[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 12th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 33809 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 1756)
---------------------------------------
Vector Time (GMT): 2013/315/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1501695
56 A = 6800918
55 meter
Y = 6575675
11 meter E =
0013708
Z = 821548
86 I = 52
02000
XDOT = -4467
460203 Wp = 57
99936
YDOT = -1773
997497 meter/sec RA = 97
40740 deg
ZDOT = 5967
396391 TA = 310
82424
MA = 310
94302
Ha = 227
754 n
mi
Hp = 220
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4926822
70 X = -1579105
52
Y = 21573737
25 feet Y = 6558449
40 meter
Z = 2695370
28 Z = 814065
41
XDOT = -14657
021664 XDOT = -4476
279335
YDOT = -5820
201763 feet/sec YDOT = -1824
004589 meter/sec
ZDOT = 19578
072150 ZDOT = 5945
672212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17906781
96 X = -5457987
14
Y = -13008486
58 feet Y = -3964986
71 meter
Z = 2662926
70 Z = 811660
06
XDOT = 10199
845292 XDOT = 3108
912845
YDOT = -10006
793603 feet/sec YDOT = -3050
070690 meter/sec
ZDOT = 19486
966262 ZDOT = 5939
627317
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 13315
60981643
00016717 00000-0 10270-3 0 9007
2 25544 51
6480 97
9461 0001060 124
7349 235
3901 15
50055785 17573
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
60981643 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 97
9461 deg
Eccentricity:
0001060
Arg of perigee: 124
7349 deg
Mean anomaly: 235
3901 deg
Mean motion: 15
50055785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1757
Checksum: 304
Coasting Arc #2 (Orbit 1771)
---------------------------------------
Vector Time (GMT): 2013/316/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1222974
49 A = 6800447
59 meter
Y = -6576663
64 meter E =
0010087
Z = -1200532
95 I = 52
02169
XDOT = 4516
698804 Wp = 140
29280
YDOT = 1908
016034 meter/sec RA = 92
48022 deg
ZDOT = -5885
969693 TA = 52
65717
MA = 52
56531
Ha = 227
648 n
mi
Hp = 220
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4012383
50 X = 1302257
27
Y = -21576980
46 feet Y = -6562544
32 meter
Z = -3938756
40 Z = -1194398
92
XDOT = 14818
565630 XDOT = 4523
620191
YDOT = 6259
895126 feet/sec YDOT = 1958
563108 meter/sec
ZDOT = -19310
924189 ZDOT = -5864
010865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18472185
20 X = 5630322
05
Y = 11859760
63 feet Y = 3614855
04 meter
Z = -3911976
59 Z = -1192370
47
XDOT = -10554
928069 XDOT = -3217
142075
YDOT = 10138
319750 feet/sec YDOT = 3090
159860 meter/sec
ZDOT = -19218
852298 ZDOT = -5857
906180
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 13316
57687200
00016717 00000-0 10270-3 0 9017
2 25544 51
6477 93
1547 0000947 123
9230 236
2010 15
50104962 17725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13316
57687200 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 93
1547 deg
Eccentricity:
0000947
Arg of perigee: 123
9230 deg
Mean anomaly: 236
2010 deg
Mean motion: 15
50104962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1772
Checksum: 286
Coasting Arc #3 (Orbit 1787)
---------------------------------------
Vector Time (GMT): 2013/317/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -930777
35 A = 6799921
08 meter
Y = 6548596
39 meter E =
0014389
Z = 1549370
39 I = 52
02169
XDOT = -4603
585760 Wp = 65
50178
YDOT = -2030
545595 meter/sec RA = 87
55270 deg
ZDOT = 5780
477334 TA = 311
31649
MA = 311
44024
Ha = 227
585 n
mi
Hp = 220
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3053731
46 X = -1011462
60
Y = 21484896
31 feet Y = 6537736
77 meter
Z = 5083236
19 Z = 1544652
45
XDOT = -15103
627821 XDOT = -4608
618176
YDOT = -6661
894998 feet/sec YDOT = -2082
053757 meter/sec
ZDOT = 18964
820650 ZDOT = 5758
100914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18930486
66 X = -5770012
33
Y = -10619514
18 feet Y = -3236827
92 meter
Z = 5062403
44 Z = 1543020
57
XDOT = 10923
072190 XDOT = 3329
352404
YDOT = -10418
683008 feet/sec YDOT = -3175
614581 meter/sec
ZDOT = 18871
013447 ZDOT = 5751
884899
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 13317
60836702
00016717 00000-0 10270-3 0 9026
2 25544 51
6486 88
0439 0000941 120
4314 239
6930 15
50148983 17883
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
60836702 = yrday
fracday
Element set: 902
Inclination: 51
6486 deg
RA of node: 88
0439 deg
Eccentricity:
0000941
Arg of perigee: 120
4314 deg
Mean anomaly: 239
6930 deg
Mean motion: 15
50148983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1788
Checksum: 313
Coasting Arc #4 (Orbit 1802)
---------------------------------------
Vector Time (GMT): 2013/318/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 691795
35 A = 6799203
59 meter
Y = -6476215
21 meter E =
0007736
Z = -1943388
23 I = 52
01766
XDOT = 4713
481985 Wp = 138
22979
YDOT = 2186
630012 meter/sec RA = 82
62501 deg
ZDOT = -5627
391811 TA = 63
03990
MA = 62
96091
Ha = 227
482 n
mi
Hp = 220
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2269669
77 X = 773603
08
Y = -21247425
23 feet Y = -6468021
75 meter
Z = -6375945
64 Z = -1939828
60
XDOT = 15464
179740 XDOT = 4716
017282
YDOT = 7173
982978 feet/sec YDOT = 2239
353205 meter/sec
ZDOT = -18462
571560 ZDOT = -5604
487492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19154606
79 X = 5838324
15
Y = 9482027
32 feet Y = 2890121
93 meter
Z = -6359981
09 Z = -1938522
24
XDOT = -11405
187301 XDOT = -3476
301089
YDOT = 10761
105635 feet/sec YDOT = 3279
984998 meter/sec
ZDOT = -18366
571521 ZDOT = -5598
131000
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 13318
57536504
00016717 00000-0 10270-3 0 9031
2 25544 51
6488 83
2526 0000854 120
9208 239
2027 15
50193174 18032
Satellite: ISS
Catalog Number: 25544
Epoch time: 13318
57536504 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 83
2526 deg
Eccentricity:
0000854
Arg of perigee: 120
9208 deg
Mean anomaly: 239
2027 deg
Mean motion: 15
50193174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1803
Checksum: 297
Coasting Arc #5 (Orbit 1818)
---------------------------------------
Vector Time (GMT): 2013/319/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -450837
08 A = 6798413
01 meter
Y = 6373630
71 meter E =
0014453
Z = 2303149
52 I = 52
01137
XDOT = -4862
828858 Wp = 74
60906
YDOT = -2322
278548 meter/sec RA = 77
69611 deg
ZDOT = 5449
999960 TA = 310
87472
MA = 310
99987
Ha = 227
421 n
mi
Hp = 220
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1479124
28 X = -533263
29
Y = 20910861
90 feet Y = 6368128
31 meter
Z = 7556264
83 Z = 2300759
06
XDOT = -15954
162921 XDOT = -4862
974509
YDOT = -7619
024107 feet/sec YDOT = -2376
658559 meter/sec
ZDOT = 17880
577297 ZDOT = 5426
375839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19253921
29 X = -5868595
21
Y = -8300921
06 feet Y = -2530120
74 meter
Z = 7545218
12 Z = 2299782
48
XDOT = 11860
383304 XDOT = 3615
044831
YDOT = -11273
596122 feet/sec YDOT = -3436
192098 meter/sec
ZDOT = 17781
574939 ZDOT = 5419
824041
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 13319
60679819
00016717 00000-0 10270-3 0 9044
2 25544 51
6495 78
1414 0000855 114
5568 245
5672 15
50245119 18198
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
60679819 = yrday
fracday
Element set: 904
Inclination: 51
6495 deg
RA of node: 78
1414 deg
Eccentricity:
0000855
Arg of perigee: 114
5568 deg
Mean anomaly: 245
5672 deg
Mean motion: 15
50245119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1819
Checksum: 326
Coasting Arc #6 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2013/320/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 274482
12 A = 6797469
79 meter
Y = -6232449
28 meter E =
0005664
Z = -2698980
07 I = 52
00128
XDOT = 5032
779074 Wp = 122
78406
YDOT = 2474
960640 meter/sec RA = 72
76697 deg
ZDOT = -5214
233574 TA = 87
47270
MA = 87
40786
Ha = 227
328 n
mi
Hp = 220
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 900531
88 X = 357265
60
Y = -20447668
25 feet Y = -6228916
96 meter
Z = -8854921
49 Z = -2697445
59
XDOT = 16511
742369 XDOT = 5030
059461
YDOT = 8119
949607 feet/sec YDOT = 2531
225215 meter/sec
ZDOT = -17107
065532 ZDOT = -5189
790735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19131679
88 X = 5831336
03
Y = 7282075
46 feet Y = 2219576
60 meter
Z = -8847481
63 Z = -2696712
40
XDOT = -12363
088610 XDOT = -3768
269408
YDOT = 11864
115196 feet/sec YDOT = 3616
182312 meter/sec
ZDOT = -17004
647713 ZDOT = -5183
016623
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 13320
57373869
00016717 00000-0 10270-3 0 9059
2 25544 51
6496 73
3503 0000777 114
9729 245
1503 15
50279536 18347
Satellite: ISS
Catalog Number: 25544
Epoch time: 13320
57373869 = yrday
fracday
Element set: 905
Inclination: 51
6496 deg
RA of node: 73
3503 deg
Eccentricity:
0000777
Arg of perigee: 114
9729 deg
Mean anomaly: 245
1503 deg
Mean motion: 15
50279536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 320
Coasting Arc #7 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2013/321/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -108425
69 A = 6796423
00 meter
Y = 6063353
37 meter E =
0013759
Z = 3055158
98 I = 51
98890
XDOT = -5239
749212 Wp = 85
06401
YDOT = -2598
970140 meter/sec RA = 67
83562 deg
ZDOT = 4954
029842 TA = 309
75907
MA = 309
88019
Ha = 227
252 n
mi
Hp = 220
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -355727
33 X = -191060
90
Y = 19892891
62 feet Y = 6061678
76 meter
Z = 10023487
46 Z = 3054431
67
XDOT = -17190
778253 XDOT = -5234
363459
YDOT = -8526
804921 feet/sec YDOT = -2657
534364 meter/sec
ZDOT = 16253
378747 ZDOT = 4928
587988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18882915
28 X = -5755512
58
Y = -6274552
97 feet Y = -1912483
74 meter
Z = 10019454
85 Z = 3053929
84
XDOT = 12794
310048 XDOT = 3899
705703
YDOT = -12625
581101 feet/sec YDOT = -3848
277120 meter/sec
ZDOT = 16146
782365 ZDOT = 4921
539265
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 13321
60511007
00016717 00000-0 10270-3 0 9063
2 25544 51
6502 68
2388 0000781 108
3182 251
8054 15
50342267 18509
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
60511007 = yrday
fracday
Element set: 906
Inclination: 51
6502 deg
RA of node: 68
2388 deg
Eccentricity:
0000781
Arg of perigee: 108
3182 deg
Mean anomaly: 251
8054 deg
Mean motion: 15
50342267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 276
Coasting Arc #8 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2013/322/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 16894
56 A = 6795315
42 meter
Y = -5865632
15 meter E =
0005611
Z = -3435523
07 I = 51
97259
XDOT = 5458
122595 Wp = 91
14495
YDOT = 2722
268690 meter/sec RA = 62
90358 deg
ZDOT = -4627
647776 TA = 128
76592
MA = 128
71578
Ha = 227
188 n
mi
Hp = 220
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 55428
35 X = 99173
33
Y = -19244199
98 feet Y = -5864983
04 meter
Z = -11271401
13 Z = -3435241
37
XDOT = 17907
226363 XDOT = 5449
756298
YDOT = 8931
327724 feet/sec YDOT = 2783
258300 meter/sec
ZDOT = -15182
571442 ZDOT = -4601
152307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18446760
32 X = 5622572
55
Y = 5487036
13 feet Y = 1672448
61 meter
Z = -11269261
58 Z = -3434870
93
XDOT = -13195
391043 XDOT = -4021
955190
YDOT = 13452
063397 feet/sec YDOT = 4100
188924 meter/sec
ZDOT = -15071
566217 ZDOT = -4593
813383
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 13322
57199343
00016717 00000-0 10270-3 0 9076
2 25544 51
6498 63
4476 0000733 105
5429 254
5803 15
50364695 18655
Satellite: ISS
Catalog Number: 25544
Epoch time: 13322
57199343 = yrday
fracday
Element set: 907
Inclination: 51
6498 deg
RA of node: 63
4476 deg
Eccentricity:
0000733
Arg of perigee: 105
5429 deg
Mean anomaly: 254
5803 deg
Mean motion: 15
50364695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 325
Coasting Arc #9 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2013/323/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 52561
00 A = 6794082
90 meter
Y = 5645913
62 meter E =
0012276
Z = 3769614
09 I = 51
95470
XDOT = -5706
598021 Wp = 96
42756
YDOT = -2811
185207 meter/sec RA = 57
96854 deg
ZDOT = 4276
732130 TA = 308
40790
MA = 308
51807
Ha = 227
092 n
mi
Hp = 220
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 172444
24 X = -28888
89
Y = 18523338
66 feet Y = 5646045
79 meter
Z = 12367500
30 Z = 3769671
88
XDOT = -18722
434451 XDOT = -5695
514218
YDOT = -9223
048581 feet/sec YDOT = -2874
938262 meter/sec
ZDOT = 14031
273392 ZDOT = 4249
036213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17900856
67 X = -5456181
11
Y = -4766563
96 feet Y = -1452848
70 meter
Z = 12366813
42 Z = 3769404
73
XDOT = 13484
918172 XDOT = 4110
203059
YDOT = -14426
747731 feet/sec YDOT = -4397
272708 meter/sec
ZDOT = 13915
235499 ZDOT = 4241
363780
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 13323
60330348
00016717 00000-0 10270-3 0 9084
2 25544 51
6502 58
3357 0000727 99
6618 260
4615 15
50436349 18819
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
60330348 = yrday
fracday
Element set: 908
Inclination: 51
6502 deg
RA of node: 58
3357 deg
Eccentricity:
0000727
Arg of perigee: 99
6618 deg
Mean anomaly: 260
4615 deg
Mean motion: 15
50436349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1881
Checksum: 307
Coasting Arc #10 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2013/324/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -41245
93 A = 6792912
09 meter
Y = -5411989
45 meter E =
0008131
Z = -4113586
00 I = 51
93288
XDOT = 5950
300239 Wp = 72
88008
YDOT = 2882
982224 meter/sec RA = 53
03193 deg
ZDOT = -3856
586732 TA = 157
34894
MA = 157
31304
Ha = 227
069 n
mi
Hp = 220
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -135321
30 X = 39258
22
Y = -17755870
92 feet Y = -5412000
35 meter
Z = -13496017
08 Z = -4113591
13
XDOT = 19521
982412 XDOT = 5936
354420
YDOT = 9458
603096 feet/sec YDOT = 2949
444501 meter/sec
ZDOT = -12652
843610 ZDOT = -3827
713938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17225493
36 X = 5250330
38
Y = 4312234
12 feet Y = 1314368
96 meter
Z = -13495138
24 Z = -4113318
13
XDOT = -13668
132279 XDOT = -4166
046719
YDOT = 15420
437258 feet/sec YDOT = 4700
149276 meter/sec
ZDOT = -12531
868948 ZDOT = -3819
713655
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 13324
57013023
00016717 00000-0 10270-3 0 9090
2 25544 51
6493 53
5439 0000762 93
8689 266
2549 15
50450161 18963
Satellite: ISS
Catalog Number: 25544
Epoch time: 13324
57013023 = yrday
fracday
Element set: 909
Inclination: 51
6493 deg
RA of node: 53
5439 deg
Eccentricity:
0000762
Arg of perigee: 93
8689 deg
Mean anomaly: 266
2549 deg
Mean motion: 15
50450161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 317
Coasting Arc #11 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2013/325/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1828
12 A = 6791631
41 meter
Y = 5165217
25 meter E =
0010108
Z = 4403364
31 I = 51
91043
XDOT = -6213
046043 Wp = 107
73843
YDOT = -2918
883909 meter/sec RA = 48
09220 deg
ZDOT = 3411
883818 TA = 307
77794
MA = 307
86945
Ha = 226
971 n
mi
Hp = 220
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5997
77 X = -80977
24
Y = 16946250
82 feet Y = 5164754
03 meter
Z = 14446733
28 Z = 4403163
44
XDOT = -20384
009327 XDOT = -6196
518905
YDOT = -9576
390779 feet/sec YDOT = -2988
269912 meter/sec
ZDOT = 11193
844546 ZDOT = 3381
740969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16475371
70 X = -5021693
29
Y = -3973288
61 feet Y = -1211058
37 meter
Z = 14445021
99 Z = 4402842
70
XDOT = 13713
966024 XDOT = 4180
016844
YDOT = -16516
475647 feet/sec YDOT = -5034
221777 meter/sec
ZDOT = 11067
535122 ZDOT = 3373
384705
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 13325
60137987
00016717 00000-0 10270-3 0 9103
2 25544 51
6496 48
4315 0000767 88
7371 271
3868 15
50525224 19121
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
60137987 = yrday
fracday
Element set: 910
Inclination: 51
6496 deg
RA of node: 48
4315 deg
Eccentricity:
0000767
Arg of perigee: 88
7371 deg
Mean anomaly: 271
3868 deg
Mean motion: 15
50525224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 318
Coasting Arc #12 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2013/326/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 125959
81 A = 6790541
72 meter
Y = -4922313
14 meter E =
0011465
Z = -4687279
33 I = 51
88479
XDOT = 6449
061708 Wp = 71
26672
YDOT = 2925
633691 meter/sec RA = 43
14982 deg
ZDOT = -2901
255546 TA = 169
93854
MA = 169
91557
Ha = 226
975 n
mi
Hp = 220
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 413253
96 X = 203762
64
Y = -16149321
31 feet Y = -4920469
35 meter
Z = -15378213
04 Z = -4686478
66
XDOT = 21158
338938 XDOT = 6429
960993
YDOT = 9598
535732 feet/sec YDOT = 2997
644534 meter/sec
ZDOT = -9518
554942 ZDOT = -2869
972479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15674934
37 X = 4777720
00
Y = 3923890
97 feet Y = 1196001
97 meter
Z = -15374013
99 Z = -4685999
46
XDOT = -13594
567725 XDOT = -4143
624243
YDOT = 17554
877949 feet/sec YDOT = 5350
726799 meter/sec
ZDOT = -9387
452452 ZDOT = -2861
295507
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 13326
56815064
00016717 00000-0 10270-3 0 9119
2 25544 51
6488 43
6386 0000883 84
8788 275
2464 15
50536831 19272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
56815064 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 43
6386 deg
Eccentricity:
0000883
Arg of perigee: 84
8788 deg
Mean anomaly: 275
2464 deg
Mean motion: 15
50536831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 335
Coasting Arc #13 (Orbit 1942)
---------------------------------------
Vector Time (GMT): 2013/327/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -287712
82 A = 6789399
79 meter
Y = 4677891
30 meter E =
0007457
Z = 4907729
59 I = 51
85881
XDOT = -6689
804945 Wp = 116
32801
YDOT = -2900
465130 meter/sec RA = 38
20483 deg
ZDOT = 2366
439823 TA = 310
52949
MA = 310
59442
Ha = 226
904 n
mi
Hp = 219
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -943939
70 X = -363841
33
Y = 15347412
41 feet Y = 4674248
09 meter
Z = 16101475
03 Z = 4906147
14
XDOT = -21948
178953 XDOT = -6668
369743
YDOT = -9515
961714 feet/sec YDOT = -2975
155017 meter/sec
ZDOT = 7763
910181 ZDOT = 2333
992975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14849173
86 X = -4526028
19
Y = -4021939
45 feet Y = -1225887
14 meter
Z = 16094024
57 Z = 4905458
69
XDOT = 13335
028370 XDOT = 4064
516647
YDOT = -18631
096289 feet/sec YDOT = -5678
758149 meter/sec
ZDOT = 7627
911062 ZDOT = 2324
987292
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 13327
59934106
00016717 00000-0 10270-3 0 9123
2 25544 51
6491 38
5259 0000941 81
6802 278
4455 15
50610458 19436
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
59934106 = yrday
fracday
Element set: 912
Inclination: 51
6491 deg
RA of node: 38
5259 deg
Eccentricity:
0000941
Arg of perigee: 81
6802 deg
Mean anomaly: 278
4455 deg
Mean motion: 15
50610458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1943
Checksum: 313
Coasting Arc #14 (Orbit 1957)
---------------------------------------
Vector Time (GMT): 2013/328/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 523035
97 A = 6788572
21 meter
Y = -4457109
90 meter E =
0014341
Z = -5106590
35 I = 51
83132
XDOT = 6878
943126 Wp = 76
87530
YDOT = 2841
327346 meter/sec RA = 33
25640 deg
ZDOT = -1776
418811 TA = 175
95525
MA = 175
94365
Ha = 226
897 n
mi
Hp = 219
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1715997
28 X = 597644
18
Y = -14623063
98 feet Y = -4450843
71 meter
Z = -16753905
36 Z = -5103868
34
XDOT = 22568
711042 XDOT = 6855
288964
YDOT = 9321
940113 feet/sec YDOT = 2918
119851 meter/sec
ZDOT = -5828
145707 ZDOT = -1743
058568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14065012
43 X = 4287015
79
Y = 4400345
67 feet Y = 1341225
36 meter
Z = -16741695
70 Z = -5102868
85
XDOT = -12884
124590 XDOT = -3927
081175
YDOT = 19553
083252 feet/sec YDOT = 5959
779775 meter/sec
ZDOT = -5688
298881 ZDOT = -1733
793499
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 13328
56605661
00016717 00000-0 10270-3 0 9133
2 25544 51
6491 33
7321 0001056 81
0179 279
1092 15
50624545 19585
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
56605661 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 33
7321 deg
Eccentricity:
0001056
Arg of perigee: 81
0179 deg
Mean anomaly: 279
1092 deg
Mean motion: 15
50624545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1958
Checksum: 302
Coasting Arc #15 (Orbit 1973)
---------------------------------------
Vector Time (GMT): 2013/329/13:07:33
156
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -796524
00 A = 6787774
09 meter
Y = 4246535
89 meter E =
0004787
Z = 5231630
93 I = 51
80286
XDOT = -7056
561051 Wp = 113
24627
YDOT = -2760
533296 meter/sec RA = 28
30596 deg
ZDOT = 1163
675711 TA = 325
60157
MA = 325
63255
Ha = 226
870 n
mi
Hp = 219
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2613267
73 X = -869364
64
Y = 13932204
37 feet Y = 4237221
32 meter
Z = 17164143
47 Z = 5227584
57
XDOT = -23151
447019 XDOT = -7030
820579
YDOT = -9056
867769 feet/sec YDOT = -2839
300346 meter/sec
ZDOT = 3817
833697 ZDOT = 1129
457676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13311570
94 X = -4057366
82
Y = -4934214
57 feet Y = -1503948
60 meter
Z = 17146396
52 Z = 5226221
66
XDOT = 12319
899285 XDOT = 3755
105302
YDOT = -20437
626013 feet/sec YDOT = -6229
388409 meter/sec
ZDOT = 3674
371061 ZDOT = 1119
948300
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 13329
59718910
00016717 00000-0 10270-3 0 9140
2 25544 51
6489 28
6191 0001184 80
3649 279
7636 15
50695062 19746
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
59718910 = yrday
fracday
Element set: 914
Inclination: 51
6489 deg
RA of node: 28
6191 deg
Eccentricity:
0001184
Arg of perigee: 80
3649 deg
Mean anomaly: 279
7636 deg
Mean motion: 15
50695062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1974
Checksum: 340
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