Date:
May 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13831 62 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 1791)
---------------------------------------
Vector Time (GMT): 2010/132/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5307490
26 A = 6727247
12 meter
Y = -2216603
08 meter E =
0007366
Z = 3491151
51 I = 51
91058
XDOT = -414
983443 Wp = 35
65484
YDOT = -6192
064441 meter/sec RA = 51
07506 deg
ZDOT = -4551
711427 TA = 103
10164
MA = 103
01942
Ha = 190
244 n
mi
Hp = 186
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17413025
78 X = -5299269
10
Y = -7272319
82 feet Y = -2275908
88 meter
Z = 11453909
15 Z = 3465386
94
XDOT = -1361
494234 XDOT = -323
599925
YDOT = -20315
172051 feet/sec YDOT = -6196
193760 meter/sec
ZDOT = -14933
436439 ZDOT = -4553
505923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18597323
63 X = 5668464
24
Y = 3546816
93 feet Y = 1081069
80 meter
Z = 11351289
82 Z = 3459873
14
XDOT = 5656
329289 XDOT = 1724
049167
YDOT = 18270
637957 feet/sec YDOT = 5568
890449 meter/sec
ZDOT = -14940
615447 ZDOT = -4553
899588
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 10132
93350123
00016717 00000-0 10270-3 0 9000
2 25544 51
6441 51
5074 0009858 305
2561 54
7679 15
73905187 17920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
93350123 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 51
5074 deg
Eccentricity:
0009858
Arg of perigee: 305
2561 deg
Mean anomaly: 54
7679 deg
Mean motion: 15
73905187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1792
Checksum: 304
Coasting Arc #2 (Orbit 1807)
---------------------------------------
Vector Time (GMT): 2010/133/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 839186
72 A = 6725351
22 meter
Y = 5356916
89 meter E =
0005012
Z = 3973077
11 I = 51
88658
XDOT = -6276
184183 Wp = 35
98526
YDOT = -1982
825599 meter/sec RA = 46
00999 deg
ZDOT = 4000
533676 TA = 12
71063
MA = 12
69800
Ha = 190
333 n
mi
Hp = 185
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2753237
26 X = 759921
42
Y = 17575186
64 feet Y = 5365857
59 meter
Z = 13035029
90 Z = 3976961
95
XDOT = -20591
155455 XDOT = -6272
979705
YDOT = -6505
333329 feet/sec YDOT = -2052
992094 meter/sec
ZDOT = 13125
110485 ZDOT = 3970
050884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6496741
73 X = -1980206
88
Y = -16548589
56 feet Y = -5044010
10 meter
Z = 13050518
60 Z = 3977798
07
XDOT = 20388
220279 XDOT = 6214
329541
YDOT = 2247
119576 feet/sec YDOT = 684
922047 meter/sec
ZDOT = 13003
704286 ZDOT = 3963
529066
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 10133
94937388
00016717 00000-0 10270-3 0 9017
2 25544 51
6455 46
2916 0009948 308
8807 51
1468 15
73978309 18084
Satellite: ISS
Catalog Number: 25544
Epoch time: 10133
94937388 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 46
2916 deg
Eccentricity:
0009948
Arg of perigee: 308
8807 deg
Mean anomaly: 51
1468 deg
Mean motion: 15
73978309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1808
Checksum: 345
Coasting Arc #3 (Orbit 1822)
---------------------------------------
Vector Time (GMT): 2010/134/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5611884
37 A = 6727084
86 meter
Y = 1227997
19 meter E =
0006952
Z = -3492000
42 I = 51
87043
XDOT = 1510
547538 Wp = 340
53703
YDOT = 6027
848267 meter/sec RA = 40
84149 deg
ZDOT = 4551
143514 TA = 338
13750
MA = 338
16715
Ha = 190
705 n
mi
Hp = 185
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18411694
14 X = 5614699
43
Y = 4028862
18 feet Y = 1290768
78 meter
Z = -11456694
30 Z = -3464730
37
XDOT = 4955
864627 XDOT = 1420
921722
YDOT = 19776
405076 feet/sec YDOT = 6044
238440 meter/sec
ZDOT = 14931
573209 ZDOT = 4558
264914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18906766
72 X = -5762782
50
Y = 482909
78 feet Y = 147190
90 meter
Z = -11348084
70 Z = -3458896
22
XDOT = -9397
366274 XDOT = -2864
317240
YDOT = -16672
479277 feet/sec YDOT = -5081
771684 meter/sec
ZDOT = 14959
943337 ZDOT = 4559
790729
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 10134
90174065
00016717 00000-0 10270-3 0 9020
2 25544 51
6458 41
4026 0010051 313
1520 46
8803 15
73958136 18231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
90174065 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 41
4026 deg
Eccentricity:
0010051
Arg of perigee: 313
1520 deg
Mean anomaly: 46
8803 deg
Mean motion: 15
73958136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1823
Checksum: 275
Coasting Arc #4 (Orbit 1838)
---------------------------------------
Vector Time (GMT): 2010/135/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1764392
94 A = 6725270
43 meter
Y = -5128854
00 meter E =
0009458
Z = -3983215
79 I = 51
84148
XDOT = 6529
879922 Wp = 358
83773
YDOT = 851
232843 meter/sec RA = 35
77307 deg
ZDOT = -3979
093896 TA = 229
99427
MA = 230
07732
Ha = 190
674 n
mi
Hp = 185
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5788690
75 X = -1687560
00
Y = -16826948
83 feet Y = -5148154
36 meter
Z = -13068293
27 Z = -3991601
40
XDOT = 21423
490559 XDOT = 6539
205973
YDOT = 2792
758672 feet/sec YDOT = 924
306529 meter/sec
ZDOT = -13054
770000 ZDOT = -3947
348486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9806872
96 X = 2989134
88
Y = 14819122
04 feet Y = 4516868
40 meter
Z = -13101690
78 Z = -3993395
35
XDOT = -20422
015927 XDOT = -6224
630455
YDOT = 2057
415171 feet/sec YDOT = 627
100144 meter/sec
ZDOT = -12928
333162 ZDOT = -3940
555948
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 10135
91758036
00016717 00000-0 10270-3 0 9039
2 25544 51
6461 36
1866 0009991 316
5726 43
4649 15
73993609 18396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
91758036 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 36
1866 deg
Eccentricity:
0009991
Arg of perigee: 316
5726 deg
Mean anomaly: 43
4649 deg
Mean motion: 15
73993609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1839
Checksum: 339
Coasting Arc #5 (Orbit 1854)
---------------------------------------
Vector Time (GMT): 2010/136/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5769248
14 A = 6727066
59 meter
Y = -258068
48 meter E =
0009990
Z = 3452527
86 I = 51
82228
XDOT = -2496
084937 Wp = 38
13359
YDOT = -5659
484050 meter/sec RA = 30
60048 deg
ZDOT = -4579
340038 TA = 101
11658
MA = 101
00423
Ha = 190
856 n
mi
Hp = 185
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18927979
45 X = -5782705
50
Y = -846681
38 feet Y = -322659
38 meter
Z = 11327191
14 Z = 3424467
85
XDOT = -8189
255044 XDOT = -2410
368229
YDOT = -18567
861058 feet/sec YDOT = -5686
916844 meter/sec
ZDOT = -15024
081488 ZDOT = -4591
258729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18512326
31 X = 5642557
06
Y = -4335722
04 feet Y = -1321528
08 meter
Z = 11215427
93 Z = 3418462
43
XDOT = 12515
717687 XDOT = 3814
790751
YDOT = 14326
272242 feet/sec YDOT = 4366
647779 meter/sec
ZDOT = -15071
546605 ZDOT = -4593
807405
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 10136
93340273
00016717 00000-0 10270-3 0 9043
2 25544 51
6461 30
9707 0009913 320
9595 39
0852 15
74012319 18555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
93340273 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 30
9707 deg
Eccentricity:
0009913
Arg of perigee: 320
9595 deg
Mean anomaly: 39
0852 deg
Mean motion: 15
74012319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1855
Checksum: 302
Coasting Arc #6 (Orbit 1870)
---------------------------------------
Vector Time (GMT): 2010/137/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2569272
45 A = 6724837
89 meter
Y = 4733162
35 meter E =
0007448
Z = 4019124
34 I = 51
78965
XDOT = -6623
510024 Wp = 38
55064
YDOT = 262
538856 meter/sec RA = 25
52719 deg
ZDOT = 3926
807184 TA = 11
01740
MA = 11
00110
Ha = 190
885 n
mi
Hp = 184
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8429371
55 X = 2496630
15
Y = 15528747
86 feet Y = 4761486
78 meter
Z = 13186103
47 Z = 4031430
11
XDOT = -21730
675933 XDOT = -6645
029314
YDOT = 861
347954 feet/sec YDOT = 188
349976 meter/sec
ZDOT = 12883
225670 ZDOT = 3894
577777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12465699
91 X = -3799545
33
Y = -12470276
93 feet Y = -3800940
41 meter
Z = 13235110
82 Z = 4034061
78
XDOT = 19727
274231 XDOT = 6012
873185
YDOT = -6189
252335 feet/sec YDOT = -1886
484112 meter/sec
ZDOT = 12754
849788 ZDOT = 3887
678215
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 10137
94920493
00016717 00000-0 10270-3 0 9054
2 25544 51
6467 25
7537 0010012 324
7058 35
3442 15
74087879 18717
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
94920493 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 25
7537 deg
Eccentricity:
0010012
Arg of perigee: 324
7058 deg
Mean anomaly: 35
3442 deg
Mean motion: 15
74087879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1871
Checksum: 315
Coasting Arc #7 (Orbit 1885)
---------------------------------------
Vector Time (GMT): 2010/138/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5753718
00 A = 6727041
60 meter
Y = -722854
02 meter E =
0008751
Z = -3400213
93 I = 51
76881
XDOT = 3378
755273 Wp = 356
20319
YDOT = 5144
913228 meter/sec RA = 20
35097 deg
ZDOT = 4631
527733 TA = 323
71212
MA = 323
77144
Ha = 191
255 n
mi
Hp = 184
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18877027
55 X = 5777891
09
Y = -2371568
30 feet Y = -658376
96 meter
Z = -11155557
52 Z = -3372203
70
XDOT = 11085
155095 XDOT = 3298
473656
YDOT = 16879
636575 feet/sec YDOT = 5182
247057 meter/sec
ZDOT = 15195
300960 ZDOT = 4647
747350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17324074
25 X = -5280377
83
Y = 8019965
45 feet Y = 2444485
47 meter
Z = -11043983
62 Z = -3366206
21
XDOT = -15023
029041 XDOT = -4579
019252
YDOT = -11473
677289 feet/sec YDOT = -3497
176838 meter/sec
ZDOT = 15259
897832 ZDOT = 4651
216859
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 10138
90150622
00016717 00000-0 10270-3 0 9061
2 25544 51
6467 20
8641 0010206 328
2833 31
7714 15
74069427 18861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
90150622 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 20
8641 deg
Eccentricity:
0010206
Arg of perigee: 328
2833 deg
Mean anomaly: 31
7714 deg
Mean motion: 15
74069427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1886
Checksum: 296
Coasting Arc #8 (Orbit 1901)
---------------------------------------
Vector Time (GMT): 2010/139/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3282407
44 A = 6724600
33 meter
Y = -4230862
12 meter E =
0011716
Z = -4077784
83 I = 51
73224
XDOT = 6526
904398 Wp = 11
62066
YDOT = -1355
838832 meter/sec RA = 15
27397 deg
ZDOT = -3837
740958 TA = 218
88210
MA = 218
96644
Ha = 191
226 n
mi
Hp = 184
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10769053
29 X = -3215044
08
Y = -13880781
23 feet Y = -4267190
92 meter
Z = -13378559
16 Z = -4093567
54
XDOT = 21413
728340 XDOT = 6560
223590
YDOT = -4448
290130 feet/sec YDOT = -1282
664442 meter/sec
ZDOT = -12591
013643 ZDOT = -3805
952443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14574377
86 X = 4442270
37
Y = 9723694
00 feet Y = 2963781
93 meter
Z = -13441418
32 Z = -4096944
30
XDOT = -18219
930183 XDOT = -5553
434720
YDOT = 10036
810662 feet/sec YDOT = 3059
219890 meter/sec
ZDOT = -12464
387969 ZDOT = -3799
145453
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
91727641
00016717 00000-0 10270-3 0 9075
2 25544 51
6465 15
6477 0010109 332
1463 27
9158 15
74102516 19028
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
91727641 = yrday
fracday
Element set: 907
Inclination: 51
6465 deg
RA of node: 15
6477 deg
Eccentricity:
0010109
Arg of perigee: 332
1463 deg
Mean anomaly: 27
9158 deg
Mean motion: 15
74102516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1902
Checksum: 297
Coasting Arc #9 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2010/140/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5629639
40 A = 6727151
55 meter
Y = 1642500
27 meter E =
0012492
Z = 3298143
86 I = 51
71138
XDOT = -4087
577885 Wp = 44
25455
YDOT = -4506
839680 meter/sec RA = 10
09297 deg
ZDOT = -4713
227225 TA = 97
09725
MA = 96
95518
Ha = 191
419 n
mi
Hp = 183
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18469945
54 X = -5663609
54
Y = 5388780
42 feet Y = 1579356
12 meter
Z = 10820681
95 Z = 3270712
62
XDOT = -13410
688600 XDOT = -4013
981747
YDOT = -14786
219422 feet/sec YDOT = -4552
137574 meter/sec
ZDOT = -15463
343913 ZDOT = -4732
906272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15636937
86 X = 4766138
66
Y = -11314450
17 feet Y = -3448644
41 meter
Z = 10711414
10 Z = 3264839
02
XDOT = 16695
073792 XDOT = 5088
658492
YDOT = 8298
674455 feet/sec YDOT = 2529
435974 meter/sec
ZDOT = -15541
722060 ZDOT = -4737
116884
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
93302931
00016717 00000-0 10270-3 0 9081
2 25544 51
6465 10
4309 0010175 336
9350 23
1355 15
74139233 19185
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
93302931 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 10
4309 deg
Eccentricity:
0010175
Arg of perigee: 336
9350 deg
Mean anomaly: 23
1355 deg
Mean motion: 15
74139233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1918
Checksum: 280
Coasting Arc #10 (Orbit 1933)
---------------------------------------
Vector Time (GMT): 2010/141/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3829666
87 A = 6724044
45 meter
Y = 3633084
00 meter E =
0009307
Z = 4155019
10 I = 51
67191
XDOT = -6308
819740 Wp = 42
44619
YDOT = 2398
601521 meter/sec RA = 5
01020 deg
ZDOT = 3719
448347 TA = 9
59291
MA = 9
57515
Ha = 191
396 n
mi
Hp = 183
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12564523
86 X = 3768572
00
Y = 11919566
94 feet Y = 3675567
78 meter
Z = 13631952
44 Z = 4173475
54
XDOT = -20698
227492 XDOT = -6353
240953
YDOT = 7869
427563 feet/sec YDOT = 2327
803953 meter/sec
ZDOT = 12202
914523 ZDOT = 3688
692169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15886803
87 X = -4842297
82
Y = -6748577
64 feet Y = -2056966
47 meter
Z = 13705459
71 Z = 4177424
12
XDOT = 16165
175844 XDOT = 4927
145597
YDOT = -13533
491182 feet/sec YDOT = -4125
008112 meter/sec
ZDOT = 12080
405289 ZDOT = 3682
107532
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
94876340
00016717 00000-0 10270-3 0 9094
2 25544 51
6467 5
2136 0010223 340
0943 19
9820 15
74184575 19342
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
94876340 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 5
2136 deg
Eccentricity:
0010223
Arg of perigee: 340
0943 deg
Mean anomaly: 19
9820 deg
Mean motion: 15
74184575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1934
Checksum: 300
Coasting Arc #11 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2010/142/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5343330
89 A = 6727277
51 meter
Y = -2540530
66 meter E =
0010911
Z = -3190805
80 I = 51
65184
XDOT = 4669
300502 Wp = 8
01282
YDOT = 3792
718927 meter/sec RA = 359
82613 deg
ZDOT = 4812
013107 TA = 314
74007
MA = 314
82883
Ha = 191
702 n
mi
Hp = 183
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17530613
14 X = 5386842
95
Y = -8335074
36 feet Y = -2480534
88 meter
Z = -10468522
97 Z = -3164742
08
XDOT = 15319
227368 XDOT = 4603
166466
YDOT = 12443
303565 feet/sec YDOT = 3844
563772 meter/sec
ZDOT = 15787
444578 ZDOT = 4834
536386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13276673
77 X = -4046730
17
Y = 14236874
77 feet Y = 4339399
43 meter
Z = -10364707
68 Z = -3159162
90
XDOT = -17704
161807 XDOT = -5396
228519
YDOT = -4981
574393 feet/sec YDOT = -1518
383875 meter/sec
ZDOT = 15877
145125 ZDOT = 4839
353834
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
90100036
00016717 00000-0 10270-3 0 9105
2 25544 51
6462
3238 0010326 343
8467 16
2366 15
74192755 19492
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
90100036 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node:
3238 deg
Eccentricity:
0010326
Arg of perigee: 343
8467 deg
Mean anomaly: 16
2366 deg
Mean motion: 15
74192755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1949
Checksum: 281
Coasting Arc #12 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2010/143/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271853
43 A = 6723650
96 meter
Y = -2993011
18 meter E =
0014389
Z = -4255962
90 I = 51
60907
XDOT = 5921
174867 Wp = 23
66969
YDOT = -3377
394866 meter/sec RA = 354
73846 deg
ZDOT = -3559
338382 TA = 210
09423
MA = 210
17698
Ha = 191
755 n
mi
Hp = 182
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14015267
16 X = -4217392
53
Y = -9819590
48 feet Y = -3040476
78 meter
Z = -13963132
88 Z = -4276583
81
XDOT = 19426
426729 XDOT = 5975
792310
YDOT = -11080
691818 feet/sec YDOT = -3310
875125 meter/sec
ZDOT = -11677
619363 ZDOT = -3530
440451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16638646
13 X = 5071459
34
Y = 3702360
92 feet Y = 1128479
61 meter
Z = -14045252
91 Z = -4280993
09
XDOT = -13459
653903 XDOT = -4102
502510
YDOT = 16516
325147 feet/sec YDOT = 5034
175905 meter/sec
ZDOT = -11562
516449 ZDOT = -3524
255014
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
91670274
00016717 00000-0 10270-3 0 9114
2 25544 51
6456 355
1067 0010344 347
9624 12
1290 15
74202508 19653
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
91670274 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 355
1067 deg
Eccentricity:
0010344
Arg of perigee: 347
9624 deg
Mean anomaly: 12
1290 deg
Mean motion: 15
74202508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1965
Checksum: 291
Coasting Arc #13 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2010/144/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987656
89 A = 6727499
27 meter
Y = 3355662
56 meter E =
0014679
Z = 3021366
80 I = 51
59298
XDOT = -5056
829046 Wp = 52
10237
YDOT = -3047
815803 meter/sec RA = 349
54951 deg
ZDOT = -4937
621540 TA = 92
93245
MA = 92
76445
Ha = 191
889 n
mi
Hp = 182
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16363703
71 X = -5039487
34
Y = 11009391
61 feet Y = 3299597
53 meter
Z = 9912620
74 Z = 2997010
74
XDOT = -16590
646475 XDOT = -4998
385471
YDOT = -9999
395678 feet/sec YDOT = -3104
037035 meter/sec
ZDOT = -16199
545734 ZDOT = -4962
046392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10635540
88 X = 3241712
86
Y = -16666633
67 feet Y = -5079989
94 meter
Z = 9815607
21 Z = 2991797
08
XDOT = 17904
119242 XDOT = 5457
175545
YDOT = 1778
385349 feet/sec YDOT = 542
051854 meter/sec
ZDOT = -16296
810176 ZDOT = -4967
267742
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
93238617
00016717 00000-0 10270-3 0 9129
2 25544 51
6461 349
8892 0010593 351
8144 8
2844 15
74277796 19812
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
93238617 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 349
8892 deg
Eccentricity:
0010593
Arg of perigee: 351
8144 deg
Mean anomaly: 8
2844 deg
Mean motion: 15
74277796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1981
Checksum: 335
Coasting Arc #14 (Orbit 1996)
---------------------------------------
Vector Time (GMT): 2010/145/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4538577
84 A = 6722958
34 meter
Y = 2335072
75 meter E =
0010723
Z = 4364757
75 I = 51
54791
XDOT = -5445
535838 Wp = 47
52847
YDOT = 4291
168716 meter/sec RA = 344
45567 deg
ZDOT = 3368
583540 TA = 8
56033
MA = 8
54206
Ha = 191
868 n
mi
Hp = 182
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14890347
24 X = 4490925
70
Y = 7660999
83 feet Y = 2385558
86 meter
Z = 14320071
36 Z = 4386691
12
XDOT = -17865
931228 XDOT = -5509
480015
YDOT = 14078
637520 feet/sec YDOT = 4229
915556 meter/sec
ZDOT = 11051
783268 ZDOT = 3341
973808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16651167
62 X = -5075275
89
Y = -801802
54 feet Y = -244389
41 meter
Z = 14407412
41 Z = 4391379
30
XDOT = 10382
897688 XDOT = 3164
707215
YDOT = -19051
735393 feet/sec YDOT = -5806
968948 meter/sec
ZDOT = 10945
788211 ZDOT = 3336
276247
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
94805370
00016717 00000-0 10270-3 0 9138
2 25544 51
6455 344
6717 0010499 355
9402 4
1674 15
74283211 19973
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
94805370 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 344
6717 deg
Eccentricity:
0010499
Arg of perigee: 355
9402 deg
Mean anomaly: 4
1674 deg
Mean motion: 15
74283211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1997
Checksum: 315
Coasting Arc #15 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2010/146/21:28:05
923
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4479797
27 A = 6727801
24 meter
Y = -4120015
09 meter E =
0013409
Z = -2853540
60 I = 51
53507
XDOT = 5326
521741 Wp = 17
52576
YDOT = 2291
810826 meter/sec RA = 339
26358 deg
ZDOT = 5071
897493 TA = 309
64344
MA = 309
76168
Ha = 192
123 n
mi
Hp = 182
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14697497
61 X = 4539397
30
Y = -13517109
89 feet Y = -4069585
68 meter
Z = -9362009
85 Z = -2831633
18
XDOT = 17475
465029 XDOT = 5275
859620
YDOT = 7519
064391 feet/sec YDOT = 2351
091168 meter/sec
ZDOT = 16640
083637 ZDOT = 5097
651467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7467172
69 X = -2275994
24
Y = 18563309
81 feet Y = 5658096
83 meter
Z = -9274739
08 Z = -2826940
47
XDOT = -17566
740125 XDOT = -5354
342390
YDOT = 1267
806753 feet/sec YDOT = 386
427498 meter/sec
ZDOT = 16742
639490 ZDOT = 5103
156517
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
90022678
00016717 00000-0 10270-3 0 9148
2 25544 51
6452 339
7803 0010568
0563
0600 15
74312747 20124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
90022678 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 339
7803 deg
Eccentricity:
0010568
Arg of perigee:
0563 deg
Mean anomaly:
0600 deg
Mean motion: 15
74312747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2012
Checksum: 266
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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