[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 22nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
There are no maneuvers
Coasting Arc #1 (Orbit 2124)
---------------------------------------
Vector Time (GMT): 2013/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5001447
03 A = 6789950
89 meter
Y = -2971318
92 meter E =
0023025
Z = 3488185
91 I = 51
65863
XDOT = 5186
552792 Wp = 74
84114
YDOT = 3371
377170 meter/sec RA = 177
59577 deg
ZDOT = -4533
905981 TA = 64
18987
MA = 63
95252
Ha = 228
188 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16408946
95 X = 5017356
72
Y = -9748421
65 feet Y = -2915300
26 meter
Z = 11444179
50 Z = 3512521
22
XDOT = 17016
249317 XDOT = 5170
492145
YDOT = 11060
948721 feet/sec YDOT = 3429
286190 meter/sec
ZDOT = -14875
019622 ZDOT = -4508
749775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16448971
28 X = 5013646
45
Y = -9559242
81 feet Y = -2913657
21 meter
Z = 11545853
36 Z = 3519176
10
XDOT = 16282
392766 XDOT = 4962
873315
YDOT = 10056
272710 feet/sec YDOT = 3065
151922 meter/sec
ZDOT = -14770
559376 ZDOT = -4502
066498
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 13081
53968030
00016717 00000-0 10270-3 0 9004
2 25544 51
6462 178
5133 0011563 60
0936 300
1363 15
52114902 21250
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
53968030 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 178
5133 deg
Eccentricity:
0011563
Arg of perigee: 60
0936 deg
Mean anomaly: 300
1363 deg
Mean motion: 15
52114902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2125
Checksum: 268
Coasting Arc #2 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2013/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5564580
20 A = 6792052
77 meter
Y = 2841243
59 meter E =
0016364
Z = -2663946
84 I = 51
69687
XDOT = -4314
240952 Wp = 60
80961
YDOT = -3592
839524 meter/sec RA = 172
63125 deg
ZDOT = 5211
794739 TA = 269
20421
MA = 269
39170
Ha = 228
171 n
mi
Hp = 213
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18256496
72 X = -5582997
40
Y = 9321665
32 feet Y = 2778913
65 meter
Z = -8739983
08 Z = -2691023
91
XDOT = -14154
333832 XDOT = -4299
061675
YDOT = -11787
531246 feet/sec YDOT = -3640
998576 meter/sec
ZDOT = 17099
064105 ZDOT = 5190
874042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18148704
20 X = -5531725
04
Y = 9424861
24 feet Y = 2872697
71 meter
Z = -8853075
59 Z = -2698417
44
XDOT = -13639
348597 XDOT = -4157
273452
YDOT = -10381
275014 feet/sec YDOT = -3164
212624 meter/sec
ZDOT = 17012
260688 ZDOT = 5185
337058
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 13082
50544742
00016717 00000-0 10270-3 0 9013
2 25544 51
6467 173
7140 0011491 62
2697 297
9619 15
52131929 21400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
50544742 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 173
7140 deg
Eccentricity:
0011491
Arg of perigee: 62
2697 deg
Mean anomaly: 297
9619 deg
Mean motion: 15
52131929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 307
Coasting Arc #3 (Orbit 2155)
---------------------------------------
Vector Time (GMT): 2013/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6027590
02 A = 6793799
28 meter
Y = -2649617
65 meter E =
0023255
Z = 1650032
23 I = 51
73281
XDOT = 3297
476222 Wp = 93
95764
YDOT = 3897
392583 meter/sec RA = 167
67200 deg
ZDOT = -5719
357624 TA = 68
00651
MA = 67
75958
Ha = 228
218 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19775557
82 X = 6048755
28
Y = -8692971
29 feet Y = -2582094
77 meter
Z = 5413491
58 Z = 1679365
29
XDOT = 10818
491541 XDOT = 3281
432568
YDOT = 12786
721072 feet/sec YDOT = 3934
176542 meter/sec
ZDOT = -18764
296667 ZDOT = -5703
378406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19537443
47 X = 5955012
77
Y = -9142626
76 feet Y = -2786672
64 meter
Z = 5535973
88 Z = 1687364
84
XDOT = 10557
404118 XDOT = 3217
896775
YDOT = 11106
843435 feet/sec YDOT = 3385
365879 meter/sec
ZDOT = -18698
104551 ZDOT = -5699
182267
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 13083
53558021
00016717 00000-0 10270-3 0 9023
2 25544 51
6462 168
5939 0011641 66
6422 293
5953 15
52180314 21566
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
53558021 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 168
5939 deg
Eccentricity:
0011641
Arg of perigee: 66
6422 deg
Mean anomaly: 293
5953 deg
Mean motion: 15
52180314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2156
Checksum: 303
Coasting Arc #4 (Orbit 2170)
---------------------------------------
Vector Time (GMT): 2013/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285485
10 A = 6794807
16 meter
Y = 2482441
59 meter E =
0021586
Z = -638395
76 I = 51
76620
XDOT = -2262
401882 Wp = 55
72481
YDOT = -4230
579062 meter/sec RA = 162
71688 deg
ZDOT = 5980
248116 TA = 297
39865
MA = 297
61810
Ha = 228
236 n
mi
Hp = 213
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20621670
27 X = -6309676
00
Y = 8144493
42 feet Y = 2412017
99 meter
Z = -2094474
28 Z = -668989
09
XDOT = -7422
578353 XDOT = -2243
976819
YDOT = -13879
852566 feet/sec YDOT = -4255
774745 meter/sec
ZDOT = 19620
236602 ZDOT = 5969
303005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20265146
18 X = -6176816
56
Y = 8964293
34 feet Y = 2732316
61 meter
Z = -2222200
59 Z = -677326
74
XDOT = -7440
304608 XDOT = -2267
804845
YDOT = -12087
027367 feet/sec YDOT = -3684
125942 meter/sec
ZDOT = 19575
049705 ZDOT = 5966
475150
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 13084
50130966
00016717 00000-0 10270-3 0 9036
2 25544 51
6465 163
7943 0011672 68
7769 291
4629 15
52178633 21717
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
50130966 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 163
7943 deg
Eccentricity:
0011672
Arg of perigee: 68
7769 deg
Mean anomaly: 291
4629 deg
Mean motion: 15
52178633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2171
Checksum: 327
Coasting Arc #5 (Orbit 2186)
---------------------------------------
Vector Time (GMT): 2013/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6407173
42 A = 6794719
58 meter
Y = -2200879
44 meter E =
0019288
Z = -492093
65 I = 51
79454
XDOT = 1145
397289 Wp = 104
98345
YDOT = 4630
158271 meter/sec RA = 157
76481 deg
ZDOT = -5995
959886 TA = 80
30645
MA = 80
08864
Ha = 228
237 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21020910
16 X = 6433698
38
Y = -7220733
07 feet Y = -2129082
16 meter
Z = -1614480
49 Z = -460903
40
XDOT = 3757
865123 XDOT = 1122
663517
YDOT = 15190
807975 feet/sec YDOT = 4642
838791 meter/sec
ZDOT = -19671
784402 ZDOT = -5990
451577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20582271
13 X = 6273476
24
Y = -8413751
19 feet Y = -2564511
36 meter
Z = -1484285
43 Z = -452410
20
XDOT = 4129
378316 XDOT = 1258
634511
YDOT = 13441
383355 feet/sec YDOT = 4096
933647 meter/sec
ZDOT = -19649
292594 ZDOT = -5989
104383
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 13085
53140227
00016717 00000-0 10270-3 0 9042
2 25544 51
6456 158
6739 0011741 73
1099 287
1339 15
52244446 21879
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
53140227 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 158
6739 deg
Eccentricity:
0011741
Arg of perigee: 73
1099 deg
Mean anomaly: 287
1339 deg
Mean motion: 15
52244446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2187
Checksum: 315
Coasting Arc #6 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2013/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6329747
41 A = 6793845
57 meter
Y = 1898242
32 meter E =
0025490
Z = 1530402
23 I = 51
81954
XDOT = -102
459388 Wp = 68
66315
YDOT = -5051
173262 meter/sec RA = 152
81344 deg
ZDOT = 5773
298274 TA = 308
01656
MA = 308
24641
Ha = 228
269 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20766887
82 X = -6357937
84
Y = 6227829
14 feet Y = 1827301
70 meter
Z = 5021004
68 Z = 1499583
97
XDOT = -336
152848 XDOT = -74
013751
YDOT = -16572
090756 feet/sec YDOT = -5052
159131 meter/sec
ZDOT = 18941
267303 ZDOT = 5772
870369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20276044
81 X = -6180138
46
Y = 7759290
83 feet Y = 2365031
85 meter
Z = 4892380
40 Z = 1491197
55
XDOT = -1119
625546 XDOT = -341
261867
YDOT = -15012
497966 feet/sec YDOT = -4575
809380 meter/sec
ZDOT = 18939
993045 ZDOT = 5772
909880
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 13086
56147409
00016717 00000-0 10270-3 0 9056
2 25544 51
6455 153
5537 0011818 76
1811 284
0655 15
52256180 22032
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
56147409 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 153
5537 deg
Eccentricity:
0011818
Arg of perigee: 76
1811 deg
Mean anomaly: 284
0655 deg
Mean motion: 15
52256180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 302
Coasting Arc #7 (Orbit 2217)
---------------------------------------
Vector Time (GMT): 2013/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6116141
80 A = 6791867
43 meter
Y = -1437466
85 meter E =
0015755
Z = -2591524
97 I = 51
83953
XDOT = -933
262612 Wp = 94
53856
YDOT = 5475
639410 meter/sec RA = 147
86110 deg
ZDOT = -5268
587382 TA = 114
47120
MA = 114
30680
Ha = 228
227 n
mi
Hp = 213
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20066082
01 X = 6144350
34
Y = -4716098
59 feet Y = -1368914
92 meter
Z = -8502378
50 Z = -2561744
32
XDOT = -3061
885209 XDOT = -968
829406
YDOT = 17964
696226 feet/sec YDOT = 5465
003523 meter/sec
ZDOT = -17285
391672 ZDOT = -5273
208238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19601555
03 X = 5974553
97
Y = -6539564
66 feet Y = -1993259
31 meter
Z = -8378114
80 Z = -2553649
39
XDOT = -1774
307014 XDOT = -540
808778
YDOT = 16729
283205 feet/sec YDOT = 5099
085521 meter/sec
ZDOT = -17305
209286 ZDOT = -5274
627790
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 13087
52714709
00016717 00000-0 10270-3 0 9067
2 25544 51
6448 148
7526 0011874 79
7244 280
5246 15
52306438 22184
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
52714709 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 148
7526 deg
Eccentricity:
0011874
Arg of perigee: 79
7244 deg
Mean anomaly: 280
5246 deg
Mean motion: 15
52306438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2218
Checksum: 325
Coasting Arc #8 (Orbit 2233)
---------------------------------------
Vector Time (GMT): 2013/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5745822
49 A = 6789530
01 meter
Y = 922891
15 meter E =
0024204
Z = 3475320
91 I = 51
85694
XDOT = 1834
608679 Wp = 87
22253
YDOT = -5886
603979 meter/sec RA = 142
90695 deg
ZDOT = 4570
166546 TA = 313
46435
MA = 313
66540
Ha = 228
274 n
mi
Hp = 213
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18851123
64 X = -5772597
77
Y = 3027858
10 feet Y = 858488
41 meter
Z = 11401971
48 Z = 3447342
77
XDOT = 6019
057347 XDOT = 1878
096702
YDOT = -19313
005179 feet/sec YDOT = -5865
844574 meter/sec
ZDOT = 14993
984732 ZDOT = 4579
185286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18479716
74 X = -5632617
66
Y = 5067609
41 feet Y = 1544607
35 meter
Z = 11285262
30 Z = 3439747
95
XDOT = 4161
473297 XDOT = 1268
417061
YDOT = -18494
196434 feet/sec YDOT = -5637
031073 meter/sec
ZDOT = 15032
186229 ZDOT = 4581
810363
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 13088
55717823
00016717 00000-0 10270-3 0 9072
2 25544 51
6443 143
6319 0011912 83
2649 276
9858 15
52337232 22347
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
55717823 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 143
6319 deg
Eccentricity:
0011912
Arg of perigee: 83
2649 deg
Mean anomaly: 276
9858 deg
Mean motion: 15
52337232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2234
Checksum: 323
Coasting Arc #9 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2013/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5278407
90 A = 6786881
48 meter
Y = -238746
54 meter E =
0019860
Z = -4278570
69 I = 51
87238
XDOT = -2640
835774 Wp = 80
19068
YDOT = 6203
284695 meter/sec RA = 137
94891 deg
ZDOT = -3615
108712 TA = 152
93885
MA = 152
83518
Ha = 228
181 n
mi
Hp = 213
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17317611
23 X = 5301469
69
Y = -783289
17 feet Y = -179591
48 meter
Z = -14037305
41 Z = -4252872
34
XDOT = -8664
159364 XDOT = -2692
444536
YDOT = 20351
983909 feet/sec YDOT = 6173
464336 meter/sec
ZDOT = -11860
592886 ZDOT = -3628
063686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17166967
22 X = 5232491
61
Y = -2967328
21 feet Y = -904441
64 meter
Z = -13930159
50 Z = -4245912
62
XDOT = -6178
941741 XDOT = -1883
341443
YDOT = 20018
314452 feet/sec YDOT = 6101
582245 meter/sec
ZDOT = -11915
249935 ZDOT = -3631
768180
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 13089
52281498
00016717 00000-0 10270-3 0 9085
2 25544 51
6445 138
8302 0011963 86
6251 273
6269 15
52357354 22492
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
52281498 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 138
8302 deg
Eccentricity:
0011963
Arg of perigee: 86
6251 deg
Mean anomaly: 273
6269 deg
Mean motion: 15
52357354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 331
Coasting Arc #10 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2013/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4716785
97 A = 6784528
69 meter
Y = -503936
67 meter E =
0018716
Z = 4836161
73 I = 51
88650
XDOT = 3298
416278 Wp = 101
17262
YDOT = -6452
517039 meter/sec RA = 132
98888 deg
ZDOT = 2532
814688 TA = 323
97077
MA = 324
09678
Ha = 228
259 n
mi
Hp = 212
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15475019
60 X = -4734293
26
Y = -1653335
55 feet Y = -556780
32 meter
Z = 15866672
34 Z = 4813205
31
XDOT = 10821
575714 XDOT = 3358
020716
YDOT = -21169
675326 feet/sec YDOT = -6415
298640 meter/sec
ZDOT = 8309
759474 ZDOT = 2548
983437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15648921
77 X = -4769791
35
Y = 589100
25 feet Y = 179557
76 meter
Z = 15771025
63 Z = 4807008
61
XDOT = 7678
857540 XDOT = 2340
515778
YDOT = -21349
267024 feet/sec YDOT = -6507
256589 meter/sec
ZDOT = 8377
857849 ZDOT = 2553
571072
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 13090
55280629
00016717 00000-0 10270-3 0 9096
2 25544 51
6439 133
7092 0012021 90
0213 270
2316 15
52404741 22655
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
55280629 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 133
7092 deg
Eccentricity:
0012021
Arg of perigee: 90
0213 deg
Mean anomaly: 270
2316 deg
Mean motion: 15
52404741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 275
Coasting Arc #11 (Orbit 2279)
---------------------------------------
Vector Time (GMT): 2013/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4124331
50 A = 6782950
49 meter
Y = 1379581
01 meter E =
0025772
Z = -5227783
28 I = 51
90259
XDOT = -3804
936446 Wp = 86
42341
YDOT = 6505
986661 meter/sec RA = 128
02554 deg
ZDOT = -1288
837647 TA = 171
23140
MA = 171
18630
Ha = 228
096 n
mi
Hp = 213
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13531271
33 X = 4133993
49
Y = 4526184
43 feet Y = 1425755
64 meter
Z = -17151519
96 Z = -5207724
15
XDOT = -12483
387290 XDOT = -3871
144130
YDOT = 21345
100595 feet/sec YDOT = 6463
067211 meter/sec
ZDOT = -4228
469970 ZDOT = -1307
482936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14184772
43 X = 4323518
64
Y = 2287042
88 feet Y = 697090
67 meter
Z = -17068038
91 Z = -5202338
26
XDOT = -8718
309658 XDOT = -2657
340784
YDOT = 22027
156228 feet/sec YDOT = 6713
877218 meter/sec
ZDOT = -4306
917541 ZDOT = -1312
748467
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 13091
51840612
00016717 00000-0 10270-3 0 9109
2 25544 51
6451 128
9075 0011983 93
4132 266
8391 15
52407150 22807
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
51840612 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 128
9075 deg
Eccentricity:
0011983
Arg of perigee: 93
4132 deg
Mean anomaly: 266
8391 deg
Mean motion: 15
52407150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2280
Checksum: 290
Coasting Arc #12 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2013/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3498271
45 A = 6782180
54 meter
Y = -2282692
43 meter E =
0014503
Z = 5330737
35 I = 51
91787
XDOT = 4191
637183 Wp = 95
91356
YDOT = -6432
085783 meter/sec RA = 123
06204 deg
ZDOT = -5
007843 TA = 354
12543
MA = 354
14242
Ha = 228
179 n
mi
Hp = 212
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11477268
55 X = -3498381
20
Y = -7489148
39 feet Y = -2321812
64 meter
Z = 17489295
76 Z = 5313742
90
XDOT = 13752
090496 XDOT = 4263
274936
YDOT = -21102
643645 feet/sec YDOT = -6384
811708 meter/sec
ZDOT = -16
429931 ZDOT = 15
529103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12726309
40 X = -3878979
11
Y = -5321739
97 feet Y = -1622066
34 meter
Z = 17418686
40 Z = 5309215
61
XDOT = 9416
293776 XDOT = 2870
086343
YDOT = -22273
522588 feet/sec YDOT = -6788
969685 meter/sec
ZDOT = 69
914490 ZDOT = 21
309936
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 13092
54835829
00016717 00000-0 10270-3 0 9118
2 25544 51
6441 123
7862 0012109 96
7545 263
4985 15
52465740 22966
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
54835829 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 123
7862 deg
Eccentricity:
0012109
Arg of perigee: 96
7545 deg
Mean anomaly: 263
4985 deg
Mean motion: 15
52465740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 328
Coasting Arc #13 (Orbit 2310)
---------------------------------------
Vector Time (GMT): 2013/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2911190
03 A = 6782764
02 meter
Y = 3235057
39 meter E =
0025993
Z = -5225372
79 I = 51
93699
XDOT = -4421
622803 Wp = 100
14213
YDOT = 6098
137849 meter/sec RA = 118
09926 deg
ZDOT = 1313
099601 TA = 182
45029
MA = 182
46305
Ha = 227
993 n
mi
Hp = 213
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9551148
39 X = 2900181
93
Y = 10613705
35 feet Y = 3267550
28 meter
Z = -17143611
51 Z = -5211257
47
XDOT = -14506
636494 XDOT = -4495
863524
YDOT = 20007
013939 feet/sec YDOT = 6048
277456 meter/sec
ZDOT = 4308
069556 ZDOT = 1291
439114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11529519
80 X = 3514197
63
Y = 8540946
17 feet Y = 2603280
39 meter
Z = -17085110
61 Z = -5207541
71
XDOT = -9759
384056 XDOT = -2974
660260
YDOT = 21602
714070 feet/sec YDOT = 6584
507249 meter/sec
ZDOT = 4217
061598 ZDOT = 1285
360375
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 13093
51392079
00016717 00000-0 10270-3 0 9122
2 25544 51
6455 118
9849 0011993 100
0788 260
1717 15
52463685 23111
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
51392079 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 118
9849 deg
Eccentricity:
0011993
Arg of perigee: 100
0788 deg
Mean anomaly: 260
1717 deg
Mean motion: 15
52463685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2311
Checksum: 317
Coasting Arc #14 (Orbit 2326)
---------------------------------------
Vector Time (GMT): 2013/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2328630
43 A = 6784151
41 meter
Y = -4149823
24 meter E =
0018140
Z = 4820085
55 I = 51
95459
XDOT = 4587
485255 Wp = 87
76925
YDOT = -5587
209920 meter/sec RA = 113
13880 deg
ZDOT = -2584
966151 TA = 27
59007
MA = 27
49391
Ha = 227
997 n
mi
Hp = 212
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7639863
63 X = -2305467
72
Y = -13614905
63 feet Y = -4175733
55 meter
Z = 15813928
95 Z = 4808829
92
XDOT = 15050
804641 XDOT = 4662
178686
YDOT = -18330
741208 feet/sec YDOT = -5535
492342 meter/sec
ZDOT = -8480
860077 ZDOT = -2562
498797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10430234
07 X = -3179135
34
Y = -11679515
20 feet Y = -3559916
23 meter
Z = 15767455
80 Z = 4805920
53
XDOT = 10052
930255 XDOT = 3064
133142
YDOT = -20339
729595 feet/sec YDOT = -6199
549581 meter/sec
ZDOT = -8386
531664 ZDOT = -2556
214851
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 13094
54383327
00016717 00000-0 10270-3 0 9133
2 25544 51
6441 113
8629 0012091 103
5535 256
6965 15
52534076 23279
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
54383327 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 113
8629 deg
Eccentricity:
0012091
Arg of perigee: 103
5535 deg
Mean anomaly: 256
6965 deg
Mean motion: 15
52534076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2327
Checksum: 306
Coasting Arc #15 (Orbit 2341)
---------------------------------------
Vector Time (GMT): 2013/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1832672
29 A = 6786503
30 meter
Y = 5003554
66 meter E =
0019947
Z = -4223190
10 I = 51
97423
XDOT = -4637
076789 Wp = 108
11732
YDOT = 4822
157260 meter/sec RA = 108
18363 deg
ZDOT = 3709
271152 TA = 199
83721
MA = 199
91489
Ha = 227
877 n
mi
Hp = 212
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6012704
37 X = 1797100
29
Y = 16415861
74 feet Y = 5023849
44 meter
Z = -13855610
57 Z = -4214374
08
XDOT = -15213
506527 XDOT = -4708
673103
YDOT = 15820
725919 feet/sec YDOT = 4769
902596 meter/sec
ZDOT = 12169
524776 ZDOT = 3686
570371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9670092
73 X = 2947444
26
Y = 14598776
45 feet Y = 4449707
06 meter
Z = -13819410
52 Z = -4212156
33
XDOT = -10226
647337 XDOT = -3117
082108
YDOT = 18177
732950 feet/sec YDOT = 5540
573003 meter/sec
ZDOT = 12074
299074 ZDOT = 3680
246358
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 13095
50935830
00016717 00000-0 10270-3 0 9143
2 25544 51
6448 109
0618 0012032 106
7854 253
4619 15
52528696 23424
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
50935830 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 109
0618 deg
Eccentricity:
0012032
Arg of perigee: 106
7854 deg
Mean anomaly: 253
4619 deg
Mean motion: 15
52528696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2342
Checksum: 311
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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