[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 29th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 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
128/06:37:46
168 2
8 4
1 4
1
N/A -0
8 -0
4 223
9
000/00:13:32
337 2
9 0
1 222
9
Coasting Arc #1 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2013/119/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5823495
73 A = 6794730
79 meter
Y = 2801487
83 meter E =
0013088
Z = 2071056
75 I = 51
59713
XDOT = -3769
234857 Wp = 144
00946
YDOT = -3738
030753 meter/sec RA = 349
02591 deg
ZDOT = -5534
706376 TA = 13
07064
MA = 13
03676
Ha = 224
928 n
mi
Hp = 220
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19105957
12 X = -5864450
50
Y = 9191233
03 feet Y = 2736136
77 meter
Z = 6794805
62 Z = 2042667
02
XDOT = -12366
256094 XDOT = -3700
268832
YDOT = -12263
880423 feet/sec YDOT = -3779
794910 meter/sec
ZDOT = -18158
485485 ZDOT = -5552
849808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3231994
76 X = -985112
00
Y = 20992157
27 feet Y = 6398409
54 meter
Z = 6676023
39 Z = 2034851
93
XDOT = -15512
250678 XDOT = -4728
134007
YDOT = 3418
322240 feet/sec YDOT = 1041
904619 meter/sec
ZDOT = -18233
590149 ZDOT = -5557
598277
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 13119
58834103
00016717 00000-0 10270-3 0 9004
2 25544 51
6470 349
3997 0007757 223
8121 136
2415 15
51671893 27168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13119
58834103 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 349
3997 deg
Eccentricity:
0007757
Arg of perigee: 223
8121 deg
Mean anomaly: 136
2415 deg
Mean motion: 15
51671893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2716
Checksum: 316
Coasting Arc #2 (Orbit 2730)
---------------------------------------
Vector Time (GMT): 2013/120/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6091971
71 A = 6795930
55 meter
Y = -2749329
16 meter E =
0001928
Z = -1223172
06 I = 51
56975
XDOT = 2964
994250 Wp = 355
55071
YDOT = 3972
194291 meter/sec RA = 344
05957 deg
ZDOT = 5840
006084 TA = 351
16378
MA = 351
16717
Ha = 224
770 n
mi
Hp = 220
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19986783
82 X = 6128204
41
Y = -9020108
79 feet Y = -2681002
27 meter
Z = -4013031
70 Z = -1193489
66
XDOT = 9727
671423 XDOT = 2891
986570
YDOT = 13032
133501 feet/sec YDOT = 4004
942348 meter/sec
ZDOT = 19160
124949 ZDOT = 5854
232650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3488984
53 X = 1063442
48
Y = -21671225
40 feet Y = -6605389
50 meter
Z = -3888867
49 Z = -1185326
81
XDOT = 14590
559460 XDOT = 4447
202523
YDOT = -1099
005568 feet/sec YDOT = -334
976897 meter/sec
ZDOT = 19218
864802 ZDOT = 5857
909992
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 13120
55441050
00016717 00000-0 10270-3 0 9019
2 25544 51
6457 344
6002 0007885 227
4670 132
5816 15
51654767 27311
Satellite: ISS
Catalog Number: 25544
Epoch time: 13120
55441050 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 344
6002 deg
Eccentricity:
0007885
Arg of perigee: 227
4670 deg
Mean anomaly: 132
5816 deg
Mean motion: 15
51654767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2731
Checksum: 294
Coasting Arc #3 (Orbit 2746)
---------------------------------------
Vector Time (GMT): 2013/121/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6236280
67 A = 6796376
90 meter
Y = 2658864
53 meter E =
0013679
Z = 325511
45 I = 51
54269
XDOT = -2139
205010 Wp = 165
61982
YDOT = -4278
619572 meter/sec RA = 339
09427 deg
ZDOT = -5993
663253 TA = 10
86890
MA = 10
83937
Ha = 224
507 n
mi
Hp = 220
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20460238
42 X = -6267130
42
Y = 8723308
83 feet Y = 2588954
01 meter
Z = 1067950
95 Z = 295141
11
XDOT = -7018
389140 XDOT = -2062
085838
YDOT = -14037
465788 feet/sec YDOT = -4302
110227 meter/sec
ZDOT = -19664
249518 ZDOT = -6003
868112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3610512
18 X = -1100484
11
Y = 21953059
85 feet Y = 6691292
64 meter
Z = 940934
10 Z = 286796
71
XDOT = -13947
381413 XDOT = -4251
161855
YDOT = -1442
653719 feet/sec YDOT = -439
720853 meter/sec
ZDOT = -19706
178170 ZDOT = -6006
443106
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 13121
58487204
00016717 00000-0 10270-3 0 9025
2 25544 51
6459 339
4826 0007821 231
4533 128
5918 15
51696565 27479
Satellite: ISS
Catalog Number: 25544
Epoch time: 13121
58487204 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 339
4826 deg
Eccentricity:
0007821
Arg of perigee: 231
4533 deg
Mean anomaly: 128
5918 deg
Mean motion: 15
51696565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2747
Checksum: 328
Coasting Arc #4 (Orbit 2762)
---------------------------------------
Vector Time (GMT): 2013/122/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6276687
93 A = 6796246
86 meter
Y = -2534220
21 meter E =
0005209
Z = 577308
95 I = 51
51290
XDOT = 1317
692010 Wp = 46
71317
YDOT = 4628
572874 meter/sec RA = 334
12538 deg
ZDOT = 5961
259750 TA = 319
51942
MA = 319
55816
Ha = 224
395 n
mi
Hp = 220
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20592808
17 X = 6301755
20
Y = -8314370
75 feet Y = -2463890
16 meter
Z = 1894058
23 Z = 607861
56
XDOT = 4323
136515 XDOT = 1236
878068
YDOT = 15185
606543 feet/sec YDOT = 4642
856303 meter/sec
ZDOT = 19557
938812 ZDOT = 5967
464695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3641051
97 X = 1109792
64
Y = -21896003
79 feet Y = -6673901
95 meter
Z = 2021812
19 Z = 616248
35
XDOT = 13552
713920 XDOT = 4130
867203
YDOT = 4070
557308 feet/sec YDOT = 1240
705867 meter/sec
ZDOT = 19583
142187 ZDOT = 5968
941739
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 13122
61532151
00016717 00000-0 10270-3 0 9033
2 25544 51
6448 334
3631 0007911 234
8185 125
2226 15
51695995 27635
Satellite: ISS
Catalog Number: 25544
Epoch time: 13122
61532151 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 334
3631 deg
Eccentricity:
0007911
Arg of perigee: 234
8185 deg
Mean anomaly: 125
2226 deg
Mean motion: 15
51695995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2763
Checksum: 302
Coasting Arc #5 (Orbit 2777)
---------------------------------------
Vector Time (GMT): 2013/123/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6201047
67 A = 6795330
82 meter
Y = 2332035
51 meter E =
0010696
Z = -1478946
55 I = 51
48311
XDOT = -519
155085 Wp = 188
53363
YDOT = -5031
363220 meter/sec RA = 329
15569 deg
ZDOT = -5761
803988 TA = 7
63458
MA = 7
61831
Ha = 224
041 n
mi
Hp = 220
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20344644
58 X = -6219479
75
Y = 7651035
15 feet Y = 2262588
40 meter
Z = -4852186
83 Z = -1509115
67
XDOT = -1703
264714 XDOT = -434
865269
YDOT = -16507
097178 feet/sec YDOT = -5036
697561 meter/sec
ZDOT = -18903
556390 ZDOT = -5764
121175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3700848
03 X = -1128018
48
Y = 21389408
81 feet Y = 6519491
81 meter
Z = -4978306
26 Z = -1517387
75
XDOT = -13475
359417 XDOT = -4107
289550
YDOT = -6729
635865 feet/sec YDOT = -2051
193012 meter/sec
ZDOT = -18912
495982 ZDOT = -5764
528775
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 13123
58135573
00016717 00000-0 10270-3 0 9048
2 25544 51
6448 329
5653 0007822 238
8461 121
1924 15
51732275 27786
Satellite: ISS
Catalog Number: 25544
Epoch time: 13123
58135573 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 329
5653 deg
Eccentricity:
0007822
Arg of perigee: 238
8461 deg
Mean anomaly: 121
1924 deg
Mean motion: 15
51732275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2778
Checksum: 318
Coasting Arc #6 (Orbit 2793)
---------------------------------------
Vector Time (GMT): 2013/124/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6035700
65 A = 6793893
93 meter
Y = -2064869
00 meter E =
0006232
Z = 2331719
92 I = 51
45186
XDOT = -220
273909 Wp = 88
40218
YDOT = 5448
255092 meter/sec RA = 324
18079 deg
ZDOT = 5382
600397 TA = 297
63566
MA = 297
69891
Ha = 224
000 n
mi
Hp = 220
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19802167
48 X = 6047014
90
Y = -6774504
59 feet Y = -1997310
66 meter
Z = 7649999
75 Z = 2361068
61
XDOT = -722
683429 XDOT = -307
328544
YDOT = 17874
852663 feet/sec YDOT = 5445
305255 meter/sec
ZDOT = 17659
450123 ZDOT = 5381
318707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3820331
22 X = 1164436
96
Y = -20531273
14 feet Y = -6257932
05 meter
Z = 7772653
24 Z = 2369104
71
XDOT = 13657
238052 XDOT = 4162
726158
YDOT = 9239
444787 feet/sec YDOT = 2816
182771 meter/sec
ZDOT = 17653
329764 ZDOT = 5380
734912
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 13124
61178030
00016717 00000-0 10270-3 0 9059
2 25544 51
6440 324
4459 0007940 241
6456 118
3896 15
51745529 27943
Satellite: ISS
Catalog Number: 25544
Epoch time: 13124
61178030 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 324
4459 deg
Eccentricity:
0007940
Arg of perigee: 241
6456 deg
Mean anomaly: 118
3896 deg
Mean motion: 15
51745529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2794
Checksum: 316
Coasting Arc #7 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2013/125/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5781799
46 A = 6791951
63 meter
Y = 1693691
35 meter E =
0004912
Z = -3128517
14 I = 51
42152
XDOT = 897
716764 Wp = 212
01302
YDOT = -5874
739134 meter/sec RA = 319
20305 deg
ZDOT = -4840
070509 TA = 4
10875
MA = 4
10472
Ha = 223
573 n
mi
Hp = 221
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18969158
35 X = -5785111
28
Y = 5556730
16 feet Y = 1629017
02 meter
Z = -10264163
83 Z = -3156613
05
XDOT = 2945
264974 XDOT = 986
854690
YDOT = -19274
078525 feet/sec YDOT = -5864
202044 meter/sec
ZDOT = -15879
496421 ZDOT = -4835
492739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4132210
44 X = -1259497
74
Y = 19266755
01 feet Y = 5872506
93 meter
Z = -10381534
86 Z = -3164291
83
XDOT = -14086
030086 XDOT = -4293
421970
YDOT = -11565
699705 feet/sec YDOT = -3525
225270 meter/sec
ZDOT = -15859
578190 ZDOT = -4833
999432
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 13125
57779221
00016717 00000-0 10270-3 0 9065
2 25544 51
6442 319
6477 0007752 245
7909 114
2432 15
51772273 28094
Satellite: ISS
Catalog Number: 25544
Epoch time: 13125
57779221 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 319
6477 deg
Eccentricity:
0007752
Arg of perigee: 245
7909 deg
Mean anomaly: 114
2432 deg
Mean motion: 15
51772273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2809
Checksum: 323
Coasting Arc #8 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2013/126/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5470757
42 A = 6789835
69 meter
Y = -1241781
88 meter E =
0005896
Z = 3825427
05 I = 51
39142
XDOT = -1481
658386 Wp = 139
57696
YDOT = 6270
120767 meter/sec RA = 314
21925 deg
ZDOT = 4146
281398 TA = 266
55764
MA = 266
62509
Ha = 223
560 n
mi
Hp = 221
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17948679
20 X = 5465653
50
Y = -4074087
54 feet Y = -1180632
88 meter
Z = 12550613
68 Z = 3851991
56
XDOT = -4861
083945 XDOT = -1571
803945
YDOT = 20571
262360 feet/sec YDOT = 6253
047988 meter/sec
ZDOT = 13603
285428 ZDOT = 4138
864417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4637835
76 X = 1413612
34
Y = -17732661
73 feet Y = -5404915
29 meter
Z = 12661530
93 Z = 3859234
63
XDOT = 14672
220537 XDOT = 4472
092820
YDOT = 13546
337936 feet/sec YDOT = 4128
923803 meter/sec
ZDOT = 13571
478867 ZDOT = 4136
586759
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 13126
60819166
00016717 00000-0 10270-3 0 9074
2 25544 51
6435 314
5282 0007943 248
8373 111
1930 15
51792557 28259
Satellite: ISS
Catalog Number: 25544
Epoch time: 13126
60819166 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 314
5282 deg
Eccentricity:
0007943
Arg of perigee: 248
8373 deg
Mean anomaly: 111
1930 deg
Mean motion: 15
51792557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2825
Checksum: 317
Coasting Arc #9 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2013/127/13:15:01
890
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5112212
51 A = 6787723
94 meter
Y = 681965
52 meter E =
0001605
Z = -4414541
66 I = 51
36457
XDOT = 1980
927832 Wp = 53
95198
YDOT = -6616
966754 meter/sec RA = 309
23206 deg
ZDOT = -3316
112663 TA = 182
40082
MA = 182
40159
Ha = 223
107 n
mi
Hp = 221
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16772350
77 X = -5098013
38
Y = 2237419
69 feet Y = 624876
89 meter
Z = -14483404
41 Z = -4439342
32
XDOT = 6499
107061 XDOT = 2070
882034
YDOT = -21709
208509 feet/sec YDOT = -6594
311836 meter/sec
ZDOT = -10879
634722 ZDOT = -3306
270754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5445399
61 X = -1659757
80
Y = 15926618
83 feet Y = 4854433
42 meter
Z = -14586885
75 Z = -4446082
78
XDOT = -15334
860172 XDOT = -4674
065380
YDOT = -15169
328540 feet/sec YDOT = -4623
611339 meter/sec
ZDOT = -10837
673659 ZDOT = -3303
322931
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 13127
57418095
00016717 00000-0 10270-3 0 9088
2 25544 51
6442 309
7300 0007697 252
6981 107
3328 15
51808784 28403
Satellite: ISS
Catalog Number: 25544
Epoch time: 13127
57418095 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 309
7300 deg
Eccentricity:
0007697
Arg of perigee: 252
6981 deg
Mean anomaly: 107
3328 deg
Mean motion: 15
51808784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 325
Coasting Arc #10 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2013/128/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3335583
00 A = 6798127
57 meter
Y = -5852605
83 meter E =
0009542
Z = -865208
25 I = 51
38163
XDOT = 4566
537771 Wp = 340
72272
YDOT = 1727
740892 meter/sec RA = 305
56896 deg
ZDOT = 5908
118849 TA = 9
89353
MA = 9
87476
Ha = 223
948 n
mi
Hp = 222
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10943513
77 X = 3404983
22
Y = -19201462
68 feet Y = -5814917
19 meter
Z = -2838609
73 Z = -848835
40
XDOT = 14982
079301 XDOT = 4518
177774
YDOT = 5668
441246 feet/sec YDOT = 1778
536379 meter/sec
ZDOT = 19383
592025 ZDOT = 5930
185671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19723528
04 X = 6011731
35
Y = -9991320
91 feet Y = -3045354
61 meter
Z = -2769533
55 Z = -844153
83
XDOT = 8554
273750 XDOT = 2607
342639
YDOT = 11479
071501 feet/sec YDOT = 3498
820993 meter/sec
ZDOT = 19475
335772 ZDOT = 5936
082343
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 13128
28256468
00016717 00000-0 10270-3 0 9092
2 25544 51
6483 306
2142 0009627 277
0696 82
9361 15
51003337 28511
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
28256468 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 306
2142 deg
Eccentricity:
0009627
Arg of perigee: 277
0696 deg
Mean anomaly: 82
9361 deg
Mean motion: 15
51003337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 317
Coasting Arc #11 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2013/129/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3324477
01 A = 6798474
39 meter
Y = 5921893
10 meter E =
0006737
Z = 190460
23 I = 51
36570
XDOT = -4255
035213 Wp = 183
02907
YDOT = -2196
871833 meter/sec RA = 300
59373 deg
ZDOT = -5981
477302 TA = 354
91425
MA = 354
92109
Ha = 224
343 n
mi
Hp = 222
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10907076
81 X = -3391375
03
Y = 19428783
13 feet Y = 5884342
65 meter
Z = 624869
54 Z = 174147
52
XDOT = -13960
089283 XDOT = -4201
096062
YDOT = -7207
584755 feet/sec YDOT = -2244
152599 meter/sec
ZDOT = -19624
269362 ZDOT = -6002
017346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19628268
41 X = -5982696
21
Y = 10547715
55 feet Y = 3214943
70 meter
Z = 556036
23 Z = 169479
84
XDOT = -7045
264573 XDOT = -2147
396642
YDOT = -12074
704191 feet/sec YDOT = -3680
369837 meter/sec
ZDOT = -19709
582432 ZDOT = -6007
480725
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 13129
31347204
00016717 00000-0 10270-3 0 9108
2 25544 51
6485 301
0994 0009623 280
3074 79
6992 15
50983034 28674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
31347204 = yrday
fracday
Element set: 910
Inclination: 51
6485 deg
RA of node: 301
0994 deg
Eccentricity:
0009623
Arg of perigee: 280
3074 deg
Mean anomaly: 79
6992 deg
Mean motion: 15
50983034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2867
Checksum: 316
Coasting Arc #12 (Orbit 2882)
---------------------------------------
Vector Time (GMT): 2013/130/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3281397
19 A = 6798213
76 meter
Y = -5924658
60 meter E =
0010798
Z = 496889
40 I = 51
35082
XDOT = 3987
595975 Wp = 2
92081
YDOT = 2708
021666 meter/sec RA = 295
61652 deg
ZDOT = 5960
326101 TA = 2
45509
MA = 2
44979
Ha = 224
607 n
mi
Hp = 222
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10765738
81 X = 3344990
31
Y = -19437856
31 feet Y = -5887608
40 meter
Z = 1630214
58 Z = 512984
70
XDOT = 13082
663960 XDOT = 3928
063679
YDOT = 8884
585517 feet/sec YDOT = 2752
280379 meter/sec
ZDOT = 19554
875660 ZDOT = 5979
553385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19316111
39 X = 5887550
75
Y = -10972381
21 feet Y = -3344381
79 meter
Z = 1698140
56 Z = 517593
24
XDOT = 5622
421308 XDOT = 1713
714015
YDOT = 12934
276767 feet/sec YDOT = 3942
367559 meter/sec
ZDOT = 19634
646171 ZDOT = 5984
640153
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 13130
34436524
00016717 00000-0 10270-3 0 9118
2 25544 51
6487 295
9837 0009761 285
4428 74
5644 15
51039228 28839
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
34436524 = yrday
fracday
Element set: 911
Inclination: 51
6487 deg
RA of node: 295
9837 deg
Eccentricity:
0009761
Arg of perigee: 285
4428 deg
Mean anomaly: 74
5644 deg
Mean motion: 15
51039228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2883
Checksum: 331
Coasting Arc #13 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2013/131/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3216944
84 A = 6797779
47 meter
Y = 5867610
49 meter E =
0005568
Z = -1177683
58 I = 51
33697
XDOT = -3766
924576 Wp = 221
18488
YDOT = -3238
224611 meter/sec RA = 290
63915 deg
ZDOT = -5832
543957 TA = 331
64054
MA = 331
67084
Ha = 224
896 n
mi
Hp = 222
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10554280
96 X = -3276597
65
Y = 19250690
60 feet Y = 5831303
12 meter
Z = -3863791
27 Z = -1193456
08
XDOT = -12358
676429 XDOT = -3702
100628
YDOT = -10624
096494 feet/sec YDOT = -3279
985969 meter/sec
ZDOT = -19135
642902 ZDOT = -5850
686402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18835385
16 X = -5741025
40
Y = 11255724
59 feet Y = 3430744
85 meter
Z = -3930362
33 Z = -1197974
44
XDOT = -4343
912131 XDOT = -1324
024417
YDOT = -13990
468796 feet/sec YDOT = -4264
294889 meter/sec
ZDOT = -19210
820254 ZDOT = -5855
458013
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 13131
31081843
00016717 00000-0 10270-3 0 9127
2 25544 51
6488 291
1889 0009808 288
1927 71
8156 15
51017549 28987
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
31081843 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 291
1889 deg
Eccentricity:
0009808
Arg of perigee: 288
1927 deg
Mean anomaly: 71
8156 deg
Mean motion: 15
51017549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 338
Coasting Arc #14 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2013/132/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3142158
57 A = 6796757
63 meter
Y = -5728284
83 meter E =
0010143
Z = 1848201
63 I = 51
32401
XDOT = 3601
782417 Wp = 20
97913
YDOT = 3785
530677 meter/sec RA = 285
65891 deg
ZDOT = 5609
073424 TA = 359
42655
MA = 359
42772
Ha = 225
073 n
mi
Hp = 222
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10308919
21 X = 3197001
74
Y = -18793585
41 feet Y = -5692840
71 meter
Z = 6063653
63 Z = 1863599
05
XDOT = 11816
871446 XDOT = 3531
936297
YDOT = 12419
720069 feet/sec YDOT = 3825
417186 meter/sec
ZDOT = 18402
471862 ZDOT = 5626
401435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18188562
54 X = 5543873
86
Y = -11307366
14 feet Y = -3446485
20 meter
Z = 6128639
86 Z = 1868009
43
XDOT = 3252
468279 XDOT = 991
352331
YDOT = 15245
373366 feet/sec YDOT = 4646
789802 meter/sec
ZDOT = 18474
183018 ZDOT = 5630
930984
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 13132
34168841
00016717 00000-0 10270-3 0 9136
2 25544 51
6486 286
0729 0009924 293
4530 66
5577 15
51071432 29147
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
34168841 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 286
0729 deg
Eccentricity:
0009924
Arg of perigee: 293
4530 deg
Mean anomaly: 66
5577 deg
Mean motion: 15
51071432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 317
Coasting Arc #15 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2013/133/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3069233
69 A = 6795596
06 meter
Y = 5528118
79 meter E =
0005030
Z = -2487227
11 I = 51
31246
XDOT = -3488
284863 Wp = 281
05686
YDOT = -4316
563316 meter/sec RA = 280
67828 deg
ZDOT = -5279
400826 TA = 286
91036
MA = 286
96550
Ha = 225
345 n
mi
Hp = 222
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10069664
35 X = -3118739
75
Y = 18136872
67 feet Y = 5493520
05 meter
Z = -8160193
94 Z = -2502257
25
XDOT = -11444
504144 XDOT = -3414
110616
YDOT = -14161
953137 feet/sec YDOT = -4355
156422 meter/sec
ZDOT = -17320
868852 ZDOT = -5296
166960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17456393
81 X = -5320708
83
Y = 11161517
21 feet Y = 3402030
44 meter
Z = -8223618
70 Z = -2506558
98
XDOT = -2395
193346 XDOT = -730
054932
YDOT = -16582
974216 feet/sec YDOT = -5054
490541 meter/sec
ZDOT = -17390
171256 ZDOT = -5300
524199
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 13133
30811887
00016717 00000-0 10270-3 0 9149
2 25544 51
6483 281
2782 0009998 296
3242 63
6882 15
51064941 29293
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
30811887 = yrday
fracday
Element set: 914
Inclination: 51
6483 deg
RA of node: 281
2782 deg
Eccentricity:
0009998
Arg of perigee: 296
3242 deg
Mean anomaly: 63
6882 deg
Mean motion: 15
51064941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 336
Coasting Arc #16 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2013/134/06:44:32
337
Vector Time (MET): N/A
Weight (LBS) : 904584
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3011822
66 A = 6794065
34 meter
Y = -5239837
60 meter E =
0007671
Z = 3092182
76 I = 51
30253
XDOT = 3428
715725 Wp = 33
81998
YDOT = 4837
488052 meter/sec RA = 275
69408 deg
ZDOT = 4858
147469 TA = 1
88452
MA = 1
88163
Ha = 225
498 n
mi
Hp = 221
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9881307
95 X = 3055170
66
Y = -17191068
23 feet Y = -5205915
33 meter
Z = 10144956
58 Z = 3106919
03
XDOT = 11249
067340 XDOT = 3350
767239
YDOT = 15871
023792 feet/sec YDOT = 4875
393951 meter/sec
ZDOT = 15938
804033 ZDOT = 4874
615035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16647047
00 X = 5074019
93
Y = -10713724
15 feet Y = -3265543
12 meter
Z = 10207113
15 Z = 3111128
09
XDOT = 1779
569634 XDOT = 542
412825
YDOT = 18013
686700 feet/sec YDOT = 5490
571706 meter/sec
ZDOT = 16006
799263 ZDOT = 4878
872415
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 13134
33896607
00016717 00000-0 10270-3 0 9157
2 25544 51
6479 276
1620 0010076 301
3221 58
6944 15
51096758 29457
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
33896607 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 276
1620 deg
Eccentricity:
0010076
Arg of perigee: 301
3221 deg
Mean anomaly: 58
6944 deg
Mean motion: 15
51096758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2945
Checksum: 318
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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