Date:
October 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
293/19:22:33
450 1
5 2
2 2
2
N/A -1
6 -0
0 195
4
000/00:05:06
900 0
3 0
1 185
3
Coasting Arc #1 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2010/286/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4862111
61 A = 6730366
04 meter
Y = -2091609
52 meter E =
0015334
Z = -4172163
39 I = 51
55080
XDOT = 5070
210997 Wp = 78
98891
YDOT = -4442
985800 meter/sec RA = 344
53093 deg
ZDOT = -3689
872251 TA = 153
23933
MA = 153
16013
Ha = 195
940 n
mi
Hp = 184
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15951809
73 X = -4818093
61
Y = -6862235
94 feet Y = -2145734
49 meter
Z = -13688200
09 Z = -4195676
87
XDOT = 16634
550514 XDOT = 5137
441405
YDOT = -14576
725065 feet/sec YDOT = -4385
911788 meter/sec
ZDOT = -12105
880087 ZDOT = -3665
077515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16563114
91 X = 5048437
42
Y = -4962372
52 feet Y = -1512531
15 meter
Z = -13782431
61 Z = -4200885
15
XDOT = -3765
308888 XDOT = -1147
666149
YDOT = 20701
189149 feet/sec YDOT = 6309
722453 meter/sec
ZDOT = -12006
423218 ZDOT = -3659
557797
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 10286
57490527
00016717 00000-0 10270-3 0 9003
2 25544 51
6458 344
9091 0007447 89
9651 270
2364 15
71955189 2097
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
57490527 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 344
9091 deg
Eccentricity:
0007447
Arg of perigee: 89
9651 deg
Mean anomaly: 270
2364 deg
Mean motion: 15
71955189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 209
Checksum: 334
Coasting Arc #2 (Orbit 224)
---------------------------------------
Vector Time (GMT): 2010/287/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3424559
25 A = 6731924
52 meter
Y = 4440364
53 meter E =
0019195
Z = 3709217
10 I = 51
52647
XDOT = -6285
523961 Wp = 86
99669
YDOT = -1260
922228 meter/sec RA = 339
35320 deg
ZDOT = -4273
723464 TA = 48
19908
MA = 48
03527
Ha = 195
915 n
mi
Hp = 184
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11235430
61 X = -3491976
58
Y = 14568125
10 feet Y = 4401692
18 meter
Z = 12169347
45 Z = 3692416
59
XDOT = -20621
797772 XDOT = -6250
195768
YDOT = -4136
883950 feet/sec YDOT = -1331
013290 meter/sec
ZDOT = -14021
402440 ZDOT = -4304
172981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1039659
64 X = -316888
26
Y = -18412505
55 feet Y = -5612131
69 meter
Z = 12101939
29 Z = 3688671
09
XDOT = 16863
217498 XDOT = 5139
908693
YDOT = -10291
484190 feet/sec YDOT = -3136
844381 meter/sec
ZDOT = -14143
451068 ZDOT = -4310
923885
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 10287
59204796
00016717 00000-0 10270-3 0 9018
2 25544 51
6449 339
7018 0007435 92
4359 267
7654 15
72013804 2250
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
59204796 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 339
7018 deg
Eccentricity:
0007435
Arg of perigee: 92
4359 deg
Mean anomaly: 267
7654 deg
Mean motion: 15
72013804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 225
Checksum: 322
Coasting Arc #3 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2010/288/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5895252
32 A = 6733223
05 meter
Y = 16271
75 meter E =
0020366
Z = 3235649
10 I = 51
50279
XDOT = -2635
908609 Wp = 90
42695
YDOT = 5462
886039 meter/sec RA = 334
27513 deg
ZDOT = 4749
237313 TA = 307
50872
MA = 307
69368
Ha = 195
866 n
mi
Hp = 184
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19341378
99 X = 5878913
89
Y = 53385
00 feet Y = 82104
76 meter
Z = 10615646
67 Z = 3264248
77
XDOT = -8647
994124 XDOT = -2719
870820
YDOT = 17922
854459 feet/sec YDOT = 5432
940435 meter/sec
ZDOT = 15581
487246 ZDOT = 4736
227832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14354568
48 X = -4375272
47
Y = 12868211
53 feet Y = 3922230
88 meter
Z = 10730295
48 Z = 3270594
06
XDOT = -4570
903007 XDOT = -1393
211237
YDOT = -18118
036141 feet/sec YDOT = -5522
377416 meter/sec
ZDOT = 15529
267071 ZDOT = 4733
320603
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 10288
60917201
00016717 00000-0 10270-3 0 9024
2 25544 51
6447 334
4942 0007633 95
7041 264
4992 15
72003851 2418
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
60917201 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 334
4942 deg
Eccentricity:
0007633
Arg of perigee: 95
7041 deg
Mean anomaly: 264
4992 deg
Mean motion: 15
72003851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 241
Checksum: 296
Coasting Arc #4 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1149669
31 A = 6728998
96 meter
Y = -4874956
23 meter E =
0017209
Z = -4510249
92 I = 51
46305
XDOT = 6912
680273 Wp = 105
12931
YDOT = -1246
462087 meter/sec RA = 329
09574 deg
ZDOT = 3114
780276 TA = 196
05760
MA = 196
11221
Ha = 195
819 n
mi
Hp = 184
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3771880
93 X = 1226006
68
Y = -15993950
89 feet Y = -4861673
35 meter
Z = -14797407
89 Z = -4504479
11
XDOT = 22679
397222 XDOT = 6910
973514
YDOT = -4089
442542 feet/sec YDOT = -1169
169723 meter/sec
ZDOT = 10219
095393 ZDOT = 3148
358256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8090424
92 X = 2465961
52
Y = 14327049
35 feet Y = 4366884
64 meter
Z = -14774217
83 Z = -4503181
59
XDOT = -12702
024955 XDOT = -3871
577206
YDOT = 17831
096735 feet/sec YDOT = 5434
918285 meter/sec
ZDOT = 10353
713411 ZDOT = 3155
811848
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 10289
56270416
00016717 00000-0 10270-3 0 9031
2 25544 51
6459 329
6123 0007447 98
9456 261
2549 15
72037137 2569
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56270416 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 329
6123 deg
Eccentricity:
0007447
Arg of perigee: 98
9456 deg
Mean anomaly: 261
2549 deg
Mean motion: 15
72037137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 324
Coasting Arc #5 (Orbit 271)
---------------------------------------
Vector Time (GMT): 2010/290/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5981103
34 A = 6735481
42 meter
Y = 2176597
38 meter E =
0012960
Z = -2202080
39 I = 51
45897
XDOT = 33
810942 Wp = 117
74529
YDOT = -5410
043634 meter/sec RA = 324
00478 deg
ZDOT = -5469
720427 TA = 86
96443
MA = 86
81614
Ha = 195
721 n
mi
Hp = 184
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19623042
46 X = -5994300
51
Y = 7141067
52 feet Y = 2109639
15 meter
Z = -7224673
20 Z = -2231169
07
XDOT = 110
928289 XDOT = 120
875712
YDOT = -17749
486989 feet/sec YDOT = -5409
179099 meter/sec
ZDOT = -17945
276990 ZDOT = -5469
344329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9122223
94 X = 2780453
86
Y = -18738860
11 feet Y = -5711604
56 meter
Z = -7341300
69 Z = -2237628
45
XDOT = 10808
632326 XDOT = 3294
471133
YDOT = 12252
998213 feet/sec YDOT = 3734
713855 meter/sec
ZDOT = -17943
711439 ZDOT = -5469
243247
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 10290
57978552
00016717 00000-0 10270-3 0 9041
2 25544 51
6449 324
4041 0007504 103
2849 256
9150 15
72075407 2729
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
57978552 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 324
4041 deg
Eccentricity:
0007504
Arg of perigee: 103
2849 deg
Mean anomaly: 256
9150 deg
Mean motion: 15
72075407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 272
Checksum: 304
Coasting Arc #6 (Orbit 287)
---------------------------------------
Vector Time (GMT): 2010/291/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1062159
58 A = 6726616
06 meter
Y = 4367090
40 meter E =
0011911
Z = 4994912
93 I = 51
40460
XDOT = -6494
379576 Wp = 84
13406
YDOT = 3709
482559 meter/sec RA = 318
83402 deg
ZDOT = -1857
222330 TA = 23
85366
MA = 23
79851
Ha = 195
628 n
mi
Hp = 184
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3484775
54 X = 988982
33
Y = 14327724
40 feet Y = 4378559
34 meter
Z = 16387509
63 Z = 4999894
88
XDOT = -21307
019607 XDOT = -6526
354849
YDOT = 12170
218369 feet/sec YDOT = 3636
679574 meter/sec
ZDOT = -6093
249115 ZDOT = -1888
850384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12525705
13 X = -3817834
93
Y = -7738252
62 feet Y = -2358619
40 meter
Z = 16407436
61 Z = 5000986
68
XDOT = 5874
284862 XDOT = 1790
482026
YDOT = -22731
624060 feet/sec YDOT = -6928
599013 meter/sec
ZDOT = -6220
064498 ZDOT = -1895
875659
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 10291
59684499
00016717 00000-0 10270-3 0 9059
2 25544 51
6439 319
1961 0007495 106
1797 254
0191 15
72129140 2888
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
59684499 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 319
1961 deg
Eccentricity:
0007495
Arg of perigee: 106
1797 deg
Mean anomaly: 254
0191 deg
Mean motion: 15
72129140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 288
Checksum: 331
Coasting Arc #7 (Orbit 303)
---------------------------------------
Vector Time (GMT): 2010/292/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5155878
52 A = 6736873
75 meter
Y = -4202907
63 meter E =
0019138
Z = 1029317
95 I = 51
41757
XDOT = 2351
739154 Wp = 74
51803
YDOT = 4350
932470 meter/sec RA = 313
72290 deg
ZDOT = 5899
841290 TA = 296
76310
MA = 296
95879
Ha = 195
540 n
mi
Hp = 183
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16915611
96 X = 5197492
69
Y = -13789067
04 feet Y = -4145018
74 meter
Z = 3377027
41 Z = 1054467
06
XDOT = 7715
679640 XDOT = 2274
250585
YDOT = 14274
712828 feet/sec YDOT = 4376
798264 meter/sec
ZDOT = 19356
434680 ZDOT = 5911
077643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1826237
01 X = -556637
04
Y = 21731311
27 feet Y = 6623703
68 meter
Z = 3477870
10 Z = 1060054
81
XDOT = -13962
194840 XDOT = -4255
676987
YDOT = -4322
162641 feet/sec YDOT = -1317
395173 meter/sec
ZDOT = 19401
433595 ZDOT = 5913
556960
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 10292
61388233
00016717 00000-0 10270-3 0 9061
2 25544 51
6438 313
9887 0007457 110
5980 249
5983 15
72181847 3046
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
61388233 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 313
9887 deg
Eccentricity:
0007457
Arg of perigee: 110
5980 deg
Mean anomaly: 249
5983 deg
Mean motion: 15
72181847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 304
Checksum: 331
Coasting Arc #8 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2010/293/13:15:24
134
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2901854
03 A = 6725467
76 meter
Y = -3084813
19 meter E =
0021992
Z = -5243419
19 I = 51
35793
XDOT = 5104
656055 Wp = 100
29559
YDOT = -5715
255062 meter/sec RA = 308
56799 deg
ZDOT = 535
386255 TA = 174
83525
MA = 174
81253
Ha = 195
538 n
mi
Hp = 183
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9520518
48 X = -2841671
28
Y = -10120778
19 feet Y = -3116927
41 meter
Z = -17202818
87 Z = -5257370
25
XDOT = 16747
559237 XDOT = 5165
584838
YDOT = -18750
836818 feet/sec YDOT = -5657
831013 meter/sec
ZDOT = 1756
516584 ZDOT = 560
333673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13825474
99 X = 4214004
78
Y = 23745
11 feet Y = 7237
51 meter
Z = -17258710
20 Z = -5260454
87
XDOT = 2284
331004 XDOT = 696
264090
YDOT = 24021
870523 feet/sec YDOT = 7321
866135 meter/sec
ZDOT = 1856
557440 ZDOT = 565
878708
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 10293
56733715
00016717 00000-0 10270-3 0 9076
2 25544 51
6430 309
1052 0007384 113
1299 247
0642 15
72159069 3192
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
56733715 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 309
1052 deg
Eccentricity:
0007384
Arg of perigee: 113
1299 deg
Mean anomaly: 247
0642 deg
Mean motion: 15
72159069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 302
Coasting Arc #9 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2010/293/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1821617
49 A = 6727766
78 meter
Y = -4171054
80 meter E =
0018391
Z = -4971264
27 I = 51
35979
XDOT = 5647
307905 Wp = 108
19271
YDOT = -4820
303783 meter/sec RA = 307
23703 deg
ZDOT = 1975
397174 TA = 181
02391
MA = 181
02769
Ha = 195
435 n
mi
Hp = 185
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5976435
32 X = -1750690
55
Y = -13684562
98 feet Y = -4191029
05 meter
Z = -16309922
13 Z = -4979941
25
XDOT = 18527
913075 XDOT = 5691
193373
YDOT = -15814
644957 feet/sec YDOT = -4756
906650 meter/sec
ZDOT = 6480
961856 ZDOT = 2002
939401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4381258
77 X = 1335407
67
Y = -14235697
85 feet Y = -4339040
70 meter
Z = -16344665
23 Z = -4981853
96
XDOT = 23291
666883 XDOT = 7099
300066
YDOT = -398
220983 feet/sec YDOT = -121
377756 meter/sec
ZDOT = 6591
393845 ZDOT = 2009
056844
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 10293
82158928
00016717 00000-0 10270-3 0 9083
2 25544 51
6456 307
8035 0005552 116
7440 243
4290 15
71783906 3234
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
82158928 = yrday
fracday
Element set: 908
Inclination: 51
6456 deg
RA of node: 307
8035 deg
Eccentricity:
0005552
Arg of perigee: 116
7440 deg
Mean anomaly: 243
4290 deg
Mean motion: 15
71783906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 311
Coasting Arc #10 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2010/294/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4227853
41 A = 6737963
39 meter
Y = 5129608
83 meter E =
0014922
Z = -1067323
09 I = 51
37688
XDOT = -3159
926375 Wp = 134
42098
YDOT = -3817
358190 meter/sec RA = 302
12523 deg
ZDOT = -5890
310587 TA = 57
28659
MA = 57
14280
Ha = 195
357 n
mi
Hp = 185
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13870910
13 X = -4279714
42
Y = 16829425
29 feet Y = 5082040
38 meter
Z = -3501716
19 Z = -1087988
89
XDOT = -10367
212515 XDOT = -3088
390292
YDOT = -12524
141043 feet/sec YDOT = -3852
294838 meter/sec
ZDOT = -19325
165968 ZDOT = -5905
487866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21382168
71 X = -6517285
02
Y = 4224609
82 feet Y = 1287661
07 meter
Z = -3584585
45 Z = -1092581
64
XDOT = 327
343515 XDOT = 99
774303
YDOT = -14626
560240 feet/sec YDOT = -4458
175561 meter/sec
ZDOT = -19385
964959 ZDOT = -5908
842120
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 10294
83884552
00016717 00000-0 10270-3 0 9095
2 25544 51
6457 302
5964 0005575 122
0067 238
1638 15
71786531 3399
Satellite: ISS
Catalog Number: 25544
Epoch time: 10294
83884552 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 302
5964 deg
Eccentricity:
0005575
Arg of perigee: 122
0067 deg
Mean anomaly: 238
1638 deg
Mean motion: 15
71786531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 328
Coasting Arc #11 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2010/295/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3523346
77 A = 6726184
98 meter
Y = 2315526
23 meter E =
0007306
Z = 5234658
07 I = 51
32289
XDOT = -3783
482287 Wp = 107
39661
YDOT = 6697
471666 meter/sec RA = 296
97141 deg
ZDOT = -417
683032 TA = 346
57615
MA = 346
59557
Ha = 195
050 n
mi
Hp = 185
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11559536
66 X = 3471762
49
Y = 7596870
84 feet Y = 2354638
29 meter
Z = 17174075
04 Z = 5251649
56
XDOT = -12412
999629 XDOT = -3856
064368
YDOT = 21973
332237 feet/sec YDOT = 6654
756640 meter/sec
ZDOT = -1370
351154 ZDOT = -436
240413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4263337
17 X = 1299465
17
Y = 13069666
35 feet Y = 3983634
30 meter
Z = 17242156
64 Z = 5255409
34
XDOT = -22414
542759 XDOT = -6831
952633
YDOT = 9210
442823 feet/sec YDOT = 2807
342972 meter/sec
ZDOT = -1444
780534 ZDOT = -440
369107
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 10295
85607777
00016717 00000-0 10270-3 0 9102
2 25544 51
6455 297
3894 0005434 124
9051 235
2622 15
71885408 3550
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
85607777 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 297
3894 deg
Eccentricity:
0005434
Arg of perigee: 124
9051 deg
Mean anomaly: 235
2622 deg
Mean motion: 15
71885408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 326
Coasting Arc #12 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2010/296/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2255389
63 A = 6738121
25 meter
Y = -6337739
24 meter E =
0013191
Z = -329030
04 I = 51
35076
XDOT = 4628
154684 Wp = 66
82143
YDOT = 1345
763645 meter/sec RA = 291
83059 deg
ZDOT = 5998
140794 TA = 289
59222
MA = 289
73457
Ha = 195
126 n
mi
Hp = 185
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7399572
27 X = 2327690
19
Y = -20793107
73 feet Y = -6312113
87 meter
Z = -1079494
89 Z = -317897
18
XDOT = 15184
234529 XDOT = 4583
623344
YDOT = 4415
235057 feet/sec YDOT = 1397
269677 meter/sec
ZDOT = 19678
939613 ZDOT = 6020
516842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18512435
97 X = 5642590
48
Y = -12020447
56 feet Y = -3663832
41 meter
Z = -1034825
12 Z = -315414
70
XDOT = 8411
010143 XDOT = 2563
675892
YDOT = 11309
409607 feet/sec YDOT = 3447
108048 meter/sec
ZDOT = 19768
609616 ZDOT = 6025
472211
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 10296
80971567
00016717 00000-0 10270-3 0 9110
2 25544 51
6458 292
5075 0005449 128
0579 232
1076 15
71896228 3705
Satellite: ISS
Catalog Number: 25544
Epoch time: 10296
80971567 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 292
5075 deg
Eccentricity:
0005449
Arg of perigee: 128
0579 deg
Mean anomaly: 232
1076 deg
Mean motion: 15
71896228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 329
Coasting Arc #13 (Orbit 385)
---------------------------------------
Vector Time (GMT): 2010/297/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4324445
83 A = 6726393
73 meter
Y = 7825
94 meter E =
0018314
Z = -5167560
50 I = 51
30142
XDOT = 1313
783401 Wp = 94
30090
YDOT = -7488
623750 meter/sec RA = 286
70075 deg
ZDOT = -1115
529797 TA = 165
00646
MA = 164
95210
Ha = 194
978 n
mi
Hp = 185
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14187814
39 X = -4299108
09
Y = 25675
67 feet Y = -40391
00 meter
Z = -16953938
66 Z = -5188507
75
XDOT = 4310
312995 XDOT = 1402
844143
YDOT = -24568
975557 feet/sec YDOT = -7473
434282 meter/sec
ZDOT = -3659
874663 ZDOT = -1108
930818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11351331
61 X = -3459885
88
Y = -8341953
33 feet Y = -2542627
37 meter
Z = -17037894
75 Z = -5193150
32
XDOT = 17462
368360 XDOT = 5322
529876
YDOT = -16372
755308 feet/sec YDOT = -4990
415818 meter/sec
ZDOT = -3633
366629 ZDOT = -1107
450148
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 10297
82690635
00016717 00000-0 10270-3 0 9128
2 25544 51
6458 287
2999 0005358 131
4901 228
6722 15
71937491 3860
Satellite: ISS
Catalog Number: 25544
Epoch time: 10297
82690635 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 287
2999 deg
Eccentricity:
0005358
Arg of perigee: 131
4901 deg
Mean anomaly: 228
6722 deg
Mean motion: 15
71937491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 386
Checksum: 342
Coasting Arc #14 (Orbit 401)
---------------------------------------
Vector Time (GMT): 2010/298/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -20301
80 A = 6736975
23 meter
Y = 6532169
58 meter E =
0019396
Z = 1607087
75 I = 51
32946
XDOT = -4961
290839 Wp = 121
94709
YDOT = 1402
669197 meter/sec RA = 281
53357 deg
ZDOT = -5723
625420 TA = 40
23523
MA = 40
09182
Ha = 194
996 n
mi
Hp = 185
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -66606
97 X = -101151
39
Y = 21431002
57 feet Y = 6531490
49 meter
Z = 5272597
62 Z = 1606792
79
XDOT = -16277
200916 XDOT = -4948
801871
YDOT = 4601
933062 feet/sec YDOT = 1347
258941 meter/sec
ZDOT = -18778
298622 ZDOT = -5747
697713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12503048
08 X = -3810929
06
Y = 17406294
82 feet Y = 5305438
66 meter
Z = 5271364
41 Z = 1606711
87
XDOT = -14570
248842 XDOT = -4441
011847
YDOT = -4709
721452 feet/sec YDOT = -1435
523099 meter/sec
ZDOT = -18874
794508 ZDOT = -5753
037366
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 10298
84407651
00016717 00000-0 10270-3 0 9136
2 25544 51
6459 282
0928 0005528 135
5717 224
5889 15
71924776 4025
Satellite: ISS
Catalog Number: 25544
Epoch time: 10298
84407651 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 282
0928 deg
Eccentricity:
0005528
Arg of perigee: 135
5717 deg
Mean anomaly: 224
5889 deg
Mean motion: 15
71924776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 402
Checksum: 335
Coasting Arc #15 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2010/299/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4102489
63 A = 6728054
46 meter
Y = -2410895
87 meter E =
0012526
Z = 4750970
51 I = 51
29484
XDOT = 1246
283045 Wp = 127
55152
YDOT = 7160
986652 meter/sec RA = 276
42480 deg
ZDOT = 2545
570847 TA = 297
32564
MA = 297
45311
Ha = 194
761 n
mi
Hp = 185
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13459611
64 X = 4106063
86
Y = -7909763
37 feet Y = -2364999
49 meter
Z = 15587173
59 Z = 4770909
54
XDOT = 4088
855135 XDOT = 1153
748700
YDOT = 23494
050695 feet/sec YDOT = 7174
405892 meter/sec
ZDOT = 8351
610389 ZDOT = 2551
400836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15496806
50 X = 4723426
62
Y = 1037301
85 feet Y = 316169
60 meter
Z = 15667114
47 Z = 4775336
49
XDOT = -9881
183445 XDOT = -3011
784714
YDOT = 20530
075223 feet/sec YDOT = 6257
566928 meter/sec
ZDOT = 8374
926006 ZDOT = 2552
677447
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 10299
86122203
00016717 00000-0 10270-3 0 9147
2 25544 51
6458 276
8850 0005366 138
7205 221
4363 15
71969027 4184
Satellite: ISS
Catalog Number: 25544
Epoch time: 10299
86122203 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 276
8850 deg
Eccentricity:
0005366
Arg of perigee: 138
7205 deg
Mean anomaly: 221
4363 deg
Mean motion: 15
71969027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 315
Coasting Arc #16 (Orbit 432)
---------------------------------------
Vector Time (GMT): 2010/300/19:25:06
900
Vector Time (MET): N/A
Weight (LBS) : 826941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2109932
82 A = 6734420
75 meter
Y = -5759168
61 meter E =
0007405
Z = -2789553
53 I = 51
31383
XDOT = 4162
818356 Wp = 104
86292
YDOT = -3985
951993 meter/sec RA = 271
23678 deg
ZDOT = 5089
966158 TA = 223
10639
MA = 223
16440
Ha = 194
653 n
mi
Hp = 185
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6922351
78 X = -2031824
48
Y = -18894910
13 feet Y = -5782326
34 meter
Z = -9152078
52 Z = -2799614
24
XDOT = 13657
540538 XDOT = 4182
353957
YDOT = -13077
270319 feet/sec YDOT = -3939
291771 meter/sec
ZDOT = 16699
364037 ZDOT = 5110
236900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4687257
36 X = 1428676
04
Y = -19550628
63 feet Y = -5959031
61 meter
Z = -9192369
81 Z = -2801834
32
XDOT = 17095
188813 XDOT = 5210
613550
YDOT = -3776
964933 feet/sec YDOT = -1151
218912 meter/sec
ZDOT = 16780
649080 ZDOT = 5114
741839
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 10300
81477451
00016717 00000-0 10270-3 0 9154
2 25544 51
6451 272
0025 0005202 144
0201 216
1312 15
72016209 4332
Satellite: ISS
Catalog Number: 25544
Epoch time: 10300
81477451 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 272
0025 deg
Eccentricity:
0005202
Arg of perigee: 144
0201 deg
Mean anomaly: 216
1312 deg
Mean motion: 15
72016209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 433
Checksum: 240
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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