Date:
June 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
156/03:22:07
072 -1
3 14
0 14
0
N/A -12
0 0
0 190
9
000/00:04:10
144 -7
1 0
1 187
6
158/23:59:56
243 -0
7 2
6 2
6
N/A -2
2 0
0 191
2
000/00:09:52
486 -1
2 0
2 188
8
159/01:30:56
154 -0
8 2
7 2
7
N/A -2
2 0
0 191
0
000/00:09:52
307 -1
3 0
2 190
2
Coasting Arc #1 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3759909
11 A = 6727767
21 meter
Y = 5398886
29 meter E =
0008720
Z = -1419713
34 I = 51
35730
XDOT = -3323
196815 Wp = 77
16511
YDOT = -3828
875202 meter/sec RA = 294
91948 deg
ZDOT = -5787
395930 TA = 118
50300
MA = 118
41516
Ha = 190
819 n
mi
Hp = 179
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12335659
81 X = -3813104
26
Y = 17712881
54 feet Y = 5356543
46 meter
Z = -4657852
16 Z = -1438107
67
XDOT = -10902
876689 XDOT = -3252
020474
YDOT = -12561
926516 feet/sec YDOT = -3865
638607 meter/sec
ZDOT = -18987
519455 ZDOT = -5803
367559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13056200
81 X = 3979530
01
Y = 17168644
54 feet Y = 5233002
86 meter
Z = -4731123
27 Z = -1442046
37
XDOT = -14025
079983 XDOT = -4274
844379
YDOT = 5440
631745 feet/sec YDOT = 1658
304556 meter/sec
ZDOT = -19051
143468 ZDOT = -5806
788529
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 10155
52897141
00016717 00000-0 10270-3 0 9006
2 25544 51
6461 295
4165 0009326 21
1728 338
9820 15
75229238 21480
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
52897141 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 295
4165 deg
Eccentricity:
0009326
Arg of perigee: 21
1728 deg
Mean anomaly: 338
9820 deg
Mean motion: 15
75229238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 310
Coasting Arc #2 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2010/156/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4630883
20 A = 6727535
07 meter
Y = 2046383
32 meter E =
0006720
Z = -4436715
90 I = 51
32620
XDOT = -1
756190 Wp = 38
45762
YDOT = -6986
913755 meter/sec RA = 291
61926 deg
ZDOT = -3218
227638 TA = 199
12693
MA = 199
15217
Ha = 190
867 n
mi
Hp = 187
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15193186
36 X = -4631869
20
Y = 6713856
03 feet Y = 1994592
95 meter
Z = -14556154
52 Z = -4459215
02
XDOT = -5
761778 XDOT = 92
006505
YDOT = -22922
945392 feet/sec YDOT = -6986
408819 meter/sec
ZDOT = -10558
489627 ZDOT = -3218
009114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13971768
73 X = -4258595
11
Y = -8836362
61 feet Y = -2693323
32 meter
Z = -14645776
98 Z = -4464032
82
XDOT = 18451
700747 XDOT = 5624
078388
YDOT = -11662
654319 feet/sec YDOT = -3554
777036 meter/sec
ZDOT = -10557
626552 ZDOT = -3217
964573
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 10156
16339712
00016717 00000-0 10270-3 0 9013
2 25544 51
6489 292
1590 0005184 291
0460 69
0148 15
72595514 21581
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
16339712 = yrday
fracday
Element set: 901
Inclination: 51
6489 deg
RA of node: 292
1590 deg
Eccentricity:
0005184
Arg of perigee: 291
0460 deg
Mean anomaly: 69
0148 deg
Mean motion: 15
72595514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 308
Coasting Arc #3 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2010/157/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 921047
87 A = 6731806
92 meter
Y = 5861309
35 meter E =
0008348
Z = 3174701
77 I = 51
32979
XDOT = -4990
510639 Wp = 80
52712
YDOT = 3383
087933 meter/sec RA = 286
42396 deg
ZDOT = -4786
136046 TA = 62
29714
MA = 62
21247
Ha = 191
013 n
mi
Hp = 187
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3021810
60 X = 840014
95
Y = 19230017
57 feet Y = 5871155
66 meter
Z = 10415688
21 Z = 3178980
01
XDOT = -16373
066401 XDOT = -5004
719668
YDOT = 11099
369860 feet/sec YDOT = 3327
202101 meter/sec
ZDOT = -15702
546083 ZDOT = -4810
414315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14121452
89 X = -4304218
84
Y = 13384840
12 feet Y = 4079699
27 meter
Z = 10432741
69 Z = 3179899
67
XDOT = -17418
578620 XDOT = -5309
182763
YDOT = -6031
762642 feet/sec YDOT = -1838
481253 meter/sec
ZDOT = -15799
251618 ZDOT = -4815
611893
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 10157
18014300
00016717 00000-0 10270-3 0 9020
2 25544 51
6482 286
9492 0005161 294
9023 65
1603 15
72589072 21741
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
18014300 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 286
9492 deg
Eccentricity:
0005161
Arg of perigee: 294
9023 deg
Mean anomaly: 65
1603 deg
Mean motion: 15
72589072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 295
Coasting Arc #4 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2010/158/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3947381
67 A = 6729419
17 meter
Y = -3798808
00 meter E =
0006392
Z = 3902013
79 I = 51
31524
XDOT = 2031
731734 Wp = 84
38562
YDOT = 6245
477311 meter/sec RA = 281
32674 deg
ZDOT = 4019
904815 TA = 323
61946
MA = 323
66289
Ha = 191
033 n
mi
Hp = 187
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12950727
26 X = 3970611
76
Y = -12463280
86 feet Y = -3754536
56 meter
Z = 12801882
52 Z = 3921246
41
XDOT = 6665
786529 XDOT = 1942
214483
YDOT = 20490
411125 feet/sec YDOT = 6267
696396 meter/sec
ZDOT = 13188
664092 ZDOT = 4029
558312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17633973
96 X = 5374835
26
Y = 3182836
81 feet Y = 970128
66 meter
Z = 12878486
50 Z = 3925362
68
XDOT = -12563
807015 XDOT = -3829
448378
YDOT = 16021
284955 feet/sec YDOT = 4883
287654 meter/sec
ZDOT = 13227
134514 ZDOT = 4031
630600
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 10158
19687126
00016717 00000-0 10270-3 0 9035
2 25544 51
6488 281
7387 0005271 299
8955 60
1684 15
72617941 21902
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
19687126 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 281
7387 deg
Eccentricity:
0005271
Arg of perigee: 299
8955 deg
Mean anomaly: 60
1684 deg
Mean motion: 15
72617941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 341
Coasting Arc #5 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:04:52
486
Vector Time (MET): N/A
Weight (LBS) : 814706
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192431
14 A = 6726894
57 meter
Y = 1908205
78 meter E =
0007881
Z = -4909252
80 I = 51
29622
XDOT = -837
601852 Wp = 49
94566
YDOT = -7341
913965 meter/sec RA = 276
88174 deg
ZDOT = -2135
735384 TA = 199
19741
MA = 199
22712
Ha = 191
194 n
mi
Hp = 188
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13754695
34 X = -4189608
86
Y = 6260517
64 feet Y = 1861339
88 meter
Z = -16106472
44 Z = -4929612
83
XDOT = -2748
037573 XDOT = -745
065832
YDOT = -24087
644243 feet/sec YDOT = -7350
762875 meter/sec
ZDOT = -7007
005854 ZDOT = -2139
580619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2954284
79 X = -900466
00
Y = -14732238
83 feet Y = -4490386
40 meter
Z = -16187573
00 Z = -4933972
25
XDOT = 22991
060413 XDOT = 7007
675214
YDOT = 3115
421031 feet/sec YDOT = 949
580330 meter/sec
ZDOT = -7022
344323 ZDOT = -2140
410550
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 10159
02295497
00016717 00000-0 10270-3 0 9045
2 25544 51
6470 277
5048 0006344 284
9612 75
0848 15
72150099 22035
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02295497 = yrday
fracday
Element set: 904
Inclination: 51
6470 deg
RA of node: 277
5048 deg
Eccentricity:
0006344
Arg of perigee: 284
9612 deg
Mean anomaly: 75
0848 deg
Mean motion: 15
72150099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 314
Coasting Arc #6 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150450
80 A = 6728655
66 meter
Y = 2166261
72 meter E =
0005468
Z = -4837557
98 I = 51
29824
XDOT = -1054
089997 Wp = 45
60229
YDOT = -7251
783263 meter/sec RA = 276
55861 deg
ZDOT = -2340
841727 TA = 201
43734
MA = 201
46025
Ha = 191
034 n
mi
Hp = 190
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13616964
56 X = -4150865
55
Y = 7107157
88 feet Y = 2119847
18 meter
Z = -15871253
22 Z = -4857721
90
XDOT = -3458
300516 XDOT = -961
549360
YDOT = -23791
939840 feet/sec YDOT = -7263
053020 meter/sec
ZDOT = -7679
926925 ZDOT = -2345
738662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9247316
66 X = -2818582
12
Y = -12159958
19 feet Y = -3706355
26 meter
Z = -15951571
94 Z = -4862039
13
XDOT = 22012
168626 XDOT = 6709
308997
YDOT = -6630
255840 feet/sec YDOT = -2020
901980 meter/sec
ZDOT = -7699
454834 ZDOT = -2346
793833
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 10159
08652384
00016717 00000-0 10270-3 0 9054
2 25544 51
6482 277
1799 0007721 272
0285 87
9992 15
71640092 22040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08652384 = yrday
fracday
Element set: 905
Inclination: 51
6482 deg
RA of node: 277
1799 deg
Eccentricity:
0007721
Arg of perigee: 272
0285 deg
Mean anomaly: 87
9992 deg
Mean motion: 15
71640092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 328
Coasting Arc #7 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2041004
15 A = 6735685
99 meter
Y = 5809399
36 meter E =
0005918
Z = 2722895
48 I = 51
31930
XDOT = -4207
766651 Wp = 107
72061
YDOT = 3889
777708 meter/sec RA = 271
37626 deg
ZDOT = -5137
568653 TA = 41
07625
MA = 41
03170
Ha = 191
492 n
mi
Hp = 190
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6696207
85 X = 1962663
17
Y = 19059709
19 feet Y = 5831784
67 meter
Z = 8933384
14 Z = 2732621
37
XDOT = -13805
008699 XDOT = -4225
992356
YDOT = 12761
737886 feet/sec YDOT = 3842
622780 meter/sec
ZDOT = -16855
540200 ZDOT = -5158
054018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17527606
07 X = -5342414
33
Y = 10010028
38 feet Y = 3051056
65 meter
Z = 8972147
09 Z = 2734710
43
XDOT = -14318
021113 XDOT = -4364
132835
YDOT = -9868
239815 feet/sec YDOT = -3007
839495 meter/sec
ZDOT = -16937
136857 ZDOT = -5162
439314
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 10160
10388864
00016717 00000-0 10270-3 0 9069
2 25544 51
6480 271
9745 0007753 275
7419 84
2859 15
71630606 22205
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10388864 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 271
9745 deg
Eccentricity:
0007753
Arg of perigee: 275
7419 deg
Mean anomaly: 84
2859 deg
Mean motion: 15
71630606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 318
Coasting Arc #8 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2966335
10 A = 6731639
33 meter
Y = -4476157
21 meter E =
0002879
Z = 4057979
40 I = 51
30698
XDOT = 3433
504755 Wp = 111
60155
YDOT = 5735
599635 meter/sec RA = 266
28346 deg
ZDOT = 3813
591365 TA = 298
97328
MA = 299
00214
Ha = 191
774 n
mi
Hp = 190
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9732070
54 X = 2996454
61
Y = -14685555
16 feet Y = -4442818
16 meter
Z = 13313580
72 Z = 4072462
49
XDOT = 11264
779379 XDOT = 3350
587043
YDOT = 18817
584104 feet/sec YDOT = 5773
530876 meter/sec
ZDOT = 12511
782695 ZDOT = 3830
071131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16314916
42 X = 4972786
53
Y = 6531682
48 feet Y = 1990856
82 meter
Z = 13371267
14 Z = 4075562
22
XDOT = -15732
756406 XDOT = -4795
344152
YDOT = 13528
164326 feet/sec YDOT = 4123
384487 meter/sec
ZDOT = 12577
455627 ZDOT = 3833
608475
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 10161
12123751
00016717 00000-0 10270-3 0 9075
2 25544 51
6486 266
7684 0007785 280
5736 79
4549 15
71660772 22362
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12123751 = yrday
fracday
Element set: 907
Inclination: 51
6486 deg
RA of node: 266
7684 deg
Eccentricity:
0007785
Arg of perigee: 280
5736 deg
Mean anomaly: 79
4549 deg
Mean motion: 15
71660772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 331
Coasting Arc #9 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2010/162/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3770450
55 A = 6732153
13 meter
Y = -4008748
56 meter E =
0001283
Z = -3876378
12 I = 51
31270
XDOT = 2328
569812 Wp = 274
87513
YDOT = -6112
045158 meter/sec RA = 261
09111 deg
ZDOT = 4054
775100 TA = 37
58538
MA = 37
57642
Ha = 192
019 n
mi
Hp = 190
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12370244
58 X = -3706512
79
Y = -13152062
22 feet Y = -4050553
76 meter
Z = -12717775
98 Z = -3894540
65
XDOT = 7639
664739 XDOT = 2377
045139
YDOT = -20052
641596 feet/sec YDOT = -6085
735435 meter/sec
ZDOT = 13303
067914 ZDOT = 4066
204020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10183238
62 X = 3103851
13
Y = -14847731
05 feet Y = -4525588
43 meter
Z = -12790154
46 Z = -3898439
08
XDOT = 20129
931532 XDOT = 6135
603131
YDOT = 2304
312489 feet/sec YDOT = 702
354447 meter/sec
ZDOT = 13348
584145 ZDOT = 4068
648447
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 10162
07498806
00016717 00000-0 10270-3 0 9087
2 25544 51
6490 261
8881 0007907 284
6790 75
3496 15
71694308 22518
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
07498806 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 261
8881 deg
Eccentricity:
0007907
Arg of perigee: 284
6790 deg
Mean anomaly: 75
3496 deg
Mean motion: 15
71694308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 339
Coasting Arc #10 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2010/163/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -964820
34 A = 6734896
70 meter
Y = 5964959
76 meter E =
0003511
Z = -2972594
18 I = 51
32781
XDOT = -4899
715830 Wp = 284
44845
YDOT = -3263
963799 meter/sec RA = 256
00089 deg
ZDOT = -4953
576055 TA = 289
98145
MA = 290
01926
Ha = 192
384 n
mi
Hp = 190
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3165421
06 X = -1017009
46
Y = 19570077
94 feet Y = 5953879
37 meter
Z = -9752605
58 Z = -2977406
85
XDOT = -16075
183168 XDOT = -4838
789681
YDOT = -10708
542648 feet/sec YDOT = -3318
413663 meter/sec
ZDOT = -16251
889944 ZDOT = -4977
231742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19755310
01 X = -6021418
49
Y = 1536742
16 feet Y = 468399
01 meter
Z = -9771760
66 Z = -2978432
65
XDOT = 6803
984717 XDOT = 2073
854542
YDOT = -16593
538214 feet/sec YDOT = -5057
710448 meter/sec
ZDOT = -16346
163625 ZDOT = -4982
310673
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 10163
09230815
00016717 00000-0 10270-3 0 9095
2 25544 51
6491 256
6827 0008032 288
0693 71
9594 15
71695575 22676
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
09230815 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 256
6827 deg
Eccentricity:
0008032
Arg of perigee: 288
0693 deg
Mean anomaly: 71
9594 deg
Mean motion: 15
71695575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 335
Coasting Arc #11 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2010/164/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4543210
04 A = 6728821
95 meter
Y = 1604734
23 meter E =
0006851
Z = 4700456
63 I = 51
31638
XDOT = 234
754975 Wp = 354
19305
YDOT = 7207
662046 meter/sec RA = 250
81549 deg
ZDOT = -2681
216040 TA = 122
35528
MA = 122
28894
Ha = 192
510 n
mi
Hp = 190
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14905544
74 X = 4502093
94
Y = 5264876
09 feet Y = 1655308
23 meter
Z = 15421445
63 Z = 4722428
05
XDOT = 770
193487 XDOT = 167
165029
YDOT = 23647
185189 feet/sec YDOT = 7209
909865 meter/sec
ZDOT = -8796
640551 ZDOT = -2680
238255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1400187
90 X = -426777
27
Y = 15659666
03 feet Y = 4773066
21 meter
Z = 15509013
62 Z = 4727147
35
XDOT = -21550
940660 XDOT = -6568
726713
YDOT = 6801
783262 feet/sec YDOT = 2073
183538 meter/sec
ZDOT = -8792
711423 ZDOT = -2680
018442
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 10164
10961219
00016717 00000-0 10270-3 0 9109
2 25544 51
6488 251
4769 0008099 293
2884 66
7425 15
71777997 22835
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
10961219 = yrday
fracday
Element set: 910
Inclination: 51
6488 deg
RA of node: 251
4769 deg
Eccentricity:
0008099
Arg of perigee: 293
2884 deg
Mean anomaly: 66
7425 deg
Mean motion: 15
71777997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 348
Coasting Arc #12 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2010/165/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1399801
59 A = 6737359
69 meter
Y = -6365042
97 meter E =
0011292
Z = 1678700
91 I = 51
35530
XDOT = 5165
447313 Wp = 29
06141
YDOT = 368
669508 meter/sec RA = 245
71157 deg
ZDOT = 5698
817761 TA = 349
56352
MA = 349
58694
Ha = 192
749 n
mi
Hp = 189
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4592524
90 X = -1336677
28
Y = -20882686
92 feet Y = -6380343
78 meter
Z = 5507548
91 Z = 1672052
73
XDOT = 16947
005619 XDOT = 5133
257164
YDOT = 1209
545629 feet/sec YDOT = 426
251475 meter/sec
ZDOT = 18696
908665 ZDOT = 5723
833295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18897067
19 X = 5759826
08
Y = -10018498
82 feet Y = -3053638
44 meter
Z = 5481015
07 Z = 1670613
39
XDOT = 2586
072956 XDOT = 788
235037
YDOT = 15172
701756 feet/sec YDOT = 4624
639495 meter/sec
ZDOT = 18796
615216 ZDOT = 5729
208318
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 10165
12690369
00016717 00000-0 10270-3 0 9118
2 25544 51
6483 246
2704 0008108 297
4801 62
5537 15
71757470 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
12690369 = yrday
fracday
Element set: 911
Inclination: 51
6483 deg
RA of node: 246
2704 deg
Eccentricity:
0008108
Arg of perigee: 297
4801 deg
Mean anomaly: 62
5537 deg
Mean motion: 15
71757470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 318
Coasting Arc #13 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2010/166/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4217593
14 A = 6726782
20 meter
Y = 932760
62 meter E =
0007526
Z = -5162599
06 I = 51
33293
XDOT = -2929
482753 Wp = 74
29932
YDOT = -7022
989074 meter/sec RA = 240
54685 deg
ZDOT = 1127
726892 TA = 206
50336
MA = 206
54187
Ha = 192
807 n
mi
Hp = 189
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13837247
84 X = -4202631
21
Y = 3060238
24 feet Y = 885681
59 meter
Z = -16937660
97 Z = -5183051
46
XDOT = -9611
163888 XDOT = -2856
210940
YDOT = -23041
302735 feet/sec YDOT = -7055
338818 meter/sec
ZDOT = 3699
891378 ZDOT = 1113
672259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6819819
04 X = -2078680
84
Y = -12310824
13 feet Y = -3752339
19 meter
Z = -17019181
02 Z = -5187446
38
XDOT = 18478
454071 XDOT = 5632
232801
YDOT = -15258
699268 feet/sec YDOT = -4650
851537 meter/sec
ZDOT = 3643
816646 ZDOT = 1110
635314
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 10166
08059966
00016717 00000-0 10270-3 0 9127
2 25544 51
6475 241
3894 0008165 300
9784 59
0576 15
71799161 23141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
08059966 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 241
3894 deg
Eccentricity:
0008165
Arg of perigee: 300
9784 deg
Mean anomaly: 59
0576 deg
Mean motion: 15
71799161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 332
Coasting Arc #14 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2010/167/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3626364
31 A = 6738508
27 meter
Y = 5668944
79 meter E =
0004218
Z = -289982
14 I = 51
38761
XDOT = -4187
281325 Wp = 162
98418
YDOT = 2372
819579 meter/sec RA = 235
42121 deg
ZDOT = -6002
992300 TA = 20
17414
MA = 20
15748
Ha = 193
078 n
mi
Hp = 189
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11897520
69 X = 3564112
29
Y = 18598900
22 feet Y = 5709148
93 meter
Z = -951384
98 Z = -272515
74
XDOT = -13737
799624 XDOT = -4184
342251
YDOT = 7784
841138 feet/sec YDOT = 2326
012293 meter/sec
ZDOT = -19694
856626 ZDOT = -6023
326402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14184195
68 X = -4323342
84
Y = 16923546
11 feet Y = 5158296
86 meter
Z = -881703
63 Z = -268743
27
XDOT = -10269
829897 XDOT = -3130
244153
YDOT = -9633
007094 feet/sec YDOT = -2936
140562 meter/sec
ZDOT = -19775
899129 ZDOT = -6027
694054
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 10167
09786297
00016717 00000-0 10270-3 0 9134
2 25544 51
6472 236
1836 0008093 303
9957 56
0436 15
71765589 23308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
09786297 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 236
1836 deg
Eccentricity:
0008093
Arg of perigee: 303
9957 deg
Mean anomaly: 56
0436 deg
Mean motion: 15
71765589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 336
Coasting Arc #15 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2010/168/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2889382
92 A = 6726413
82 meter
Y = -3076746
10 meter E =
0005640
Z = 5240343
66 I = 51
36497
XDOT = 5189
747245 Wp = 317
49321
YDOT = 5662
658602 meter/sec RA = 230
28420 deg
ZDOT = 467
601994 TA = 128
07071
MA = 128
01981
Ha = 193
174 n
mi
Hp = 189
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9479602
74 X = 2898116
48
Y = -10094311
36 feet Y = -3044387
17 meter
Z = 17192728
55 Z = 5254400
97
XDOT = 17026
729805 XDOT = 5123
769150
YDOT = 18578
276252 feet/sec YDOT = 5720
324482 meter/sec
ZDOT = 1534
127276 ZDOT = 492
654075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12537808
11 X = 3821523
91
Y = 5712457
61 feet Y = 1741157
08 meter
Z = 17248742
01 Z = 5257416
56
XDOT = -11840
602411 XDOT = -3609
015615
YDOT = 21097
253829 feet/sec YDOT = 6430
442967 meter/sec
ZDOT = 1634
066768 ZDOT = 498
063551
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 10168
11511022
00016717 00000-0 10270-3 0 9141
2 25544 51
6467 230
9761 0008184 309
1030 50
9404 15
71814235 23460
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
11511022 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 230
9761 deg
Eccentricity:
0008184
Arg of perigee: 309
1030 deg
Mean anomaly: 50
9404 deg
Mean motion: 15
71814235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 275
Coasting Arc #16 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2010/169/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5264596
06 A = 6737793
37 meter
Y = -4043752
56 meter E =
0013143
Z = -1101277
70 I = 51
42275
XDOT = 2192
260969 Wp = 358
74048
YDOT = -4454
403606 meter/sec RA = 225
13195 deg
ZDOT = 5887
627169 TA = 349
17556
MA = 349
20382
Ha = 193
363 n
mi
Hp = 188
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17272296
80 X = -5213637
03
Y = -13266904
72 feet Y = -4102339
36 meter
Z = -3613115
83 Z = -1126729
67
XDOT = 7192
457248 XDOT = 2213
307110
YDOT = -14614
185060 feet/sec YDOT = -4429
771450 meter/sec
ZDOT = 19316
362102 ZDOT = 5898
327717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6789091
70 X = 2069315
15
Y = -20676248
44 feet Y = -6302120
52 meter
Z = -3714645
09 Z = -1132223
82
XDOT = 14626
755116 XDOT = 4458
234959
YDOT = 1331
390807 feet/sec YDOT = 405
807918 meter/sec
ZDOT = 19358
975680 ZDOT = 5900
615787
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 10169
06876654
00016717 00000-0 10270-3 0 9152
2 25544 51
6457 226
0939 0008366 312
6986 47
3470 15
71833604 23614
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
06876654 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 226
0939 deg
Eccentricity:
0008366
Arg of perigee: 312
6986 deg
Mean anomaly: 47
3470 deg
Mean motion: 15
71833604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 330
Coasting Arc #17 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2010/170/01:35:52
307
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -816129
31 A = 6727583
33 meter
Y = 4482176
58 meter E =
0011496
Z = -4958816
38 I = 51
40963
XDOT = -6581
630749 Wp = 35
61887
YDOT = -3431
255632 meter/sec RA = 220
02379 deg
ZDOT = -2011
373352 TA = 214
79349
MA = 214
86871
Ha = 193
526 n
mi
Hp = 188
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2677589
59 X = -842100
15
Y = 14705303
74 feet Y = 4472905
48 meter
Z = -16269082
60 Z = -4962843
71
XDOT = -21593
276737 XDOT = -6533
001785
YDOT = -11257
400369 feet/sec YDOT = -3504
583228 meter/sec
ZDOT = -6598
993936 ZDOT = -2043
229153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14683722
55 X = -4475598
63
Y = 2698658
22 feet Y = 822551
03 meter
Z = -16285086
08 Z = -4963694
24
XDOT = 3247
533813 XDOT = 989
848306
YDOT = -23053
890126 feet/sec YDOT = -7026
825711 meter/sec
ZDOT = -6726
060500 ZDOT = -2050
103241
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 10170
08598699
00016717 00000-0 10270-3 0 9167
2 25544 51
6447 220
8866 0008317 316
4229 43
6275 15
71867423 23777
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
08598699 = yrday
fracday
Element set: 916
Inclination: 51
6447 deg
RA of node: 220
8866 deg
Eccentricity:
0008317
Arg of perigee: 316
4229 deg
Mean anomaly: 43
6275 deg
Mean motion: 15
71867423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 338
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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