 XDOT = -2965
239803
YDOT = -20852
324329 feet/sec YDOT = -6355
788455 meter/sec
ZDOT = -7613
110967 ZDOT = -2320
476223
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 11020
51991223
00016717 00000-0 10270-3 0 9014
2 25544 51
6393 197
9842 0004549 206
2847 153
8076 15
72069607 17663
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
51991223 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 197
9842 deg
Eccentricity:
0004549
Arg of perigee: 206
2847 deg
Mean anomaly: 153
8076 deg
Mean motion: 15
72069607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1766
Checksum: 321
Coasting Arc #3 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2011/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6178168
12 A = 6734714
50 meter
Y = -764993
77 meter E =
0012941
Z = 2549054
93 I = 51
57643
XDOT = 2785
988008 Wp = 123
17824
YDOT = 4866
844926 meter/sec RA = 191
89559 deg
ZDOT = -5279
549746 TA = 27
89613
MA = 27
82681
Ha = 192
755 n
mi
Hp = 187
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20269580
46 X = 6173880
78
Y = -2509822
10 feet Y = -695929
82 meter
Z = 8363041
10 Z = 2579057
13
XDOT = 9140
380603 XDOT = 2757
005303
YDOT = 15967
338996 feet/sec YDOT = 4897
837647 meter/sec
ZDOT = -17321
357436 ZDOT = -5266
086059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12204004
39 X = 3719780
54
Y = 16315032
54 feet Y = 4972821
92 meter
Z = 8483958
11 Z = 2585910
43
XDOT = -8093
383305 XDOT = -2466
863231
YDOT = 15053
769782 feet/sec YDOT = 4588
389029 meter/sec
ZDOT = -17267
150665 ZDOT = -5263
027523
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 11021
53699042
00016717 00000-0 10270-3 0 9022
2 25544 51
6394 192
7750 0004621 213
0568 147
0306 15
72090866 17822
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
53699042 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 192
7750 deg
Eccentricity:
0004621
Arg of perigee: 213
0568 deg
Mean anomaly: 147
0306 deg
Mean motion: 15
72090866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 298
Coasting Arc #4 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3495413
99 A = 6729628
57 meter
Y = -3836981
37 meter E =
0009582
Z = 4281825
28 I = 51
58985
XDOT = 6541
891288 Wp = 135
38972
YDOT = -2024
563342 meter/sec RA = 186
81679 deg
ZDOT = 3514
712322 TA = 278
91336
MA = 279
02183
Ha = 192
771 n
mi
Hp = 187
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11467893
67 X = -3473048
13
Y = -12588521
55 feet Y = -3875944
19 meter
Z = 14047983
21 Z = 4264899
30
XDOT = 21462
897928 XDOT = 6546
970750
YDOT = -6642
268183 feet/sec YDOT = -1951
379599 meter/sec
ZDOT = 11531
208404 ZDOT = 3546
504295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4923963
26 X = 1500824
00
Y = -16359981
83 feet Y = -4986522
46 meter
Z = 13979802
30 Z = 4261043
74
XDOT = 15442
456945 XDOT = 4706
860877
YDOT = 14643
129437 feet/sec YDOT = 4463
225852 meter/sec
ZDOT = 11659
361434 ZDOT = 3553
773365
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 11022
55405300
00016717 00000-0 10270-3 0 9038
2 25544 51
6397 187
5661 0004653 215
4554 144
6299 15
72129417 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
55405300 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 187
5661 deg
Eccentricity:
0004653
Arg of perigee: 215
4554 deg
Mean anomaly: 144
6299 deg
Mean motion: 15
72129417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 312
Coasting Arc #5 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2011/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5070863
13 A = 6731943
70 meter
Y = 2662043
65 meter E =
0005056
Z = -3544548
62 I = 51
62985
XDOT = -5059
531753 Wp = 149
54025
YDOT = -3685
034238 meter/sec RA = 181
64333 deg
ZDOT = 4469
160100 TA = 168
29665
MA = 168
28489
Ha = 192
636 n
mi
Hp = 187
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16636690
05 X = -5083035
33
Y = 8733739
00 feet Y = 2605270
13 meter
Z = -11629096
53 Z = -3569211
89
XDOT = -16599
513624 XDOT = -5039
658861
YDOT = -12090
007343 feet/sec YDOT = -3741
501861 meter/sec
ZDOT = 14662
598753 ZDOT = 4444
629713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16134774
51 X = -4917879
27
Y = -9508109
63 feet Y = -2898071
82 meter
Z = -11728531
10 Z = -3574856
28
XDOT = 826
379304 XDOT = 251
880412
YDOT = -19373
162042 feet/sec YDOT = -5904
939791 meter/sec
ZDOT = 14563
757830 ZDOT = 4439
033386
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 11023
50753478
00016717 00000-0 10270-3 0 9047
2 25544 51
6411 182
6833 0004533 217
0776 143
0073 15
72136902 18133
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
50753478 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 182
6833 deg
Eccentricity:
0004533
Arg of perigee: 217
0776 deg
Mean anomaly: 143
0073 deg
Mean motion: 15
72136902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 284
Coasting Arc #6 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2011/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5201053
26 A = 6732174
99 meter
Y = 2458231
01 meter E =
0003624
Z = -3495785
50 I = 51
66143
XDOT = -4869
993003 Wp = 145
19266
YDOT = 3876
444247 meter/sec RA = 176
57424 deg
ZDOT = -4524
914548 TA = 76
26621
MA = 76
22587
Ha = 192
487 n
mi
Hp = 187
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17063823
04 X = 5190159
90
Y = 8065062
36 feet Y = 2516331
43 meter
Z = -11469112
53 Z = -3470545
68
XDOT = -15977
667332 XDOT = -4890
997355
YDOT = 12717
992935 feet/sec YDOT = 3821
867615 meter/sec
ZDOT = -14845
520169 ZDOT = -4548
623562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2462104
58 X = 750449
48
Y = 18774457
28 feet Y = 5722454
58 meter
Z = -11367393
06 Z = -3464781
40
XDOT = -17914
161962 XDOT = -5460
236566
YDOT = -6686
684069 feet/sec YDOT = -2038
101304 meter/sec
ZDOT = -14941
127075 ZDOT = -4554
055533
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 11024
52456401
00016717 00000-0 10270-3 0 9057
2 25544 51
6413 177
4751 0004412 222
2984 137
7838 15
72171406 18295
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
52456401 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 177
4751 deg
Eccentricity:
0004412
Arg of perigee: 222
2984 deg
Mean anomaly: 137
7838 deg
Mean motion: 15
72171406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 296
Coasting Arc #7 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2011/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3309413
67 A = 6729234
14 meter
Y = -3952856
06 meter E =
0005895
Z = 4319885
49 I = 51
68175
XDOT = 6643
712955 Wp = 90
35413
YDOT = 1767
712283 meter/sec RA = 171
40501 deg
ZDOT = -3468
126868 TA = 34
69932
MA = 34
66088
Ha = 192
293 n
mi
Hp = 187
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10857656
39 X = 3332384
37
Y = -12968687
87 feet Y = -3915719
84 meter
Z = 14172852
65 Z = 4336018
11
XDOT = 21796
958513 XDOT = 6640
299578
YDOT = 5799
580980 feet/sec YDOT = 1841
987266 meter/sec
ZDOT = -11378
368991 ZDOT = -3435
860437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16765053
90 X = 5109988
43
Y = 1777557
32 feet Y = 541799
47 meter
Z = 14237927
41 Z = 4339720
28
XDOT = 7423
240382 XDOT = 2262
603668
YDOT = 20189
817555 feet/sec YDOT = 6153
856391 meter/sec
ZDOT = -11248
308495 ZDOT = -3428
484429
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 11025
54157712
00016717 00000-0 10270-3 0 9064
2 25544 51
6409 172
2662 0004458 225
2130 134
8670 15
72160965 18458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
54157712 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 172
2662 deg
Eccentricity:
0004458
Arg of perigee: 225
2130 deg
Mean anomaly: 134
8670 deg
Mean motion: 15
72160965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 296
Coasting Arc #8 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2011/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6210304
37 A = 6734467
52 meter
Y = -549641
99 meter E =
0009976
Z = 2536937
14 I = 51
73104
XDOT = 2608
617037 Wp = 87
42617
YDOT = -4936
218724 meter/sec RA = 166
33415 deg
ZDOT = 5298
906782 TA = 301
26348
MA = 301
36116
Ha = 192
113 n
mi
Hp = 187
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20375014
32 X = -6216020
42
Y = -1803287
37 feet Y = -619121
42 meter
Z = 8323284
57 Z = 2506753
97
XDOT = 8558
454845 XDOT = 2637
880094
YDOT = -16194
943320 feet/sec YDOT = -4906
884171 meter/sec
ZDOT = 17384
864770 ZDOT = 5311
650173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10129434
65 X = -3087451
68
Y = -17826902
34 feet Y = -5433639
83 meter
Z = 8201599
04 Z = 2499847
39
XDOT = 16828
988438 XDOT = 5129
475676
YDOT = -1513
853117 feet/sec YDOT = -461
422430 meter/sec
ZDOT = 17436
294997 ZDOT = 5314
582715
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 11026
55856971
00016717 00000-0 10270-3 0 9070
2 25544 51
6421 167
0577 0004513 229
8197 130
2571 15
72245166 18619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
55856971 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 167
0577 deg
Eccentricity:
0004513
Arg of perigee: 229
8197 deg
Mean anomaly: 130
2571 deg
Mean motion: 15
72245166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 313
Coasting Arc #9 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2011/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1208330
67 A = 6726816
91 meter
Y = 4478852
04 meter E =
0010240
Z = -4880554
87 I = 51
73497
XDOT = -7310
577533 Wp = 126
67685
YDOT = 558
448909 meter/sec RA = 161
18002 deg
ZDOT = 2319
798485 TA = 165
93179
MA = 165
90324
Ha = 191
925 n
mi
Hp = 187
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3964339
48 X = -1234615
72
Y = 14694396
47 feet Y = 4465193
07 meter
Z = -16012319
11 Z = -4886488
44
XDOT = -23984
834425 XDOT = -7327
547875
YDOT = 1832
181461 feet/sec YDOT = 476
602600 meter/sec
ZDOT = 7610
887419 ZDOT = 2284
243015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14196146
35 X = -4326985
41
Y = 5416850
90 feet Y = 1651056
15 meter
Z = -16036296
13 Z = -4887863
06
XDOT = -15094
918073 XDOT = -4600
931029
YDOT = -17427
015303 feet/sec YDOT = -5311
754264 meter/sec
ZDOT = 7467
513251 ZDOT = 2276
098039
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 11027
51198705
00016717 00000-0 10270-3 0 9082
2 25544 51
6421 162
1755 0004367 234
5561 125
5194 15
72248003 18765
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
51198705 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 162
1755 deg
Eccentricity:
0004367
Arg of perigee: 234
5561 deg
Mean anomaly: 125
5194 deg
Mean motion: 15
72248003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 301
Coasting Arc #10 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6378887
72 A = 6736140
81 meter
Y = -1528165
01 meter E =
0009000
Z = -1508689
44 I = 51
79506
XDOT = -155
899819 Wp = 171
47972
YDOT = 5061
380074 meter/sec RA = 156
09813 deg
ZDOT = -5798
976401 TA = 25
09420
MA = 25
05049
Ha = 191
810 n
mi
Hp = 187
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20928109
31 X = 6402830
67
Y = -5013664
74 feet Y = -1456698
46 meter
Z = -4949768
50 Z = -1477643
29
XDOT = -511
482346 XDOT = -184
315650
YDOT = 16605
577672 feet/sec YDOT = 5059
478238 meter/sec
ZDOT = -19025
513128 ZDOT = -5799
802412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16525689
30 X = 5037030
10
Y = 13829249
01 feet Y = 4215155
10 meter
Z = -4824548
33 Z = -1470522
33
XDOT = -12555
801896 XDOT = -3827
008418
YDOT = 8380
796954 feet/sec YDOT = 2554
466912 meter/sec
ZDOT = -19028
906884 ZDOT = -5800
010818
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 11028
52894685
00016717 00000-0 10270-3 0 9095
2 25544 51
6421 156
9658 0004300 239
6023 120
4715 15
72278543 18927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
52894685 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 156
9658 deg
Eccentricity:
0004300
Arg of perigee: 239
6023 deg
Mean anomaly: 120
4715 deg
Mean motion: 15
72278543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 316
Coasting Arc #11 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -910805
05 A = 6725329
07 meter
Y = -4172812
49 meter E =
0000745
Z = 5195647
30 I = 51
78743
XDOT = 7039
499786 Wp = 290
85244
YDOT = -2912
726422 meter/sec RA = 150
96390 deg
ZDOT = -1105
147762 TA = 169
67620
MA = 169
67467
Ha = 191
633 n
mi
Hp = 187
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2988205
54 X = -889315
14
Y = -13690329
68 feet Y = -4182877
90 meter
Z = 17046086
95 Z = 5191274
59
XDOT = 23095
471740 XDOT = 7076
915742
YDOT = -9556
189047 feet/sec YDOT = -2833
797198 meter/sec
ZDOT = -3625
812867 ZDOT = -1070
859957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8959494
23 X = 2730853
84
Y = -10801900
35 feet Y = -3292419
23 meter
Z = 17028505
26 Z = 5190288
40
XDOT = 20889
817627 XDOT = 6367
216413
YDOT = 11828
303742 feet/sec YDOT = 3605
266981 meter/sec
ZDOT = -3487
481767 ZDOT = -1062
984443
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 11029
54588930
00016717 00000-0 10270-3 0 9103
2 25544 51
6432 151
7572 0004210 244
9818 115
0908 15
72296174 19080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11029
54588930 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 151
7572 deg
Eccentricity:
0004210
Arg of perigee: 244
9818 deg
Mean anomaly: 115
0908 deg
Mean motion: 15
72296174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 307
Coasting Arc #12 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2011/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5741162
02 A = 6736898
00 meter
Y = 3489669
23 meter E =
0009155
Z = 423840
57 I = 51
85341
XDOT = -2145
730386 Wp = 40
36624
YDOT = -4270
940884 meter/sec RA = 145
86732 deg
ZDOT = 6034
044053 TA = 324
22565
MA = 324
28694
Ha = 191
438 n
mi
Hp = 187
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18835833
41 X = -5781816
35
Y = 11449046
03 feet Y = 3425240
75 meter
Z = 1390553
05 Z = 395852
25
XDOT = -7039
797855 XDOT = -2127
123961
YDOT = -14012
273240 feet/sec YDOT = -4294
832135 meter/sec
ZDOT = 19796
732457 ZDOT = 6023
665258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20703019
61 X = -6310280
38
Y = -7586541
87 feet Y = -2312377
96 meter
Z = 1277604
96 Z = 389413
99
XDOT = 5933
171989 XDOT = 1808
430822
YDOT = -12824
985854 feet/sec YDOT = -3909
055688 meter/sec
ZDOT = 19754
924018 ZDOT = 6021
300841
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 11030
56281321
00016717 00000-0 10270-3 0 9112
2 25544 51
6439 146
5482 0004162 249
7043 110
3672 15
72320161 19246
Satellite: ISS
Catalog Number: 25544
Epoch time: 11030
56281321 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 146
5482 deg
Eccentricity:
0004162
Arg of perigee: 249
7043 deg
Mean anomaly: 110
3672 deg
Mean motion: 15
72320161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 272
Coasting Arc #13 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2733597
91 A = 6724783
94 meter
Y = 3137113
57 meter E =
0011021
Z = -5292252
13 I = 51
83806
XDOT = -5895
397942 Wp = 94
47806
YDOT = 4936
947870 meter/sec RA = 140
75728 deg
ZDOT = -119
695995 TA = 174
39387
MA = 174
38153
Ha = 191
264 n
mi
Hp = 187
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8968497
09 X = 2724022
97
Y = 10292367
35 feet Y = 3167629
09 meter
Z = -17363031
93 Z = -5278995
79
XDOT = -19341
856765 XDOT = -5949
584223
YDOT = 16197
335532 feet/sec YDOT = 4870
719006 meter/sec
ZDOT = -392
703395 ZDOT = -148
466288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2152241
02 X = -656003
06
Y = 13549444
32 feet Y = 4129870
63 meter
Z = -17309594
47 Z = -5275964
39
XDOT = -23817
731112 XDOT = -7259
644443
YDOT = -4428
910803 feet/sec YDOT = -1349
932013 meter/sec
ZDOT = -508
841807 ZDOT = -155
094983
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 11031
51616282
00016717 00000-0 10270-3 0 9127
2 25544 51
6443 141
6657 0004188 254
6653 105
4046 15
72360704 19394
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
51616282 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 141
6657 deg
Eccentricity:
0004188
Arg of perigee: 254
6653 deg
Mean anomaly: 105
4046 deg
Mean motion: 15
72360704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 295
Coasting Arc #14 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2011/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4435392
61 A = 6736640
28 meter
Y = -5022838
86 meter E =
0011159
Z = 625558
76 I = 51
90111
XDOT = 3951
114659 Wp = 145
18588
YDOT = 2734
297156 meter/sec RA = 135
64357 deg
ZDOT = -6016
483458 TA = 28
03075
MA = 27
97071
Ha = 191
223 n
mi
Hp = 187
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14551813
03 X = 4488190
55
Y = -16479130
13 feet Y = -4972944
44 meter
Z = 2052358
13 Z = 647233
22
XDOT = 12962
974603 XDOT = 3949
471600
YDOT = 8970
791195 feet/sec YDOT = 2778
471968 meter/sec
ZDOT = -19739
118956 ZDOT = -5997
293455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21973663
54 X = 6697572
65
Y = 328915
93 feet Y = 100253
58 meter
Z = 2139881
17 Z = 652235
78
XDOT = 1715
959846 XDOT = 523
024561
YDOT = 14167
888931 feet/sec YDOT = 4318
372546 meter/sec
ZDOT = -19661
728557 ZDOT = -5992
894864
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 11032
53305266
00016717 00000-0 10270-3 0 9138
2 25544 51
6444 136
4569 0004154 257
6297 102
4401 15
72368780 19551
Satellite: ISS
Catalog Number: 25544
Epoch time: 11032
53305266 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 136
4569 deg
Eccentricity:
0004154
Arg of perigee: 257
6297 deg
Mean anomaly: 102
4401 deg
Mean motion: 15
72368780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 303
Coasting Arc #15 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2011/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4023417
56 A = 6725135
23 meter
Y = -1533276
14 meter E =
0003038
Z = 5167198
74 I = 51
88480
XDOT = 4109
572282 Wp = 191
88934
YDOT = -6376
837987 meter/sec RA = 130
55533 deg
ZDOT = 1304
911902 TA = 245
65223
MA = 245
68395
Ha = 191
151 n
mi
Hp = 187
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13200188
84 X = -4031073
61
Y = -5030433
54 feet Y = -1578311
34 meter
Z = 16952751
78 Z = 5147635
02
XDOT = 13482
848693 XDOT = 4174
235046
YDOT = -20921
384471 feet/sec YDOT = -6330
520745 meter/sec
ZDOT = 4281
207027 ZDOT = 1325
032453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5058096
71 X = -1541707
88
Y = -13290432
24 feet Y = -4050923
75 meter
Z = 16873829
10 Z = 5143143
11
XDOT = 23613
521336 XDOT = 7197
401303
YDOT = -3436
557307 feet/sec YDOT = -1047
462667 meter/sec
ZDOT = 4362
487465 ZDOT = 1329
686179
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 11033
54992261
00016717 00000-0 10270-3 0 9148
2 25544 51
6452 131
2475 0004162 263
5075 96
5614 15
72438704 19719
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
54992261 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 131
2475 deg
Eccentricity:
0004162
Arg of perigee: 263
5075 deg
Mean anomaly: 96
5614 deg
Mean motion: 15
72438704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 301
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list