Date:
May 22nd 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
There are no maneuvers
Coasting Arc #1 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2010/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6304453
10 A = 6729560
94 meter
Y = -15478
83 meter E =
0009789
Z = 2355074
10 I = 51
76143
XDOT = -2016
032398 Wp = 59
76722
YDOT = -5089
603831 meter/sec RA = 17
26026 deg
ZDOT = -5408
819032 TA = 93
77552
MA = 93
66358
Ha = 191
263 n
mi
Hp = 184
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20683901
24 X = -6315251
98
Y = -50783
55 feet Y = -86039
60 meter
Z = 7726621
07 Z = 2324420
82
XDOT = -6614
279522 XDOT = -1932
694623
YDOT = -16698
175299 feet/sec YDOT = -5111
681778 meter/sec
ZDOT = -17745
469265 ZDOT = -5418
411022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11550670
39 X = -3520644
33
Y = 17212795
02 feet Y = 5246459
92 meter
Z = 7604519
96 Z = 2317857
68
XDOT = -16247
544482 XDOT = -4952
251558
YDOT = -3014
571421 feet/sec YDOT = -918
841369 meter/sec
ZDOT = -17783
666998 ZDOT = -5420
461701
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 10139
53636341
00016717 00000-0 10270-3 0 9002
2 25544 51
6477 17
6130 0010216 331
6772 28
3835 15
74098918 18964
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
53636341 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 17
6130 deg
Eccentricity:
0010216
Arg of perigee: 331
6772 deg
Mean anomaly: 28
3835 deg
Mean motion: 15
74098918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 310
Coasting Arc #2 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2010/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2071275
73 A = 6721960
90 meter
Y = 4280641
13 meter E =
0006134
Z = 4746683
01 I = 51
70712
XDOT = -7215
994765 Wp = 19
88289
YDOT = 573
224545 meter/sec RA = 12
17079 deg
ZDOT = 2636
516469 TA = 44
28990
MA = 44
24084
Ha = 191
385 n
mi
Hp = 183
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6795524
06 X = 2000196
35
Y = 14044098
19 feet Y = 4303405
56 meter
Z = 15573107
00 Z = 4756572
97
XDOT = -23674
523506 XDOT = -7234
676084
YDOT = 1880
657957 feet/sec YDOT = 492
426331 meter/sec
ZDOT = 8649
988414 ZDOT = 2601
415803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15438884
35 X = 4705771
95
Y = 1956629
08 feet Y = 596380
54 meter
Z = 15612493
57 Z = 4758688
04
XDOT = -11105
799629 XDOT = -3385
047727
YDOT = 19847
755558 feet/sec YDOT = 6049
595894 meter/sec
ZDOT = 8510
172038 ZDOT = 2593
900437
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 10140
55211737
00016717 00000-0 10270-3 0 9015
2 25544 51
6478 12
3955 0010345 335
4181 24
6488 15
74122495 19121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
55211737 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 12
3955 deg
Eccentricity:
0010345
Arg of perigee: 335
4181 deg
Mean anomaly: 24
6488 deg
Mean motion: 15
74122495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 290
Coasting Arc #3 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2010/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6251329
96 A = 6729602
46 meter
Y = -1020581
63 meter E =
0014243
Z = -2247328
37 I = 51
70270
XDOT = 2727
968519 Wp =
33200
YDOT = 4689
179967 meter/sec RA = 6
99851 deg
ZDOT = 5472
949957 TA = 334
45004
MA = 334
52037
Ha = 191
592 n
mi
Hp = 183
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20509612
72 X = 6273194
82
Y = -3348364
93 feet Y = -950553
14 meter
Z = -7373124
57 Z = -2216906
24
XDOT = 8950
027951 XDOT = 2648
743812
YDOT = 15384
448712 feet/sec YDOT = 4719
242428 meter/sec
ZDOT = 17955
872562 ZDOT = 5486
010332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7968563
13 X = 2428818
04
Y = -19238762
92 feet Y = -5863974
94 meter
Z = -7251946
66 Z = -2210393
34
XDOT = 16333
540038 XDOT = 4978
463004
YDOT = -4
956434 feet/sec YDOT = -1
510721 meter/sec
ZDOT = 18007
885772 ZDOT = 5488
803583
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 10141
50436874
00016717 00000-0 10270-3 0 9023
2 25544 51
6474 7
5044 0010531 337
9667 22
1042 15
74156262 19279
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
50436874 = yrday
fracday
Element set: 902
Inclination: 51
6474 deg
RA of node: 7
5044 deg
Eccentricity:
0010531
Arg of perigee: 337
9667 deg
Mean anomaly: 22
1042 deg
Mean motion: 15
74156262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 286
Coasting Arc #4 (Orbit 1942)
---------------------------------------
Vector Time (GMT): 2010/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2646812
73 A = 6721519
79 meter
Y = -3894872
86 meter E =
0015766
Z = -4808236
34 I = 51
64503
XDOT = 7071
116407 Wp = 30
14067
YDOT = -1729
706527 meter/sec RA = 1
90337 deg
ZDOT = -2481
465120 TA = 215
51106
MA = 215
61610
Ha = 191
567 n
mi
Hp = 183
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8683768
80 X = -2579705
10
Y = -12778454
27 feet Y = -3924095
61 meter
Z = -15775053
60 Z = -4820931
88
XDOT = 23199
200810 XDOT = 7101
987363
YDOT = -5674
890180 feet/sec YDOT = -1650
460343 meter/sec
ZDOT = -8141
289765 ZDOT = -2447
038456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15374847
91 X = -4686253
64
Y = 844450
67 feet Y = 257388
57 meter
Z = -15825612
32 Z = -4823646
64
XDOT = 7077
084499 XDOT = 2157
095355
YDOT = -21756
870829 feet/sec YDOT = -6631
494229 meter/sec
ZDOT = -8004
165038 ZDOT = -2439
669504
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 10142
52008616
00016717 00000-0 10270-3 0 9036
2 25544 51
6465 2
2872 0010520 341
4973 18
5807 15
74197600 19435
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
52008616 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 2
2872 deg
Eccentricity:
0010520
Arg of perigee: 341
4973 deg
Mean anomaly: 18
5807 deg
Mean motion: 15
74197600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1943
Checksum: 285
Coasting Arc #5 (Orbit 1958)
---------------------------------------
Vector Time (GMT): 2010/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6083645
57 A = 6729653
87 meter
Y = 1993388
19 meter E =
0011725
Z = 2076167
07 I = 51
64298
XDOT = -3281
158602 Wp = 63
22090
YDOT = -4207
933993 meter/sec RA = 356
72900 deg
ZDOT = -5545
194472 TA = 93
61291
MA = 93
47881
Ha = 191
699 n
mi
Hp = 183
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19959467
10 X = -6115569
62
Y = 6539987
51 feet Y = 1925178
61 meter
Z = 6811571
76 Z = 2046534
91
XDOT = -10764
956044 XDOT = -3206
922948
YDOT = -13805
557720 feet/sec YDOT = -4244
210430 meter/sec
ZDOT = -18192
895250 ZDOT = -5560
954507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4257108
18 X = -1297566
57
Y = 20606375
96 feet Y = 6280823
39 meter
Z = 6693547
12 Z = 2040193
16
XDOT = -15773
531482 XDOT = -4807
772396
YDOT = 2702
942629 feet/sec YDOT = 823
856913 meter/sec
ZDOT = -18255
654329 ZDOT = -5564
323439
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 10143
53578483
00016717 00000-0 10270-3 0 9043
2 25544 51
6470 357
0703 0010604 345
6494 14
4367 15
74250822 19591
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
53578483 = yrday
fracday
Element set: 904
Inclination: 51
6470 deg
RA of node: 357
0703 deg
Eccentricity:
0010604
Arg of perigee: 345
6494 deg
Mean anomaly: 14
4367 deg
Mean motion: 15
74250822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1959
Checksum: 308
Coasting Arc #6 (Orbit 1974)
---------------------------------------
Vector Time (GMT): 2010/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3066083
07 A = 6721120
95 meter
Y = 3456906
86 meter E =
0007733
Z = 4875418
27 I = 51
58282
XDOT = -6797
559417 Wp = 26
81756
YDOT = 2825
723259 meter/sec RA = 351
62573 deg
ZDOT = 2276
706212 TA = 41
05704
MA = 40
99886
Ha = 191
814 n
mi
Hp = 182
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10059327
66 X = 3003515
13
Y = 11341557
93 feet Y = 3490843
38 meter
Z = 15995466
77 Z = 4890161
87
XDOT = -22301
704124 XDOT = -6839
711967
YDOT = 9270
745599 feet/sec YDOT = 2749
473020 meter/sec
ZDOT = 7469
508571 ZDOT = 2243
580944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14739455
07 X = 4492585
90
Y = -3269236
23 feet Y = -996463
20 meter
Z = 16054174
70 Z = 4893312
45
XDOT = -2877
404421 XDOT = -877
032868
YDOT = 22973
091726 feet/sec YDOT = 7002
198358 meter/sec
ZDOT = 7337
571956 ZDOT = 2236
491932
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 10144
55146656
00016717 00000-0 10270-3 0 9050
2 25544 51
6459 351
8520 0010559 349
6201 10
4742 15
74216265 19750
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
55146656 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 351
8520 deg
Eccentricity:
0010559
Arg of perigee: 349
6201 deg
Mean anomaly: 10
4742 deg
Mean motion: 15
74216265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1975
Checksum: 304
Coasting Arc #7 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2010/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5741900
36 A = 6729892
23 meter
Y = -2931870
23 meter E =
0016343
Z = -1897334
27 I = 51
58183
XDOT = 3740
853221 Wp = 10
31326
YDOT = 3695
011083 meter/sec RA = 346
44832 deg
ZDOT = 5634
429064 TA = 328
56604
MA = 328
66361
Ha = 191
918 n
mi
Hp = 182
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18838255
78 X = 5783475
39
Y = -9618996
81 feet Y = -2867428
21 meter
Z = -6224849
95 Z = -1869338
91
XDOT = 12273
140490 XDOT = 3671
885351
YDOT = 12122
739773 feet/sec YDOT = 3736
457292 meter/sec
ZDOT = 18485
659659 ZDOT = 5652
435358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 297716
01 X = 90743
84
Y = -21182354
32 feet Y = -6456381
60 meter
Z = -6113343
45 Z = -1863347
08
XDOT = 14853
393143 XDOT = 4527
314230
YDOT = -5124
591151 feet/sec YDOT = -1561
975383 meter/sec
ZDOT = 18557
356125 ZDOT = 5656
282147
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 10145
50364802
00016717 00000-0 10270-3 0 9062
2 25544 51
6448 346
9600 0010539 352
1550 7
9446 15
74270954 19900
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
50364802 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 346
9600 deg
Eccentricity:
0010539
Arg of perigee: 352
1550 deg
Mean anomaly: 7
9446 deg
Mean motion: 15
74270954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1990
Checksum: 306
Coasting Arc #8 (Orbit 2005)
---------------------------------------
Vector Time (GMT): 2010/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3421243
93 A = 6720552
99 meter
Y = -3003909
15 meter E =
0018199
Z = -4957821
47 I = 51
52062
XDOT = 6339
169182 Wp = 40
29102
YDOT = -3847
356392 meter/sec RA = 341
33803 deg
ZDOT = -2033
896152 TA = 209
90839
MA = 210
01250
Ha = 191
921 n
mi
Hp = 182
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11224553
56 X = -3363314
75
Y = -9855344
97 feet Y = -3041842
96 meter
Z = -16265818
48 Z = -4974301
88
XDOT = 20797
799155 XDOT = 6391
600352
YDOT = -12622
560341 feet/sec YDOT = -3776
174595 meter/sec
ZDOT = -6672
887637 ZDOT = -2002
973053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13817099
47 X = -4211451
92
Y = 5483353
70 feet Y = 1671326
21 meter
Z = -16331438
15 Z = -4977822
35
XDOT = -1461
766771 XDOT = -445
546512
YDOT = -23283
191048 feet/sec YDOT = -7096
716631 meter/sec
ZDOT = -6549
714050 ZDOT = -1996
352843
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 10146
51929183
00016717 00000-0 10270-3 0 9074
2 25544 51
6437 341
7420 0010492 356
4941 3
6147 15
74308699 20068
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
51929183 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 341
7420 deg
Eccentricity:
0010492
Arg of perigee: 356
4941 deg
Mean anomaly: 3
6147 deg
Mean motion: 15
74308699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2006
Checksum: 306
Coasting Arc #9 (Orbit 2021)
---------------------------------------
Vector Time (GMT): 2010/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5321483
54 A = 6729936
79 meter
Y = 3778733
94 meter E =
0013198
Z = 1642641
71 I = 51
52525
XDOT = -4041
335386 Wp = 70
20629
YDOT = -3185
789999 meter/sec RA = 336
15972 deg
ZDOT = -5722
071791 TA = 91
62841
MA = 91
47722
Ha = 191
999 n
mi
Hp = 182
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17458935
49 X = -5371322
30
Y = 12397421
06 feet Y = 3718947
02 meter
Z = 5389244
45 Z = 1616669
05
XDOT = -13258
974364 XDOT = -3977
613714
YDOT = -10452
066926 feet/sec YDOT = -3230
625440 meter/sec
ZDOT = -18773
201413 ZDOT = -5741
550627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3535010
06 X = 1077471
07
Y = 21145180
06 feet Y = 6445050
88 meter
Z = 5285782
58 Z = 1611106
53
XDOT = -13596
166400 XDOT = -4144
111519
YDOT = 7019
998883 feet/sec YDOT = 2139
695660 meter/sec
ZDOT = -18850
760845 ZDOT = -5745
711906
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 10147
53491474
00016717 00000-0 10270-3 0 9085
2 25544 51
6443 336
5236 0010736 359
3914
7235 15
74390253 20226
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
53491474 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 336
5236 deg
Eccentricity:
0010736
Arg of perigee: 359
3914 deg
Mean anomaly:
7235 deg
Mean motion: 15
74390253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2022
Checksum: 295
Coasting Arc #10 (Orbit 2037)
---------------------------------------
Vector Time (GMT): 2010/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3630000
14 A = 6720110
28 meter
Y = 2570906
96 meter E =
0009030
Z = 5031007
42 I = 51
46346
XDOT = -5787
329491 Wp = 33
17440
YDOT = 4783
948541 meter/sec RA = 331
03977 deg
ZDOT = 1737
029852 TA = 40
11232
MA = 40
04569
Ha = 192
101 n
mi
Hp = 181
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11909449
27 X = 3576541
99
Y = 8434734
12 feet Y = 2611200
03 meter
Z = 16505929
86 Z = 5048512
76
XDOT = -18987
301480 XDOT = -5848
832613
YDOT = 15695
369230 feet/sec YDOT = 4718
887001 meter/sec
ZDOT = 5698
916837 ZDOT = 1708
766083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12618534
76 X = 3846129
40
Y = -7172612
04 feet Y = -2186212
15 meter
Z = 16575634
50 Z = 5052253
40
XDOT = 5724
572998 XDOT = 1744
849850
YDOT = 22935
665373 feet/sec YDOT = 6990
790806 meter/sec
ZDOT = 5586
319517 ZDOT = 1702
710189
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 10148
55052359
00016717 00000-0 10270-3 0 9094
2 25544 51
6433 331
3045 0010559 4
4075 355
7180 15
74326800 20381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
55052359 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 331
3045 deg
Eccentricity:
0010559
Arg of perigee: 4
4075 deg
Mean anomaly: 355
7180 deg
Mean motion: 15
74326800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2038
Checksum: 289
Coasting Arc #11 (Orbit 2052)
---------------------------------------
Vector Time (GMT): 2010/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4744520
70 A = 6730256
07 meter
Y = -4552293
72 meter E =
0018569
Z = -1388092
43 I = 51
47232
XDOT = 4276
981935 Wp = 20
92540
YDOT = 2696
239584 meter/sec RA = 325
86131 deg
ZDOT = 5817
277394 TA = 323
76500
MA = 323
89063
Ha = 192
154 n
mi
Hp = 181
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15566012
79 X = 4801815
79
Y = -14935346
84 feet Y = -4498917
07 meter
Z = -4554109
01 Z = -1364905
00
XDOT = 14032
092964 XDOT = 4218
254737
YDOT = 8845
930393 feet/sec YDOT = 2743
737959 meter/sec
ZDOT = 19085
555755 ZDOT = 5837
912952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7349032
24 X = -2239985
03
Y = -20302461
83 feet Y = -6188190
37 meter
Z = -4461728
04 Z = -1359934
71
XDOT = 12241
621812 XDOT = 3731
246328
YDOT = -8613
451522 feet/sec YDOT = -2625
380024 meter/sec
ZDOT = 19167
730090 ZDOT = 5842
324132
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 10149
50263548
00016717 00000-0 10270-3 0 9106
2 25544 51
6434 326
4119 0010415 7
8761 352
2564 15
74391924 20533
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
50263548 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 326
4119 deg
Eccentricity:
0010415
Arg of perigee: 7
8761 deg
Mean anomaly: 352
2564 deg
Mean motion: 15
74391924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2053
Checksum: 293
Coasting Arc #12 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2010/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803647
82 A = 6719497
05 meter
Y = -2163163
44 meter E =
0020543
Z = -5115910
95 I = 51
41242
XDOT = 5080
036225 Wp = 51
24781
YDOT = -5597
257027 meter/sec RA = 320
73412 deg
ZDOT = -1401
414136 TA = 205
21551
MA = 205
31593
Ha = 192
194 n
mi
Hp = 181
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12479159
53 X = -3754324
00
Y = -7096992
92 feet Y = -2205421
43 meter
Z = -16784484
76 Z = -5134269
70
XDOT = 16666
785514 XDOT = 5149
056037
YDOT = -18363
704158 feet/sec YDOT = -5540
062886 meter/sec
ZDOT = -4597
815407 ZDOT = -1376
568559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11352763
69 X = -3460322
37
Y = 8645912
70 feet Y = 2635274
19 meter
Z = -16857597
98 Z = -5138195
87
XDOT = -9797
158438 XDOT = -2986
173892
YDOT = -21692
632627 feet/sec YDOT = -6611
914425 meter/sec
ZDOT = -4498
822988 ZDOT = -1371
241247
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 10150
51820476
00016717 00000-0 10270-3 0 9119
2 25544 51
6437 321
1940 0010449 12
5949 347
5474 15
74434158 20699
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
51820476 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 321
1940 deg
Eccentricity:
0010449
Arg of perigee: 12
5949 deg
Mean anomaly: 347
5474 deg
Mean motion: 15
74434158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 302
Coasting Arc #13 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2010/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4125944
97 A = 6730318
91 meter
Y = 5213473
51 meter E =
0014326
Z = 1044670
14 I = 51
42651
XDOT = -4390
699410 Wp = 79
40609
YDOT = -2279
285717 meter/sec RA = 315
55697 deg
ZDOT = -5895
254691 TA = 89
14218
MA = 88
97804
Ha = 192
239 n
mi
Hp = 181
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13536564
87 X = -4189011
14
Y = 17104571
88 feet Y = 5166981
95 meter
Z = 3427395
48 Z = 1024473
96
XDOT = -14405
181792 XDOT = -4336
247630
YDOT = -7477
971513 feet/sec YDOT = -2328
079723 meter/sec
ZDOT = -19341
386781 ZDOT = -5916
452810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10815051
25 X = 3296427
62
Y = 18957446
05 feet Y = 5778229
56 meter
Z = 3346925
94 Z = 1020143
03
XDOT = -10886
166171 XDOT = -3318
103449
YDOT = 9682
200840 feet/sec YDOT = 2951
134816 meter/sec
ZDOT = -19425
813840 ZDOT = -5920
988059
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 10151
53375277
00016717 00000-0 10270-3 0 9127
2 25544 51
6434 315
9746 0010600 14
8732 345
2742 15
74492911 20857
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
53375277 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 315
9746 deg
Eccentricity:
0010600
Arg of perigee: 14
8732 deg
Mean anomaly: 345
2742 deg
Mean motion: 15
74492911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 298
Coasting Arc #14 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2010/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3871205
03 A = 6719085
64 meter
Y = 1829028
31 meter E =
0010335
Z = 5171516
21 I = 51
36779
XDOT = -4315
183174 Wp = 38
97019
YDOT = 6307
316556 meter/sec RA = 310
41901 deg
ZDOT = 1006
295646 TA = 41
44853
MA = 41
37019
Ha = 192
281 n
mi
Hp = 180
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12700803
91 X = 3825342
56
Y = 6000749
06 feet Y = 1872061
25 meter
Z = 16966916
70 Z = 5190211
35
XDOT = -14157
425110 XDOT = -4390
280403
YDOT = 20693
295786 feet/sec YDOT = 6258
641571 meter/sec
ZDOT = 3301
494903 ZDOT = 985
151033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10103327
55 X = 3079494
24
Y = -9628593
45 feet Y = -2934795
28 meter
Z = 17041380
00 Z = 5194212
63
XDOT = 13568
443052 XDOT = 4135
661442
YDOT = 19891
999722 feet/sec YDOT = 6063
081515 meter/sec
ZDOT = 3217
247533 ZDOT = 980
617048
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 10152
54928572
00016717 00000-0 10270-3 0 9132
2 25544 51
6436 310
7559 0010527 19
8832 340
2740 15
74461569 21015
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
54928572 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 310
7559 deg
Eccentricity:
0010527
Arg of perigee: 19
8832 deg
Mean anomaly: 340
2740 deg
Mean motion: 15
74461569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 301
Coasting Arc #15 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2010/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3379106
92 A = 6730516
77 meter
Y = -5764619
87 meter E =
0020921
Z = -710098
14 I = 51
38923
XDOT = 4488
608387 Wp = 31
67333
YDOT = 1907
799080 meter/sec RA = 305
24638 deg
ZDOT = 5968
874352 TA = 320
55430
MA = 320
70643
Ha = 192
357 n
mi
Hp = 180
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11086308
80 X = 3446766
32
Y = -18912794
85 feet Y = -5726454
29 meter
Z = -2329718
30 Z = -693518
86
XDOT = 14726
405469 XDOT = 4437
945782
YDOT = 6259
183334 feet/sec YDOT = 1957
709342 meter/sec
ZDOT = 19582
921101 ZDOT = 5990
557151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13997915
06 X = -4266564
51
Y = -16880812
70 feet Y = -5145271
71 meter
Z = -2263664
23 Z = -689964
86
XDOT = 9633
319566 XDOT = 2936
235804
YDOT = -10581
907177 feet/sec YDOT = -3225
365308 meter/sec
ZDOT = 19669
288898 ZDOT = 5995
199256
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 10153
50132726
00016717 00000-0 10270-3 0 9148
2 25544 51
6448 305
8641 0010443 23
7336 336
4307 15
74511381 21165
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
50132726 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 305
8641 deg
Eccentricity:
0010443
Arg of perigee: 23
7336 deg
Mean anomaly: 336
4307 deg
Mean motion: 15
74511381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2116
Checksum: 277
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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