Date:
June 9th 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
159/00:14:50
537 0
8 2
5 2
5
N/A -2
2 -0
1 192
1
000/00:09:41
074 0
8 0
2 189
2
159/01:48:37
850 0
8 1
9 1
9
N/A -1
6 -0
0 193
0
000/00:07:15
699 0
8 0
1 189
9
Coasting Arc #1 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2010/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 799347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3998810
59 A = 6724339
28 meter
Y = -1443190
00 meter E =
0009928
Z = -5218402
74 I = 51
29473
XDOT = 1796
285367 Wp = 85
87200
YDOT = -7447
539352 meter/sec RA = 279
45156 deg
ZDOT = 685
024958 TA = 190
67066
MA = 190
69174
Ha = 190
945 n
mi
Hp = 187
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13119457
33 X = -3957025
01
Y = -4734875
33 feet Y = -1487672
86 meter
Z = -17120743
91 Z = -5237727
87
XDOT = 5893
324694 XDOT = 1876
103825
YDOT = -24434
184226 feet/sec YDOT = -7427
006007 meter/sec
ZDOT = 2247
457210 ZDOT = 693
944468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7942871
47 X = -2420987
22
Y = 11349358
86 feet Y = 3459284
58 meter
Z = -17197730
18 Z = -5241868
16
XDOT = -21252
659617 XDOT = -6477
810651
YDOT = -11423
359751 feet/sec YDOT = -3481
840052 meter/sec
ZDOT = 2282
968694 ZDOT = 695
848858
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
51472515
00016717 00000-0 10270-3 0 9002
2 25544 51
6480 280
1107 0005261 293
4449 66
6160 15
72568775 21959
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
51472515 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 280
1107 deg
Eccentricity:
0005261
Arg of perigee: 293
4449 deg
Mean anomaly: 66
6160 deg
Mean motion: 15
72568775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 305
Coasting Arc #2 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:19:41
074
Vector Time (MET): N/A
Weight (LBS) : 799097
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2885820
81 A = 6729859
70 meter
Y = -4374017
39 meter E =
0001298
Z = -4223293
64 I = 51
30571
XDOT = 3572
770112 Wp = 62
67814
YDOT = -5804
890663 meter/sec RA = 276
79117 deg
ZDOT = 3572
176498 TA = 243
80888
MA = 243
82222
Ha = 192
092 n
mi
Hp = 189
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9467916
03 X = -2816178
99
Y = -14350450
75 feet Y = -4405898
46 meter
Z = -13855950
28 Z = -4237144
52
XDOT = 11721
686720 XDOT = 3620
062686
YDOT = -19044
916874 feet/sec YDOT = -5764
673822 meter/sec
ZDOT = 11719
739167 ZDOT = 3589
647434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15711593
16 X = 4788893
59
Y = -6869518
68 feet Y = -2093829
29 meter
Z = -13911138
78 Z = -4240115
10
XDOT = 16341
387584 XDOT = 4980
854936
YDOT = 13510
596779 feet/sec YDOT = 4118
029898 meter/sec
ZDOT = 11789
319766 ZDOT = 3593
384665
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
02311036
00016717 00000-0 10270-3 0 9010
2 25544 51
6474 277
5086 0007560 297
7172 62
3223 15
72074301 22032
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02311036 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 277
5086 deg
Eccentricity:
0007560
Arg of perigee: 297
7172 deg
Mean anomaly: 62
3223 deg
Mean motion: 15
72074301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 276
Coasting Arc #3 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2682362
84 A = 6731706
02 meter
Y = -4709924
82 meter E =
0002321
Z = -3989679
02 I = 51
30962
XDOT = 3767
904036 Wp = 329
75086
YDOT = -5455
777168 meter/sec RA = 276
45991 deg
ZDOT = 3908
424926 TA = 340
83089
MA = 340
83963
Ha = 192
976 n
mi
Hp = 189
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8800403
03 X = -2610114
84
Y = -15452509
25 feet Y = -4739516
15 meter
Z = -13089498
09 Z = -4002535
20
XDOT = 12361
889882 XDOT = 3809
644798
YDOT = -17899
531391 feet/sec YDOT = -5413
409309 meter/sec
ZDOT = 12822
916423 ZDOT = 3926
830388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12960505
09 X = 3950361
95
Y = -12120591
70 feet Y = -3694356
35 meter
Z = -13140725
26 Z = -4005293
06
XDOT = 19407
453012 XDOT = 5915
391678
YDOT = 6774
188911 feet/sec YDOT = 2064
772780 meter/sec
ZDOT = 12896
220806 ZDOT = 3930
768102
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
08667749
00016717 00000-0 10270-3 0 9022
2 25544 51
6487 277
1834 0009022 298
1274 61
8975 15
71721542 22040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08667749 = yrday
fracday
Element set: 902
Inclination: 51
6487 deg
RA of node: 277
1834 deg
Eccentricity:
0009022
Arg of perigee: 298
1274 deg
Mean anomaly: 61
8975 deg
Mean motion: 15
71721542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 326
Coasting Arc #4 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2405344
69 A = 6735113
61 meter
Y = 5615622
21 meter E =
0004519
Z = -2836144
04 I = 51
31957
XDOT = -3946
922518 Wp = 306
66068
YDOT = -4247
896939 meter/sec RA = 271
36803 deg
ZDOT = -5055
286196 TA = 265
98261
MA = 266
03427
Ha = 193
253 n
mi
Hp = 189
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7891550
83 X = -2454183
14
Y = 18423957
39 feet Y = 5588451
55 meter
Z = -9304934
51 Z = -2847947
21
XDOT = -12949
220860 XDOT = -3874
570379
YDOT = -13936
669748 feet/sec YDOT = -4291
628515 meter/sec
ZDOT = -16585
584634 ZDOT = -5074
285503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19805282
82 X = -6036650
20
Y = -2931314
80 feet Y = -893464
75 meter
Z = -9351938
43 Z = -2850470
83
XDOT = 10027
517818 XDOT = 3056
387431
YDOT = -14509
226763 feet/sec YDOT = -4422
412317 meter/sec
ZDOT = -16661
285790 ZDOT = -5078
359909
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
10398191
00016717 00000-0 10270-3 0 9030
2 25544 51
6493 271
9776 0009124 301
9248 58
1027 15
71733156 22200
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10398191 = yrday
fracday
Element set: 903
Inclination: 51
6493 deg
RA of node: 271
9776 deg
Eccentricity:
0009124
Arg of perigee: 301
9248 deg
Mean anomaly: 58
1027 deg
Mean motion: 15
71733156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 294
Coasting Arc #5 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3998303
21 A = 6728532
44 meter
Y = 2573011
09 meter E =
0009148
Z = 4765510
51 I = 51
29818
XDOT = -1552
064739 Wp = 352
96695
YDOT = 7099
977123 meter/sec RA = 266
18288 deg
ZDOT = -2522
807823 TA = 121
92513
MA = 121
83613
Ha = 193
366 n
mi
Hp = 189
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13117792
69 X = 3946083
84
Y = 8441637
43 feet Y = 2617429
73 meter
Z = 15634877
00 Z = 4784808
15
XDOT = -5092
075915 XDOT = -1619
087088
YDOT = 23293
888198 feet/sec YDOT = 7082
246690 meter/sec
ZDOT = -8276
928552 ZDOT = -2530
509479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4626069
70 X = -1410026
04
Y = 14816442
81 feet Y = 4516051
77 meter
Z = 15711766
55 Z = 4788946
44
XDOT = -22711
088218 XDOT = -6922
339689
YDOT = 1747
844283 feet/sec YDOT = 532
742938 meter/sec
ZDOT = -8307
589668 ZDOT = -2532
153331
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
12127037
00016717 00000-0 10270-3 0 9043
2 25544 51
6490 266
7716 0009227 306
4384 53
5927 15
71791059 22369
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12127037 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 266
7716 deg
Eccentricity:
0009227
Arg of perigee: 306
4384 deg
Mean anomaly: 53
5927 deg
Mean motion: 15
71791059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 306
Coasting Arc #6 (Orbit 2251)
---------------------------------------
Vector Time (GMT): 2010/162/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 219508
15 A = 6737498
08 meter
Y = -6546054
52 meter E =
0013665
Z = 1540019
55 I = 51
33174
XDOT = 4895
468466 Wp = 23
46197
YDOT = 1517
907670 meter/sec RA = 261
07524 deg
ZDOT = 5749
153718 TA = 353
58471
MA = 353
60219
Ha = 193
598 n
mi
Hp = 189
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 720171
11 X = 285209
78
Y = -21476556
83 feet Y = -6543232
79 meter
Z = 5052557
58 Z = 1541244
28
XDOT = 16061
248249 XDOT = 4850
202418
YDOT = 4980
012040 feet/sec YDOT = 1572
397524 meter/sec
ZDOT = 18862
052881 ZDOT = 5772
826535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20779045
51 X = 6333453
07
Y = -5472046
41 feet Y = -1667879
75 meter
Z = 5057415
71 Z = 1541500
31
XDOT = -617
019868 XDOT = -188
067656
YDOT = 15192
534856 feet/sec YDOT = 4630
684624 meter/sec
ZDOT = 18956
377893 ZDOT = 5777
903982
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
13854544
00016717 00000-0 10270-3 0 9056
2 25544 51
6495 261
5651 0009249 310
8317 49
2043 15
71772436 22521
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
13854544 = yrday
fracday
Element set: 905
Inclination: 51
6495 deg
RA of node: 261
5651 deg
Eccentricity:
0009249
Arg of perigee: 310
8317 deg
Mean anomaly: 49
2043 deg
Mean motion: 15
71772436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2252
Checksum: 301
Coasting Arc #7 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2010/163/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4292946
51 A = 6726605
71 meter
Y = -43212
85 meter E =
0009008
Z = -5184450
38 I = 51
30157
XDOT = -1091
895072 Wp = 59
42265
YDOT = -7552
270791 meter/sec RA = 255
91122 deg
ZDOT = 972
856227 TA = 219
86982
MA = 219
93602
Ha = 193
648 n
mi
Hp = 188
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14084470
17 X = -4266958
92
Y = -141774
44 feet Y = -91072
76 meter
Z = -17009351
63 Z = -5205242
56
XDOT = -3582
332914 XDOT = -1012
089056
YDOT = -24777
791309 feet/sec YDOT = -7564
034993 meter/sec
ZDOT = 3191
785523 ZDOT = 967
744054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4088000
56 X = -1246022
57
Y = -13373678
76 feet Y = -4076297
28 meter
Z = -17092203
22 Z = -5209703
54
XDOT = 21557
535082 XDOT = 6570
736693
YDOT = -10618
702674 feet/sec YDOT = -3236
580575 meter/sec
ZDOT = 3171
386743 ZDOT = 966
638679
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
09222496
00016717 00000-0 10270-3 0 9068
2 25544 51
6495 256
6846 0009313 314
1297 45
9099 15
71825724 22677
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
09222496 = yrday
fracday
Element set: 906
Inclination: 51
6495 deg
RA of node: 256
6846 deg
Eccentricity:
0009313
Arg of perigee: 314
1297 deg
Mean anomaly: 45
9099 deg
Mean motion: 15
71825724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 329
Coasting Arc #8 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2010/164/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2092958
96 A = 6738445
85 meter
Y = 6401826
39 meter E =
0002715
Z = -163940
42 I = 51
34937
XDOT = -4612
898698 Wp = 131
99211
YDOT = 1356
009762 meter/sec RA = 250
78040 deg
ZDOT = -6004
693662 TA = 49
79340
MA = 49
76964
Ha = 193
911 n
mi
Hp = 188
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6866663
24 X = 2022013
41
Y = 21003367
42 feet Y = 6424834
46 meter
Z = -537862
27 Z = -153943
78
XDOT = -15134
182081 XDOT = -4598
549244
YDOT = 4448
850926 feet/sec YDOT = 1304
507080 meter/sec
ZDOT = -19700
438524 ZDOT = -6027
068025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17723022
15 X = -5401977
15
Y = 13199556
44 feet Y = 4023224
80 meter
Z = -497994
65 Z = -151788
77
XDOT = -8035
704979 XDOT = -2449
282878
YDOT = -11527
391176 feet/sec YDOT = -3513
548830 meter/sec
ZDOT = -19789
599014 ZDOT = -6031
869779
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
10947050
00016717 00000-0 10270-3 0 9072
2 25544 51
6493 251
4788 0009228 317
3243 42
7201 15
71794325 22834
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
10947050 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 251
4788 deg
Eccentricity:
0009228
Arg of perigee: 317
3243 deg
Mean anomaly: 42
7201 deg
Mean motion: 15
71794325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 300
Coasting Arc #9 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2010/165/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3537016
87 A = 6726333
45 meter
Y = -2332498
52 meter E =
0006923
Z = 5226406
92 I = 51
31986
XDOT = 3594
873443 Wp = 332
93540
YDOT = 6778
516358 meter/sec RA = 245
64313 deg
ZDOT = 598
717316 TA = 111
38228
MA = 111
30839
Ha = 193
969 n
mi
Hp = 188
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11604386
05 X = 3537447
58
Y = -7652554
20 feet Y = -2292944
14 meter
Z = 17147004
34 Z = 5243590
26
XDOT = 11794
204210 XDOT = 3515
899219
YDOT = 22239
226896 feet/sec YDOT = 6818
274684 meter/sec
ZDOT = 1964
295657 ZDOT = 615
990691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11060283
62 X = 3371174
45
Y = 8278921
04 feet Y = 2523415
13 meter
Z = 17215478
84 Z = 5247277
95
XDOT = -16410
275656 XDOT = -5001
852020
YDOT = 17738
967956 feet/sec YDOT = 5406
837433 meter/sec
ZDOT = 2033
180963 ZDOT = 619
713557
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
12669891
00016717 00000-0 10270-3 0 9080
2 25544 51
6489 246
2721 0009392 322
1075 37
9425 15
71857273 22990
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
12669891 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 246
2721 deg
Eccentricity:
0009392
Arg of perigee: 322
1075 deg
Mean anomaly: 37
9425 deg
Mean motion: 15
71857273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 334
Coasting Arc #10 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2010/166/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4064012
11 A = 6737574
59 meter
Y = -5224295
42 meter E =
0015169
Z = -1204987
06 I = 51
37053
XDOT = 3204
977501 Wp =
88180
YDOT = -3840
594175 meter/sec RA = 240
48577 deg
ZDOT = 5857
740366 TA = 345
86382
MA = 345
90623
Ha = 194
170 n
mi
Hp = 188
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13333373
08 X = -3999437
49
Y = -17140076
85 feet Y = -5269380
35 meter
Z = -3953369
60 Z = -1224573
98
XDOT = 10515
018048 XDOT = 3219
229911
YDOT = -12600
374590 feet/sec YDOT = -3804
675596 meter/sec
ZDOT = 19218
308286 ZDOT = 5873
343935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11381614
18 X = 3469116
00
Y = -18476909
82 feet Y = -5631762
11 meter
Z = -4031484
24 Z = -1228796
40
XDOT = 14100
548306 XDOT = 4297
847124
YDOT = 4490
166336 feet/sec YDOT = 1368
602699 meter/sec
ZDOT = 19280
479095 ZDOT = 5876
690028
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
08033764
00016717 00000-0 10270-3 0 9091
2 25544 51
6480 241
3905 0009572 325
6369 34
4173 15
71875847 23142
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
08033764 = yrday
fracday
Element set: 909
Inclination: 51
6480 deg
RA of node: 241
3905 deg
Eccentricity:
0009572
Arg of perigee: 325
6369 deg
Mean anomaly: 34
4173 deg
Mean motion: 15
71875847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 317
Coasting Arc #11 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2010/167/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1889819
27 A = 6727608
86 meter
Y = 4190454
49 meter E =
0013745
Z = -4922204
94 I = 51
35178
XDOT = -5479
669778 Wp = 31
85917
YDOT = -4962
895548 meter/sec RA = 235
37516 deg
ZDOT = -2112
432892 TA = 217
49671
MA = 217
59266
Ha = 194
348 n
mi
Hp = 187
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6200194
45 X = -1912626
29
Y = 13748210
27 feet Y = 4169194
67 meter
Z = -16148966
34 Z = -4931440
33
XDOT = -17977
919218 XDOT = -5413
504803
YDOT = -16282
465708 feet/sec YDOT = -5023
802196 meter/sec
ZDOT = -6930
554108 ZDOT = -2138
892950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15028726
81 X = -4580755
93
Y = -635435
87 feet Y = -193680
85 meter
Z = -16185746
88 Z = -4933415
65
XDOT = 8520
581954 XDOT = 2597
073380
YDOT = -21563
705872 feet/sec YDOT = -6572
617550 meter/sec
ZDOT = -7036
083334 ZDOT = -2144
598200
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
09753789
00016717 00000-0 10270-3 0 9101
2 25544 51
6467 236
1834 0009628 329
2172 30
8424 15
71905470 23307
Satellite: ISS
Catalog Number: 25544
Epoch time: 10167
09753789 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 236
1834 deg
Eccentricity:
0009628
Arg of perigee: 329
2172 deg
Mean anomaly: 30
8424 deg
Mean motion: 15
71905470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 312
Coasting Arc #12 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2010/168/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5318985
51 A = 6735336
27 meter
Y = 3327217
63 meter E =
0010416
Z = 2450620
33 I = 51
39694
XDOT = -964
440365 Wp = 60
51420
YDOT = 5474
550229 meter/sec RA = 230
19821 deg
ZDOT = -5317
523169 TA = 91
73891
MA = 91
61960
Ha = 194
477 n
mi
Hp = 187
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17450739
87 X = 5269480
08
Y = 10916068
35 feet Y = 3386420
57 meter
Z = 8040092
93 Z = 2476339
94
XDOT = -3164
174425 XDOT = -999
754756
YDOT = 17961
122798 feet/sec YDOT = 5463
568543 meter/sec
ZDOT = -17445
942154 ZDOT = -5322
293423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3422619
60 X = -1043214
45
Y = 20256222
97 feet Y = 6174096
76 meter
Z = 8142669
74 Z = 2481885
74
XDOT = -16287
125967 XDOT = -4964
315995
YDOT = 4297
295225 feet/sec YDOT = 1309
815584 meter/sec
ZDOT = -17464
903821 ZDOT = -5323
302685
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
11472342
00016717 00000-0 10270-3 0 9119
2 25544 51
6471 230
9764 0009718 333
5322 26
5343 15
71954239 23467
Satellite: ISS
Catalog Number: 25544
Epoch time: 10168
11472342 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 230
9764 deg
Eccentricity:
0009718
Arg of perigee: 333
5322 deg
Mean anomaly: 26
5343 deg
Mean motion: 15
71954239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 300
Coasting Arc #13 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2010/169/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -288842
85 A = 6730074
30 meter
Y = -5158684
45 meter E =
0008037
Z = 4304319
35 I = 51
39775
XDOT = 6405
351538 Wp = 43
34374
YDOT = 2521
877843 meter/sec RA = 225
10594 deg
ZDOT = 3454
229485 TA = 11
64409
MA = 11
62551
Ha = 194
669 n
mi
Hp = 187
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -947647
16 X = -252045
54
Y = -16924817
76 feet Y = -5161709
23 meter
Z = 14121782
65 Z = 4303004
94
XDOT = 21014
932868 XDOT = 6359
895450
YDOT = 8273
877437 feet/sec YDOT = 2593
251740 meter/sec
ZDOT = 11332
773900 ZDOT = 3485
236405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15110350
61 X = 4605634
87
Y = -7692495
03 feet Y = -2344672
49 meter
Z = 14116481
90 Z = 4302703
68
XDOT = 201
530980 XDOT = 61
426643
YDOT = 21407
799477 feet/sec YDOT = 6525
097281 meter/sec
ZDOT = 11456
434338 ZDOT = 3491
921186
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
13189638
00016717 00000-0 10270-3 0 9126
2 25544 51
6459 225
7680 0009708 337
4558 22
6176 15
71913765 23623
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
13189638 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 225
7680 deg
Eccentricity:
0009708
Arg of perigee: 337
4558 deg
Mean anomaly: 22
6176 deg
Mean motion: 15
71913765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 333
Coasting Arc #14 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2010/170/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5629673
41 A = 6732415
39 meter
Y = -1029642
36 meter E =
0008578
Z = -3539695
39 I = 51
42775
XDOT = -1689
040024 Wp = 14
54026
YDOT = -6046
227581 meter/sec RA = 219
91899 deg
ZDOT = 4455
573039 TA = 303
17561
MA = 303
25785
Ha = 194
586 n
mi
Hp = 186
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18470057
12 X = -5600546
17
Y = -3378091
72 feet Y = -1092433
47 meter
Z = -11613173
84 Z = -3566973
69
XDOT = -5541
469896 XDOT = -1642
948827
YDOT = -19836
704663 feet/sec YDOT = -6064
858221 meter/sec
ZDOT = 14618
021783 ZDOT = 4447
478970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4550068
90 X = -1386861
00
Y = -18146980
19 feet Y = -5531199
56 meter
Z = -11721958
16 Z = -3572852
85
XDOT = 14397
901363 XDOT = 4388
480335
YDOT = -13009
543339 feet/sec YDOT = -3965
308810 meter/sec
ZDOT = 14585
672004 ZDOT = 4445
712827
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
08548002
00016717 00000-0 10270-3 0 9137
2 25544 51
6451 220
8854 0009601 340
3750 19
7042 15
71969419 23775
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
08548002 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 220
8854 deg
Eccentricity:
0009601
Arg of perigee: 340
3750 deg
Mean anomaly: 19
7042 deg
Mean motion: 15
71969419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 296
Coasting Arc #15 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2010/171/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2625036
19 A = 6732818
77 meter
Y = 5166059
15 meter E =
0009741
Z = -3439641
01 I = 51
45235
XDOT = -6192
831431 Wp = 14
55267
YDOT = 110
556499 meter/sec RA = 214
83675 deg
ZDOT = -4553
665707 TA = 206
18899
MA = 206
23829
Ha = 194
838 n
mi
Hp = 186
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8612323
46 X = 2583782
49
Y = 16949012
94 feet Y = 5195183
62 meter
Z = -11284911
44 Z = -3426988
12
XDOT = -20317
688422 XDOT = -6171
486464
YDOT = 362
718173 feet/sec YDOT = 41
424457 meter/sec
ZDOT = -14939
848119 ZDOT = -4583
698733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11570474
36 X = -3526680
58
Y = 15122929
52 feet Y = 4609468
92 meter
Z = -11234389
50 Z = -3424241
92
XDOT = -7921
994918 XDOT = -2414
624051
YDOT = -17264
294006 feet/sec YDOT = -5262
156813 meter/sec
ZDOT = -15059
611008 ZDOT = -4590
169435
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 10171
10262333
00016717 00000-0 10270-3 0 9142
2 25544 51
6444 215
6785 0009651 344
7016 15
3853 15
71992634 23935
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
10262333 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 215
6785 deg
Eccentricity:
0009651
Arg of perigee: 344
7016 deg
Mean anomaly: 15
3853 deg
Mean motion: 15
71992634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 301
Coasting Arc #16 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2010/172/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4986505
79 A = 6729460
66 meter
Y = -1163795
78 meter E =
0014313
Z = 4367907
07 I = 51
46716
XDOT = 4231
990318 Wp = 28
26559
YDOT = 5482
603709 meter/sec RA = 209
65367 deg
ZDOT = -3353
651419 TA = 95
67329
MA = 95
51006
Ha = 194
838 n
mi
Hp = 186
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16359927
14 X = 4977930
32
Y = -3818227
63 feet Y = -1108082
25 meter
Z = 14330403
78 Z = 4392110
69
XDOT = 13884
482671 XDOT = 4186
659856
YDOT = 17987
544977 feet/sec YDOT = 5529
675356 meter/sec
ZDOT = -11002
793370 ZDOT = -3333
201619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10667450
90 X = 3251439
03
Y = 12870748
18 feet Y = 3923004
04 meter
Z = 14426915
24 Z = 4397323
77
XDOT = -8952
314078 XDOT = -2728
665331
YDOT = 19723
116462 feet/sec YDOT = 6011
605898 meter/sec
ZDOT = -10921
169196 ZDOT = -3328
772371
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 10172
11975152
00016717 00000-0 10270-3 0 9155
2 25544 51
6447 210
4702 0009605 347
7656 12
3272 15
72011022 24096
Satellite: ISS
Catalog Number: 25544
Epoch time: 10172
11975152 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 210
4702 deg
Eccentricity:
0009605
Arg of perigee: 347
7656 deg
Mean anomaly: 12
3272 deg
Mean motion: 15
72011022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 275
Coasting Arc #17 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2010/173/01:52:15
699
Vector Time (MET): N/A
Weight (LBS) : 798910
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4669250
89 A = 6735366
62 meter
Y = -4213263
61 meter E =
0017997
Z = 2377903
66 I = 51
51279
XDOT = 4947
996372 Wp = 42
34665
YDOT = -2441
256457 meter/sec RA = 204
56684 deg
ZDOT = 5379
916987 TA = 344
51386
MA = 344
56886
Ha = 194
998 n
mi
Hp = 186
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15319064
59 X = -4633341
89
Y = -13823043
33 feet Y = -4265277
56 meter
Z = 7801521
21 Z = 2355306
81
XDOT = 16233
583896 XDOT = 4948
792337
YDOT = -8009
371578 feet/sec YDOT = -2385
921433 meter/sec
ZDOT = 17650
646282 ZDOT = 5403
956077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5188475
98 X = 1581447
48
Y = -20005721
85 feet Y = -6097744
02 meter
Z = 7711342
95 Z = 2350417
33
XDOT = 13080
811708 XDOT = 3987
031409
YDOT = 10246
385248 feet/sec YDOT = 3123
098224 meter/sec
ZDOT = 17746
496052 ZDOT = 5409
131997
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 10173
13686574
00016717 00000-0 10270-3 0 9166
2 25544 51
6436 205
2619 0009493 352
1876 7
9136 15
72039952 24251
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
13686574 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 205
2619 deg
Eccentricity:
0009493
Arg of perigee: 352
1876 deg
Mean anomaly: 7
9136 deg
Mean motion: 15
72039952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 321
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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