Date:
January 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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
013/09:06:04
407 -3
8 5
1 5
1
N/A -2
9 -0
0 194
2
000/00:12:04
815 -1
7 0
2 187
1
Coasting Arc #1 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2011/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990061
81 A = 6728260
64 meter
Y = -4240465
20 meter E =
0014534
Z = 4274535
16 I = 51
29965
XDOT = 3441
109121 Wp = 109
42689
YDOT = 5948
948530 meter/sec RA = 263
88750 deg
ZDOT = 3480
069172 TA = 305
13459
MA = 305
27071
Ha = 193
915 n
mi
Hp = 184
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9809914
07 X = 3016492
78
Y = -13912287
41 feet Y = -4206881
08 meter
Z = 14024065
49 Z = 4289124
45
XDOT = 11289
728088 XDOT = 3357
425923
YDOT = 19517
547669 feet/sec YDOT = 5986
960920 meter/sec
ZDOT = 11417
549776 ZDOT = 3496
582924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16046320
75 X = 4890918
56
Y = 5536108
46 feet Y = 1687405
86 meter
Z = 14082885
41 Z = 4292463
47
XDOT = -15286
673569 XDOT = -4659
378104
YDOT = 14975
658871 feet/sec YDOT = 4564
580824 meter/sec
ZDOT = 11483
867553 ZDOT = 3500
282830
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 11007
55393327
00016717 00000-0 10270-3 0 9003
2 25544 51
6464 264
3954 0004762 111
9864 248
1805 15
72562501 15626
Satellite: ISS
Catalog Number: 25544
Epoch time: 11007
55393327 = yrday
fracday
Element set: 900
Inclination: 51
6464 deg
RA of node: 264
3954 deg
Eccentricity:
0004762
Arg of perigee: 111
9864 deg
Mean anomaly: 248
1805 deg
Mean motion: 15
72562501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1562
Checksum: 303
Coasting Arc #2 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2011/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3676345
68 A = 6731089
43 meter
Y = -4507071
50 meter E =
0009334
Z = -3397971
47 I = 51
31404
XDOT = 2624
353038 Wp = 103
09296
YDOT = -5589
286806 meter/sec RA = 258
68870 deg
ZDOT = 4582
783376 TA = 216
64876
MA = 216
71264
Ha = 193
830 n
mi
Hp = 184
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12061501
59 X = -3609167
12
Y = -14786980
00 feet Y = -4547806
80 meter
Z = -11148200
35 Z = -3415667
90
XDOT = 8610
082145 XDOT = 2664
396543
YDOT = -18337
555139 feet/sec YDOT = -5559
716086 meter/sec
ZDOT = 15035
378531 ZDOT = 4595
629169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10659324
80 X = 3248962
20
Y = -15777278
76 feet Y = -4808914
57 meter
Z = -11219324
36 Z = -3419650
06
XDOT = 18871
855789 XDOT = 5752
141645
YDOT = 2041
153468 feet/sec YDOT = 622
143577 meter/sec
ZDOT = 15087
206536 ZDOT = 4598
580552
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 11008
50713456
00016717 00000-0 10270-3 0 9019
2 25544 51
6464 259
5109 0004593 115
5054 244
6584 15
72600354 15777
Satellite: ISS
Catalog Number: 25544
Epoch time: 11008
50713456 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 259
5109 deg
Eccentricity:
0004593
Arg of perigee: 115
5054 deg
Mean anomaly: 244
6584 deg
Mean motion: 15
72600354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1577
Checksum: 300
Coasting Arc #3 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2011/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1523844
12 A = 6730055
14 meter
Y = 5396105
24 meter E =
0009688
Z = -3729537
40 I = 51
31755
XDOT = -4792
390957 Wp = 95
62955
YDOT = -4272
802737 meter/sec RA = 253
59206 deg
ZDOT = -4234
397241 TA = 129
56145
MA = 129
47583
Ha = 193
714 n
mi
Hp = 184
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4999488
58 X = -1565954
01
Y = 17703757
33 feet Y = 5378829
42 meter
Z = -12236015
09 Z = -3737042
13
XDOT = -15723
067444 XDOT = -4723
685899
YDOT = -14018
381683 feet/sec YDOT = -4326
009788 meter/sec
ZDOT = -13892
379401 ZDOT = -4257
511615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18360556
60 X = -5596297
65
Y = 751643
76 feet Y = 229101
02 meter
Z = -12266334
74 Z = -3738778
83
XDOT = 8589
807626 XDOT = 2618
173364
YDOT = -17852
077503 feet/sec YDOT = -5441
313223 meter/sec
ZDOT = -13985
325515 ZDOT = -4262
727217
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 11009
52386443
00016717 00000-0 10270-3 0 9025
2 25544 51
6462 254
3004 0004449 120
6655 239
4947 15
72615586 15932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11009
52386443 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 254
3004 deg
Eccentricity:
0004449
Arg of perigee: 120
6655 deg
Mean anomaly: 239
4947 deg
Mean motion: 15
72615586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1593
Checksum: 311
Coasting Arc #4 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2011/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4576781
15 A = 6728886
20 meter
Y = 2884666
56 meter E =
0014300
Z = 3988820
84 I = 51
32413
XDOT = -747
068713 Wp = 90
36492
YDOT = 6600
450278 meter/sec RA = 248
39244 deg
ZDOT = -3904
216490 TA = 40
15817
MA = 40
05258
Ha = 193
478 n
mi
Hp = 184
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15015686
19 X = 4524807
40
Y = 9464129
14 feet Y = 2935556
11 meter
Z = 13086682
54 Z = 4010928
43
XDOT = -2451
012838 XDOT = -801
854942
YDOT = 21655
020598 feet/sec YDOT = 6591
789951 meter/sec
ZDOT = -12809
109218 ZDOT = -3907
978483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4121729
86 X = -1256303
26
Y = 17196406
53 feet Y = 5241464
71 meter
Z = 13175612
98 Z = 4015926
84
XDOT = -20003
802247 XDOT = -6097
158925
YDOT = 5061
077494 feet/sec YDOT = 1542
616420 meter/sec
ZDOT = -12824
381635 ZDOT = -3908
871522
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 11010
54057487
00016717 00000-0 10270-3 0 9033
2 25544 51
6461 249
0900 0004408 122
2759 237
8831 15
72692079 16099
Satellite: ISS
Catalog Number: 25544
Epoch time: 11010
54057487 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 249
0900 deg
Eccentricity:
0004408
Arg of perigee: 122
2759 deg
Mean anomaly: 237
8831 deg
Mean motion: 15
72692079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1609
Checksum: 306
Coasting Arc #5 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2011/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -259550
68 A = 6731881
18 meter
Y = -5979181
00 meter E =
0016673
Z = 3069553
57 I = 51
34570
XDOT = 5510
217917 Wp = 94
71187
YDOT = 2276
094976 meter/sec RA = 243
29502 deg
ZDOT = 4875
442559 TA = 301
04795
MA = 301
21153
Ha = 193
575 n
mi
Hp = 184
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -851544
24 X = -207582
25
Y = -19616735
56 feet Y = -5981793
02 meter
Z = 10070713
80 Z = 3068418
63
XDOT = 18078
142771 XDOT = 5460
672891
YDOT = 7467
503202 feet/sec YDOT = 2337
436309 meter/sec
ZDOT = 15995
546452 ZDOT = 4902
090681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18139150
73 X = 5528813
14
Y = -7523456
74 feet Y = -2293149
61 meter
Z = 10066256
88 Z = 3068195
10
XDOT = -1461
462053 XDOT = -445
453634
YDOT = 18127
408052 feet/sec YDOT = 5525
233974 meter/sec
ZDOT = 16102
772780 ZDOT = 4908
125143
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 11011
55726805
00016717 00000-0 10270-3 0 9043
2 25544 51
6457 243
8789 0004365 126
0598 234
0970 15
72669798 16259
Satellite: ISS
Catalog Number: 25544
Epoch time: 11011
55726805 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 243
8789 deg
Eccentricity:
0004365
Arg of perigee: 126
0598 deg
Mean anomaly: 234
0970 deg
Mean motion: 15
72669798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 336
Coasting Arc #6 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2011/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4904529
51 A = 6726974
49 meter
Y = -1085353
44 meter E =
0014032
Z = -4488482
15 I = 51
34417
XDOT = -1339
341233 Wp = 116
89902
YDOT = -6891
340113 meter/sec RA = 238
10016 deg
ZDOT = 3131
154694 TA = 184
53531
MA = 184
54804
Ha = 193
408 n
mi
Hp = 184
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16090976
08 X = -4870224
30
Y = -3560870
85 feet Y = -1140006
79 meter
Z = -14725991
30 Z = -4512224
90
XDOT = -4394
164150 XDOT = -1277
391893
YDOT = -22609
383572 feet/sec YDOT = -6905
971227 meter/sec
ZDOT = 10272
817236 ZDOT = 3124
798324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2368041
83 X = -721779
15
Y = -16222457
61 feet Y = -4944605
08 meter
Z = -14821551
16 Z = -4517608
79
XDOT = 18359
316005 XDOT = 5595
919518
YDOT = -12038
580118 feet/sec YDOT = -3669
359220 meter/sec
ZDOT = 10247
352507 ZDOT = 3123
393044
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 11012
51039848
00016717 00000-0 10270-3 0 9055
2 25544 51
6452 238
9934 0004277 131
4039 228
7492 15
72723414 16405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
51039848 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 238
9934 deg
Eccentricity:
0004277
Arg of perigee: 131
4039 deg
Mean anomaly: 228
7492 deg
Mean motion: 15
72723414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1640
Checksum: 304
Coasting Arc #7 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3143782
91 A = 6726604
68 meter
Y = 2813120
55 meter E =
0015031
Z = -5251516
45 I = 51
34892
XDOT = -4785
367759 Wp = 106
18316
YDOT = -6005
204850 meter/sec RA = 233
58117 deg
ZDOT = -357
098212 TA = 160
43552
MA = 160
37778
Ha = 194
157 n
mi
Hp = 187
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10314248
40 X = -3149495
35
Y = 9229398
14 feet Y = 2777933
28 meter
Z = -17229384
68 Z = -5266802
54
XDOT = -15700
025457 XDOT = -4716
126063
YDOT = -19702
115648 feet/sec YDOT = -6058
330543 meter/sec
ZDOT = -1171
582060 ZDOT = -380
177582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5124174
52 X = -1561848
39
Y = -12774281
35 feet Y = -3893600
96 meter
Z = -17290973
89 Z = -5270288
84
XDOT = 22984
291910 XDOT = 7005
612174
YDOT = -7530
277761 feet/sec YDOT = -2295
228661 meter/sec
ZDOT = -1264
391884 ZDOT = -385
386646
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 11013
39998017
00016717 00000-0 10270-3 0 9065
2 25544 51
6458 234
4345 0004928 185
7595 174
3511 15
71738212 16544
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
39998017 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 234
4345 deg
Eccentricity:
0004928
Arg of perigee: 185
7595 deg
Mean anomaly: 174
3511 deg
Mean motion: 15
71738212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 323
Coasting Arc #8 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4992199
30 A = 6738198
29 meter
Y = 4392398
26 meter E =
0016457
Z = 1028115
10 I = 51
40663
XDOT = -2521
657832 Wp = 140
05333
YDOT = 4257
006472 meter/sec RA = 228
43135 deg
ZDOT = -5903
021580 TA = 28
67278
MA = 28
58239
Ha = 194
097 n
mi
Hp = 187
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16378606
61 X = 4937717
28
Y = 14410755
44 feet Y = 4447919
33 meter
Z = 3373081
04 Z = 1052235
07
XDOT = -8273
155618 XDOT = -2540
397439
YDOT = 13966
556666 feet/sec YDOT = 4228
703476 meter/sec
ZDOT = -19366
868700 ZDOT = -5915
316886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19000827
79 X = -5791452
31
Y = 10687989
59 feet Y = 3257699
23 meter
Z = 3470118
83 Z = 1057692
22
XDOT = -9713
195420 XDOT = -2960
581964
YDOT = -10922
683477 feet/sec YDOT = -3329
233924 meter/sec
ZDOT = -19416
445348 ZDOT = -5918
132542
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 11014
41727818
00016717 00000-0 10270-3 0 9079
2 25544 51
6456 229
2283 0005025 189
7030 170
4036 15
71718322 16709
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41727818 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 229
2283 deg
Eccentricity:
0005025
Arg of perigee: 189
7030 deg
Mean anomaly: 170
4036 deg
Mean motion: 15
71718322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 292
Coasting Arc #9 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1104653
32 A = 6727790
38 meter
Y = -4405195
65 meter E =
0008859
Z = 4962807
06 I = 51
39328
XDOT = 6372
675561 Wp = 155
28174
YDOT = 3837
902268 meter/sec RA = 223
32228 deg
ZDOT = 1979
010461 TA = 275
46043
MA = 275
56149
Ha = 193
866 n
mi
Hp = 187
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3624190
67 X = 1129722
72
Y = -14452741
62 feet Y = -4392703
07 meter
Z = 16282175
40 Z = 4968233
88
XDOT = 20907
728220 XDOT = 6319
672189
YDOT = 12591
542874 feet/sec YDOT = 3908
868815 meter/sec
ZDOT = 6492
816473 ZDOT = 2009
840305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12616756
00 X = 3845587
23
Y = 7881591
34 feet Y = 2402309
04 meter
Z = 16304101
33 Z = 4969490
09
XDOT = -17926
716635 XDOT = -5464
063230
YDOT = 14946
594653 feet/sec YDOT = 4555
722050 meter/sec
ZDOT = 6616
894180 ZDOT = 2016
829346
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 11015
43455629
00016717 00000-0 10270-3 0 9081
2 25544 51
6457 224
0219 0004843 194
5625 165
5398 15
71777580 16867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43455629 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 224
0219 deg
Eccentricity:
0004843
Arg of perigee: 194
5625 deg
Mean anomaly: 165
5398 deg
Mean motion: 15
71777580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 332
Coasting Arc #10 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2011/016/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5898228
35 A = 6735868
68 meter
Y = -2214985
26 meter E =
0002513
Z = -2385907
80 I = 51
44378
XDOT = -97
726727 Wp = 107
23175
YDOT = -5512
264464 meter/sec RA = 218
15048 deg
ZDOT = 5362
882477 TA = 225
83992
MA = 225
86058
Ha = 193
660 n
mi
Hp = 187
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19351142
89 X = -5861431
43
Y = -7267012
02 feet Y = -2280736
80 meter
Z = -7827781
49 Z = -2414471
93
XDOT = -320
625745 XDOT = -62
131892
YDOT = -18084
857165 feet/sec YDOT = -5513
158891 meter/sec
ZDOT = 17594
758784 ZDOT = 5362
493559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12676924
40 X = 3863926
56
Y = -16271392
42 feet Y = -4959520
41 meter
Z = -7942778
75 Z = -2420958
96
XDOT = 16206
717807 XDOT = 4939
807588
YDOT = 4044
667039 feet/sec YDOT = 1232
814513 meter/sec
ZDOT = 17593
282458 ZDOT = 5362
432493
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 11016
38823843
00016717 00000-0 10270-3 0 9094
2 25544 51
6455 219
1406 0004764 200
1262 159
9713 15
71810813 17014
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
38823843 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 219
1406 deg
Eccentricity:
0004764
Arg of perigee: 200
1262 deg
Mean anomaly: 159
9713 deg
Mean motion: 15
71810813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 292
Coasting Arc #11 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2011/017/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1303008
59 A = 6730207
27 meter
Y = 4977729
49 meter E =
0006330
Z = -4342859
66 I = 51
44875
XDOT = -6795
299829 Wp = 100
81298
YDOT = -1186
580150 meter/sec RA = 213
06312 deg
ZDOT = -3404
232538 TA = 134
74951
MA = 134
69797
Ha = 193
463 n
mi
Hp = 187
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4274962
56 X = 1268346
31
Y = 16331133
50 feet Y = 4992107
23 meter
Z = -14248227
24 Z = -4336613
35
XDOT = -22294
290776 XDOT = -6764
989357
YDOT = -3892
979496 feet/sec YDOT = -1262
399409 meter/sec
ZDOT = -11168
741922 ZDOT = -3437
170073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16897772
22 X = -5150440
97
Y = -400749
22 feet Y = -122148
36 meter
Z = -14223146
61 Z = -4335215
09
XDOT = 9948
523406 XDOT = 3032
309934
YDOT = -19007
723101 feet/sec YDOT = -5793
554001 meter/sec
ZDOT = -11301
388039 ZDOT = -3444
663074
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 11017
40548162
00016717 00000-0 10270-3 0 9108
2 25544 51
6448 213
9338 0004773 206
1065 153
9857 15
71831573 17175
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
40548162 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 213
9338 deg
Eccentricity:
0004773
Arg of perigee: 206
1065 deg
Mean anomaly: 153
9857 deg
Mean motion: 15
71831573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 307
Coasting Arc #12 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2011/018/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5729313
39 A = 6732688
79 meter
Y = -139768
66 meter E =
0010378
Z = 3521673
86 I = 51
48409
XDOT = 2891
517627 Wp = 109
08997
YDOT = 5560
150492 meter/sec RA = 207
88193 deg
ZDOT = -4476
084231 TA = 28
91049
MA = 28
85304
Ha = 193
112 n
mi
Hp = 187
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18796959
96 X = 5713343
23
Y = -458558
61 feet Y = -75789
72 meter
Z = 11554048
09 Z = 3549467
44
XDOT = 9486
606387 XDOT = 2850
871593
YDOT = 18241
963558 feet/sec YDOT = 5592
258427 meter/sec
ZDOT = -14685
315717 ZDOT = -4462
135651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4506562
07 X = -1373600
12
Y = 18183152
87 feet Y = 5542225
00 meter
Z = 11666012
89 Z = 3555800
73
XDOT = -18796
857018 XDOT = -5729
282019
YDOT = 4742
567461 feet/sec YDOT = 1445
534562 meter/sec
ZDOT = -14629
207655 ZDOT = -4458
982493
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 11018
42270641
00016717 00000-0 10270-3 0 9116
2 25544 51
6448 208
7269 0004607 210
0802 150
0096 15
71893285 17338
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
42270641 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 208
7269 deg
Eccentricity:
0004607
Arg of perigee: 210
0802 deg
Mean anomaly: 150
0096 deg
Mean motion: 15
71893285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 288
Coasting Arc #13 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2011/019/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3668307
08 A = 6733238
21 meter
Y = -4490466
35 meter E =
0010619
Z = 3418229
01 I = 51
51212
XDOT = 6020
255407 Wp = 111
44477
YDOT = -1419
650285 meter/sec RA = 202
80299 deg
ZDOT = 4580
518180 TA = 289
00637
MA = 289
12139
Ha = 193
154 n
mi
Hp = 187
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12035128
23 X = -3634425
89
Y = -14732501
16 feet Y = -4531298
45 meter
Z = 11214662
10 Z = 3400490
73
XDOT = 19751
494118 XDOT = 6013
432048
YDOT = -4657
645292 feet/sec YDOT = -1352
366737 meter/sec
ZDOT = 15027
946785 ZDOT = 4609
747077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17269715
51 X = 5263809
29
Y = -8077395
36 feet Y = -2461990
11 meter
Z = 11143256
17 Z = 3396464
48
XDOT = -945
133836 XDOT = -288
076793
YDOT = 18943
010721 feet/sec YDOT = 5773
829668 meter/sec
ZDOT = 15145
727807 ZDOT = 4616
417836
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11019
43991375
00016717 00000-0 10270-3 0 9123
2 25544 51
6439 203
5188 0004584 214
9200 145
1662 15
71872558 17491
Satellite: ISS
Catalog Number: 25544
Epoch time: 11019
43991375 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 203
5188 deg
Eccentricity:
0004584
Arg of perigee: 214
9200 deg
Mean anomaly: 145
1662 deg
Mean motion: 15
71872558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1749
Checksum: 318
Coasting Arc #14 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2011/020/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579289
03 A = 6729547
39 meter
Y = 2222745
01 meter E =
0009137
Z = -4410841
25 I = 51
52857
XDOT = -5337
498087 Wp = 140
16630
YDOT = -4445
470613 meter/sec RA = 197
62503 deg
ZDOT = 3298
011221 TA = 163
06665
MA = 163
03613
Ha = 192
903 n
mi
Hp = 187
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15023914
13 X = -4582377
42
Y = 7292470
51 feet Y = 2171519
66 meter
Z = -14471263
96 Z = -4433094
13
XDOT = -17511
476662 XDOT = -5303
411963
YDOT = -14584
877340 feet/sec YDOT = -4504
967367 meter/sec
ZDOT = 10820
246788 ZDOT = 3272
164939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3645885
86 X = -1111266
01
Y = -16217324
10 feet Y = -4943040
39 meter
Z = -14560958
69 Z = -4438180
21
XDOT = 17065
916133 XDOT = 5201
691237
YDOT = -13467
470623 feet/sec YDOT = -4104
885046 meter/sec
ZDOT = 10716
153414 ZDOT = 3266
283561
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11020
39352634
00016717 00000-0 10270-3 0 9130
2 25544 51
6434 198
6362 0004691 219
2931 140
7892 15
71928791 17646
Satellite: ISS
Catalog Number: 25544
Epoch time: 11020
39352634 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 198
6362 deg
Eccentricity:
0004691
Arg of perigee: 219
2931 deg
Mean anomaly: 140
7892 deg
Mean motion: 15
71928791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 320
Coasting Arc #15 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2011/021/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5503232
22 A = 6735810
81 meter
Y = 3107468
05 meter E =
0007695
Z = -2317296
70 I = 51
57863
XDOT = -4232
316547 Wp = 174
29893
YDOT = 3461
373110 meter/sec RA = 192
54375 deg
ZDOT = -5418
508356 TA = 31
76655
MA = 31
72016
Ha = 192
828 n
mi
Hp = 188
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18055223
81 X = 5479331
58
Y = 10195105
16 feet Y = 3168874
96 meter
Z = -7602679
47 Z = -2290620
75
XDOT = -13885
552976 XDOT = -4244
386377
YDOT = 11356
210992 feet/sec YDOT = 3413
977500 meter/sec
ZDOT = -17777
258385 ZDOT = -5439
097524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13834060
89 X = -4216621
76
Y = 15497502
79 feet Y = 4723638
85 meter
Z = -7495210
32 Z = -2284540
10
XDOT = -7011
542760 XDOT = -2137
118233
YDOT = -14882
319397 feet/sec YDOT = -4536
130952 meter/sec
ZDOT = -17860
269041 ZDOT = -5443
810004
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11021
41069607
00016717 00000-0 10270-3 0 9140
2 25544 51
6432 193
4293 0004739 223
8133 136
2653 15
71928896 17807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
41069607 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 193
4293 deg
Eccentricity:
0004739
Arg of perigee: 223
8133 deg
Mean anomaly: 136
2653 deg
Mean motion: 15
71928896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1780
Checksum: 311
Coasting Arc #16 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2011/022/09:12:06
815
Vector Time (MET): N/A
Weight (LBS) : 828127
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2666280
64 A = 6727059
42 meter
Y = -3642649
14 meter E =
0001195
Z = 4986527
46 I = 51
58028
XDOT = 7025
323389 Wp = 85
53936
YDOT = 2470
730895 meter/sec RA = 187
38297 deg
ZDOT = -1951
062717 TA = 23
33651
MA = 23
33108
Ha = 192
488 n
mi
Hp = 188
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8747639
89 X = 2682592
27
Y = -11950948
62 feet Y = -3612742
04 meter
Z = 16359998
24 Z = 4999519
48
XDOT = 23048
961251 XDOT = 7006
650727
YDOT = 8106
072489 feet/sec YDOT = 2549
187922 meter/sec
ZDOT = -6401
124401 ZDOT = -1916
979951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10008867
83 X = 3050702
91
Y = 10837515
56 feet Y = 3303274
74 meter
Z = 16412395
93 Z = 5002498
28
XDOT = -11711
015686 XDOT = -3569
517581
YDOT = 20303
922699 feet/sec YDOT = 6188
635639 meter/sec
ZDOT = -6263
783630 ZDOT = -1909
201250
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11022
42784568
00016717 00000-0 10270-3 0 9153
2 25544 51
6436 188
2210 0004690 228
3278 131
7483 15
71981462 17964
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
42784568 = yrday
fracday
Element set: 915
Inclination: 51
6436 deg
RA of node: 188
2210 deg
Eccentricity:
0004690
Arg of perigee: 228
3278 deg
Mean anomaly: 131
7483 deg
Mean motion: 15
71981462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
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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