Date:
October 21st 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
293/19:42:54
398 0
8 1
6 1
6
N/A 0
5 -0
0 195
8
000/00:03:48
797 1
3 -0
1 184
6
Coasting Arc #1 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620499
94 A = 6737321
96 meter
Y = 4828044
65 meter E =
0020701
Z = 785226
38 I = 51
44299
XDOT = -3984
345543 Wp = 119
42736
YDOT = -2827
293591 meter/sec RA = 319
11558 deg
ZDOT = -5953
638611 TA = 51
99021
MA = 51
80348
Ha = 195
701 n
mi
Hp = 184
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15159120
53 X = -4677959
15
Y = 15840041
52 feet Y = 4776054
24 meter
Z = 2576202
03 Z = 762639
77
XDOT = -13071
999814 XDOT = -3923
512026
YDOT = -9275
897609 feet/sec YDOT = -2871
509260 meter/sec
ZDOT = -19532
935076 ZDOT = -5972
846819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6662066
08 X = 2030597
74
Y = -20899312
18 feet Y = -6370110
35 meter
Z = 2485617
28 Z = 757616
15
XDOT = 14191
270439 XDOT = 4325
499230
YDOT = 2148
005584 feet/sec YDOT = 654
712102 meter/sec
ZDOT = -19609
902149 ZDOT = -5977
098175
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10291
53330723
00016717 00000-0 10270-3 0 9006
2 25544 51
6452 319
5263 0007544 106
9328 253
2662 15
72108297 2878
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53330723 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 319
5263 deg
Eccentricity:
0007544
Arg of perigee: 106
9328 deg
Mean anomaly: 253
2662 deg
Mean motion: 15
72108297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 298
Coasting Arc #2 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2010/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147190
02 A = 6726214
43 meter
Y = 1526630
05 meter E =
0012357
Z = 5062423
52 I = 51
38293
XDOT = -4246
870085 Wp = 115
89715
YDOT = 6228
927152 meter/sec RA = 313
99921 deg
ZDOT = 1592
347372 TA = 318
71938
MA = 318
81273
Ha = 195
546 n
mi
Hp = 183
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13606266
46 X = 4105217
98
Y = 5008628
78 feet Y = 1572772
17 meter
Z = 16609001
05 Z = 5082468
82
XDOT = -13933
300803 XDOT = -4323
942927
YDOT = 20436
112704 feet/sec YDOT = 6181
005293 meter/sec
ZDOT = 5224
236786 ZDOT = 1571
528004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14307116
31 X = -4360809
05
Y = 1687691
65 feet Y = 514408
42 meter
Z = 16689334
48 Z = 5086909
15
XDOT = 3255
230924 XDOT = 992
194386
YDOT = -23509
237509 feet/sec YDOT = -7165
615593 meter/sec
ZDOT = 5140
730122 ZDOT = 1566
894541
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10292
55035675
00016717 00000-0 10270-3 0 9018
2 25544 51
6443 314
3183 0007599 110
3890 249
8089 15
72139055 3034
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
55035675 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 314
3183 deg
Eccentricity:
0007599
Arg of perigee: 110
3890 deg
Mean anomaly: 249
8089 deg
Mean motion: 15
72139055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 306
Coasting Arc #3 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2010/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2700950
68 A = 6735632
40 meter
Y = -5852250
05 meter E =
0011575
Z = -1960548
48 I = 51
39579
XDOT = 5261
713091 Wp = 78
60760
YDOT = 568
917175 meter/sec RA = 308
82962 deg
ZDOT = 5580
670102 TA = 259
52954
MA = 259
66000
Ha = 195
555 n
mi
Hp = 183
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8861386
75 X = 2775715
07
Y = -19200295
46 feet Y = -5821628
53 meter
Z = -6432245
65 Z = -1947244
89
XDOT = 17262
838225 XDOT = 5227
849829
YDOT = 1866
526166 feet/sec YDOT = 627
567943 meter/sec
ZDOT = 18309
285111 ZDOT = 5606
149733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1178639
00 X = 359249
17
Y = 21129838
88 feet Y = 6440374
89 meter
Z = -6378873
26 Z = -1944280
57
XDOT = -14474
916643 XDOT = -4411
954593
YDOT = 6335
577801 feet/sec YDOT = 1931
084114 meter/sec
ZDOT = 18411
405842 ZDOT = 5611
796501
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10293
50382062
00016717 00000-0 10270-3 0 9020
2 25544 51
6451 309
4362 0007640 114
2452 245
9509 15
72208115 3185
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
50382062 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 309
4362 deg
Eccentricity:
0007640
Arg of perigee: 114
2452 deg
Mean anomaly: 245
9509 deg
Mean motion: 15
72208115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 279
Coasting Arc #4 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2010/293/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4410057
69 A = 6738092
29 meter
Y = -5054425
49 meter E =
0018204
Z = 573038
20 I = 51
39541
XDOT = 3288
338122 Wp = 68
29761
YDOT = 3563
435534 meter/sec RA = 307
19415 deg
ZDOT = 5978
830919 TA = 297
95543
MA = 298
13956
Ha = 195
822 n
mi
Hp = 184
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14468693
21 X = 4463465
67
Y = -16582760
78 feet Y = -5004810
90 meter
Z = 1880046
57 Z = 594592
88
XDOT = 10788
510898 XDOT = 3219
201993
YDOT = 11691
061464 feet/sec YDOT = 3599
821640 meter/sec
ZDOT = 19615
587006 ZDOT = 5994
637792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21392196
75 X = 6520341
57
Y = -5135414
36 feet Y = -1565274
30 meter
Z = 1966481
91 Z = 599383
69
XDOT = 1546
667873 XDOT = 471
424368
YDOT = 14152
909073 feet/sec YDOT = 4313
806685 meter/sec
ZDOT = 19678
912292 ZDOT = 5998
132467
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10293
88521400
00016717 00000-0 10270-3 0 9033
2 25544 51
6458 307
4832 0006799 104
1030 256
0888 15
71870440 3241
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
88521400 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 307
4832 deg
Eccentricity:
0006799
Arg of perigee: 104
1030 deg
Mean anomaly: 256
0888 deg
Mean motion: 15
71870440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 298
Coasting Arc #5 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2010/294/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3623352
00 A = 6726022
00 meter
Y = -2146990
77 meter E =
0021566
Z = -5262647
86 I = 51
33818
XDOT = 4012
825400 Wp = 94
89127
YDOT = -6549
602542 meter/sec RA = 302
04981 deg
ZDOT = -92
954474 TA = 174
23322
MA = 174
20835
Ha = 195
704 n
mi
Hp = 184
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11887637
79 X = -3573508
98
Y = -7043932
98 feet Y = -2187230
97 meter
Z = -17265905
05 Z = -5280129
34
XDOT = 13165
437664 XDOT = 4086
217592
YDOT = -21488
197317 feet/sec YDOT = -6504
318365 meter/sec
ZDOT = -304
968747 ZDOT = -73
280904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5736882
10 X = -1748601
67
Y = -12473865
74 feet Y = -3802034
28 meter
Z = -17335952
77 Z = -5283998
41
XDOT = 22100
640806 XDOT = 6736
275318
YDOT = -9859
874449 feet/sec YDOT = -3005
289732 meter/sec
ZDOT = -226
064850 ZDOT = -68
904566
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10294
83883194
00016717 00000-0 10270-3 0 9041
2 25544 51
6461 302
6012 0006767 107
8385 252
3516 15
71927762 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 10294
83883194 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 302
6012 deg
Eccentricity:
0006767
Arg of perigee: 107
8385 deg
Mean anomaly: 252
3516 deg
Mean motion: 15
71927762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 318
Coasting Arc #6 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2010/295/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2497718
40 A = 6737916
50 meter
Y = 6206077
91 meter E =
0020092
Z = 726295
89 I = 51
36280
XDOT = -4733
026806 Wp = 122
30888
YDOT = -1194
968207 meter/sec RA = 296
90156 deg
ZDOT = -5956
713298 TA = 49
74871
MA = 49
57316
Ha = 195
714 n
mi
Hp = 184
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8194614
16 X = -2570458
59
Y = 20361147
99 feet Y = 6177740
25 meter
Z = 2382860
53 Z = 713984
58
XDOT = -15528
303170 XDOT = -4690
375189
YDOT = -3920
499368 feet/sec YDOT = -1247
657618 meter/sec
ZDOT = -19543
022631 ZDOT = -5979
603342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18071625
50 X = -5508231
45
Y = 12465045
08 feet Y = 3799345
74 meter
Z = 2333468
63 Z = 711241
24
XDOT = -9789
536580 XDOT = -2983
850750
YDOT = -10448
535708 feet/sec YDOT = -3184
713684 meter/sec
ZDOT = -19634
753848 ZDOT = -5984
672973
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10295
85600481
00016717 00000-0 10270-3 0 9051
2 25544 51
6459 297
3937 0006846 112
8573 247
3312 15
71910195 3557
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
85600481 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 297
3937 deg
Eccentricity:
0006846
Arg of perigee: 112
8573 deg
Mean anomaly: 247
3312 deg
Mean motion: 15
71910195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 322
Coasting Arc #7 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2010/296/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4420505
63 A = 6726664
54 meter
Y = -141007
77 meter E =
0011575
Z = 5060902
53 I = 51
31322
XDOT = -1583
255307 Wp = 119
38794
YDOT = 7372
341312 meter/sec RA = 291
77998 deg
ZDOT = 1580
004033 TA = 315
33311
MA = 315
42629
Ha = 195
438 n
mi
Hp = 184
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14502971
23 X = 4397168
15
Y = -462623
93 feet Y = -91705
33 meter
Z = 16604010
92 Z = 5082321
32
XDOT = -5194
407174 XDOT = -1673
252132
YDOT = 24187
471497 feet/sec YDOT = 7354
133256 meter/sec
ZDOT = 5183
740266 ZDOT = 1572
093476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12401530
52 X = 3779986
50
Y = 7341260
95 feet Y = 2237616
34 meter
Z = 16689856
28 Z = 5087068
19
XDOT = -16855
599234 XDOT = -5137
586647
YDOT = 16699
626167 feet/sec YDOT = 5090
046056 meter/sec
ZDOT = 5151
976897 ZDOT = 1570
322558
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10296
87315298
00016717 00000-0 10270-3 0 9064
2 25544 51
6462 292
1861 0006749 115
3781 244
8080 15
71982843 3712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10296
87315298 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 292
1861 deg
Eccentricity:
0006749
Arg of perigee: 115
3781 deg
Mean anomaly: 244
8080 deg
Mean motion: 15
71982843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 371
Checksum: 330
Coasting Arc #8 (Orbit 385)
---------------------------------------
Vector Time (GMT): 2010/297/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 251657
86 A = 6736090
06 meter
Y = -6430249
12 meter E =
0010321
Z = -1995203
06 I = 51
33502
XDOT = 5093
946999 Wp = 78
45068
YDOT = -1517
288796 meter/sec RA = 286
60533 deg
ZDOT = 5558
848097 TA = 259
26080
MA = 259
37701
Ha = 195
427 n
mi
Hp = 184
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 825649
16 X = 333236
03
Y = -21096617
85 feet Y = -6426978
83 meter
Z = -6545941
80 Z = -1993782
24
XDOT = 16712
424538 XDOT = 5083
530300
YDOT = -4977
981613 feet/sec YDOT = -1460
383397 meter/sec
ZDOT = 18237
690608 ZDOT = 5583
569962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11752744
50 X = 3582236
52
Y = -17541298
89 feet Y = -5346587
90 meter
Z = -6540196
10 Z = -1993451
77
XDOT = 15480
493088 XDOT = 4718
454293
YDOT = 3567
454312 feet/sec YDOT = 1087
360074 meter/sec
ZDOT = 18336
787198 ZDOT = 5589
052738
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10297
82670936
00016717 00000-0 10270-3 0 9074
2 25544 51
6461 287
3036 0006591 118
7336 241
4489 15
72018496 3866
Satellite: ISS
Catalog Number: 25544
Epoch time: 10297
82670936 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 287
3036 deg
Eccentricity:
0006591
Arg of perigee: 118
7336 deg
Mean anomaly: 241
4489 deg
Mean motion: 15
72018496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 386
Checksum: 334
Coasting Arc #9 (Orbit 401)
---------------------------------------
Vector Time (GMT): 2010/298/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263264
73 A = 6728453
81 meter
Y = 2453964
93 meter E =
0015446
Z = -4604082
55 I = 51
30161
XDOT = -936
566582 Wp = 89
68931
YDOT = -7055
721070 meter/sec RA = 281
50146 deg
ZDOT = -2901
767086 TA = 151
42428
MA = 151
33953
Ha = 195
272 n
mi
Hp = 184
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13987089
00 X = -4268022
11
Y = 8051066
05 feet Y = 2406263
98 meter
Z = -15105257
72 Z = -4624805
62
XDOT = -3072
725005 XDOT = -843
501928
YDOT = -23148
691176 feet/sec YDOT = -7065
673942 meter/sec
ZDOT = -9520
233222 ZDOT = -2906
091059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16060153
78 X = -4895134
87
Y = -113971
04 feet Y = -34738
37 meter
Z = -15188337
79 Z = -4629405
36
XDOT = 9138
201685 XDOT = 2785
323873
YDOT = -20307
134048 feet/sec YDOT = -6189
614458 meter/sec
ZDOT = -9537
509242 ZDOT = -2907
032817
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10298
84381394
00016717 00000-0 10270-3 0 9085
2 25544 51
6456 282
0953 0006487 123
1210 237
0576 15
72051025 4027
Satellite: ISS
Catalog Number: 25544
Epoch time: 10298
84381394 = yrday
fracday
Element set: 908
Inclination: 51
6456 deg
RA of node: 282
0953 deg
Eccentricity:
0006487
Arg of perigee: 123
1210 deg
Mean anomaly: 237
0576 deg
Mean motion: 15
72051025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 402
Checksum: 296
Coasting Arc #10 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2010/299/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1829422
24 A = 6733463
09 meter
Y = 5703755
77 meter E =
0019038
Z = 3053823
41 I = 51
31463
XDOT = -4383
490024 Wp = 105
35229
YDOT = 4033
620047 meter/sec RA = 276
31071 deg
ZDOT = -4887
467378 TA = 39
06557
MA = 38
92824
Ha = 195
128 n
mi
Hp = 184
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6002041
47 X = 1750670
52
Y = 18713109
49 feet Y = 5723773
08 meter
Z = 10019105
68 Z = 3062519
81
XDOT = -14381
528949 XDOT = -4404
525881
YDOT = 13233
661570 feet/sec YDOT = 3984
483722 meter/sec
ZDOT = -16034
997959 ZDOT = -4908
813917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4044420
56 X = -1232739
39
Y = 19213244
52 feet Y = 5856196
93 meter
Z = 10053921
84 Z = 3064435
38
XDOT = -17549
523525 XDOT = -5349
094770
YDOT = 4776
164198 feet/sec YDOT = 1455
774847 meter/sec
ZDOT = -16120
592671 ZDOT = -4913
556646
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10299
86089547
00016717 00000-0 10270-3 0 9094
2 25544 51
6461 276
8877 0006504 125
9292 234
2475 15
72117324 4188
Satellite: ISS
Catalog Number: 25544
Epoch time: 10299
86089547 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 276
8877 deg
Eccentricity:
0006504
Arg of perigee: 125
9292 deg
Mean anomaly: 234
2475 deg
Mean motion: 15
72117324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 336
Coasting Arc #11 (Orbit 433)
---------------------------------------
Vector Time (GMT): 2010/300/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3199401
69 A = 6731008
59 meter
Y = -4470699
52 meter E =
0017135
Z = 3874612
40 I = 51
30303
XDOT = 3121
449512 Wp = 110
63166
YDOT = 5760
071265 meter/sec RA = 271
21590 deg
ZDOT = 4048
331487 TA = 296
94085
MA = 297
11579
Ha = 195
099 n
mi
Hp = 184
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10496724
69 X = 3230333
52
Y = -14667649
33 feet Y = -4434749
04 meter
Z = 12711982
93 Z = 3890230
43
XDOT = 10240
976089 XDOT = 3037
140852
YDOT = 18897
871605 feet/sec YDOT = 5794
505680 meter/sec
ZDOT = 13281
927452 ZDOT = 4063
291183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16159372
53 X = 4925376
75
Y = -7911980
42 feet Y = -2411571
63 meter
Z = 12774620
20 Z = 3893704
24
XDOT = -671
065052 XDOT = -204
540628
YDOT = 20278
637155 feet/sec YDOT = 6180
928605 meter/sec
ZDOT = 13341
857166 ZDOT = 4066
598064
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10300
87795492
00016717 00000-0 10270-3 0 9103
2 25544 51
6450 271
6791 0006483 130
0683 230
1049 15
72100053 4342
Satellite: ISS
Catalog Number: 25544
Epoch time: 10300
87795492 = yrday
fracday
Element set: 910
Inclination: 51
6450 deg
RA of node: 271
6791 deg
Eccentricity:
0006483
Arg of perigee: 130
0683 deg
Mean anomaly: 230
1049 deg
Mean motion: 15
72100053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 434
Checksum: 279
Coasting Arc #12 (Orbit 448)
---------------------------------------
Vector Time (GMT): 2010/301/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3469635
34 A = 6730559
23 meter
Y = -4210943
73 meter E =
0013116
Z = -3955629
70 I = 51
30181
XDOT = 2758
944158 Wp = 120
95510
YDOT = -5985
032540 meter/sec RA = 266
01817 deg
ZDOT = 3954
424273 TA = 190
27476
MA = 190
30159
Ha = 194
995 n
mi
Hp = 184
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11383318
04 X = -3403073
85
Y = -13815432
18 feet Y = -4249371
02 meter
Z = -12977787
74 Z = -3972323
90
XDOT = 9051
654061 XDOT = 2806
454644
YDOT = -19635
933531 feet/sec YDOT = -5953
914815 meter/sec
ZDOT = 12973
832917 ZDOT = 3967
942717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3638960
52 X = -1109155
17
Y = -17477502
32 feet Y = -5327142
71 meter
Z = -13044690
49 Z = -3976021
66
XDOT = 15760
288936 XDOT = 4803
736068
YDOT = -12997
709649 feet/sec YDOT = -3961
701901 meter/sec
ZDOT = 13028
061503 ZDOT = 3970
953146
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 10301
83142418
00016717 00000-0 10270-3 0 9115
2 25544 51
6441 266
7957 0006512 135
0653 225
1037 15
72165477 4494
Satellite: ISS
Catalog Number: 25544
Epoch time: 10301
83142418 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 266
7957 deg
Eccentricity:
0006512
Arg of perigee: 135
0653 deg
Mean anomaly: 225
1037 deg
Mean motion: 15
72165477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 449
Checksum: 293
Coasting Arc #13 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2010/302/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1521021
40 A = 6733345
14 meter
Y = 5821216
83 meter E =
0010628
Z = -3022505
79 I = 51
31375
XDOT = -4585
086721 Wp = 126
42646
YDOT = -3741
655462 meter/sec RA = 260
92348 deg
ZDOT = -4917
117031 TA = 88
67890
MA = 88
55716
Ha = 194
869 n
mi
Hp = 184
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4990227
69 X = -1571319
29
Y = 19098480
41 feet Y = 5803926
65 meter
Z = -9916357
58 Z = -3030017
14
XDOT = -15042
935435 XDOT = -4519
019261
YDOT = -12275
772512 feet/sec YDOT = -3792
559211 meter/sec
ZDOT = -16132
273724 ZDOT = -4939
231243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12947049
33 X = -3946260
64
Y = 14880509
98 feet Y = 4535579
44 meter
Z = -9946497
40 Z = -3031692
41
XDOT = -6798
976191 XDOT = -2072
327943
YDOT = -16718
213666 feet/sec YDOT = -5095
711526 meter/sec
ZDOT = -16220
919331 ZDOT = -4944
136212
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 10302
84843608
00016717 00000-0 10270-3 0 9127
2 25544 51
6432 261
5877 0006495 139
1245 221
0405 15
72188392 4653
Satellite: ISS
Catalog Number: 25544
Epoch time: 10302
84843608 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 261
5877 deg
Eccentricity:
0006495
Arg of perigee: 139
1245 deg
Mean anomaly: 221
0405 deg
Mean motion: 15
72188392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 304
Coasting Arc #14 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2010/303/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4366535
08 A = 6727895
74 meter
Y = 2230980
80 meter E =
0011347
Z = 4596137
06 I = 51
30193
XDOT = -583
563827 Wp = 98
33199
YDOT = 7116
680051 meter/sec RA = 255
73103 deg
ZDOT = -2895
581997 TA = 20
47432
MA = 20
42888
Ha = 194
621 n
mi
Hp = 184
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14325902
50 X = 4318935
82
Y = 7319490
80 feet Y = 2279543
93 meter
Z = 15079189
84 Z = 4617234
31
XDOT = -1914
579485 XDOT = -649
034100
YDOT = 23348
687833 feet/sec YDOT = 7109
788191 meter/sec
ZDOT = -9499
940934 ZDOT = -2898
576100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9684123
03 X = 2951720
70
Y = 12746220
08 feet Y = 3885047
88 meter
Z = 15163773
57 Z = 4621918
18
XDOT = -10821
298083 XDOT = -3298
331656
YDOT = 19555
059022 feet/sec YDOT = 5960
381990 meter/sec
ZDOT = -9511
965429 ZDOT = -2899
247063
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 10303
86542304
00016717 00000-0 10270-3 0 9130
2 25544 51
6432 256
3784 0006485 143
7330 216
4273 15
72239043 4816
Satellite: ISS
Catalog Number: 25544
Epoch time: 10303
86542304 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 256
3784 deg
Eccentricity:
0006485
Arg of perigee: 143
7330 deg
Mean anomaly: 216
4273 deg
Mean motion: 15
72239043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 290
Coasting Arc #15 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2010/304/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -539741
63 A = 6735310
23 meter
Y = -6399335
00 meter E =
0016670
Z = 2016812
02 I = 51
33457
XDOT = 5170
357400 Wp = 91
70287
YDOT = 1324
568908 meter/sec RA = 250
62525 deg
ZDOT = 5546
553310 TA = 290
86189
MA = 291
04031
Ha = 194
665 n
mi
Hp = 184
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1770805
89 X = -477940
41
Y = -20995193
58 feet Y = -6405025
10 meter
Z = 6616837
33 Z = 2014340
25
XDOT = 16963
114828 XDOT = 5128
217019
YDOT = 4345
698518 feet/sec YDOT = 1382
151519 meter/sec
ZDOT = 18197
353379 ZDOT = 5571
568849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7085834
66 X = 2159762
41
Y = -19845800
79 feet Y = -6049000
08 meter
Z = 6606934
35 Z = 2013793
59
XDOT = 12072
946261 XDOT = 3679
834020
YDOT = 10445
865166 feet/sec YDOT = 3183
899703 meter/sec
ZDOT = 18297
657211 ZDOT = 5577
125918
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 10304
88238602
00016717 00000-0 10270-3 0 9147
2 25544 51
6419 251
1686 0006623 147
8913 212
2654 15
72284121 4972
Satellite: ISS
Catalog Number: 25544
Epoch time: 10304
88238602 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 251
1686 deg
Eccentricity:
0006623
Arg of perigee: 147
8913 deg
Mean anomaly: 212
2654 deg
Mean motion: 15
72284121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 497
Checksum: 303
Coasting Arc #16 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2010/305/19:44:48
797
Vector Time (MET): N/A
Weight (LBS) : 827002
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4477791
05 A = 6725926
22 meter
Y = -100430
60 meter E =
0018685
Z = -5034188
42 I = 51
31389
XDOT = -1792
523340 Wp = 118
56088
YDOT = -7267
861780 meter/sec RA = 245
44633 deg
ZDOT = 1735
487515 TA = 168
27920
MA = 168
23565
Ha = 194
604 n
mi
Hp = 184
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14690915
53 X = -4451879
61
Y = -329496
71 feet Y = -150359
31 meter
Z = -16516366
21 Z = -5055878
96
XDOT = -5880
982085 XDOT = -1719
550365
YDOT = -23844
690880 feet/sec YDOT = -7287
498757 meter/sec
ZDOT = 5693
856678 ZDOT = 1726
956890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13240892
60 X = -4035824
06
Y = -6142449
34 feet Y = -1872218
56 meter
Z = -16603343
01 Z = -5060698
95
XDOT = 3674
299393 XDOT = 1119
926455
YDOT = -23253
272869 feet/sec YDOT = -7087
597570 meter/sec
ZDOT = 5659
650024 ZDOT = 1725
061327
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 10305
83576755
00016717 00000-0 10270-3 0 9158
2 25544 51
6414 246
2839 0006720 150
5339 209
6204 15
72306875 5123
Satellite: ISS
Catalog Number: 25544
Epoch time: 10305
83576755 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 246
2839 deg
Eccentricity:
0006720
Arg of perigee: 150
5339 deg
Mean anomaly: 209
6204 deg
Mean motion: 15
72306875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 305
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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