[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 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 1894)
---------------------------------------
Vector Time (GMT): 2013/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5246782
38 A = 6796735
30 meter
Y = 3147843
73 meter E =
0005113
Z = -2961226
88 I = 51
94729
XDOT = -616
016684 Wp = 69
77997
YDOT = 5745
170211 meter/sec RA = 53
22351 deg
ZDOT = 5024
500513 TA = 256
63161
MA = 256
68861
Ha = 227
222 n
mi
Hp = 220
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17213852
96 X = 5225577
62
Y = 10327571
31 feet Y = 3206398
19 meter
Z = -9715311
29 Z = -2935789
39
XDOT = -2021
052112 XDOT = -704
622741
YDOT = 18848
983632 feet/sec YDOT = 5737
785823 meter/sec
ZDOT = 16484
581734 ZDOT = 5021
292996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17774071
51 X = -5417536
99
Y = 9440099
53 feet Y = 2877342
34 meter
Z = -9608831
32 Z = -2928771
79
XDOT = -14344
612405 XDOT = -4372
237861
YDOT = -10273
423904 feet/sec YDOT = -3131
339606 meter/sec
ZDOT = 16470
133734 ZDOT = 5020
096762
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
50597430
00016717 00000-0 10270-3 0 9003
2 25544 51
6511 53
8704 0000645 101
8142 258
3081 15
50342553 18953
Satellite: ISS
Catalog Number: 25544
Epoch time: 13324
50597430 = yrday
fracday
Element set: 900
Inclination: 51
6511 deg
RA of node: 53
8704 deg
Eccentricity:
0000645
Arg of perigee: 101
8142 deg
Mean anomaly: 258
3081 deg
Mean motion: 15
50342553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 280
Coasting Arc #2 (Orbit 1910)
---------------------------------------
Vector Time (GMT): 2013/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5461356
09 A = 6797568
54 meter
Y = -3134968
99 meter E =
0014509
Z = 2542020
21 I = 51
93071
XDOT = 672
322421 Wp = 104
09940
YDOT = -5491
102832 meter/sec RA = 48
28867 deg
ZDOT = -5305
625722 TA = 47
51012
MA = 47
38761
Ha = 227
249 n
mi
Hp = 220
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17917834
95 X = -5438242
89
Y = -10285331
32 feet Y = -3195912
24 meter
Z = 8339961
31 Z = 2515545
03
XDOT = 2205
782220 XDOT = 759
448834
YDOT = -18015
429240 feet/sec YDOT = -5483
097069 meter/sec
ZDOT = -17406
908538 ZDOT = -5302
148249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17922118
59 X = 5462661
75
Y = -10366827
43 feet Y = -3159809
00 meter
Z = 8229116
51 Z = 2508234
71
XDOT = 13657
517692 XDOT = 4162
811393
YDOT = 9748
137141 feet/sec YDOT = 2971
232201 meter/sec
ZDOT = -17391
359436 ZDOT = -5300
886356
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
53729953
00016717 00000-0 10270-3 0 9015
2 25544 51
6505 48
7590 0000842 102
0853 258
0392 15
50388950 19115
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
53729953 = yrday
fracday
Element set: 901
Inclination: 51
6505 deg
RA of node: 48
7590 deg
Eccentricity:
0000842
Arg of perigee: 102
0853 deg
Mean anomaly: 258
0392 deg
Mean motion: 15
50388950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1911
Checksum: 304
Coasting Arc #3 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2013/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679254
62 A = 6798342
30 meter
Y = 3067576
24 meter E =
0006919
Z = -2128400
98 I = 51
91223
XDOT = -763
853658 Wp = 45
11603
YDOT = 5241
615562 meter/sec RA = 43
35244 deg
ZDOT = 5532
064552 TA = 291
43844
MA = 291
51222
Ha = 227
156 n
mi
Hp = 220
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18632725
13 X = 5654869
52
Y = 10064226
52 feet Y = 3130949
03 meter
Z = -6982942
85 Z = -2100870
44
XDOT = -2506
081556 XDOT = -849
283383
YDOT = 17196
901449 feet/sec YDOT = 5232
595753 meter/sec
ZDOT = 18149
818085 ZDOT = 5528
146501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17892663
16 X = -5453683
73
Y = 11398095
66 feet Y = 3474139
56 meter
Z = -6867649
70 Z = -2093259
63
XDOT = -12907
088724 XDOT = -3934
080643
YDOT = -9367
847726 feet/sec YDOT = -2855
319987 meter/sec
ZDOT = 18132
451615 ZDOT = 5526
771252
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
50414531
00016717 00000-0 10270-3 0 9027
2 25544 51
6506 43
9668 0000673 90
0970 270
0258 15
50397643 19267
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
50414531 = yrday
fracday
Element set: 902
Inclination: 51
6506 deg
RA of node: 43
9668 deg
Eccentricity:
0000673
Arg of perigee: 90
0970 deg
Mean anomaly: 270
0258 deg
Mean motion: 15
50397643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 298
Coasting Arc #4 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2013/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5866049
29 A = 6798905
57 meter
Y = -2999560
78 meter E =
0014671
Z = 1650645
37 I = 51
89120
XDOT = 933
533406 Wp = 115
02576
YDOT = -4999
582851 meter/sec RA = 38
41538 deg
ZDOT = -5733
887771 TA = 46
98361
MA = 46
86079
Ha = 227
111 n
mi
Hp = 220
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19245568
54 X = -5840090
03
Y = -9841078
68 feet Y = -3065013
59 meter
Z = 5415503
18 Z = 1622211
28
XDOT = 3062
773642 XDOT = 1017
224435
YDOT = -16402
830875 feet/sec YDOT = -4988
675345 meter/sec
ZDOT = -18811
967753 ZDOT = -5729
149590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17782365
33 X = 5420064
95
Y = -12341071
03 feet Y = -3761558
45 meter
Z = 5296400
82 Z = 1614342
97
XDOT = 12055
100383 XDOT = 3674
394597
YDOT = 9257
063513 feet/sec YDOT = 2821
552959 meter/sec
ZDOT = -18791
187861 ZDOT = -5727
554060
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
53542710
00016717 00000-0 10270-3 0 9033
2 25544 51
6501 38
8548 0000853 92
3872 267
7377 15
50463978 19426
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
53542710 = yrday
fracday
Element set: 903
Inclination: 51
6501 deg
RA of node: 38
8548 deg
Eccentricity:
0000853
Arg of perigee: 92
3872 deg
Mean anomaly: 267
7377 deg
Mean motion: 15
50463978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 323
Coasting Arc #5 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2013/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6040553
40 A = 6799479
70 meter
Y = 2877932
81 meter E =
0009912
Z = -1186536
24 I = 51
86813
XDOT = -1131
176572 Wp = 40
89883
YDOT = 4782
740829 meter/sec RA = 33
47658 deg
ZDOT = 5876
813276 TA = 306
27590
MA = 306
36743
Ha = 227
112 n
mi
Hp = 220
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19818088
58 X = 6013686
70
Y = 9442036
77 feet Y = 2945331
93 meter
Z = -3892835
44 Z = -1157256
67
XDOT = -3711
209227 XDOT = -1213
122431
YDOT = 15691
406920 feet/sec YDOT = 4769
632971 meter/sec
ZDOT = 19280
883453 ZDOT = 5871
119132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17470153
63 X = -5324902
83
Y = 13328258
93 feet Y = 4062453
32 meter
Z = -3770160
08 Z = -1149144
79
XDOT = -11232
233788 XDOT = -3423
584859
YDOT = -9309
374134 feet/sec YDOT = -2837
497236 meter/sec
ZDOT = 19256
115934 ZDOT = 5869
264137
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
50223309
00016717 00000-0 10270-3 0 9042
2 25544 51
6499 34
0621 0000795 80
4574 279
6666 15
50450720 19574
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
50223309 = yrday
fracday
Element set: 904
Inclination: 51
6499 deg
RA of node: 34
0621 deg
Eccentricity:
0000795
Arg of perigee: 80
4574 deg
Mean anomaly: 279
6666 deg
Mean motion: 15
50450720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 310
Coasting Arc #6 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2013/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6170562
38 A = 6799633
75 meter
Y = -2763047
70 meter E =
0013804
Z = 662376
55 I = 51
84332
XDOT = 1402
447680 Wp = 125
20030
YDOT = -4584
492710 meter/sec RA = 28
53658 deg
ZDOT = -5978
767544 TA = 47
67668
MA = 47
55981
Ha = 227
005 n
mi
Hp = 220
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20244627
22 X = -6142424
43
Y = -9065117
13 feet Y = -2831893
54 meter
Z = 2173151
41 Z = 632468
49
XDOT = 4601
206298 XDOT = 1482
651818
YDOT = -15040
986582 feet/sec YDOT = -4568
361127 meter/sec
ZDOT = -19615
379082 ZDOT = -5971
759745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17084076
55 X = 5207226
53
Y = -14166320
44 feet Y = -4317894
47 meter
Z = 2047818
38 Z = 624175
04
XDOT = 10373
701754 XDOT = 3161
904295
YDOT = 9638
843213 feet/sec YDOT = 2937
919411 meter/sec
ZDOT = -19585
117308 ZDOT = -5969
543755
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
53347244
00016717 00000-0 10270-3 0 9052
2 25544 51
6500 28
9495 0000947 85
4596 274
6663 15
50534462 19732
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
53347244 = yrday
fracday
Element set: 905
Inclination: 51
6500 deg
RA of node: 28
9495 deg
Eccentricity:
0000947
Arg of perigee: 85
4596 deg
Mean anomaly: 274
6663 deg
Mean motion: 15
50534462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 328
Coasting Arc #7 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2013/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6274184
07 A = 6799868
69 meter
Y = 2601629
75 meter E =
0012703
Z = -161726
06 I = 51
81607
XDOT = -1689
240994 Wp = 46
56531
YDOT = 4429
130097 meter/sec RA = 23
59465 deg
ZDOT = 6020
581684 TA = 311
69930
MA = 311
80792
Ha = 227
083 n
mi
Hp = 219
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20584593
41 X = 6245411
39
Y = 8535530
68 feet Y = 2671630
80 meter
Z = -530597
32 Z = -131316
12
XDOT = -5542
129247 XDOT = -1767
889698
YDOT = 14531
266721 feet/sec YDOT = 4409
800159 meter/sec
ZDOT = 19752
564580 ZDOT = 6012
184373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16499575
14 X = -5029070
50
Y = 14982116
27 feet Y = 4566549
04 meter
Z = -403132
59 Z = -122874
81
XDOT = -9637
121250 XDOT = -2937
394557
YDOT = -10118
137423 feet/sec YDOT = -3084
008287 meter/sec
ZDOT = 19716
483077 ZDOT = 6009
584042
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 13330
50023949
00016717 00000-0 10270-3 0 9065
2 25544 51
6498 24
1566 0001007 76
8138 283
3125 15
50507106 19880
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
50023949 = yrday
fracday
Element set: 906
Inclination: 51
6498 deg
RA of node: 24
1566 deg
Eccentricity:
0001007
Arg of perigee: 76
8138 deg
Mean anomaly: 283
3125 deg
Mean motion: 15
50507106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 299
Coasting Arc #8 (Orbit 2003)
---------------------------------------
Vector Time (GMT): 2013/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6321786
68 A = 6799535
59 meter
Y = -2458955
18 meter E =
0011855
Z = -391363
52 I = 51
78792
XDOT = 2037
310562 Wp = 133
22688
YDOT = -4301
571400 meter/sec RA = 18
65091 deg
ZDOT = -6004
604141 TA = 50
97715
MA = 50
87168
Ha = 226
937 n
mi
Hp = 219
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20740769
95 X = -6291919
08
Y = -8067438
26 feet Y = -2529482
43 meter
Z = -1284001
06 Z = -422002
13
XDOT = 6684
089769 XDOT = 2114
429469
YDOT = -14112
767062 feet/sec YDOT = -4278
357705 meter/sec
ZDOT = -19700
144820 ZDOT = -5994
519588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15872301
99 X = 4837877
65
Y = -15588033
51 feet Y = -4751232
61 meter
Z = -1412443
96 Z = -430512
92
XDOT = 8935
552882 XDOT = 2723
556518
YDOT = 10846
555528 feet/sec YDOT = 3306
030125 meter/sec
ZDOT = -19656
987203 ZDOT = -5991
449700
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 13331
53143730
00016717 00000-0 10270-3 0 9071
2 25544 51
6505 19
0437 0001092 84
5683 275
5592 15
50596609 20041
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
53143730 = yrday
fracday
Element set: 907
Inclination: 51
6505 deg
RA of node: 19
0437 deg
Eccentricity:
0001092
Arg of perigee: 84
5683 deg
Mean anomaly: 275
5592 deg
Mean motion: 15
50596609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2004
Checksum: 296
Coasting Arc #9 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2013/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6332600
60 A = 6799307
25 meter
Y = 2282301
15 meter E =
0014614
Z = 909710
52 I = 51
75685
XDOT = -2384
898437 Wp = 56
78162
YDOT = 4229
200781 meter/sec RA = 13
70501 deg
ZDOT = 5930
179000 TA = 313
03669
MA = 313
15901
Ha = 227
042 n
mi
Hp = 219
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20776248
69 X = 6302189
53
Y = 7487864
67 feet Y = 2352946
28 meter
Z = 2984614
58 Z = 940400
44
XDOT = -7824
469939 XDOT = -2460
820790
YDOT = 13875
330645 feet/sec YDOT = 4202
106802 meter/sec
ZDOT = 19455
967848 ZDOT = 5918
408758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15079351
89 X = -4596186
46
Y = 16110527
34 feet Y = 4910488
73 meter
Z = 3113295
12 Z = 948932
35
XDOT = -8434
397874 XDOT = -2570
804472
YDOT = -11681
740067 feet/sec YDOT = -3560
594372 meter/sec
ZDOT = 19405
731561 ZDOT = 5914
866980
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 13332
56261571
00016717 00000-0 10270-3 0 9080
2 25544 51
6499 13
9312 0001238 79
1551 280
9739 15
50573133 20202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
56261571 = yrday
fracday
Element set: 908
Inclination: 51
6499 deg
RA of node: 13
9312 deg
Eccentricity:
0001238
Arg of perigee: 79
1551 deg
Mean anomaly: 280
9739 deg
Mean motion: 15
50573133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2020
Checksum: 296
Coasting Arc #10 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2013/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6280134
52 A = 6798489
60 meter
Y = -2140128
40 meter E =
0009012
Z = -1469057
25 I = 51
72564
XDOT = 2773
790686 Wp = 135
50294
YDOT = -4189
237942 meter/sec RA = 8
75650 deg
ZDOT = -5782
672095 TA = 60
48126
MA = 60
39142
Ha = 226
885 n
mi
Hp = 219
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20604115
89 X = -6248599
94
Y = -7021418
64 feet Y = -2210180
52 meter
Z = -4819741
63 Z = -1499489
67
XDOT = 9100
363144 XDOT = 2848
520775
YDOT = -13744
218969 feet/sec YDOT = -4157
801709 meter/sec
ZDOT = -18972
021310 ZDOT = -5769
015532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14298925
20 X = 4358312
40
Y = -16374499
45 feet Y = -4990947
43 meter
Z = -4947355
51 Z = -1507953
96
XDOT = 8029
563273 XDOT = 2447
410886
YDOT = 12699
532013 feet/sec YDOT = 3870
817357 meter/sec
ZDOT = -18913
856977 ZDOT = -5764
943607
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 13333
52932278
00016717 00000-0 10270-3 0 9097
2 25544 51
6508 9
1377 0001218 87
7766 272
3525 15
50652116 20355
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
52932278 = yrday
fracday
Element set: 909
Inclination: 51
6508 deg
RA of node: 9
1377 deg
Eccentricity:
0001218
Arg of perigee: 87
7766 deg
Mean anomaly: 272
3525 deg
Mean motion: 15
50652116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 306
Coasting Arc #11 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2013/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6185865
97 A = 6797749
92 meter
Y = 1980454
90 meter E =
0015257
Z = 1981729
53 I = 51
69143
XDOT = -3145
101674 Wp = 69
50843
YDOT = 4209
455837 meter/sec RA = 3
80529 deg
ZDOT = 5580
924003 TA = 312
32470
MA = 312
45386
Ha = 226
954 n
mi
Hp = 219
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20294835
88 X = 6153633
41
Y = 6497555
45 feet Y = 2049448
89 meter
Z = 6501737
30 Z = 2011702
39
XDOT = -10318
575046 XDOT = -3219
050229
YDOT = 13810
550646 feet/sec YDOT = 4173
871616 meter/sec
ZDOT = 18310
118120 ZDOT = 5565
465575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13411052
56 X = -4087688
82
Y = 16510357
21 feet Y = 5032356
88 meter
Z = 6627439
33 Z = 2020043
51
XDOT = -7875
448330 XDOT = -2400
436651
YDOT = -13758
811850 feet/sec YDOT = -4193
685852 meter/sec
ZDOT = 18244
370154 ZDOT = 5560
884023
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 13334
56046003
00016717 00000-0 10270-3 0 9106
2 25544 51
6497 4
0249 0001394 84
3035 275
8275 15
50646946 20513
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
56046003 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 4
0249 deg
Eccentricity:
0001394
Arg of perigee: 84
3035 deg
Mean anomaly: 275
8275 deg
Mean motion: 15
50646946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 293
Coasting Arc #12 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2013/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6027581
00 A = 6796529
86 meter
Y = -1872734
38 meter E =
0006266
Z = -2520069
09 I = 51
65773
XDOT = 3531
716706 Wp = 121
35047
YDOT = -4259
593937 meter/sec RA = 358
85076 deg
ZDOT = -5294
768507 TA = 86
86362
MA = 86
79193
Ha = 226
824 n
mi
Hp = 219
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19775528
23 X = -5993949
60
Y = -6144141
68 feet Y = -1939950
42 meter
Z = -8267943
20 Z = -2549269
63
XDOT = 11586
997067 XDOT = 3604
807072
YDOT = -13975
045726 feet/sec YDOT = -4219
691012 meter/sec
ZDOT = -17371
287752 ZDOT = -5277
434100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12609681
50 X = 3843430
92
Y = -16363917
79 feet Y = -4987722
14 meter
Z = -8390411
51 Z = -2557397
43
XDOT = 7854
180563 XDOT = 2393
954236
YDOT = 14900
009372 feet/sec YDOT = 4541
522857 meter/sec
ZDOT = -17297
638706 ZDOT = -5272
320278
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 13335
52712942
00016717 00000-0 10270-3 0 9116
2 25544 51
6503 359
2311 0001292 91
8725 268
2574 15
50706763 20660
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
52712942 = yrday
fracday
Element set: 911
Inclination: 51
6503 deg
RA of node: 359
2311 deg
Eccentricity:
0001292
Arg of perigee: 91
8725 deg
Mean anomaly: 268
2574 deg
Mean motion: 15
50706763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 300
Coasting Arc #13 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2013/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5828705
66 A = 6795358
83 meter
Y = 1765635
55 meter E =
0014491
Z = 2999764
13 I = 51
62187
XDOT = -3885
412609 Wp = 83
77886
YDOT = 4366
582880 meter/sec RA = 353
89285 deg
ZDOT = 4960
344662 TA = 310
52950
MA = 310
65562
Ha = 226
815 n
mi
Hp = 219
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19123050
06 X = 5793956
39
Y = 5792767
57 feet Y = 1830621
29 meter
Z = 9841745
84 Z = 3027995
77
XDOT = -12747
416695 XDOT = -3958
048414
YDOT = 14326
059318 feet/sec YDOT = 4322
727151 meter/sec
ZDOT = 16274
096659 ZDOT = 4941
293261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11775701
78 X = -3589233
90
Y = 16069701
01 feet Y = 4898044
87 meter
Z = 9960156
51 Z = 3035855
71
XDOT = -8095
773421 XDOT = -2467
591739
YDOT = -16007
559783 feet/sec YDOT = -4879
104222 meter/sec
ZDOT = 16193
204724 ZDOT = 4935
688800
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 13336
55822555
00016717 00000-0 10270-3 0 9123
2 25544 51
6490 354
1176 0001427 90
1237 270
0077 15
50722200 20829
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
55822555 = yrday
fracday
Element set: 912
Inclination: 51
6490 deg
RA of node: 354
1176 deg
Eccentricity:
0001427
Arg of perigee: 90
1237 deg
Mean anomaly: 270
0077 deg
Mean motion: 15
50722200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 276
Coasting Arc #14 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2013/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5573242
40 A = 6793898
15 meter
Y = -1726749
06 meter E =
0006431
Z = -3486454
25 I = 51
58704
XDOT = 4225
562631 Wp = 87
19319
YDOT = -4492
287999 meter/sec RA = 348
93127 deg
ZDOT = -4536
768768 TA = 133
69931
MA = 133
64601
Ha = 226
755 n
mi
Hp = 219
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18284916
01 X = -5536582
79
Y = -5665187
21 feet Y = -1788867
27 meter
Z = -11438498
19 Z = -3513440
09
XDOT = 13863
394460 XDOT = 4297
521049
YDOT = -14738
477687 feet/sec YDOT = -4444
632257 meter/sec
ZDOT = -14884
411969 ZDOT = -4516
066741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11109697
25 X = 3386235
72
Y = -15505003
04 feet Y = -4725924
93 meter
Z = -11551677
29 Z = -3520951
24
XDOT = 8468
611221 XDOT = 2581
232700
YDOT = 17075
015225 feet/sec YDOT = 5204
464640 meter/sec
ZDOT = -14796
553198 ZDOT = -4509
989415
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 13337
52485760
00016717 00000-0 10270-3 0 9135
2 25544 51
6492 349
3233 0001335 95
4385 264
6918 15
50763249 20978
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
52485760 = yrday
fracday
Element set: 913
Inclination: 51
6492 deg
RA of node: 349
3233 deg
Eccentricity:
0001335
Arg of perigee: 95
4385 deg
Mean anomaly: 264
6918 deg
Mean motion: 15
50763249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 327
Coasting Arc #15 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2013/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5284450
42 A = 6792500
94 meter
Y = 1705501
73 meter E =
0012440
Z = 3902879
15 I = 51
55163
XDOT = -4521
893951 Wp = 98
78693
YDOT = 4663
275455 meter/sec RA = 343
96609 deg
ZDOT = 4071
827208 TA = 308
45590
MA = 308
56747
Ha = 226
654 n
mi
Hp = 219
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17337435
76 X = 5246027
07
Y = 5595478
12 feet Y = 1764380
57 meter
Z = 12804721
62 Z = 3928457
61
XDOT = -14835
610077 XDOT = -4593
483654
YDOT = 15299
460155 feet/sec YDOT = 4612
308050 meter/sec
ZDOT = 13359
013151 ZDOT = 4049
686662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10489745
89 X = -3197274
55
Y = 14802119
61 feet Y = 4511686
06 meter
Z = 12911988
09 Z = 3935573
97
XDOT = -9074
232160 XDOT = -2765
825962
YDOT = -18038
636153 feet/sec YDOT = -5498
176299 meter/sec
ZDOT = 13265
072857 ZDOT = 4043
194207
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 13338
55591287
00016717 00000-0 10270-3 0 9142
2 25544 51
6483 344
2093 0001371 95
2806 264
8501 15
50791658 21136
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
55591287 = yrday
fracday
Element set: 914
Inclination: 51
6483 deg
RA of node: 344
2093 deg
Eccentricity:
0001371
Arg of perigee: 95
2806 deg
Mean anomaly: 264
8501 deg
Mean motion: 15
50791658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 312
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