Date:
September 24th 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) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 3877)
---------------------------------------
Vector Time (GMT): 2010/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1854798
68 A = 6738153
70 meter
Y = -6129656
13 meter E =
0006518
Z = -2103928
80 I = 51
99480
XDOT = 4241
032906 Wp = 74
91198
YDOT = 3188
643899 meter/sec RA = 91
95992 deg
ZDOT = -5563
639532 TA = 128
42308
MA = 128
36455
Ha = 196
078 n
mi
Hp = 186
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6085297
51 X = 1933424
32
Y = -20110420
37 feet Y = -6108475
27 meter
Z = -6902653
56 Z = -2094726
51
XDOT = 13914
149954 XDOT = 4232
088948
YDOT = 10461
430115 feet/sec YDOT = 3236
019062 meter/sec
ZDOT = -18253
410537 ZDOT = -5543
058599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5963344
07 X = -1817627
27
Y = 20159506
88 feet Y = 6144617
70 meter
Z = -6865805
80 Z = -2092697
61
XDOT = -12636
259091 XDOT = -3851
531771
YDOT = -9912
298799 feet/sec YDOT = -3021
268674 meter/sec
ZDOT = -18170
867730 ZDOT = -5538
480484
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 10265
52771905
00016717 00000-0 10270-3 0 9007
2 25544 51
6411 92
5879 0006900 17
4524 342
6874 15
71235321 38788
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
52771905 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 92
5879 deg
Eccentricity:
0006900
Arg of perigee: 17
4524 deg
Mean anomaly: 342
6874 deg
Mean motion: 15
71235321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3878
Checksum: 309
Coasting Arc #2 (Orbit 3893)
---------------------------------------
Vector Time (GMT): 2010/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4109353
58 A = 6728673
15 meter
Y = -1357165
27 meter E =
0010838
Z = 5148899
84 I = 51
96224
XDOT = 696
459741 Wp = 34
56063
YDOT = -7535
459901 meter/sec RA = 86
83769 deg
ZDOT = -1420
200951 TA = 69
04122
MA = 68
92528
Ha = 196
245 n
mi
Hp = 186
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13482131
18 X = -4118884
72
Y = -4452641
97 feet Y = -1403171
25 meter
Z = 16892716
02 Z = 5128913
45
XDOT = 2284
972904 XDOT = 787
570017
YDOT = -24722
637472 feet/sec YDOT = -7527
162403 meter/sec
ZDOT = -4659
451940 ZDOT = -1416
595378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13690339
11 X = 4172815
36
Y = 4107276
24 feet Y = 1251897
80 meter
Z = 16812573
67 Z = 5124472
45
XDOT = -1387
220968 XDOT = -422
824951
YDOT = 23775
035339 feet/sec YDOT = 7246
630771 meter/sec
ZDOT = -4645
045032 ZDOT = -1415
809726
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 10266
54533862
00016717 00000-0 10270-3 0 9019
2 25544 51
6407 87
3823 0006771 21
5772 338
5674 15
71228724 38940
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
54533862 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 87
3823 deg
Eccentricity:
0006771
Arg of perigee: 21
5772 deg
Mean anomaly: 338
5674 deg
Mean motion: 15
71228724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3894
Checksum: 323
Coasting Arc #3 (Orbit 3909)
---------------------------------------
Vector Time (GMT): 2010/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 697232
51 A = 6739891
49 meter
Y = 6684488
35 meter E =
0019282
Z = 342826
85 I = 51
99746
XDOT = -4755
708180 Wp = 40
61512
YDOT = 176
489259 meter/sec RA = 81
76098 deg
ZDOT = 6056
022646 TA = 323
09169
MA = 323
22423
Ha = 196
160 n
mi
Hp = 186
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2287508
25 X = 620768
10
Y = 21930736
04 feet Y = 6691857
72 meter
Z = 1124760
00 Z = 346027
60
XDOT = -15602
717127 XDOT = -4786
747688
YDOT = 579
033003 feet/sec YDOT = 123
135166 meter/sec
ZDOT = 19868
840703 ZDOT = 6032
843720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3210285
04 X = -978494
88
Y = -21814097
25 feet Y = -6648936
84 meter
Z = 1137626
17 Z = 346748
46
XDOT = 14090
796839 XDOT = 4294
874876
YDOT = -1012
777924 feet/sec YDOT = -308
694711 meter/sec
ZDOT = 19775
908699 ZDOT = 6027
696971
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 10267
56293781
00016717 00000-0 10270-3 0 9026
2 25544 51
6406 82
1766 0006781 25
5776 334
5720 15
71277772 39101
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
56293781 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 82
1766 deg
Eccentricity:
0006781
Arg of perigee: 25
5776 deg
Mean anomaly: 334
5720 deg
Mean motion: 15
71277772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 321
Coasting Arc #4 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2010/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3865736
58 A = 6727876
33 meter
Y = -1612198
97 meter E =
0019573
Z = -5281295
64 I = 51
95236
XDOT = 2222
987142 Wp = 68
70848
YDOT = 7329
078785 meter/sec RA = 76
67144 deg
ZDOT = -605
017026 TA = 195
52219
MA = 195
58230
Ha = 196
188 n
mi
Hp = 186
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12682862
79 X = 3909133
16
Y = -5289366
71 feet Y = -1568727
84 meter
Z = -17327085
43 Z = -5262410
04
XDOT = 7293
264901 XDOT = 2143
805921
YDOT = 24045
534070 feet/sec YDOT = 7353
494779 meter/sec
ZDOT = -1984
963996 ZDOT = -594
410611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12447087
20 X = -3793872
18
Y = 6043218
69 feet Y = 1841973
06 meter
Z = -17251371
73 Z = -5258218
10
XDOT = -8285
687618 XDOT = -2525
477586
YDOT = -22659
207637 feet/sec YDOT = -6906
526488 meter/sec
ZDOT = -1942
416093 ZDOT = -592
048425
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 10268
51691913
00016717 00000-0 10270-3 0 9032
2 25544 51
6411 77
2974 0006821 30
4783 329
6774 15
71319561 39254
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
51691913 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 77
2974 deg
Eccentricity:
0006821
Arg of perigee: 30
4783 deg
Mean anomaly: 329
6774 deg
Mean motion: 15
71319561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 320
Coasting Arc #5 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2010/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3075794
28 A = 6738861
97 meter
Y = -5832799
65 meter E =
0015746
Z = 1372391
02 I = 51
98171
XDOT = 3708
307344 Wp = 94
00737
YDOT = -3345
974088 meter/sec RA = 71
56042 deg
ZDOT = -5853
493807 TA = 71
00342
MA = 70
83287
Ha = 196
142 n
mi
Hp = 186
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10091188
58 X = -3017009
18
Y = -19136481
81 feet Y = -5866866
24 meter
Z = 4502595
21 Z = 1357591
79
XDOT = 12166
362677 XDOT = 3773
882752
YDOT = -10977
605274 feet/sec YDOT = -3304
139363 meter/sec
ZDOT = -19204
376007 ZDOT = -5835
318993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11557845
52 X = 3522831
31
Y = 18302570
77 feet Y = 5578623
57 meter
Z = 4443252
94 Z = 1354303
49
XDOT = -10065
826404 XDOT = -3068
063888
YDOT = 11046
293086 feet/sec YDOT = 3366
910132 meter/sec
ZDOT = -19131
510995 ZDOT = -5831
284551
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 10269
53447796
00016717 00000-0 10270-3 0 9044
2 25544 51
6410 72
0915 0006872 31
7928 328
3647 15
71375704 39416
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
53447796 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 72
0915 deg
Eccentricity:
0006872
Arg of perigee: 31
7928 deg
Mean anomaly: 328
3647 deg
Mean motion: 15
71375704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 324
Coasting Arc #6 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2347578
67 A = 6729583
09 meter
Y = 4059563
94 meter E =
0010375
Z = 4817157
40 I = 51
94048
XDOT = -4600
350362 Wp = 79
60847
YDOT = -5645
524260 meter/sec RA = 66
49953 deg
ZDOT = 2513
018913 TA = 345
90245
MA = 345
93139
Ha = 196
262 n
mi
Hp = 186
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7702029
76 X = -2416200
29
Y = 13318779
34 feet Y = 4032928
50 meter
Z = 15804322
17 Z = 4805585
74
XDOT = -15093
012998 XDOT = -4549
087169
YDOT = -18522
061222 feet/sec YDOT = -5696
681371 meter/sec
ZDOT = 8244
812706 ZDOT = 2490
794848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6509730
13 X = 1984165
74
Y = -13992819
19 feet Y = -4265011
29 meter
Z = 15757924
03 Z = 4803015
24
XDOT = 15794
565817 XDOT = 4814
183661
YDOT = 16542
498364 feet/sec YDOT = 5042
153501 meter/sec
ZDOT = 8155
712171 ZDOT = 2485
861070
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 10270
55201885
00016717 00000-0 10270-3 0 9056
2 25544 51
6415 66
8863 0006785 36
7992 323
3634 15
71390455 39571
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55201885 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 66
8863 deg
Eccentricity:
0006785
Arg of perigee: 36
7992 deg
Mean anomaly: 323
3634 deg
Mean motion: 15
71390455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 331
Coasting Arc #7 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4709950
96 A = 6735846
18 meter
Y = 3802328
93 meter E =
0011162
Z = -2953238
74 I = 51
94996
XDOT = -1409
808843 Wp = 51
32192
YDOT = 5642
580385 meter/sec RA = 61
36279 deg
ZDOT = 5035
976014 TA = 274
84213
MA = 274
96957
Ha = 196
292 n
mi
Hp = 185
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15452595
01 X = 4681429
10
Y = 12474832
45 feet Y = 3854838
84 meter
Z = -9689103
49 Z = -2930426
85
XDOT = -4625
357097 XDOT = -1497
264710
YDOT = 18512
402838 feet/sec YDOT = 5626
326257 meter/sec
ZDOT = 16522
231018 ZDOT = 5028
914399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16799375
42 X = -5120449
63
Y = -10674687
99 feet Y = -3253644
90 meter
Z = -9597650
01 Z = -2925363
72
XDOT = 1859
464318 XDOT = 566
764724
YDOT = -17697
968912 feet/sec YDOT = -5394
340924 meter/sec
ZDOT = 16493
903145 ZDOT = 5027
341678
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 10271
50594437
00016717 00000-0 10270-3 0 9061
2 25544 51
6430 62
0071 0006850 41
6025 318
5657 15
71408490 39729
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50594437 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 62
0071 deg
Eccentricity:
0006850
Arg of perigee: 41
6025 deg
Mean anomaly: 318
5657 deg
Mean motion: 15
71408490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 294
Coasting Arc #8 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355
32 A = 6732883
21 meter
Y = -5500108
03 meter E =
0013106
Z = -3898352
33 I = 51
92519
XDOT = 5806
204064 Wp = 58
44977
YDOT = 2912
239084 meter/sec RA = 56
31748 deg
ZDOT = -4105
714604 TA = 168
82117
MA = 168
79202
Ha = 196
242 n
mi
Hp = 185
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14289
09 X = 84795
97
Y = -18044973
85 feet Y = -5499609
66 meter
Z = -12789869
84 Z = -3898135
63
XDOT = 19049
225932 XDOT = 5793
152432
YDOT = 9554
590170 feet/sec YDOT = 2977
094461 meter/sec
ZDOT = -13470
192269 ZDOT = -4077
539453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2223029
59 X = 677579
42
Y = 17908161
15 feet Y = 5458407
52 meter
Z = -12788978
05 Z = -3898080
51
XDOT = -18889
556586 XDOT = -5757
536848
YDOT = -7186
190618 feet/sec YDOT = -2190
350900 meter/sec
ZDOT = -13357
234205 ZDOT = -4071
284986
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 10272
52344350
00016717 00000-0 10270-3 0 9072
2 25544 51
6433 56
8022 0006925 44
5990 315
5728 15
71446254 39888
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52344350 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 56
8022 deg
Eccentricity:
0006925
Arg of perigee: 44
5990 deg
Mean anomaly: 315
5728 deg
Mean motion: 15
71446254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 314
Coasting Arc #9 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2010/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5153701
02 A = 6732081
18 meter
Y = -1215155
03 meter E =
0016893
Z = 4149163
27 I = 51
90439
XDOT = -1494
404753 Wp = 64
73789
YDOT = -6553
784011 meter/sec RA = 51
16971 deg
ZDOT = -3756
713617 TA = 63
65768
MA = 63
48430
Ha = 196
379 n
mi
Hp = 185
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16908467
93 X = -5159885
99
Y = -3986729
09 feet Y = -1272821
30 meter
Z = 13612740
39 Z = 4124111
35
XDOT = -4902
902733 XDOT = -1402
758442
YDOT = -21501
916045 feet/sec YDOT = -6569
983002 meter/sec
ZDOT = -12325
175910 ZDOT = -3763
750753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17387694
73 X = 5299769
35
Y = 1477468
83 feet Y = 450332
50 meter
Z = 13512296
45 Z = 4118547
96
XDOT = 8008
114789 XDOT = 2440
873388
YDOT = 19305
339179 feet/sec YDOT = 5884
267382 meter/sec
ZDOT = -12353
357186 ZDOT = -3765
303270
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 10273
54092217
00016717 00000-0 10270-3 0 9088
2 25544 51
6431 51
5965 0006893 48
8493 311
3263 15
71450770 40049
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54092217 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 51
5965 deg
Eccentricity:
0006893
Arg of perigee: 48
8493 deg
Mean anomaly: 311
3263 deg
Mean motion: 15
71450770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 301
Coasting Arc #10 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2010/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2604845
76 A = 6736260
92 meter
Y = 5635293
15 meter E =
0020140
Z = 2587269
30 I = 51
90082
XDOT = -5603
487293 Wp = 68
55454
YDOT = 151
818184 meter/sec RA = 46
11933 deg
ZDOT = 5285
377641 TA = 320
70912
MA = 320
85510
Ha = 196
158 n
mi
Hp = 185
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8546081
90 X = 2529068
71
Y = 18488494
59 feet Y = 5663998
48 meter
Z = 8488416
35 Z = 2599739
50
XDOT = -18384
144661 XDOT = -5630
444053
YDOT = 498
091154 feet/sec YDOT = 89
006049 meter/sec
ZDOT = 17340
477826 ZDOT = 5258
090252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11381685
99 X = -3469137
89
Y = -16866131
08 feet Y = -5140796
75 meter
Z = 8538384
31 Z = 2602499
54
XDOT = 16931
195073 XDOT = 5160
628258
YDOT = -2660
354111 feet/sec YDOT = -810
875933 meter/sec
ZDOT = 17231
059697 ZDOT = 5252
026996
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 10274
55837645
00016717 00000-0 10270-3 0 9093
2 25544 51
6444 46
3915 0006841 52
2315 307
9466 15
71537433 40201
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55837645 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 46
3915 deg
Eccentricity:
0006841
Arg of perigee: 52
2315 deg
Mean anomaly: 307
9466 deg
Mean motion: 15
71537433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 308
Coasting Arc #11 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2010/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4343345
27 A = 6728623
06 meter
Y = -1389896
74 meter E =
0017845
Z = -4962564
39 I = 51
85325
XDOT = 4334
465864 Wp = 87
85949
YDOT = 5977
880771 meter/sec RA = 40
98137 deg
ZDOT = 2126
556560 TA = 202
70483
MA = 202
78386
Ha = 196
240 n
mi
Hp = 185
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14249820
45 X = 4382671
87
Y = -4560028
68 feet Y = -1341107
18 meter
Z = -16281379
22 Z = -4941368
76
XDOT = 14220
688530 XDOT = 4256
967486
YDOT = 19612
469720 feet/sec YDOT = 6025
918148 meter/sec
ZDOT = 6976
891601 ZDOT = 2147
424955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13297183
60 X = -4052981
56
Y = 7056684
40 feet Y = 2150877
41 meter
Z = -16196378
22 Z = -4936656
08
XDOT = -16948
416039 XDOT = -5165
877209
YDOT = -15785
848063 feet/sec YDOT = -4811
526490 meter/sec
ZDOT = 7060
531357 ZDOT = 2152
049958
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 10275
51222268
00016717 00000-0 10270-3 0 9101
2 25544 51
6445 41
5123 0006965 54
9275 305
2540 15
71550369 40354
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51222268 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 41
5123 deg
Eccentricity:
0006965
Arg of perigee: 54
9275 deg
Mean anomaly: 305
2540 deg
Mean motion: 15
71550369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 289
Coasting Arc #12 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4818388
20 A = 6738477
58 meter
Y = -4574472
19 meter E =
0012276
Z = -1120049
88 I = 51
86348
XDOT = 4032
850648 Wp = 107
23026
YDOT = -2813
484799 meter/sec RA = 35
90660 deg
ZDOT = -5914
917595 TA = 84
97119
MA = 84
83107
Ha = 196
203 n
mi
Hp = 185
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15808360
24 X = -4761436
48
Y = -15008110
87 feet Y = -4628035
95 meter
Z = -3674704
33 Z = -1143319
01
XDOT = 13231
137297 XDOT = 4092
745488
YDOT = -9230
593171 feet/sec YDOT = -2768
052549 meter/sec
ZDOT = -19405
897620 ZDOT = -5895
180292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18422066
47 X = 5615045
86
Y = 11622430
75 feet Y = 3542516
89 meter
Z = -3767979
29 Z = -1148480
09
XDOT = -10430
001729 XDOT = -3179
064527
YDOT = 10324
997394 feet/sec YDOT = 3147
059206 meter/sec
ZDOT = -19326
734402 ZDOT = -5890
788646
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 10276
52963568
00016717 00000-0 10270-3 0 9119
2 25544 51
6447 36
3055 0007014 58
0388 302
1455 15
71585768 40518
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52963568 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 36
3055 deg
Eccentricity:
0007014
Arg of perigee: 58
0388 deg
Mean anomaly: 302
1455 deg
Mean motion: 15
71585768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 311
Coasting Arc #13 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2010/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2488122
17 A = 6726901
27 meter
Y = 3346162
72 meter E =
0009621
Z = 5271499
71 I = 51
80065
XDOT = -6452
368343 Wp = 63
01750
YDOT = -4192
359024 meter/sec RA = 30
78909 deg
ZDOT = -379
516790 TA = 30
60447
MA = 30
54838
Ha = 196
267 n
mi
Hp = 185
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8163130
48 X = -2550962
74
Y = 10978224
15 feet Y = 3317988
17 meter
Z = 17294946
55 Z = 5259259
42
XDOT = -21169
187478 XDOT = -6403
165422
YDOT = -13754
458740 feet/sec YDOT = -4264
238210 meter/sec
ZDOT = -1245
133827 ZDOT = -410
742602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5739137
62 X = 1749289
15
Y = -12486652
35 feet Y = -3805931
63 meter
Z = 17245842
79 Z = 5256532
88
XDOT = 22693
795938 XDOT = 6917
069002
YDOT = 8516
119582 feet/sec YDOT = 2595
713249 meter/sec
ZDOT = -1370
313320 ZDOT = -417
671500
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 10277
54702595
00016717 00000-0 10270-3 0 9124
2 25544 51
6457 31
0999 0007027 60
6524 299
5339 15
71632648 40670
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54702595 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 31
0999 deg
Eccentricity:
0007027
Arg of perigee: 60
6524 deg
Mean anomaly: 299
5339 deg
Mean motion: 15
71632648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 328
Coasting Arc #14 (Orbit 4081)
---------------------------------------
Vector Time (GMT): 2010/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6199919
98 A = 6738852
52 meter
Y = 2582418
20 meter E =
0018157
Z = -457377
51 I = 51
81478
XDOT = -1465
807084 Wp = 49
90921
YDOT = 4557
285017 meter/sec RA = 25
68322 deg
ZDOT = 6029
609329 TA = 305
13198
MA = 305
30200
Ha = 196
274 n
mi
Hp = 185
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20340944
83 X = 6172803
98
Y = 8472500
64 feet Y = 2651597
76 meter
Z = -1500582
38 Z = -427324
23
XDOT = -4809
078358 XDOT = -1545
949520
YDOT = 14951
722497 feet/sec YDOT = 4540
446046 meter/sec
ZDOT = 19782
182838 ZDOT = 6022
293216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21751301
03 X = -6629796
55
Y = -3572853
26 feet Y = -1089005
67 meter
Z = -1380099
39 Z = -420654
29
XDOT = 1100
463992 XDOT = 335
421425
YDOT = -14097
936564 feet/sec YDOT = -4297
051065 meter/sec
ZDOT = 19752
815855 ZDOT = 6020
658273
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 10278
50080985
00016717 00000-0 10270-3 0 9134
2 25544 51
6463 26
2200 0007137 63
7880 296
4015 15
71629653 40825
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
50080985 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 26
2200 deg
Eccentricity:
0007137
Arg of perigee: 63
7880 deg
Mean anomaly: 296
4015 deg
Mean motion: 15
71629653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4082
Checksum: 303
Coasting Arc #15 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 9293
55 A = 6727341
13 meter
Y = -4340587
36 meter E =
0021036
Z = -5158183
19 I = 51
74893
XDOT = 7382
489038 Wp = 75
30488
YDOT = 1630
137902 meter/sec RA = 20
59164 deg
ZDOT = -1357
830936 TA = 181
68289
MA = 181
68998
Ha = 196
169 n
mi
Hp = 184
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 30490
64 X = 82887
97
Y = -14240772
19 feet Y = -4340072
54 meter
Z = -16923173
20 Z = -5157958
78
XDOT = 24220
764559 XDOT = 7370
308032
YDOT = 5348
221463 feet/sec YDOT = 1712
625068 meter/sec
ZDOT = -4454
825905 ZDOT = -1321
996111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3381496
66 X = 1030680
18
Y = 13834651
20 feet Y = 4216801
69 meter
Z = -16922240
39 Z = -5157898
87
XDOT = -23808
174087 XDOT = -7256
731462
YDOT = 543
432671 feet/sec YDOT = 165
638278 meter/sec
ZDOT = -4311
163978 ZDOT = -1314
042781
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 10279
51815675
00016717 00000-0 10270-3 0 9149
2 25544 51
6467 21
0145 0007022 67
2536 292
9367 15
71665965 40984
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51815675 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 21
0145 deg
Eccentricity:
0007022
Arg of perigee: 67
2536 deg
Mean anomaly: 292
9367 deg
Mean motion: 15
71665965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 327
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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