[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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
200/03:16:13
873 6
8 7
7 7
7
N/A -1
3 -0
1 219
3
000/00:18:27
745 3
3 0
1 215
4
Coasting Arc #1 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2012/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839071
08 A = 6776878
52 meter
Y = 2395561
94 meter E =
0015596
Z = 4079920
00 I = 51
69922
XDOT = -5263
756663 Wp = 100
60083
YDOT = -4051
002097 meter/sec RA = 10
30030 deg
ZDOT = -3854
920189 TA = 29
20691
MA = 29
11979
Ha = 220
431 n
mi
Hp = 209
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15876217
45 X = -4885318
23
Y = 7859455
18 feet Y = 2341189
55 meter
Z = 13385564
31 Z = 4056300
09
XDOT = -17269
542856 XDOT = -5199
340166
YDOT = -13290
689293 feet/sec YDOT = -4109
504223 meter/sec
ZDOT = -12647
375949 ZDOT = -3880
334874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12188054
56 X = 3714919
03
Y = 12956938
76 feet Y = 3949274
93 meter
Z = 13287878
40 Z = 4050145
34
XDOT = -6730
610961 XDOT = -2051
490221
YDOT = 19441
432057 feet/sec YDOT = 5925
748491 meter/sec
ZDOT = -12751
713182 ZDOT = -3886
722178
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 12191
54103046
00016717 00000-0 10270-3 0 9004
2 25544 51
6371 10
6495 0007163 137
4657 222
7053 15
56009020 21495
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
54103046 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 10
6495 deg
Eccentricity:
0007163
Arg of perigee: 137
4657 deg
Mean anomaly: 222
7053 deg
Mean motion: 15
56009020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 273
Coasting Arc #2 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2012/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6289511
43 A = 6781708
86 meter
Y = -1197570
67 meter E =
0008888
Z = -2245580
16 I = 51
68550
XDOT = 2814
594579 Wp = 96
97073
YDOT = 4589
122819 meter/sec RA = 5
30893 deg
ZDOT = 5453
320083 TA = 238
07977
MA = 238
16624
Ha = 220
299 n
mi
Hp = 209
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20634880
02 X = 6313343
90
Y = -3929037
64 feet Y = -1127104
02 meter
Z = -7367388
98 Z = -2214968
42
XDOT = 9234
234184 XDOT = 2736
578068
YDOT = 15056
177229 feet/sec YDOT = 4620
160705 meter/sec
ZDOT = 17891
470090 ZDOT = 5466
804036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10130880
70 X = -3087892
44
Y = -18451206
03 feet Y = -5623927
60 meter
Z = -7241013
94 Z = -2207061
05
XDOT = 10152
723746 XDOT = 3094
550198
YDOT = -12594
557664 feet/sec YDOT = -3838
821176 meter/sec
ZDOT = 17946
538758 ZDOT = 5470
105013
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 12192
50438344
00016717 00000-0 10270-3 0 9014
2 25544 51
6371 5
8320 0007313 140
4829 219
6859 15
56037819 21643
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
50438344 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 5
8320 deg
Eccentricity:
0007313
Arg of perigee: 140
4829 deg
Mean anomaly: 219
6859 deg
Mean motion: 15
56037819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 301
Coasting Arc #3 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2012/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6773093
35 A = 6783600
20 meter
Y = -97777
73 meter E =
0018890
Z = -74228
49 I = 51
66209
XDOT = 124
838722 Wp = 137
87521
YDOT = -4760
443150 meter/sec RA =
33054 deg
ZDOT = -6020
384057 TA = 42
92523
MA = 42
77796
Ha = 220
018 n
mi
Hp = 209
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22221434
88 X = -6771136
00
Y = -320793
07 feet Y = -173507
71 meter
Z = -243531
78 Z = -107126
96
XDOT = 409
575859 XDOT = 207
307216
YDOT = -15618
251803 feet/sec YDOT = -4758
585463 meter/sec
ZDOT = -19751
916198 ZDOT = -6019
577725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6929208
24 X = 2112022
67
Y = 21113897
78 feet Y = 6435516
04 meter
Z = -379179
99 Z = -115574
06
XDOT = -13401
823727 XDOT = -4084
875872
YDOT = 4077
648387 feet/sec YDOT = 1242
867228 meter/sec
ZDOT = -19748
033314 ZDOT = -6019
200554
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 12193
53194351
00016717 00000-0 10270-3 0 9026
2 25544 51
6371
6939 0007032 143
2663 216
8974 15
56100988 21800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
53194351 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node:
6939 deg
Eccentricity:
0007032
Arg of perigee: 143
2663 deg
Mean anomaly: 216
8974 deg
Mean motion: 15
56100988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 300
Coasting Arc #4 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6218187
84 A = 6781250
54 meter
Y = 1348710
66 meter E =
0017278
Z = 2334202
78 I = 51
62365
XDOT = -3023
593681 Wp = 97
05752
YDOT = 4534
915538 meter/sec RA = 355
34881 deg
ZDOT = 5398
030082 TA = 289
00332
MA = 289
19045
Ha = 220
050 n
mi
Hp = 209
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20400878
75 X = 6191305
15
Y = 4424903
74 feet Y = 1418095
74 meter
Z = 7658145
61 Z = 2364345
18
XDOT = -9919
926775 XDOT = -3100
301618
YDOT = 14878
331817 feet/sec YDOT = 4500
674368 meter/sec
ZDOT = 17710
072448 ZDOT = 5383
155818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2796287
43 X = -852308
41
Y = -20640730
33 feet Y = -6291294
61 meter
Z = 7782277
88 Z = 2372038
30
XDOT = 15905
345260 XDOT = 4847
949235
YDOT = 4543
494625 feet/sec YDOT = 1384
857162 meter/sec
ZDOT = 17648
205673 ZDOT = 5379
173089
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 12194
55949083
00016717 00000-0 10270-3 0 9030
2 25544 51
6371 355
5555 0007297 148
0319 212
1279 15
56088819 21962
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55949083 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 355
5555 deg
Eccentricity:
0007297
Arg of perigee: 148
0319 deg
Mean anomaly: 212
1279 deg
Mean motion: 15
56088819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 336
Coasting Arc #5 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2012/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4669853
34 A = 6776012
45 meter
Y = -2575390
96 meter E =
0011666
Z = -4187510
31 I = 51
57690
XDOT = 5460
137724 Wp = 107
23251
YDOT = -3904
985314 meter/sec RA = 350
35032 deg
ZDOT = -3699
334717 TA = 124
79343
MA = 124
68359
Ha = 219
919 n
mi
Hp = 209
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15321041
15 X = -4620365
83
Y = -8449445
40 feet Y = -2627334
96 meter
Z = -13738550
88 Z = -4210076
25
XDOT = 17913
837677 XDOT = 5521
368711
YDOT = -12811
631607 feet/sec YDOT = -3843
583865 meter/sec
ZDOT = -12136
924925 ZDOT = -3672
661466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2438503
05 X = -743255
73
Y = 17251788
04 feet Y = 5258345
00 meter
Z = -13831295
02 Z = -4215778
72
XDOT = -17142
629524 XDOT = -5225
073479
YDOT = -12033
990734 feet/sec YDOT = -3667
960376 meter/sec
ZDOT = -12026
480607 ZDOT = -3665
671289
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 12195
52280180
00016717 00000-0 10270-3 0 9045
2 25544 51
6379 350
7388 0007228 150
3775 209
7789 15
56114852 22110
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
52280180 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 350
7388 deg
Eccentricity:
0007228
Arg of perigee: 150
3775 deg
Mean anomaly: 209
7789 deg
Mean motion: 15
56114852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 319
Coasting Arc #6 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2012/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2454478
40 A = 6772058
91 meter
Y = 3607492
36 meter E =
0010926
Z = 5175032
07 I = 51
53335
XDOT = -6992
069434 Wp = 143
21341
YDOT = 2890
784142 meter/sec RA = 345
32999 deg
ZDOT = 1291
140953 TA = 294
32318
MA = 294
43723
Ha = 219
768 n
mi
Hp = 210
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8052750
66 X = 2388817
27
Y = 11835604
87 feet Y = 3634572
06 meter
Z = 16978451
66 Z = 5186796
72
XDOT = -22939
860347 XDOT = -7030
147140
YDOT = 9484
199942 feet/sec YDOT = 2812
381413 meter/sec
ZDOT = 4236
026749 ZDOT = 1257
081881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8006780
36 X = 2440466
65
Y = -11797657
11 feet Y = -3595925
89 meter
Z = 17026535
51 Z = 5189688
02
XDOT = 16521
931190 XDOT = 5035
884627
YDOT = 17170
521366 feet/sec YDOT = 5233
574912 meter/sec
ZDOT = 4095
248401 ZDOT = 1248
231713
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 12196
55031877
00016717 00000-0 10270-3 0 9057
2 25544 51
6375 345
5997 0007148 154
8376 205
3127 15
56125122 22278
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
55031877 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 345
5997 deg
Eccentricity:
0007148
Arg of perigee: 154
8376 deg
Mean anomaly: 205
3127 deg
Mean motion: 15
56125122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 319
Coasting Arc #7 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2012/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 109625
02 A = 6772160
94 meter
Y = -4400251
93 meter E =
0018747
Z = -5162695
73 I = 51
50557
XDOT = 7385
829214 Wp = 119
42859
YDOT = -1462
997063 meter/sec RA = 340
30072 deg
ZDOT = 1398
588411 TA = 164
09470
MA = 164
03575
Ha = 219
756 n
mi
Hp = 210
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 359662
15 X = 183900
39
Y = -14436522
10 feet Y = -4398610
03 meter
Z = -16937978
12 Z = -5161983
38
XDOT = 24231
723144 XDOT = 7394
845847
YDOT = -4799
859132 feet/sec YDOT = -1380
353918 meter/sec
ZDOT = 4588
544655 ZDOT = 1434
489835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13476434
77 X = -4107617
32
Y = 5200509
30 feet Y = 1585115
23 meter
Z = -16934522
11 Z = -5161642
34
XDOT = -13473
864597 XDOT = -4106
833929
YDOT = -19436
020208 feet/sec YDOT = -5924
098959 meter/sec
ZDOT = 4736
751107 ZDOT = 1443
761737
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 12197
51360177
00016717 00000-0 10270-3 0 9063
2 25544 51
6385 340
7834 0007226 157
9936 202
1529 15
56154957 22425
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
51360177 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 340
7834 deg
Eccentricity:
0007226
Arg of perigee: 157
9936 deg
Mean anomaly: 202
1529 deg
Mean motion: 15
56154957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 322
Coasting Arc #8 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2012/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2542526
39 A = 6776390
69 meter
Y = 4754329
71 meter E =
0013384
Z = 4090982
78 I = 51
49107
XDOT = -6659
496798 Wp = 109
13923
YDOT = -274
570679 meter/sec RA = 335
27661 deg
ZDOT = -3813
866748 TA = 20
28413
MA = 20
23101
Ha = 219
713 n
mi
Hp = 210
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8341622
02 X = -2615374
15
Y = 15598194
59 feet Y = 4725489
72 meter
Z = 13421859
50 Z = 4078455
16
XDOT = -21848
742775 XDOT = -6637
404860
YDOT = -900
822439 feet/sec YDOT = -348
917246 meter/sec
ZDOT = -12512
686180 ZDOT = -3846
164285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17674776
56 X = 5387271
89
Y = 1373865
70 feet Y = 418754
26 meter
Z = 13369645
16 Z = 4075067
85
XDOT = 8105
115313 XDOT = 2470
439147
YDOT = 18978
113921 feet/sec YDOT = 5784
529123 meter/sec
ZDOT = -12645
829074 ZDOT = -3854
448702
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 12198
54108953
00016717 00000-0 10270-3 0 9070
2 25544 51
6383 335
6440 0007198 161
8283 198
3129 15
56147073 22586
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
54108953 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 335
6440 deg
Eccentricity:
0007198
Arg of perigee: 161
8283 deg
Mean anomaly: 198
3129 deg
Mean motion: 15
56147073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 330
Coasting Arc #9 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2012/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4478751
22 A = 6781297
49 meter
Y = -4588846
74 meter E =
0006370
Z = -2216023
63 I = 51
48197
XDOT = 4926
418621 Wp = 110
42671
YDOT = 2181
671641 meter/sec RA = 330
27084 deg
ZDOT = 5449
505971 TA = 224
89803
MA = 224
94958
Ha = 219
480 n
mi
Hp = 210
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14694065
68 X = 4540496
55
Y = -15055271
47 feet Y = -4538417
03 meter
Z = -7270418
72 Z = -2194117
03
XDOT = 16162
790750 XDOT = 4875
184515
YDOT = 7157
715357 feet/sec YDOT = 2236
474706 meter/sec
ZDOT = 17878
956598 ZDOT = 5473
313780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19862730
72 X = -6054160
32
Y = -7025787
95 feet Y = -2141460
17 meter
Z = -7179553
32 Z = -2188327
85
XDOT = -780
918758 XDOT = -238
024038
YDOT = -16126
731304 feet/sec YDOT = -4915
427702 meter/sec
ZDOT = 17976
872312 ZDOT = 5479
350681
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 12199
50434410
00016717 00000-0 10270-3 0 9088
2 25544 51
6396 330
8270 0007049 165
3642 194
7717 15
56191848 22730
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
50434410 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 330
8270 deg
Eccentricity:
0007049
Arg of perigee: 165
3642 deg
Mean anomaly: 194
7717 deg
Mean motion: 15
56191848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 322
Coasting Arc #10 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2012/200/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4436405
23 A = 6786371
42 meter
Y = -4741599
56 meter E =
0002642
Z = -1967061
68 I = 51
46824
XDOT = 4795
540908 Wp = 8
36662
YDOT = 2177
681414 meter/sec RA = 327
05502 deg
ZDOT = 5569
811671 TA = 329
87962
MA = 329
89481
Ha = 219
349 n
mi
Hp = 215
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14555135
26 X = 4498652
42
Y = -15556429
02 feet Y = -4691640
63 meter
Z = -6453614
45 Z = -1945359
61
XDOT = 15733
401930 XDOT = 4743
776796
YDOT = 7144
624061 feet/sec YDOT = 2231
017983 meter/sec
ZDOT = 18273
660339 ZDOT = 5592
982341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17738630
21 X = 5406734
49
Y = -11846918
08 feet Y = -3610940
63 meter
Z = -6363577
29 Z = -1939618
36
XDOT = 12733
079975 XDOT = 3881
042776
YDOT = 9204
871222 feet/sec YDOT = 2805
644748 meter/sec
ZDOT = 18368
951736 ZDOT = 5598
856489
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 12200
14650632
00016717 00000-0 10270-3 0 9098
2 25544 51
6413 327
6199 0004850 235
7006 124
3688 15
54595867 22831
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
14650632 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 327
6199 deg
Eccentricity:
0004850
Arg of perigee: 235
7006 deg
Mean anomaly: 124
3688 deg
Mean motion: 15
54595867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 313
Coasting Arc #11 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2012/201/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5282965
22 A = 6788046
97 meter
Y = 4248390
12 meter E =
0011975
Z = 129769
11 I = 51
44881
XDOT = -3088
810372 Wp = 156
48481
YDOT = -3652
289276 meter/sec RA = 322
06892 deg
ZDOT = -5997
620879 TA = 22
11290
MA = 22
06129
Ha = 219
244 n
mi
Hp = 215
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17332563
07 X = -5330709
33
Y = 13938287
81 feet Y = 4189045
76 meter
Z = 425751
68 Z = 103989
72
XDOT = -10133
892295 XDOT = -3018
605645
YDOT = -11982
576366 feet/sec YDOT = -3686
437063 meter/sec
ZDOT = -19677
233854 ZDOT = -6012
455772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19872411
21 X = -6057110
94
Y = 9993018
01 feet Y = 3045871
89 meter
Z = 318963
75 Z = 97220
15
XDOT = -6548
962110 XDOT = -1996
123651
YDOT = -12368
220634 feet/sec YDOT = -3769
833649 meter/sec
ZDOT = -19737
987830 ZDOT = -6016
138691
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 12201
17503226
00016717 00000-0 10270-3 0 9100
2 25544 51
6415 322
4888 0004907 238
9908 121
0763 15
54569126 22994
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
17503226 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 322
4888 deg
Eccentricity:
0004907
Arg of perigee: 238
9908 deg
Mean anomaly: 121
0763 deg
Mean motion: 15
54569126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 308
Coasting Arc #12 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5630537
91 A = 6786623
78 meter
Y = -3371425
06 meter E =
0009155
Z = 1711521
20 I = 51
42120
XDOT = 1265
156824 Wp = 63
98535
YDOT = 5002
757427 meter/sec RA = 317
08088 deg
ZDOT = 5672
830910 TA = 314
84731
MA = 314
92165
Ha = 218
962 n
mi
Hp = 215
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18472893
40 X = 5659505
39
Y = -11061105
84 feet Y = -3308299
08 meter
Z = 5615227
03 Z = 1738943
58
XDOT = 4150
776982 XDOT = 1181
564178
YDOT = 16413
246153 feet/sec YDOT = 5016
437288 meter/sec
ZDOT = 18611
649966 ZDOT = 5678
774271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20225290
51 X = 6164668
55
Y = -7297014
91 feet Y = -2224130
14 meter
Z = 5728684
35 Z = 1746102
99
XDOT = 263
362717 XDOT = 80
272956
YDOT = 15410
023527 feet/sec YDOT = 4696
975171 meter/sec
ZDOT = 18635
593307 ZDOT = 5680
128840
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 12202
20354327
00016717 00000-0 10270-3 0 9112
2 25544 51
6415 317
3571 0004798 246
3280 113
7369 15
54615009 23151
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20354327 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 317
3571 deg
Eccentricity:
0004798
Arg of perigee: 246
3280 deg
Mean anomaly: 113
7369 deg
Mean motion: 15
54615009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 287
Coasting Arc #13 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2012/203/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5506650
60 A = 6783000
39 meter
Y = 2093716
76 meter E =
0001773
Z = -3360132
37 I = 51
38755
XDOT = 511
466893 Wp = 175
42424
YDOT = -6087
127458 meter/sec RA = 312
08432 deg
ZDOT = -4633
027733 TA = 43
92548
MA = 43
91138
Ha = 218
709 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18066438
97 X = -5513331
27
Y = 6869149
49 feet Y = 2032100
86 meter
Z = -11024056
34 Z = -3386898
97
XDOT = 1678
040988 XDOT = 602
002132
YDOT = -19970
890609 feet/sec YDOT = -6080
901386 meter/sec
ZDOT = -15200
222220 ZDOT = -4630
323618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18926483
60 X = -5768792
20
Y = 3594271
99 feet Y = 1095534
10 meter
Z = -11134661
09 Z = -3393844
70
XDOT = 5519
513951 XDOT = 1682
347852
YDOT = -17968
535005 feet/sec YDOT = -5476
809469 meter/sec
ZDOT = -15188
395861 ZDOT = -4629
423058
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 12203
16776005
00016717 00000-0 10270-3 0 9120
2 25544 51
6414 312
5468 0005002 250
1744 109
8870 15
54624363 23302
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
16776005 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 312
5468 deg
Eccentricity:
0005002
Arg of perigee: 250
1744 deg
Mean anomaly: 109
8870 deg
Mean motion: 15
54624363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 276
Coasting Arc #14 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2012/204/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4975935
83 A = 6778829
82 meter
Y = -518920
80 meter E =
0005653
Z = 4573876
96 I = 51
35392
XDOT = -2072
746311 Wp = 146
52015
YDOT = 6740
092071 meter/sec RA = 307
07322 deg
ZDOT = 3013
217872 TA = 273
24149
MA = 273
30617
Ha = 218
563 n
mi
Hp = 215
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16325248
79 X = 4959150
24
Y = -1702496
07 feet Y = -463370
88 meter
Z = 15006158
02 Z = 4598008
60
XDOT = -6800
348789 XDOT = -2162
598617
YDOT = 22113
162962 feet/sec YDOT = 6716
410790 meter/sec
ZDOT = 9885
885406 ZDOT = 3002
930844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16297304
25 X = 4967418
34
Y = 901170
71 feet Y = 274676
83 meter
Z = 15105720
27 Z = 4604223
54
XDOT = -10223
663308 XDOT = -3116
172576
YDOT = 19553
250284 feet/sec YDOT = 5959
830686 meter/sec
ZDOT = 9842
730577 ZDOT = 3000
064280
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 12204
19624636
00016717 00000-0 10270-3 0 9137
2 25544 51
6412 307
4149 0004760 255
0897 104
9729 15
54645641 23460
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
19624636 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 307
4149 deg
Eccentricity:
0004760
Arg of perigee: 255
0897 deg
Mean anomaly: 104
9729 deg
Mean motion: 15
54645641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 311
Coasting Arc #15 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2012/205/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4142842
86 A = 6776002
78 meter
Y = -1257474
70 meter E =
0009490
Z = -5220811
57 I = 51
32636
XDOT = 3331
065226 Wp = 83
55128
YDOT = -6827
843318 meter/sec RA = 302
04932 deg
ZDOT = -999
263049 TA = 176
83608
MA = 176
83008
Ha = 218
403 n
mi
Hp = 215
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13592004
12 X = -4103112
47
Y = -4125573
17 feet Y = -1303580
20 meter
Z = -17128646
90 Z = -5240840
56
XDOT = 10928
691685 XDOT = 3412
022122
YDOT = -22401
060755 feet/sec YDOT = -6790
140585 meter/sec
ZDOT = -3278
422077 ZDOT = -982
884747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12764501
88 X = -3890620
17
Y = -5999921
95 feet Y = -1828776
21 meter
Z = -17211098
25 Z = -5245942
75
XDOT = 13580
849688 XDOT = 4139
442985
YDOT = -19688
898933 feet/sec YDOT = -6001
176395 meter/sec
ZDOT = -3210
152579 ZDOT = -978
454506
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 12205
16043820
00016717 00000-0 10270-3 0 9146
2 25544 51
6402 302
6034 0004903 259
9645 100
0954 15
54701337 23611
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
16043820 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 302
6034 deg
Eccentricity:
0004903
Arg of perigee: 259
9645 deg
Mean anomaly: 100
0954 deg
Mean motion: 15
54701337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 271
Coasting Arc #16 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/03:25:27
745
Vector Time (MET): N/A
Weight (LBS) : 907923
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3115984
59 A = 6776097
28 meter
Y = 3043094
01 meter E =
0002317
Z = 5192621
85 I = 51
31148
XDOT = -4235
194519 Wp = 315
18363
YDOT = 6289
534177 meter/sec RA = 297
02068 deg
ZDOT = -1143
175487 TA = 145
83445
MA = 145
81954
Ha = 218
198 n
mi
Hp = 215
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10223046
56 X = 3056500
20
Y = 9983904
25 feet Y = 3077606
12 meter
Z = 17036160
93 Z = 5207614
62
XDOT = -13894
995141 XDOT = -4299
657387
YDOT = 20634
954650 feet/sec YDOT = 6241
813209 meter/sec
ZDOT = -3750
575745 ZDOT = -1163
906006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8791924
80 X = 2679778
68
Y = 11171034
24 feet Y = 3404931
24 meter
Z = 17097656
47 Z = 5211365
69
XDOT = -15526
684598 XDOT = -4732
533465
YDOT = 18098
703461 feet/sec YDOT = 5516
484815 meter/sec
ZDOT = -3836
723231 ZDOT = -1169
433241
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 12206
18889806
00016717 00000-0 10270-3 0 9152
2 25544 51
6402 297
4718 0004950 263
7068 96
3522 15
54714173 23772
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18889806 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 297
4718 deg
Eccentricity:
0004950
Arg of perigee: 263
7068 deg
Mean anomaly: 96
3522 deg
Mean motion: 15
54714173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 328
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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