[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 2008)
---------------------------------------
Vector Time (GMT): 2013/331/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -708578
75 A = 6788644
77 meter
Y = -4429451
76 meter E =
0014387
Z = -5108426
82 I = 51
74139
XDOT = 7404
130147 Wp = 76
61339
YDOT = 826
435157 meter/sec RA = 17
00970 deg
ZDOT = -1744
494531 TA = 176
51270
MA = 176
50266
Ha = 226
943 n
mi
Hp = 219
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2324733
42 X = -634179
20
Y = -14532322
05 feet Y = -4436959
55 meter
Z = -16759930
52 Z = -5111688
37
XDOT = 24291
765574 XDOT = 7402
812894
YDOT = 2711
401435 feet/sec YDOT = 909
225491 meter/sec
ZDOT = -5723
407255 ZDOT = -1708
528530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3857570
25 X = -1175787
41
Y = -14187232
55 feet Y = -4324268
48 meter
Z = -16772883
62 Z = -5112374
93
XDOT = 23442
860960 XDOT = 7145
384021
YDOT = 210
162641 feet/sec YDOT = 64
057573 meter/sec
ZDOT = -5572
278534 ZDOT = -1698
430497
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
85366743
00016717 00000-0 10270-3 0 9000
2 25544 51
6500 17
4513 0001036 75
0844 285
0421 15
50585904 20093
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
85366743 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 17
4513 deg
Eccentricity:
0001036
Arg of perigee: 75
0844 deg
Mean anomaly: 285
0421 deg
Mean motion: 15
50585904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 277
Coasting Arc #2 (Orbit 2024)
---------------------------------------
Vector Time (GMT): 2013/332/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 420914
58 A = 6787989
26 meter
Y = 4308243
56 meter E =
0004509
Z = 5225428
96 I = 51
70980
XDOT = -7547
262722 Wp = 114
99425
YDOT = -674
275200 meter/sec RA = 12
05431 deg
ZDOT = 1161
219136 TA = 323
86272
MA = 323
89318
Ha = 226
835 n
mi
Hp = 219
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1380953
36 X = 347323
35
Y = 14134657
33 feet Y = 4312538
98 meter
Z = 17143795
80 Z = 5227295
04
XDOT = -24761
360636 XDOT = -7544
802892
YDOT = -2212
188977 feet/sec YDOT = -758
659753 meter/sec
ZDOT = 3809
774068 ZDOT = 1124
560459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3111026
63 X = 948240
92
Y = 13848233
72 feet Y = 4220941
64 meter
Z = 17150896
20 Z = 5227593
16
XDOT = -23851
248302 XDOT = -7269
860482
YDOT = 819
907060 feet/sec YDOT = 249
907672 meter/sec
ZDOT = 3655
714229 ZDOT = 1114
261697
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
88485484
00016717 00000-0 10270-3 0 9019
2 25544 51
6500 12
3392 0000879 78
6968 281
4282 15
50619944 20257
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
88485484 = yrday
fracday
Element set: 901
Inclination: 51
6500 deg
RA of node: 12
3392 deg
Eccentricity:
0000879
Arg of perigee: 78
6968 deg
Mean anomaly: 281
4282 deg
Mean motion: 15
50619944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2025
Checksum: 320
Coasting Arc #3 (Orbit 2039)
---------------------------------------
Vector Time (GMT): 2013/333/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -104581
24 A = 6787712
81 meter
Y = -4242875
41 meter E =
0015765
Z = -5310884
46 I = 51
67887
XDOT = 7614
156170 Wp = 85
09315
YDOT = 506
183903 meter/sec RA = 7
09533 deg
ZDOT = -554
434077 TA = 179
60778
MA = 179
60655
Ha = 226
921 n
mi
Hp = 219
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -343114
30 X = -31329
28
Y = -13920194
92 feet Y = -4243635
20 meter
Z = -17424161
61 Z = -5311214
69
XDOT = 24980
827328 XDOT = 7610
623352
YDOT = 1660
708342 feet/sec YDOT = 591
310506 meter/sec
ZDOT = -1819
009440 ZDOT = -517
452941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2288933
22 X = -697666
85
Y = -13734182
25 feet Y = -4186178
75 meter
Z = -17424809
46 Z = -5311081
92
XDOT = 23961
220584 XDOT = 7303
380034
YDOT = -1883
203735 feet/sec YDOT = -574
000499 meter/sec
ZDOT = -1663
571830 ZDOT = -507
056694
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
85158889
00016717 00000-0 10270-3 0 9024
2 25544 51
6506 7
5457 0001057 78
3234 281
8035 15
50607360 20409
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
85158889 = yrday
fracday
Element set: 902
Inclination: 51
6506 deg
RA of node: 7
5457 deg
Eccentricity:
0001057
Arg of perigee: 78
3234 deg
Mean anomaly: 281
8035 deg
Mean motion: 15
50607360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 297
Coasting Arc #4 (Orbit 2055)
---------------------------------------
Vector Time (GMT): 2013/334/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -222991
31 A = 6787509
59 meter
Y = 4204662
40 meter E =
0003323
Z = 5320812
00 I = 51
64747
XDOT = -7658
384891 Wp = 82
88674
YDOT = -331
703234 meter/sec RA = 2
13467 deg
ZDOT = -58
402100 TA = 7
67244
MA = 7
66735
Ha = 226
821 n
mi
Hp = 219
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -731598
78 X = -295839
86
Y = 13794824
14 feet Y = 4201761
19 meter
Z = 17456732
28 Z = 5319551
95
XDOT = -25125
934682 XDOT = -7653
822809
YDOT = -1088
265205 feet/sec YDOT = -417
318660 meter/sec
ZDOT = -191
607940 ZDOT = -95
595642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1443974
88 X = 440123
54
Y = 13746203
65 feet Y = 4189842
87 meter
Z = 17450694
35 Z = 5318971
64
XDOT = -23957
884115 XDOT = -7302
363078
YDOT = 2960
207843 feet/sec YDOT = 902
271350 meter/sec
ZDOT = -347
963777 ZDOT = -106
059359
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
88276204
00016717 00000-0 10270-3 0 9031
2 25544 51
6502 2
4332 0000903 79
2074 280
9179 15
50644255 20562
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
88276204 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 2
4332 deg
Eccentricity:
0000903
Arg of perigee: 79
2074 deg
Mean anomaly: 280
9179 deg
Mean motion: 15
50644255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2056
Checksum: 287
Coasting Arc #5 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2013/335/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 555032
10 A = 6787738
87 meter
Y = -4226987
32 meter E =
0015580
Z = -5295420
67 I = 51
61765
XDOT = 7619
885105 Wp = 94
14935
YDOT = 157
586738 meter/sec RA = 357
17109 deg
ZDOT = 673
490091 TA = 182
29452
MA = 182
30168
Ha = 226
882 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1820971
46 X = 627982
24
Y = -13868068
62 feet Y = -4220372
31 meter
Z = -17373427
38 Z = -5292547
43
XDOT = 24999
623049 XDOT = 7614
284898
YDOT = 517
016858 feet/sec YDOT = 242
765782 meter/sec
ZDOT = 2209
613160 ZDOT = 710
494029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -622802
59 X = -189830
23
Y = -13989175
19 feet Y = -4263900
60 meter
Z = -17360597
27 Z = -5291510
05
XDOT = 23643
424371 XDOT = 7206
515748
YDOT = -3985
330376 feet/sec YDOT = -1214
728699 meter/sec
ZDOT = 2365
199608 ZDOT = 720
912841
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
84948257
00016717 00000-0 10270-3 0 9043
2 25544 51
6507 357
6396 0001031 80
8072 279
3196 15
50628053 20717
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
84948257 = yrday
fracday
Element set: 904
Inclination: 51
6507 deg
RA of node: 357
6396 deg
Eccentricity:
0001031
Arg of perigee: 80
8072 deg
Mean anomaly: 279
3196 deg
Mean motion: 15
50628053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 314
Coasting Arc #6 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2013/336/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -888719
99 A = 6788028
75 meter
Y = 4277124
39 meter E =
0005175
Z = 5192218
10 I = 51
58791
XDOT = -7556
386718 Wp = 58
91339
YDOT = 1
236188 meter/sec RA = 352
20575 deg
ZDOT = -1290
829986 TA = 43
51665
MA = 43
47583
Ha = 226
801 n
mi
Hp = 219
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2915747
98 X = -961704
53
Y = 14032560
35 feet Y = 4266777
59 meter
Z = 17034836
30 Z = 5187723
83
XDOT = -24791
295005 XDOT = -7549
568311
YDOT = 4
055736 feet/sec YDOT = -83
225891 meter/sec
ZDOT = -4235
006517 ZDOT = -1327
522342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -174895
72 X = -53308
22
Y = 14354551
33 feet Y = 4375267
25 meter
Z = 17015177
09 Z = 5186225
98
XDOT = -23223
823959 XDOT = -7078
621543
YDOT = 4933
807652 feet/sec YDOT = 1503
824572 meter/sec
ZDOT = -4389
311037 ZDOT = -1337
862004
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
88064156
00016717 00000-0 10270-3 0 9056
2 25544 51
6504 352
5266 0000911 79
3738 280
7515 15
50668723 20878
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
88064156 = yrday
fracday
Element set: 905
Inclination: 51
6504 deg
RA of node: 352
5266 deg
Eccentricity:
0000911
Arg of perigee: 79
3738 deg
Mean anomaly: 280
7515 deg
Mean motion: 15
50668723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 318
Coasting Arc #7 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2013/337/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1201797
64 A = 6788743
64 meter
Y = -4385090
75 meter E =
0013804
Z = -5053745
73 I = 51
56002
XDOT = 7414
056005 Wp = 102
44626
YDOT = -142
527257 meter/sec RA = 347
23831 deg
ZDOT = 1888
221716 TA = 185
90897
MA = 185
92527
Ha = 226
826 n
mi
Hp = 219
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3942905
64 X = 1275293
41
Y = -14386780
67 feet Y = -4371240
01 meter
Z = -16580530
62 Z = -5047729
38
XDOT = 24324
330725 XDOT = 7405
926157
YDOT = -467
609111 feet/sec YDOT = -59
664219 meter/sec
ZDOT = 6194
953137 ZDOT = 1924
219230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 851934
56 X = 259669
65
Y = -14921942
35 feet Y = -4548208
03 meter
Z = -16554449
64 Z = -5045796
25
XDOT = 22526
480263 XDOT = 6866
071184
YDOT = -5749
236844 feet/sec YDOT = -1752
367390 meter/sec
ZDOT = 6346
363047 ZDOT = 1934
371457
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
84734852
00016717 00000-0 10270-3 0 9061
2 25544 51
6508 347
7327 0000962 82
2631 277
8630 15
50648713 21027
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
84734852 = yrday
fracday
Element set: 906
Inclination: 51
6508 deg
RA of node: 347
7327 deg
Eccentricity:
0000962
Arg of perigee: 82
2631 deg
Mean anomaly: 277
8630 deg
Mean motion: 15
50648713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 312
Coasting Arc #8 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2013/338/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1506983
23 A = 6789486
32 meter
Y = 4515746
92 meter E =
0008081
Z = 4836180
22 I = 51
53310
XDOT = -7248
658438 Wp = 62
09847
YDOT = 246
953402 meter/sec RA = 342
26955 deg
ZDOT = -2482
436147 TA = 52
36869
MA = 52
29538
Ha = 226
769 n
mi
Hp = 219
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4944170
70 X = -1580860
32
Y = 14815442
64 feet Y = 4498481
30 meter
Z = 15866733
01 Z = 4828680
40
XDOT = -23781
687790 XDOT = -7238
822103
YDOT = 810
214575 feet/sec YDOT = 165
949543 meter/sec
ZDOT = -8144
475547 ZDOT = -2517
625801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1465197
88 X = -446592
31
Y = 15582703
57 feet Y = 4749608
05 meter
Z = 15834390
59 Z = 4826322
25
XDOT = -21757
854323 XDOT = -6631
793998
YDOT = 6403
604160 feet/sec YDOT = 1951
818548 meter/sec
ZDOT = -8292
509527 ZDOT = -2527
556904
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
87849349
00016717 00000-0 10270-3 0 9074
2 25544 51
6509 342
6194 0000900 79
2280 280
8972 15
50692331 21187
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
87849349 = yrday
fracday
Element set: 907
Inclination: 51
6509 deg
RA of node: 342
6194 deg
Eccentricity:
0000900
Arg of perigee: 79
2280 deg
Mean anomaly: 280
8972 deg
Mean motion: 15
50692331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 325
Coasting Arc #9 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2013/339/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1768757
24 A = 6790581
70 meter
Y = -4694240
79 meter E =
0010740
Z = -4587401
25 I = 51
50751
XDOT = 7018
508924 Wp = 107
67795
YDOT = -319
337154 meter/sec RA = 337
29933 deg
ZDOT = 3035
582333 TA = 192
75588
MA = 192
78308
Ha = 226
766 n
mi
Hp = 219
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5803009
32 X = 1843402
22
Y = -15401052
46 feet Y = -4674043
65 meter
Z = -15050529
04 Z = -4578627
88
XDOT = 23026
604081 XDOT = 7006
812122
YDOT = -1047
694074 feet/sec YDOT = -240
917391 meter/sec
ZDOT = 9959
259624 ZDOT = 3069
649251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1878106
19 X = 572446
77
Y = -16385184
07 feet Y = -4994204
10 meter
Z = -15012801
82 Z = -4575901
99
XDOT = 20786
308175 XDOT = 6335
666732
YDOT = -6865
733091 feet/sec YDOT = -2092
675446 meter/sec
ZDOT = 10102
586646 ZDOT = 3079
268410
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 13339
84518703
00016717 00000-0 10270-3 0 9080
2 25544 51
6510 337
8255 0000876 83
7368 276
3883 15
50669147 21339
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
84518703 = yrday
fracday
Element set: 908
Inclination: 51
6510 deg
RA of node: 337
8255 deg
Eccentricity:
0000876
Arg of perigee: 83
7368 deg
Mean anomaly: 276
3883 deg
Mean motion: 15
50669147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 333
Coasting Arc #10 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2013/340/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2015030
60 A = 6791650
62 meter
Y = 4884745
02 meter E =
0010879
Z = 4259661
68 I = 51
48368
XDOT = -6771
616081 Wp = 73
85992
YDOT = 335
674114 meter/sec RA = 332
32852 deg
ZDOT = -3577
663240 TA = 52
80697
MA = 52
70771
Ha = 226
724 n
mi
Hp = 219
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6610992
80 X = -2090195
42
Y = 16026066
34 feet Y = 4861791
09 meter
Z = 13975267
97 Z = 4249690
62
XDOT = -22216
588191 XDOT = -6757
487069
YDOT = 1101
293025 feet/sec YDOT = 260
028844 meter/sec
ZDOT = -11737
740288 ZDOT = -3610
524785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2202596
81 X = -671351
51
Y = 17230288
59 feet Y = 5251791
96 meter
Z = 13932475
19 Z = 4246618
44
XDOT = -19799
876487 XDOT = -6035
002353
YDOT = 7100
053799 feet/sec YDOT = 2164
096398 meter/sec
ZDOT = -11876
000845 ZDOT = -3619
805058
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 13340
87631808
00016717 00000-0 10270-3 0 9098
2 25544 51
6513 332
7125 0000867 79
4981 280
6268 15
50713963 21493
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
87631808 = yrday
fracday
Element set: 909
Inclination: 51
6513 deg
RA of node: 332
7125 deg
Eccentricity:
0000867
Arg of perigee: 79
4981 deg
Mean anomaly: 280
6268 deg
Mean motion: 15
50713963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 325
Coasting Arc #11 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2013/341/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2200460
01 A = 6792952
88 meter
Y = -5107124
28 meter E =
0007174
Z = -3908587
99 I = 51
46031
XDOT = 6482
246579 Wp = 103
11171
YDOT = -311
159396 meter/sec RA = 327
35632 deg
ZDOT = 4060
670070 TA = 209
56703
MA = 209
60761
Ha = 226
711 n
mi
Hp = 219
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7219356
98 X = 2276392
31
Y = -16755657
10 feet Y = -5082092
57 meter
Z = -12823451
40 Z = -3897714
19
XDOT = 21267
213187 XDOT = 6465
518635
YDOT = -1020
864161 feet/sec YDOT = -238
764529 meter/sec
ZDOT = 13322
408367 ZDOT = 4092
119571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2276926
06 X = 694007
06
Y = -18135057
07 feet Y = -5527565
40 meter
Z = -12776829
75 Z = -3894377
71
XDOT = 18713
843494 XDOT = 5703
979497
YDOT = -7118
823960 feet/sec YDOT = -2169
817543 meter/sec
ZDOT = 13454
724092 ZDOT = 4100
999903
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 13341
84299827
00016717 00000-0 10270-3 0 9109
2 25544 51
6508 327
9185 0000793 86
6814 273
4428 15
50687898 21644
Satellite: ISS
Catalog Number: 25544
Epoch time: 13341
84299827 = yrday
fracday
Element set: 910
Inclination: 51
6508 deg
RA of node: 327
9185 deg
Eccentricity:
0000793
Arg of perigee: 86
6814 deg
Mean anomaly: 273
4428 deg
Mean motion: 15
50687898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 347
Coasting Arc #12 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2013/342/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2366444
30 A = 6794144
34 meter
Y = 5326256
07 meter E =
0013095
Z = 3480638
75 I = 51
43939
XDOT = -6186
411267 Wp = 88
23896
YDOT = 216
266310 meter/sec RA = 322
38411 deg
ZDOT = -4521
851625 TA = 50
78823
MA = 50
67204
Ha = 226
665 n
mi
Hp = 219
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7763924
88 X = -2442735
81
Y = 17474593
40 feet Y = 5299366
28 meter
Z = 11419418
49 Z = 3468957
67
XDOT = -20296
624893 XDOT = -6166
403867
YDOT = 709
535137 feet/sec YDOT = 147
197959 meter/sec
ZDOT = -14835
471211 ZDOT = -4551
856074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2261469
01 X = -689295
76
Y = 19017524
13 feet Y = 5796541
35 meter
Z = 11369370
99 Z = 3465384
28
XDOT = -17684
573655 XDOT = -5390
258050
YDOT = 6871
543356 feet/sec YDOT = 2094
446415 meter/sec
ZDOT = -14961
689805 ZDOT = -4560
323053
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 13342
87411525
00016717 00000-0 10270-3 0 9115
2 25544 51
6510 322
8055 0000814 81
2768 278
8476 15
50733312 21803
Satellite: ISS
Catalog Number: 25544
Epoch time: 13342
87411525 = yrday
fracday
Element set: 911
Inclination: 51
6510 deg
RA of node: 322
8055 deg
Eccentricity:
0000814
Arg of perigee: 81
2768 deg
Mean anomaly: 278
8476 deg
Mean motion: 15
50733312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 292
Coasting Arc #13 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2013/343/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2461813
60 A = 6795437
42 meter
Y = -5557661
60 meter E =
0005208
Z = -3040517
65 I = 51
41828
XDOT = 5875
180784 Wp = 73
17025
YDOT = -79
427301 meter/sec RA = 317
41017 deg
ZDOT = 4910
611980 TA = 251
92034
MA = 251
97708
Ha = 226
666 n
mi
Hp = 219
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8076816
26 X = 2538547
70
Y = -18233797
90 feet Y = -5529702
89 meter
Z = -9975451
61 Z = -3028372
14
XDOT = 19275
527508 XDOT = 5851
777793
YDOT = -260
588258 feet/sec YDOT = -13
858299 meter/sec
ZDOT = 16110
931692 ZDOT = 4939
096331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1983434
66 X = 604550
88
Y = -19869769
54 feet Y = -6056305
76 meter
Z = -9923418
12 Z = -3024657
84
XDOT = 16668
944961 XDOT = 5080
694424
YDOT = -6428
114175 feet/sec YDOT = -1959
289201 meter/sec
ZDOT = 16230
730198 ZDOT = 4947
126564
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 13343
84078202
00016717 00000-0 10270-3 0 9125
2 25544 51
6497 318
0110 0000732 92
3528 267
7707 15
50704309 21956
Satellite: ISS
Catalog Number: 25544
Epoch time: 13343
84078202 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 318
0110 deg
Eccentricity:
0000732
Arg of perigee: 92
3528 deg
Mean anomaly: 267
7707 deg
Mean motion: 15
50704309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 295
Coasting Arc #14 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2013/344/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2538822
73 A = 6796500
31 meter
Y = 5767726
70 meter E =
0014380
Z = 2528189
53 I = 51
40029
XDOT = -5570
564967 Wp = 103
21510
YDOT = -134
912760 meter/sec RA = 312
43667 deg
ZDOT = -5264
114790 TA = 48
33248
MA = 48
20947
Ha = 226
599 n
mi
Hp = 219
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8329470
88 X = -2615411
37
Y = 18922987
85 feet Y = 5738907
64 meter
Z = 8294585
08 Z = 2515670
25
XDOT = -18276
131781 XDOT = -5543
070513
YDOT = -442
627166 feet/sec YDOT = -197
052455 meter/sec
ZDOT = -17270
717815 ZDOT = -5291
109491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1641696
04 X = -500388
95
Y = 20631317
83 feet Y = 6288425
67 meter
Z = 8240949
87 Z = 2511841
52
XDOT = -15785
731370 XDOT = -4811
490922
YDOT = 5716
953570 feet/sec YDOT = 1742
527448 meter/sec
ZDOT = -17384
211807 ZDOT = -5298
707759
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 13344
87188469
00016717 00000-0 10270-3 0 9137
2 25544 51
6498 312
8978 0000750 85
7600 274
3637 15
50751996 22117
Satellite: ISS
Catalog Number: 25544
Epoch time: 13344
87188469 = yrday
fracday
Element set: 913
Inclination: 51
6498 deg
RA of node: 312
8978 deg
Eccentricity:
0000750
Arg of perigee: 85
7600 deg
Mean anomaly: 274
3637 deg
Mean motion: 15
50751996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 338
Coasting Arc #15 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2013/345/20:01:48
169
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2544177
90 A = 6797560
14 meter
Y = -5969820
86 meter E =
0007111
Z = -2017379
41 I = 51
38185
XDOT = 5278
348169 Wp = 44
96306
YDOT = 383
961780 meter/sec RA = 307
46112 deg
ZDOT = 5537
386063 TA = 292
70652
MA = 292
78168
Ha = 226
631 n
mi
Hp = 219
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8347040
35 X = 2620544
64
Y = -19586026
45 feet Y = -5940943
17 meter
Z = -6618698
87 Z = -2004834
68
XDOT = 17317
415254 XDOT = 5246
762958
YDOT = 1259
717126 feet/sec YDOT = 442
810790 meter/sec
ZDOT = 18167
277111 ZDOT = 5562
951332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1063010
76 X = 324005
68
Y = -21280611
62 feet Y = -6486330
42 meter
Z = -6564927
01 Z = -2000989
75
XDOT = 15019
112899 XDOT = 4577
825612
YDOT = -4870
126429 feet/sec YDOT = -1484
414536 meter/sec
ZDOT = 18274
715441 ZDOT = 5570
133267
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 13345
83853808
00016717 00000-0 10270-3 0 9141
2 25544 51
6482 308
1028 0000717 101
3514 258
7717 15
50720041 22264
Satellite: ISS
Catalog Number: 25544
Epoch time: 13345
83853808 = yrday
fracday
Element set: 914
Inclination: 51
6482 deg
RA of node: 308
1028 deg
Eccentricity:
0000717
Arg of perigee: 101
3514 deg
Mean anomaly: 258
7717 deg
Mean motion: 15
50720041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 289
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