Date:
December 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
356/16:56:17
205 4
9 7
1 7
2
N/A -4
4 -0
6 193
4
000/00:18:34
409 -2
8 0
4 187
5
Coasting Arc #1 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2010/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 719612
71 A = 6723133
48 meter
Y = -4309208
39 meter E =
0015198
Z = -5121804
51 I = 51
81165
XDOT = 6932
008514 Wp = 45
84758
YDOT = 2964
794172 meter/sec RA = 32
23770 deg
ZDOT = -1512
870014 TA = 209
61344
MA = 209
69959
Ha = 192
448 n
mi
Hp = 185
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2360934
10 X = 792626
53
Y = -14137822
79 feet Y = -4300752
68 meter
Z = -16803820
57 Z = -5118131
54
XDOT = 22742
810085 XDOT = 6905
689711
YDOT = 9727
015000 feet/sec YDOT = 3042
165005 meter/sec
ZDOT = -4963
484298 ZDOT = -1479
257886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13602250
45 X = 4145965
94
Y = 4575152
72 feet Y = 1394506
55 meter
Z = -16788900
77 Z = -5117256
96
XDOT = -12731
858556 XDOT = -3880
670488
YDOT = 20042
991450 feet/sec YDOT = 6109
103794 meter/sec
ZDOT = -4828
377028 ZDOT = -1471
689318
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 10347
51838328
00016717 00000-0 10270-3 0 9000
2 25544 51
6461 32
6849 0008253 341
1827 18
9039 15
73190007 11680
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
51838328 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 32
6849 deg
Eccentricity:
0008253
Arg of perigee: 341
1827 deg
Mean anomaly: 18
9039 deg
Mean motion: 15
73190007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1168
Checksum: 304
Coasting Arc #2 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2010/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285689
83 A = 6733287
39 meter
Y = -1852504
97 meter E =
0010459
Z = 1543354
18 I = 51
82019
XDOT = 66
899923 Wp = 81
19739
YDOT = -5074
885091 meter/sec RA = 27
09403 deg
ZDOT = -5784
226451 TA = 81
84675
MA = 81
72813
Ha = 192
553 n
mi
Hp = 184
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20622341
95 X = -6272005
00
Y = -6077772
20 feet Y = -1922718
92 meter
Z = 5063497
95 Z = 1512851
16
XDOT = 219
487936 XDOT = 151
742219
YDOT = -16649
885470 feet/sec YDOT = -5073
662222 meter/sec
ZDOT = -18977
120902 ZDOT = -5783
695694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8800481
63 X = 2682386
80
Y = -19646849
36 feet Y = -5988359
68 meter
Z = 4940865
05 Z = 1505975
67
XDOT = 15021
907390 XDOT = 4578
677372
YDOT = 1927
576139 feet/sec YDOT = 587
525207 meter/sec
ZDOT = -18974
810698 ZDOT = -5783
522301
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 10348
53471848
00016717 00000-0 10270-3 0 9014
2 25544 51
6462 27
4720 0008408 346
0178 14
0751 15
73263551 11847
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
53471848 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 27
4720 deg
Eccentricity:
0008408
Arg of perigee: 346
0178 deg
Mean anomaly: 14
0751 deg
Mean motion: 15
73263551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 295
Coasting Arc #3 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2010/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 610118
50 A = 6723447
49 meter
Y = 4475771
18 meter E =
0006015
Z = 4975519
62 I = 51
75918
XDOT = -7328
765155 Wp = 34
83444
YDOT = -1243
807495 meter/sec RA = 22
00554 deg
ZDOT = 2021
208274 TA = 35
67019
MA = 35
63001
Ha = 192
677 n
mi
Hp = 184
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2001701
12 X = 535853
81
Y = 14684288
64 feet Y = 4482178
29 meter
Z = 16323883
28 Z = 4978303
54
XDOT = -24044
505102 XDOT = -7324
130744
YDOT = -4080
733252 feet/sec YDOT = -1325
736395 meter/sec
ZDOT = 6631
260740 ZDOT = 1985
615906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14806988
91 X = -4513170
22
Y = 166447
42 feet Y = 50733
17 meter
Z = 16334922
11 Z = 4978884
26
XDOT = 6893
131084 XDOT = 2101
026355
YDOT = -22357
838039 feet/sec YDOT = -6814
669034 meter/sec
ZDOT = 6488
140432 ZDOT = 1977
585204
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 10349
55103531
00016717 00000-0 10270-3 0 9029
2 25544 51
6458 22
2591 0008326 350
7605 9
3403 15
73274752 12002
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
55103531 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 22
2591 deg
Eccentricity:
0008326
Arg of perigee: 350
7605 deg
Mean anomaly: 9
3403 deg
Mean motion: 15
73274752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 275
Coasting Arc #4 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2010/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6418526
30 A = 6732451
41 meter
Y = 312273
22 meter E =
0014115
Z = -1981897
84 I = 51
76207
XDOT = 1479
065783 Wp = 14
36959
YDOT = 5067
245412 meter/sec RA = 16
85066 deg
ZDOT = 5610
348824 TA = 323
59256
MA = 323
68848
Ha = 192
781 n
mi
Hp = 184
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21058157
15 X = 6424185
18
Y = 1024518
44 feet Y = 384080
86 meter
Z = -6502289
50 Z = -1950702
46
XDOT = 4852
578029 XDOT = 1395
038556
YDOT = 16624
820905 feet/sec YDOT = 5083
314908 meter/sec
ZDOT = 18406
656247 ZDOT = 5617
330555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3136263
96 X = -955933
26
Y = 20887205
05 feet Y = 6366420
10 meter
Z = -6376825
43 Z = -1943656
39
XDOT = -15494
493681 XDOT = -4722
721674
YDOT = 3279
159668 feet/sec YDOT = 999
487867 meter/sec
ZDOT = 18434
552631 ZDOT = 5618
851642
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 10350
50381422
00016717 00000-0 10270-3 0 9034
2 25544 51
6468 17
3723 0008320 354
5919 5
5153 15
73325481 12151
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
50381422 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 17
3723 deg
Eccentricity:
0008320
Arg of perigee: 354
5919 deg
Mean anomaly: 5
5153 deg
Mean motion: 15
73325481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1215
Checksum: 279
Coasting Arc #5 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2010/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1931546
77 A = 6723991
77 meter
Y = -4289040
38 meter E =
0016359
Z = -4818851
26 I = 51
70419
XDOT = 7262
735292 Wp = 42
52668
YDOT = -483
089222 meter/sec RA = 11
76439 deg
ZDOT = -2474
214798 TA = 203
22673
MA = 203
30074
Ha = 192
830 n
mi
Hp = 184
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6337095
72 X = -1860032
94
Y = -14071654
80 feet Y = -4310239
73 meter
Z = -15809879
47 Z = -4828061
59
XDOT = 23827
871693 XDOT = 7279
616949
YDOT = -1584
938392 feet/sec YDOT = -401
778289 meter/sec
ZDOT = -8117
502619 ZDOT = -2438
890991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14543051
11 X = 4432721
98
Y = -5049980
68 feet Y = -1539234
11 meter
Z = -15846763
05 Z = -4830093
38
XDOT = -775
605237 XDOT = -236
404476
YDOT = 22864
393250 feet/sec YDOT = 6969
067063 meter/sec
ZDOT = -7975
404862 ZDOT = -2430
903402
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 10351
52009201
00016717 00000-0 10270-3 0 9040
2 25544 51
6468 12
1591 0008379 358
4089 1
7046 15
73325316 12316
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
52009201 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 12
1591 deg
Eccentricity:
0008379
Arg of perigee: 358
4089 deg
Mean anomaly: 1
7046 deg
Mean motion: 15
73325316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 280
Coasting Arc #6 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2010/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6210719
19 A = 6731674
30 meter
Y = 1135042
79 meter E =
0014431
Z = 2331272
90 I = 51
69879
XDOT = -2892
970473 Wp = 72
19013
YDOT = -4640
652812 meter/sec RA = 6
59853 deg
ZDOT = -5415
988369 TA = 81
61719
MA = 81
45361
Ha = 192
962 n
mi
Hp = 183
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20376375
28 X = -6234274
89
Y = 3723893
66 feet Y = 1065458
78 meter
Z = 7648533
12 Z = 2301043
77
XDOT = -9491
372944 XDOT = -2814
552595
YDOT = -15225
238883 feet/sec YDOT = -4672
564589 meter/sec
ZDOT = -17768
990713 ZDOT = -5429
852718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2366742
38 X = -721383
08
Y = -20623006
68 feet Y = -6285892
43 meter
Z = 7526901
00 Z = 2294199
43
XDOT = 14308
966136 XDOT = 4361
372878
YDOT = -8186
262386 feet/sec YDOT = -2495
172775 meter/sec
ZDOT = -17824
575439 ZDOT = -5432
930594
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 10352
53634959
00016717 00000-0 10270-3 0 9057
2 25544 51
6454 6
9454 0008516 3
0156 357
1057 15
73374397 12471
Satellite: ISS
Catalog Number: 25544
Epoch time: 10352
53634959 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 6
9454 deg
Eccentricity:
0008516
Arg of perigee: 3
0156 deg
Mean anomaly: 357
1057 deg
Mean motion: 15
73374397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 312
Coasting Arc #7 (Orbit 1262)
---------------------------------------
Vector Time (GMT): 2010/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3092225
65 A = 6724499
61 meter
Y = 3751799
84 meter E =
0009494
Z = 4636303
85 I = 51
64389
XDOT = -6839
500376 Wp = 58
82695
YDOT = 2091
316786 meter/sec RA = 1
51183 deg
ZDOT = 2869
849706 TA = 2
82314
MA = 2
81779
Ha = 192
988 n
mi
Hp = 183
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10145097
29 X = 3027519
97
Y = 12309054
60 feet Y = 3786016
49 meter
Z = 15210970
65 Z = 4651169
42
XDOT = -22439
305694 XDOT = -6876
318878
YDOT = 6861
275545 feet/sec YDOT = 2014
627084 meter/sec
ZDOT = 9415
517407 ZDOT = 2836
533980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12786610
98 X = -3897359
03
Y = 9440357
49 feet Y = 2877420
96 meter
Z = 15270614
98 Z = 4654483
45
XDOT = -5065
045987 XDOT = -1543
826017
YDOT = -21871
191208 feet/sec YDOT = -6666
339080 meter/sec
ZDOT = 9281
428817 ZDOT = 2828
979503
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 10353
55258779
00016717 00000-0 10270-3 0 9063
2 25544 51
6448 1
7314 0008534 6
9249 353
2030 15
73380523 12631
Satellite: ISS
Catalog Number: 25544
Epoch time: 10353
55258779 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 1
7314 deg
Eccentricity:
0008534
Arg of perigee: 6
9249 deg
Mean anomaly: 353
2030 deg
Mean motion: 15
73380523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1263
Checksum: 298
Coasting Arc #8 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2010/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5652340
17 A = 6730763
08 meter
Y = -2480773
00 meter E =
0012645
Z = -2671421
56 I = 51
63522
XDOT = 4149
364288 Wp = 25
95765
YDOT = 3866
490780 meter/sec RA = 356
33780 deg
ZDOT = 5209
302601 TA = 303
60784
MA = 303
72846
Ha = 193
136 n
mi
Hp = 183
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18544423
13 X = 5692637
88
Y = -8139019
02 feet Y = -2417339
38 meter
Z = -8764506
41 Z = -2643864
88
XDOT = 13613
399896 XDOT = 4080
514114
YDOT = 12685
337204 feet/sec YDOT = 3912
505666 meter/sec
ZDOT = 17090
887800 ZDOT = 5229
293692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7545559
66 X = 2299886
58
Y = 18845058
33 feet Y = 5743973
78 meter
Z = -8653562
19 Z = -2637605
75
XDOT = -11733
932027 XDOT = -3576
502482
YDOT = 12552
038708 feet/sec YDOT = 3825
861398 meter/sec
ZDOT = 17171
144415 ZDOT = 5233
764818
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 10354
50529171
00016717 00000-0 10270-3 0 9077
2 25544 51
6453 356
8444 0008549 10
6836 349
4507 15
73431903 12786
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
50529171 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 356
8444 deg
Eccentricity:
0008549
Arg of perigee: 10
6836 deg
Mean anomaly: 349
4507 deg
Mean motion: 15
73431903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1278
Checksum: 317
Coasting Arc #9 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2010/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4079654
57 A = 6725017
26 meter
Y = -2958068
97 meter E =
0016280
Z = -4469309
17 I = 51
58466
XDOT = 6049
211546 Wp = 43
30591
YDOT = -3499
421864 meter/sec RA = 351
24957 deg
ZDOT = -3200
926781 TA = 194
56536
MA = 194
61233
Ha = 193
142 n
mi
Hp = 183
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13384693
47 X = -4024562
61
Y = -9704950
70 feet Y = -3003381
37 meter
Z = -14663087
83 Z = -4488994
77
XDOT = 19846
494572 XDOT = 6103
442645
YDOT = -11481
042860 feet/sec YDOT = -3431
472200 meter/sec
ZDOT = -10501
728284 ZDOT = -3171
408580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9897537
79 X = 3016769
52
Y = -13154840
77 feet Y = -4009595
47 meter
Z = -14742155
28 Z = -4493408
93
XDOT = 10232
032096 XDOT = 3118
723383
YDOT = 19351
508419 feet/sec YDOT = 5898
339766 meter/sec
ZDOT = -10382
848194 ZDOT = -3164
692129
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 10355
52149023
00016717 00000-0 10270-3 0 9085
2 25544 51
6442 351
6295 0008575 14
0139 346
1260 15
73443133 12940
Satellite: ISS
Catalog Number: 25544
Epoch time: 10355
52149023 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 351
6295 deg
Eccentricity:
0008575
Arg of perigee: 14
0139 deg
Mean anomaly: 346
1260 deg
Mean motion: 15
73443133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1294
Checksum: 289
Coasting Arc #10 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2010/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4879863
08 A = 6729955
38 meter
Y = 3596223
48 meter E =
0017048
Z = 2918250
82 I = 51
57143
XDOT = -5106
086975 Wp = 67
57119
YDOT = -2833
884094 meter/sec RA = 346
06639 deg
ZDOT = -5016
407948 TA = 78
80703
MA = 78
61544
Ha = 193
200 n
mi
Hp = 183
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16010049
46 X = -4933890
28
Y = 11798633
47 feet Y = 3541351
40 meter
Z = 9574313
71 Z = 2894413
90
XDOT = -16752
253854 XDOT = -5049
649815
YDOT = -9297
519992 feet/sec YDOT = -2890
667124 meter/sec
ZDOT = -16458
031326 ZDOT = -5041
076499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11842156
69 X = -3609489
36
Y = -16035037
59 feet Y = -4887479
46 meter
Z = 9478281
13 Z = 2888980
09
XDOT = 8084
123720 XDOT = 2464
040910
YDOT = -15815
294287 feet/sec YDOT = -4820
501699 meter/sec
ZDOT = -16557
153052 ZDOT = -5046
620250
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 10356
53766732
00016717 00000-0 10270-3 0 9090
2 25544 51
6439 346
4150 0008718 17
0200 343
1253 15
73508045 13101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
53766732 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 346
4150 deg
Eccentricity:
0008718
Arg of perigee: 17
0200 deg
Mean anomaly: 343
1253 deg
Mean motion: 15
73508045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1310
Checksum: 285
Coasting Arc #11 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/356/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1201515
97 A = 6725931
80 meter
Y = -4013899
30 meter E =
0013652
Z = -5272474
79 I = 51
53871
XDOT = 7403
520934 Wp = 68
60826
YDOT = -2070
850462 meter/sec RA = 345
00035 deg
ZDOT = -105
954545 TA = 200
35606
MA = 200
41053
Ha = 193
352 n
mi
Hp = 187
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3941981
52 X = -1130929
96
Y = -13168960
97 feet Y = -4026939
94 meter
Z = -17298145
63 Z = -5278140
84
XDOT = 24289
766845 XDOT = 7426
642028
YDOT = -6794
128811 feet/sec YDOT = -1987
930541 meter/sec
ZDOT = -347
619898 ZDOT = -69
932647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -719723
18 X = -219371
63
Y = -13698875
56 feet Y = -4175417
27 meter
Z = -17320779
45 Z = -5279373
58
XDOT = 24202
914021 XDOT = 7377
048193
YDOT = -996
042577 feet/sec YDOT = -303
593777 meter/sec
ZDOT = -202
630592 ZDOT = -61
761804
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 10356
72821170
00016717 00000-0 10270-3 0 9101
2 25544 51
6458 345
4369 0005278 334
3332 25
7567 15
71956910 13132
Satellite: ISS
Catalog Number: 25544
Epoch time: 10356
72821170 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 345
4369 deg
Eccentricity:
0005278
Arg of perigee: 334
3332 deg
Mean anomaly: 25
7567 deg
Mean motion: 15
71956910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 307
Coasting Arc #12 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/357/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6060943
35 A = 6737771
10 meter
Y = 2843047
63 meter E =
0009243
Z = 734269
95 I = 51
54972
XDOT = -2642
433071 Wp = 110
77570
YDOT = -4077
439432 meter/sec RA = 339
86595 deg
ZDOT = -5966
901257 TA = 61
22182
MA = 61
12901
Ha = 193
459 n
mi
Hp = 187
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19884984
74 X = -6095851
29
Y = 9327584
10 feet Y = 2775075
24 meter
Z = 2409022
14 Z = 704741
76
XDOT = -8669
399838 XDOT = -2567
656180
YDOT = -13377
425958 feet/sec YDOT = -4106
569871 meter/sec
ZDOT = -19576
447692 ZDOT = -5979
556931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21425706
14 X = -6530555
23
Y = 4890222
66 feet Y = 1490539
87 meter
Z = 2290124
42 Z = 698029
92
XDOT = -5160
663001 XDOT = -1572
970083
YDOT = -13326
671960 feet/sec YDOT = -4061
969613 meter/sec
ZDOT = -19627
201612 ZDOT = -5982
371051
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 10357
74536254
00016717 00000-0 10270-3 0 9111
2 25544 51
6461 340
2295 0005216 337
8913 22
2023 15
71961508 13297
Satellite: ISS
Catalog Number: 25544
Epoch time: 10357
74536254 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 340
2295 deg
Eccentricity:
0005216
Arg of perigee: 337
8913 deg
Mean anomaly: 22
2023 deg
Mean motion: 15
71961508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 292
Coasting Arc #13 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/358/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3305061
51 A = 6726502
81 meter
Y = 2912453
25 meter E =
0003102
Z = 5080935
20 I = 51
48447
XDOT = -6193
494893 Wp = 44
19165
YDOT = 4298
450163 meter/sec RA = 334
75696 deg
ZDOT = 1566
454833 TA = 30
74724
MA = 30
72907
Ha = 193
396 n
mi
Hp = 187
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10843377
66 X = 3247566
31
Y = 9555292
83 feet Y = 2949090
47 meter
Z = 16669734
90 Z = 5096851
63
XDOT = -20319
865136 XDOT = -6248
710116
YDOT = 14102
526782 feet/sec YDOT = 4228
881894 meter/sec
ZDOT = 5139
287510 ZDOT = 1536
233497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8668681
99 X = 2642214
27
Y = 11471758
54 feet Y = 3496592
00 meter
Z = 16733655
62 Z = 5100418
23
XDOT = -21877
710814 XDOT = -6668
326256
YDOT = 9220
673895 feet/sec YDOT = 2810
461403 meter/sec
ZDOT = 5017
548866 ZDOT = 1529
348894
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 10358
76249296
00016717 00000-0 10270-3 0 9122
2 25544 51
6463 335
0220 0005269 341
3888 18
7081 15
72023657 13455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10358
76249296 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 335
0220 deg
Eccentricity:
0005269
Arg of perigee: 341
3888 deg
Mean anomaly: 18
7081 deg
Mean motion: 15
72023657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 311
Coasting Arc #14 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/359/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4582010
67 A = 6736081
89 meter
Y = -4514872
36 meter E =
0010910
Z = -1979304
46 I = 51
49033
XDOT = 4740
435193 Wp = 15
70742
YDOT = 2370
408724 meter/sec RA = 329
59512 deg
ZDOT = 5584
405734 TA = 322
21682
MA = 322
29337
Ha = 193
594 n
mi
Hp = 187
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15032843
40 X = 4641771
27
Y = -14812573
36 feet Y = -4463299
27 meter
Z = -6493781
02 Z = -1956900
47
XDOT = 15552
608902 XDOT = 4686
448770
YDOT = 7776
931509 feet/sec YDOT = 2423
116847 meter/sec
ZDOT = 18321
541122 ZDOT = 5607
303578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17474201
59 X = 5326136
65
Y = -11883413
40 feet Y = -3622064
41 meter
Z = -6403488
64 Z = -1951783
34
XDOT = 12939
499755 XDOT = 3943
959525
YDOT = 9136
167338 feet/sec YDOT = 2784
703804 meter/sec
ZDOT = 18413
569673 ZDOT = 5612
456036
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 10359
71603692
00016717 00000-0 10270-3 0 9133
2 25544 51
6469 330
1400 0005321 345
2354 14
8652 15
72047561 13605
Satellite: ISS
Catalog Number: 25544
Epoch time: 10359
71603692 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 330
1400 deg
Eccentricity:
0005321
Arg of perigee: 345
2354 deg
Mean anomaly: 14
8652 deg
Mean motion: 15
72047561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 282
Coasting Arc #15 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/360/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4778288
68 A = 6728302
07 meter
Y = -1112201
00 meter E =
0012704
Z = -4616444
86 I = 51
43908
XDOT = 4146
854173 Wp = 45
07082
YDOT = -5790
599067 meter/sec RA = 324
50210 deg
ZDOT = -2893
188706 TA = 196
13873
MA = 196
17923
Ha = 193
622 n
mi
Hp = 186
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15676800
13 X = -4743071
01
Y = -3648953
41 feet Y = -1165437
50 meter
Z = -15145816
48 Z = -4639572
15
XDOT = 13605
164608 XDOT = 4225
352019
YDOT = -18998
028436 feet/sec YDOT = -5743
787361 meter/sec
ZDOT = -9492
088929 ZDOT = -2872
853119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14791502
92 X = -4508450
09
Y = -6120677
70 feet Y = -1865582
56 meter
Z = -15238813
15 Z = -4644790
25
XDOT = 16106
109598 XDOT = 4909
142205
YDOT = -15462
021754 feet/sec YDOT = -4712
824231 meter/sec
ZDOT = -9410
078412 ZDOT = -2868
191900
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 10360
73313093
00016717 00000-0 10270-3 0 9141
2 25544 51
6470 324
9326 0005415 348
7758 11
3283 15
72082648 13769
Satellite: ISS
Catalog Number: 25544
Epoch time: 10360
73313093 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 324
9326 deg
Eccentricity:
0005415
Arg of perigee: 348
7758 deg
Mean anomaly: 11
3283 deg
Mean motion: 15
72082648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 304
Coasting Arc #16 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/361/17:05:34
409
Vector Time (MET): N/A
Weight (LBS) : 812550
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2583149
42 A = 6733637
69 meter
Y = 5419708
58 meter E =
0013114
Z = 3043006
19 I = 51
43239
XDOT = -5930
727457 Wp = 72
27258
YDOT = -60
390065 meter/sec RA = 319
32071 deg
ZDOT = -4905
650426 TA = 72
40229
MA = 72
25909
Ha = 193
746 n
mi
Hp = 186
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8474899
68 X = -2658343
96
Y = 17781196
13 feet Y = 5390401
63 meter
Z = 9983616
09 Z = 3030274
96
XDOT = -19457
767248 XDOT = -5905
780686
YDOT = -198
130136 feet/sec YDOT = -126
571254 meter/sec
ZDOT = -16094
653629 ZDOT = -4934
401225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11016147
97 X = -3357721
90
Y = 16360411
10 feet Y = 4986653
30 meter
Z = 9932214
41 Z = 3027338
95
XDOT = -17936
194612 XDOT = -5466
952118
YDOT = -2193
510829 feet/sec YDOT = -668
582101 meter/sec
ZDOT = -16210
306867 ZDOT = -4940
901533
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 10361
75020690
00016717 00000-0 10270-3 0 9153
2 25544 51
6466 319
7248 0005369 353
5627 6
5465 15
72092695 13925
Satellite: ISS
Catalog Number: 25544
Epoch time: 10361
75020690 = yrday
fracday
Element set: 915
Inclination: 51
6466 deg
RA of node: 319
7248 deg
Eccentricity:
0005369
Arg of perigee: 353
5627 deg
Mean anomaly: 6
5465 deg
Mean motion: 15
72092695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 322
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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