[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 8th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
133/23:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
8
000/00:00:00
000 0
0 0
0 221
0
137/02:03:18
747 -2
8 4
8 4
9
N/A -3
4 -0
5 225
4
000/00:14:33
493 -2
1 0
2 223
3
Coasting Arc #1 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2013/128/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4343
39 A = 6792037
25 meter
Y = -5550515
84 meter E =
0001648
Z = -3916446
96 I = 51
35344
XDOT = 5852
111215 Wp = 123
83363
YDOT = -2851
923166 meter/sec RA = 304
30280 deg
ZDOT = 4035
675060 TA = 188
58965
MA = 188
59247
Ha = 224
244 n
mi
Hp = 221
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14249
97 X = 76749
43
Y = -18210353
82 feet Y = -5550110
97 meter
Z = -12849235
43 Z = -3916271
13
XDOT = 19199
839944 XDOT = 5863
962463
YDOT = -9356
703302 feet/sec YDOT = -2786
414938 meter/sec
ZDOT = 13240
403739 ZDOT = 4064
133442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15252400
85 X = -4648931
78
Y = -9950898
51 feet Y = -3033033
87 meter
Z = -12847720
71 Z = -3915985
27
XDOT = 1809
344280 XDOT = 551
488137
YDOT = -20020
439586 feet/sec YDOT = -6102
229986 meter/sec
ZDOT = 13359
435981 ZDOT = 4071
956087
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
54010618
00016717 00000-0 10270-3 0 9007
2 25544 51
6454 304
9365 0004982 280
1506 79
9083 15
50974883 28558
Satellite: ISS
Catalog Number: 25544
Epoch time: 13128
54010618 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 304
9365 deg
Eccentricity:
0004982
Arg of perigee: 280
1506 deg
Mean anomaly: 79
9083 deg
Mean motion: 15
50974883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 319
Coasting Arc #2 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2013/129/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -150252
12 A = 6793561
43 meter
Y = 5862193
19 meter E =
0007581
Z = 3424785
12 I = 51
34147
XDOT = -5609
984911 Wp = 80
16640
YDOT = 2529
519372 meter/sec RA = 299
32075 deg
ZDOT = -4565
958419 TA = 59
60582
MA = 59
53091
Ha = 224
345 n
mi
Hp = 221
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -492953
14 X = -232430
28
Y = 19232917
30 feet Y = 5860053
41 meter
Z = 11236171
65 Z = 3423855
73
XDOT = -18405
462307 XDOT = -5615
672932
YDOT = 8298
948070 feet/sec YDOT = 2466
753301 meter/sec
ZDOT = -14980
178540 ZDOT = -4593
225546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16026070
15 X = 4884746
18
Y = 10649823
75 feet Y = 3246066
28 meter
Z = 11231473
36 Z = 3423353
08
XDOT = -1866
495603 XDOT = -568
907860
YDOT = 18761
703251 feet/sec YDOT = 5718
567151 meter/sec
ZDOT = -15094
198505 ZDOT = -4600
711704
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
57102723
00016717 00000-0 10270-3 0 9011
2 25544 51
6448 299
8213 0005059 284
2801 75
7788 15
50975455 28714
Satellite: ISS
Catalog Number: 25544
Epoch time: 13129
57102723 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 299
8213 deg
Eccentricity:
0005059
Arg of perigee: 284
2801 deg
Mean anomaly: 75
7788 deg
Mean motion: 15
50975455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 329
Coasting Arc #3 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2013/130/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 243686
47 A = 6794882
85 meter
Y = -6143786
46 meter E =
0003636
Z = -2886889
67 I = 51
33360
XDOT = 5377
450801 Wp = 350
45381
YDOT = -2143
758034 meter/sec RA = 294
33918 deg
ZDOT = 5018
801645 TA = 336
56791
MA = 336
58448
Ha = 224
403 n
mi
Hp = 221
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 799496
30 X = 326393
51
Y = -20156779
71 feet Y = -6140598
83 meter
Z = -9471422
79 Z = -2885505
21
XDOT = 17642
555122 XDOT = 5376
642623
YDOT = -7033
326883 feet/sec YDOT = -2083
628726 meter/sec
ZDOT = 16465
884663 ZDOT = 5044
923292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16847118
14 X = -5135001
61
Y = -11101133
77 feet Y = -3383625
57 meter
Z = -9464790
10 Z = -2884868
02
XDOT = 2178
928046 XDOT = 664
137268
YDOT = -17431
309320 feet/sec YDOT = -5313
063081 meter/sec
ZDOT = 16575
076030 ZDOT = 5052
083174
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
53750359
00016717 00000-0 10270-3 0 9024
2 25544 51
6463 295
0259 0004980 288
1498 71
9111 15
51013164 28861
Satellite: ISS
Catalog Number: 25544
Epoch time: 13130
53750359 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 295
0259 deg
Eccentricity:
0004980
Arg of perigee: 288
1498 deg
Mean anomaly: 71
9111 deg
Mean motion: 15
51013164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 309
Coasting Arc #4 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2013/131/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -310682
30 A = 6796185
23 meter
Y = 6390537
16 meter E =
0008777
Z = 2280278
63 I = 51
32569
XDOT = -5171
139082 Wp = 105
30504
YDOT = 1680
607916 meter/sec RA = 289
35818 deg
ZDOT = -5399
337675 TA = 49
22656
MA = 49
15043
Ha = 224
537 n
mi
Hp = 221
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1019298
88 X = -393196
75
Y = 20966329
28 feet Y = 6386601
42 meter
Z = 7481229
11 Z = 2278569
27
XDOT = -16965
679402 XDOT = -5163
318665
YDOT = 5513
805498 feet/sec YDOT = 1622
825015 meter/sec
ZDOT = -17714
362451 ZDOT = -5424
439974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17633203
03 X = 5374600
28
Y = 11393682
19 feet Y = 3472794
33 meter
Z = 7473210
78 Z = 2277834
65
XDOT = -2810
876975 XDOT = -856
755302
YDOT = 16070
649124 feet/sec YDOT = 4898
333853 meter/sec
ZDOT = -17819
241624 ZDOT = -5431
304847
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
56839871
00016717 00000-0 10270-3 0 9036
2 25544 51
6457 289
9106 0005066 292
2229 67
8384 15
51021630 29023
Satellite: ISS
Catalog Number: 25544
Epoch time: 13131
56839871 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 289
9106 deg
Eccentricity:
0005066
Arg of perigee: 292
2229 deg
Mean anomaly: 67
8384 deg
Mean motion: 15
51021630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 313
Coasting Arc #5 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2013/132/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 326505
14 A = 6797150
54 meter
Y = -6581105
16 meter E =
0008449
Z = -1646330
60 I = 51
32162
XDOT = 5001
018367 Wp = 1
99717
YDOT = -1172
445688 meter/sec RA = 284
37811 deg
ZDOT = 5687
763223 TA = 339
91312
MA = 339
94635
Ha = 224
626 n
mi
Hp = 221
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1071211
10 X = 408069
76
Y = -21591552
35 feet Y = -6576997
81 meter
Z = -5401347
10 Z = -1644546
75
XDOT = 16407
540575 XDOT = 4986
127169
YDOT = -3846
606588 feet/sec YDOT = -1116
604785 meter/sec
ZDOT = 18660
640494 ZDOT = 5712
021856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18354492
22 X = -5594449
23
Y = -11425645
73 feet Y = -3482536
82 meter
Z = -5392996
53 Z = -1643785
34
XDOT = 3694
856139 XDOT = 1126
192151
YDOT = -14777
091121 feet/sec YDOT = -4504
057374 meter/sec
ZDOT = 18761
934811 ZDOT = 5718
637730
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
53485075
00016717 00000-0 10270-3 0 9048
2 25544 51
6474 285
1156 0005044 296
6788 63
3846 15
51049609 29175
Satellite: ISS
Catalog Number: 25544
Epoch time: 13132
53485075 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 285
1156 deg
Eccentricity:
0005044
Arg of perigee: 296
6788 deg
Mean anomaly: 63
3846 deg
Mean motion: 15
51049609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 327
Coasting Arc #6 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2013/133/12:45:32
930
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -332693
99 A = 6797837
97 meter
Y = 6717232
38 meter E =
0008371
Z = 960049
00 I = 51
31694
XDOT = -4873
318050 Wp = 127
02503
YDOT = 603
657055 meter/sec RA = 279
39834 deg
ZDOT = -5881
765168 TA = 42
54514
MA = 42
48031
Ha = 224
766 n
mi
Hp = 221
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1091515
71 X = -412446
52
Y = 22038163
97 feet Y = 6713066
00 meter
Z = 3149767
05 Z = 958239
52
XDOT = -15988
576279 XDOT = -4851
133683
YDOT = 1980
502150 feet/sec YDOT = 549
284986 meter/sec
ZDOT = -19297
129816 ZDOT = -5905
385690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18939539
71 X = 5772771
70
Y = 11323391
57 feet Y = 3451369
75 meter
Z = 3141297
34 Z = 957467
43
XDOT = -4873
872426 XDOT = -1485
556316
YDOT = 13560
731845 feet/sec YDOT = 4133
311066 meter/sec
ZDOT = -19395
689065 ZDOT = -5911
806027
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
56571981
00016717 00000-0 10270-3 0 9055
2 25544 51
6469 280
0005 0005130 300
7536 59
3110 15
51072919 29337
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
56571981 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 280
0005 deg
Eccentricity:
0005130
Arg of perigee: 300
7536 deg
Mean anomaly: 59
3110 deg
Mean motion: 15
51072919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 286
Coasting Arc #7 (Orbit 2939)
---------------------------------------
Vector Time (GMT): 2013/133/23:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4176436
27 A = 6788360
85 meter
Y = -2379491
05 meter E =
0001998
Z = 4791871
80 I = 51
28232
XDOT = 1145
378084 Wp = 99
12074
YDOT = 7137
859129 meter/sec RA = 277
27609 deg
ZDOT = 2544
937629 TA = 325
68475
MA = 325
69766
Ha = 224
836 n
mi
Hp = 221
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13702218
73 X = 4179455
96
Y = -7806729
17 feet Y = -2332770
95 meter
Z = 15721364
18 Z = 4812167
97
XDOT = 3757
802114 XDOT = 1053
113118
YDOT = 23418
172994 feet/sec YDOT = 7150
151412 meter/sec
ZDOT = 8349
532904 ZDOT = 2550
278216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5902325
66 X = -1799028
86
Y = 14532042
00 feet Y = 4429366
40 meter
Z = 15806309
42 Z = 4817763
11
XDOT = -16293
151814 XDOT = -4966
152673
YDOT = -15726
784908 feet/sec YDOT = -4793
524040 meter/sec
ZDOT = 8370
818700 ZDOT = 2551
425540
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
01672014
00016717 00000-0 10270-3 0 9066
2 25544 51
6457 277
7669 0005449 306
7229 53
3421 15
51090803 29400
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
01672014 = yrday
fracday
Element set: 906
Inclination: 51
6457 deg
RA of node: 277
7669 deg
Eccentricity:
0005449
Arg of perigee: 306
7229 deg
Mean anomaly: 53
3421 deg
Mean motion: 15
51090803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2940
Checksum: 300
Coasting Arc #8 (Orbit 2954)
---------------------------------------
Vector Time (GMT): 2013/134/23:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4130584
28 A = 6787301
88 meter
Y = 1887772
94 meter E =
0010995
Z = -5053454
23 I = 51
27596
XDOT = -1151
822711 Wp = 52
62043
YDOT = -7350
969809 meter/sec RA = 272
28420 deg
ZDOT = -1800
720495 TA = 199
81049
MA = 199
85323
Ha = 225
143 n
mi
Hp = 220
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13551785
70 X = -4126838
23
Y = 6193480
77 feet Y = 1841603
41 meter
Z = -16579574
25 Z = -5073511
21
XDOT = -3778
945902 XDOT = -1060
789485
YDOT = -24117
355017 feet/sec YDOT = -7363
341107 meter/sec
ZDOT = -5907
875641 ZDOT = -1806
095349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6546598
51 X = 1995403
23
Y = -13280197
36 feet Y = -4047804
16 meter
Z = -16663456
67 Z = -5079021
59
XDOT = 17128
171829 XDOT = 5220
666773
YDOT = 15899
049630 feet/sec YDOT = 4846
030327 meter/sec
ZDOT = -5929
286345 ZDOT = -1807
246478
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
98314295
00016717 00000-0 10270-3 0 9077
2 25544 51
6459 272
9710 0005409 311
6535 48
4152 15
51089434 29557
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
98314295 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 272
9710 deg
Eccentricity:
0005409
Arg of perigee: 311
6535 deg
Mean anomaly: 48
4152 deg
Mean motion: 15
51089434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2955
Checksum: 318
Coasting Arc #9 (Orbit 2970)
---------------------------------------
Vector Time (GMT): 2013/135/23:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4125072
77 A = 6786454
40 meter
Y = -1348834
09 meter E =
0002186
Z = 5217748
02 I = 51
27334
XDOT = 1170
994741 Wp = 337
27037
YDOT = 7504
970456 meter/sec RA = 267
29202 deg
ZDOT = 1016
454445 TA = 102
95310
MA = 102
92868
Ha = 225
140 n
mi
Hp = 220
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13533703
31 X = 4114502
53
Y = -4425308
68 feet Y = -1302764
31 meter
Z = 17118595
87 Z = 5237761
66
XDOT = 3841
846262 XDOT = 1082
047817
YDOT = 24622
606482 feet/sec YDOT = 7517
567871 meter/sec
ZDOT = 3334
824294 ZDOT = 1021
927440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7437894
61 X = -2267070
28
Y = 12022974
91 feet Y = 3664602
75 meter
Z = 17202226
75 Z = 5243238
71
XDOT = -17884
002947 XDOT = -5451
044098
YDOT = -15856
446662 feet/sec YDOT = -4833
044942 meter/sec
ZDOT = 3356
636024 ZDOT = 1023
102660
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 13136
01397970
00016717 00000-0 10270-3 0 9085
2 25544 51
6460 267
8563 0005589 315
4918 44
5783 15
51123844 29713
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
01397970 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 267
8563 deg
Eccentricity:
0005589
Arg of perigee: 315
4918 deg
Mean anomaly: 44
5783 deg
Mean motion: 15
51123844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2971
Checksum: 332
Coasting Arc #10 (Orbit 2985)
---------------------------------------
Vector Time (GMT): 2013/136/23:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4176498
00 A = 6786112
43 meter
Y = 810159
30 meter E =
0012134
Z = -5296825
62 I = 51
27471
XDOT = -1193
116766 Wp = 67
17656
YDOT = -7558
867915 meter/sec RA = 262
29807 deg
ZDOT = -211
151065 TA = 200
77266
MA = 200
82201
Ha = 225
374 n
mi
Hp = 220
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13702421
27 X = -4159516
24
Y = 2658002
96 feet Y = 763550
25 meter
Z = -17378036
80 Z = -5317073
53
XDOT = -3914
425086 XDOT = -1107
477482
YDOT = -24799
435417 feet/sec YDOT = -7571
731253 meter/sec
ZDOT = -692
752837 ZDOT = -216
739480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8515730
74 X = 2595594
73
Y = -10925122
08 feet Y = -3329977
21 meter
Z = -17462575
10 Z = -5322592
89
XDOT = 18426
349895 XDOT = 5616
351448
YDOT = 15527
668209 feet/sec YDOT = 4732
833270 meter/sec
ZDOT = -715
052020 ZDOT = -217
947856
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 13136
98037696
00016717 00000-0 10270-3 0 9098
2 25544 51
6460 263
0603 0005617 319
6250 40
4484 15
51130762 29869
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
98037696 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 263
0603 deg
Eccentricity:
0005617
Arg of perigee: 319
6250 deg
Mean anomaly: 40
4484 deg
Mean motion: 15
51130762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2986
Checksum: 311
Coasting Arc #11 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859633
41 A = 6789535
86 meter
Y = 2168184
90 meter E =
0008188
Z = -5154792
84 I = 51
27899
XDOT = -2183
161831 Wp = 58
67947
YDOT = -7204
803745 meter/sec RA = 261
67564 deg
ZDOT = -1393
285667 TA = 197
81762
MA = 197
84635
Ha = 225
431 n
mi
Hp = 223
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12662839
27 X = -3858550
89
Y = 7113467
53 feet Y = 2125030
32 meter
Z = -16912050
01 Z = -5173540
01
XDOT = -7162
604431 XDOT = -2095
665654
YDOT = -23637
807562 feet/sec YDOT = -7228
727958 meter/sec
ZDOT = -4571
147200 ZDOT = -1403
679130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6395657
46 X = -1949396
39
Y = -12937714
78 feet Y = -3943415
47 meter
Z = -16990510
76 Z = -5178707
68
XDOT = 23058
092239 XDOT = 7028
106515
YDOT = -5328
994123 feet/sec YDOT = -1624
277409 meter/sec
ZDOT = -4613
531446 ZDOT = -1406
204385
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 13137
10923758
00016717 00000-0 10270-3 0 9108
2 25544 51
6477 262
4211 0006803 284
4965 75
5431 15
50177533 29884
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10923758 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 262
4211 deg
Eccentricity:
0006803
Arg of perigee: 284
4965 deg
Mean anomaly: 75
5431 deg
Mean motion: 15
50177533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 316
Coasting Arc #12 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3833525
94 A = 6789110
17 meter
Y = -2013834
69 meter E =
0003605
Z = 5231911
48 I = 51
28284
XDOT = 2480
706582 Wp = 274
30278
YDOT = 7184
489913 meter/sec RA = 256
69273 deg
ZDOT = 948
578705 TA = 166
56938
MA = 166
55978
Ha = 225
553 n
mi
Hp = 223
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12577184
84 X = 3830344
74
Y = -6607069
19 feet Y = -1970983
74 meter
Z = 17165063
92 Z = 5250526
77
XDOT = 8138
801123 XDOT = 2395
575722
YDOT = 23571
161132 feet/sec YDOT = 7211
754715 meter/sec
ZDOT = 3112
134859 ZDOT = 960
423298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6114625
00 X = 1863737
70
Y = 12718892
87 feet Y = 3876718
55 meter
Z = 17242954
69 Z = 5255652
59
XDOT = -22942
507344 XDOT = -6992
876238
YDOT = 6748
534362 feet/sec YDOT = 2056
953273 meter/sec
ZDOT = 3160
586549 ZDOT = 963
346780
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 13138
14069960
00016717 00000-0 10270-3 0 9110
2 25544 51
6473 257
3098 0006939 287
9542 72
0852 15
50202678 30043
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14069960 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 257
3098 deg
Eccentricity:
0006939
Arg of perigee: 287
9542 deg
Mean anomaly: 72
0852 deg
Mean motion: 15
50202678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 317
Coasting Arc #13 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2013/139/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3843323
24 A = 6788852
14 meter
Y = 1865117
88 meter E =
0009076
Z = -5283730
63 I = 51
29063
XDOT = -2770
899900 Wp = 66
15392
YDOT = -7119
738696 meter/sec RA = 251
70977 deg
ZDOT = -494
771977 TA = 199
07845
MA = 199
11247
Ha = 225
840 n
mi
Hp = 223
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12609328
20 X = -3838226
55
Y = 6119153
16 feet Y = 1822168
03 meter
Z = -17335074
24 Z = -5302388
91
XDOT = -9090
878937 XDOT = -2688
676016
YDOT = -23358
722757 feet/sec YDOT = -7150
264896 meter/sec
ZDOT = -1623
267641 ZDOT = -508
033335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5844011
80 X = -1781254
80
Y = -12632283
16 feet Y = -3850319
91 meter
Z = -17413125
51 Z = -5307520
66
XDOT = 22629
980169 XDOT = 6897
617956
YDOT = -8143
461034 feet/sec YDOT = -2482
126923 meter/sec
ZDOT = -1677
648543 ZDOT = -511
347276
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 13139
10768496
00016717 00000-0 10270-3 0 9128
2 25544 51
6479 252
5179 0006919 292
7590 67
2829 15
50216789 30195
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
10768496 = yrday
fracday
Element set: 912
Inclination: 51
6479 deg
RA of node: 252
5179 deg
Eccentricity:
0006919
Arg of perigee: 292
7590 deg
Mean anomaly: 67
2829 deg
Mean motion: 15
50216789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 347
Coasting Arc #14 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2013/140/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3889891
19 A = 6788683
97 meter
Y = -1702643
65 meter E =
0004939
Z = 5300173
02 I = 51
30080
XDOT = 3045
311829 Wp = 307
81181
YDOT = 7028
172839 meter/sec RA = 246
72708 deg
ZDOT = 25
731424 TA = 141
95901
MA = 141
92412
Ha = 225
972 n
mi
Hp = 223
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12762110
20 X = 3882894
26
Y = -5586101
21 feet Y = -1659183
65 meter
Z = 17389019
10 Z = 5319052
99
XDOT = 9991
180541 XDOT = 2966
369953
YDOT = 23058
309839 feet/sec YDOT = 7061
786047 meter/sec
ZDOT = 84
420684 ZDOT = 40
333850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5526688
68 X = 1684534
71
Y = 12679886
73 feet Y = 3864829
47 meter
Z = 17467975
09 Z = 5324238
81
XDOT = -22179
262266 XDOT = -6760
239139
YDOT = 9481
606069 feet/sec YDOT = 2889
993530 meter/sec
ZDOT = 144
417089 ZDOT = 44
018329
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 13140
13912216
00016717 00000-0 10270-3 0 9135
2 25544 51
6478 247
4063 0007044 296
3149 63
7278 15
50243704 30353
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
13912216 = yrday
fracday
Element set: 913
Inclination: 51
6478 deg
RA of node: 247
4063 deg
Eccentricity:
0007044
Arg of perigee: 296
3149 deg
Mean anomaly: 63
7278 deg
Mean motion: 15
50243704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 292
Coasting Arc #15 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2013/141/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3968019
46 A = 6788715
33 meter
Y = 1563241
96 meter E =
0009081
Z = -5289185
59 I = 51
31435
XDOT = -3301
875671 Wp = 72
41545
YDOT = -6893
298249 meter/sec RA = 241
74506 deg
ZDOT = 443
090001 TA = 201
81710
MA = 201
85580
Ha = 226
200 n
mi
Hp = 222
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13018436
55 X = -3959511
18
Y = 5128746
58 feet Y = 1518916
75 meter
Z = -17352971
11 Z = -5308441
50
XDOT = -10832
925431 XDOT = -3226
700369
YDOT = -22615
807905 feet/sec YDOT = -6929
801587 meter/sec
ZDOT = 1453
707354 ZDOT = 427
231963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5289900
46 X = -1612361
66
Y = -12845235
94 feet Y = -3915227
91 meter
Z = -17433479
42 Z = -5313724
53
XDOT = 21540
436003 XDOT = 6565
524894
YDOT = -10740
410545 feet/sec YDOT = -3273
677134 meter/sec
ZDOT = 1388
448130 ZDOT = 423
198990
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 13141
10608447
00016717 00000-0 10270-3 0 9142
2 25544 51
6482 242
6141 0007080 300
7784 59
2669 15
50253620 30506
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
10608447 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 242
6141 deg
Eccentricity:
0007080
Arg of perigee: 300
7784 deg
Mean anomaly: 59
2669 deg
Mean motion: 15
50253620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 282
Coasting Arc #16 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2013/142/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084071
61 A = 6788838
08 meter
Y = -1415884
84 meter E =
0006524
Z = 5238251
66 I = 51
33065
XDOT = 3528
329769 Wp = 332
93084
YDOT = 6735
291569 meter/sec RA = 236
76409 deg
ZDOT = -925
134186 TA = 125
99859
MA = 125
93809
Ha = 226
331 n
mi
Hp = 222
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13399185
08 X = 4074154
27
Y = -4645291
46 feet Y = -1370269
81 meter
Z = 17185865
04 Z = 5258067
98
XDOT = 11575
885070 XDOT = 3457
246196
YDOT = 22097
413283 feet/sec YDOT = 6774
350160 meter/sec
ZDOT = -3035
217145 ZDOT = -908
165946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5038223
62 X = 1535650
56
Y = 13148357
25 feet Y = 4007619
29 meter
Z = 17268695
81 Z = 5263498
48
XDOT = -20782
895976 XDOT = -6334
626694
YDOT = 11880
679111 feet/sec YDOT = 3621
230993 meter/sec
ZDOT = -2965
300184 ZDOT = -903
823496
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 13142
13749755
00016717 00000-0 10270-3 0 9155
2 25544 51
6484 237
5025 0007185 304
4357 55
6114 15
50284079 30669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
13749755 = yrday
fracday
Element set: 915
Inclination: 51
6484 deg
RA of node: 237
5025 deg
Eccentricity:
0007185
Arg of perigee: 304
4357 deg
Mean anomaly: 55
6114 deg
Mean motion: 15
50284079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 308
Coasting Arc #17 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2013/143/02:10:35
493
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4222340
81 A = 6789179
13 meter
Y = 1307688
61 meter E =
0008214
Z = -5159661
15 I = 51
34918
XDOT = -3727
905622 Wp = 76
29040
YDOT = -6540
414837 meter/sec RA = 231
78412 deg
ZDOT = 1396
837123 TA = 207
19710
MA = 207
24014
Ha = 226
521 n
mi
Hp = 222
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13852824
19 X = -4211585
05
Y = 4290316
95 feet Y = 1260532
17 meter
Z = -16928022
15 Z = -5180147
16
XDOT = -12230
661488 XDOT = -3661
277835
YDOT = -21458
053928 feet/sec YDOT = -6581
730175 meter/sec
ZDOT = 4582
798960 ZDOT = 1378
888332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4930476
62 X = -1502809
27
Y = -13531149
14 feet Y = -4124294
26 meter
Z = -17013638
49 Z = -5185757
01
XDOT = 19871
085698 XDOT = 6056
706921
YDOT = -12894
247026 feet/sec YDOT = -3930
166494 meter/sec
ZDOT = 4508
760866 ZDOT = 1374
270312
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 13143
10443764
00016717 00000-0 10270-3 0 9165
2 25544 51
6482 232
7102 0007242 308
5001 51
5500 15
50287689 30816
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
10443764 = yrday
fracday
Element set: 916
Inclination: 51
6482 deg
RA of node: 232
7102 deg
Eccentricity:
0007242
Arg of perigee: 308
5001 deg
Mean anomaly: 51
5500 deg
Mean motion: 15
50287689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 275
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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