[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 18th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 3275)
---------------------------------------
Vector Time (GMT): 2014/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6137653
49 A = 6800032
85 meter
Y = 2887704
25 meter E =
0014824
Z = -364920
38 I = 51
50667
XDOT = -1749
699648 Wp = 139
33032
YDOT = -4456
464372 meter/sec RA = 332
35143 deg
ZDOT = -5984
974782 TA = 44
60541
MA = 44
48622
Ha = 227
754 n
mi
Hp = 219
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20136658
42 X = -6167715
64
Y = 9474095
32 feet Y = 2818900
95 meter
Z = -1197245
34 Z = -394809
10
XDOT = -5740
484410 XDOT = -1670
663799
YDOT = -14620
946101 feet/sec YDOT = -4475
589403 meter/sec
ZDOT = -19635
744035 ZDOT = -5993
281961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22017773
29 X = -6711017
30
Y = -3184645
22 feet Y = -970679
86 meter
Z = -1323852
43 Z = -403510
22
XDOT = 3136
688813 XDOT = 956
062750
YDOT = -13692
389553 feet/sec YDOT = -4173
440336 meter/sec
ZDOT = -19670
047451 ZDOT = -5995
430463
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 14048
53149692
00016717 00000-0 10270-3 0 9003
2 25544 51
6497 332
7600 0003620 146
1969 213
9413 15
50430275 32765
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
53149692 = yrday
fracday
Element set: 900
Inclination: 51
6497 deg
RA of node: 332
7600 deg
Eccentricity:
0003620
Arg of perigee: 146
1969 deg
Mean anomaly: 213
9413 deg
Mean motion: 15
50430275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 302
Coasting Arc #2 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2014/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6011320
30 A = 6799671
30 meter
Y = -3055569
56 meter E =
0013570
Z = 836734
98 I = 51
47830
XDOT = 1516
037484 Wp = 69
01312
YDOT = 4623
245340 meter/sec RA = 327
38690 deg
ZDOT = 5918
418088 TA = 300
04242
MA = 300
17696
Ha = 227
662 n
mi
Hp = 219
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19722179
47 X = 6040977
05
Y = -10024834
50 feet Y = -2988181
21 meter
Z = 2745193
51 Z = 866009
14
XDOT = 4973
876260 XDOT = 1435
477223
YDOT = 15168
127756 feet/sec YDOT = 4639
748876 meter/sec
ZDOT = 19417
382180 ZDOT = 5925
586495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22006808
35 X = 6707675
18
Y = 2113217
89 feet Y = 644108
81 meter
Z = 2869225
34 Z = 874539
88
XDOT = -3890
508456 XDOT = -1185
826977
YDOT = 13800
019312 feet/sec YDOT = 4206
245886 meter/sec
ZDOT = 19446
854514 ZDOT = 5927
401256
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 14049
56276485
00016717 00000-0 10270-3 0 9019
2 25544 51
6492 327
6480 0003514 149
3099 210
8258 15
50467274 32920
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
56276485 = yrday
fracday
Element set: 901
Inclination: 51
6492 deg
RA of node: 327
6480 deg
Eccentricity:
0003514
Arg of perigee: 149
3099 deg
Mean anomaly: 210
8258 deg
Mean motion: 15
50467274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 323
Coasting Arc #3 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2014/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5864672
37 A = 6799106
42 meter
Y = 3149924
64 meter E =
0012117
Z = -1355835
66 I = 51
45168
XDOT = -1272
274353 Wp = 145
51628
YDOT = -4848
382896 meter/sec RA = 322
42006 deg
ZDOT = -5795
931762 TA = 49
26796
MA = 49
16281
Ha = 227
515 n
mi
Hp = 219
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19241051
08 X = -5892873
50
Y = 10334398
43 feet Y = 3084184
29 meter
Z = -4448279
73 Z = -1384393
98
XDOT = -4174
128454 XDOT = -1189
809575
YDOT = -15906
768030 feet/sec YDOT = -4862
149811 meter/sec
ZDOT = -19015
524153 ZDOT = -5801
911418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21781950
40 X = -6639138
48
Y = -1213747
15 feet Y = -369950
13 meter
Z = -4569298
06 Z = -1392722
05
XDOT = 4756
047816 XDOT = 1449
643374
YDOT = -14097
601447 feet/sec YDOT = -4296
948921 meter/sec
ZDOT = -19039
945285 ZDOT = -5803
375323
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 14050
52955880
00016717 00000-0 10270-3 0 9021
2 25544 51
6498 322
8550 0003578 154
6716 205
4611 15
50489659 33077
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
52955880 = yrday
fracday
Element set: 902
Inclination: 51
6498 deg
RA of node: 322
8550 deg
Eccentricity:
0003578
Arg of perigee: 154
6716 deg
Mean anomaly: 205
4611 deg
Mean motion: 15
50489659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 322
Coasting Arc #4 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2014/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5684959
04 A = 6798352
78 meter
Y = -3238629
14 meter E =
0014327
Z = 1828590
46 I = 51
42515
XDOT = 1081
912887 Wp = 80
11695
YDOT = 5093
242245 meter/sec RA = 317
45063 deg
ZDOT = 5621
796169 TA = 300
02189
MA = 300
16397
Ha = 227
426 n
mi
Hp = 219
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18651440
44 X = 5711868
96
Y = -10625423
68 feet Y = -3174905
65 meter
Z = 5999312
54 Z = 1856272
65
XDOT = 3549
582962 XDOT = 997
570018
YDOT = 16710
112353 feet/sec YDOT = 5104
869831 meter/sec
ZDOT = 18444
213153 ZDOT = 5626
846568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21430667
72 X = 6532067
52
Y = 284217
62 feet Y = 86629
53 meter
Z = 6116642
15 Z = 1864352
53
XDOT = -5495
896877 XDOT = -1675
149368
YDOT = 14581
570004 feet/sec YDOT = 4444
462537 meter/sec
ZDOT = 18464
675347 ZDOT = 5628
033046
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 14051
56078567
00016717 00000-0 10270-3 0 9035
2 25544 51
6493 317
7424 0003463 157
0598 203
0708 15
50527718 33231
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
56078567 = yrday
fracday
Element set: 903
Inclination: 51
6493 deg
RA of node: 317
7424 deg
Eccentricity:
0003463
Arg of perigee: 157
0598 deg
Mean anomaly: 203
0708 deg
Mean motion: 15
50527718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 310
Coasting Arc #5 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2014/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5495715
33 A = 6797377
88 meter
Y = 3241914
90 meter E =
0008873
Z = -2334916
39 I = 51
40049
XDOT = -895
816094 Wp = 144
93617
YDOT = -5380
524516 meter/sec RA = 312
47891 deg
ZDOT = -5379
417163 TA = 61
14963
MA = 61
06060
Ha = 227
253 n
mi
Hp = 219
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18030562
11 X = -5520216
50
Y = 10636203
75 feet Y = 3180321
11 meter
Z = -7660486
86 Z = -2361673
39
XDOT = -2939
029179 XDOT = -809
451982
YDOT = -17652
639489 feet/sec YDOT = -5390
059647 meter/sec
ZDOT = -17649
006439 ZDOT = -5383
558678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20888173
34 X = -6366715
23
Y = 404497
07 feet Y = 123290
71 meter
Z = -7773908
65 Z = -2369487
36
XDOT = 6258
688340 XDOT = 1907
648206
YDOT = -15235
841152 feet/sec YDOT = -4643
884383 meter/sec
ZDOT = -17665
589600 ZDOT = -5384
471710
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 14052
52754090
00016717 00000-0 10270-3 0 9045
2 25544 51
6499 312
9491 0003503 163
7937 196
3326 15
50549940 33381
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
52754090 = yrday
fracday
Element set: 904
Inclination: 51
6499 deg
RA of node: 312
9491 deg
Eccentricity:
0003503
Arg of perigee: 163
7937 deg
Mean anomaly: 196
3326 deg
Mean motion: 15
50549940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 320
Coasting Arc #6 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2014/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5285120
51 A = 6796286
96 meter
Y = -3229509
66 meter E =
0014063
Z = 2786798
07 I = 51
37679
XDOT = 771
479338 Wp = 93
71632
YDOT = 5675
686470 meter/sec RA = 307
50443 deg
ZDOT = 5091
046446 TA = 297
96509
MA = 298
10735
Ha = 227
158 n
mi
Hp = 219
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17339634
22 X = 5307303
55
Y = -10595504
13 feet Y = -3170283
84 meter
Z = 9143038
28 Z = 2812526
32
XDOT = 2531
100191 XDOT = 683
224739
YDOT = 18621
018604 feet/sec YDOT = 5683
820523 meter/sec
ZDOT = 16702
908289 ZDOT = 5094
579415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20243349
77 X = 6170173
01
Y = -1062043
48 feet Y = -323710
85 meter
Z = 9252114
64 Z = 2820044
54
XDOT = -6832
847845 XDOT = -2082
652023
YDOT = 16046
571667 feet/sec YDOT = 4890
995044 meter/sec
ZDOT = 16716
879703 ZDOT = 5095
304934
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 14053
55872712
00016717 00000-0 10270-3 0 9052
2 25544 51
6497 307
8360 0003375 165
4285 194
6963 15
50587996 33548
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
55872712 = yrday
fracday
Element set: 905
Inclination: 51
6497 deg
RA of node: 307
8360 deg
Eccentricity:
0003375
Arg of perigee: 165
4285 deg
Mean anomaly: 194
6963 deg
Mean motion: 15
50587996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 344
Coasting Arc #7 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2014/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5080241
73 A = 6795000
19 meter
Y = 3125095
53 meter E =
0006334
Z = -3255364
06 I = 51
35499
XDOT = -662
393446 Wp = 127
36247
YDOT = -5989
982772 meter/sec RA = 302
52784 deg
ZDOT = -4726
695203 TA = 90
47292
MA = 90
40033
Ha = 226
964 n
mi
Hp = 219
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16667459
76 X = -5098996
35
Y = 10252938
10 feet Y = 3068179
97 meter
Z = -10680328
27 Z = -3280088
60
XDOT = -2173
206843 XDOT = -572
402377
YDOT = -19652
174449 feet/sec YDOT = -5996
887174 meter/sec
ZDOT = -15507
530194 ZDOT = -4729
694067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19459111
44 X = -5931137
17
Y = 1421220
51 feet Y = 433188
01 meter
Z = -10785150
94 Z = -3287314
01
XDOT = 7343
822185 XDOT = 2238
397002
YDOT = -16969
829367 feet/sec YDOT = -5172
403991 meter/sec
ZDOT = -15519
202958 ZDOT = -4730
253062
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 14054
52544399
00016717 00000-0 10270-3 0 9068
2 25544 51
6500 303
0426 0003394 173
4367 186
6829 15
50614352 33690
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
52544399 = yrday
fracday
Element set: 906
Inclination: 51
6500 deg
RA of node: 303
0426 deg
Eccentricity:
0003394
Arg of perigee: 173
4367 deg
Mean anomaly: 186
6829 deg
Mean motion: 15
50614352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 312
Coasting Arc #8 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2014/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4868804
16 A = 6793718
28 meter
Y = -2999054
98 meter E =
0012773
Z = 3661465
22 I = 51
33502
XDOT = 616
019543 Wp = 109
34522
YDOT = 6298
098460 meter/sec RA = 297
54853 deg
ZDOT = 4323
004543 TA = 294
33282
MA = 294
46614
Ha = 226
868 n
mi
Hp = 219
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15973766
94 X = 4884192
46
Y = -9839419
22 feet Y = -2944522
66 meter
Z = 12012681
16 Z = 3685154
35
XDOT = 2021
061493 XDOT = 524
547563
YDOT = 20663
052691 feet/sec YDOT = 6304
475965 meter/sec
ZDOT = 14183
085772 ZDOT = 4325
774525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18618935
25 X = 5675051
46
Y = -1699307
54 feet Y = -517948
94 meter
Z = 12113113
29 Z = 3692076
93
XDOT = -7626
997906 XDOT = -2324
708962
YDOT = 17992
932512 feet/sec YDOT = 5484
245830 meter/sec
ZDOT = 14193
751578 ZDOT = 4326
255481
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 14055
55659007
00016717 00000-0 10270-3 0 9076
2 25544 51
6499 297
9292 0003265 174
5190 185
5998 15
50645662 33853
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
55659007 = yrday
fracday
Element set: 907
Inclination: 51
6499 deg
RA of node: 297
9292 deg
Eccentricity:
0003265
Arg of perigee: 174
5190 deg
Mean anomaly: 185
5998 deg
Mean motion: 15
50645662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 353
Coasting Arc #9 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2014/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4681003
86 A = 6792289
63 meter
Y = 2781984
19 meter E =
0006839
Z = -4065290
41 I = 51
31679
XDOT = -589
642215 Wp = 97
52365
YDOT = -6597
053963 meter/sec RA = 292
56707 deg
ZDOT = -3842
044586 TA = 132
50542
MA = 132
44763
Ha = 226
664 n
mi
Hp = 219
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15357624
22 X = -4692017
24
Y = 9127244
70 feet Y = 2729576
38 meter
Z = -13337566
95 Z = -4088056
54
XDOT = -1934
521702 XDOT = -497
165597
YDOT = -21643
877831 feet/sec YDOT = -6603
130883 meter/sec
ZDOT = -12605
133156 ZDOT = -3844
683919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17716387
11 X = -5399954
79
Y = 1646013
18 feet Y = 501704
82 meter
Z = -13434067
81 Z = -4094703
87
XDOT = 7781
299075 XDOT = 2371
739958
YDOT = -19036
666451 feet/sec YDOT = -5802
375934 meter/sec
ZDOT = -12615
211442 ZDOT = -3845
116448
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 14056
52326875
00016717 00000-0 10270-3 0 9089
2 25544 51
6495 293
1357 0003280 183
1456 176
9674 15
50683033 34004
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
52326875 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 293
1357 deg
Eccentricity:
0003280
Arg of perigee: 183
1456 deg
Mean anomaly: 176
9674 deg
Mean motion: 15
50683033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 317
Coasting Arc #10 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4502372
02 A = 6791031
90 meter
Y = -2542489
96 meter E =
0010615
Z = 4398839
07 I = 51
30145
XDOT = 618
686892 Wp = 126
65663
YDOT = 6875
499689 meter/sec RA = 287
58326 deg
ZDOT = 3328
895717 TA = 289
46869
MA = 289
58335
Ha = 226
567 n
mi
Hp = 220
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14771561
75 X = 4509100
42
Y = -8341502
48 feet Y = -2492103
59 meter
Z = 14431886
71 Z = 4420727
00
XDOT = 2029
812637 XDOT = 525
587187
YDOT = 22557
413678 feet/sec YDOT = 6881
897946 meter/sec
ZDOT = 10921
573876 ZDOT = 3331
674490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16819532
53 X = 5126593
52
Y = -1482287
33 feet Y = -451801
18 meter
Z = 14524641
26 Z = 4427110
66
XDOT = -7702
029206 XDOT = -2347
578502
YDOT = 20105
557888 feet/sec YDOT = 6128
174044 meter/sec
ZDOT = 10932
210935 ZDOT = 3332
137893
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 14057
55437480
00016717 00000-0 10270-3 0 9099
2 25544 51
6492 288
0222 0003170 184
2113 175
9012 15
50700965 34161
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55437480 = yrday
fracday
Element set: 909
Inclination: 51
6492 deg
RA of node: 288
0222 deg
Eccentricity:
0003170
Arg of perigee: 184
2113 deg
Mean anomaly: 175
9012 deg
Mean motion: 15
50700965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 294
Coasting Arc #11 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2014/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4365185
15 A = 6789697
77 meter
Y = 2221829
95 meter E =
0009671
Z = -4710596
97 I = 51
28778
XDOT = -664
277205 Wp = 87
25546
YDOT = -7115
309573 meter/sec RA = 282
59689 deg
ZDOT = -2744
931744 TA = 155
41112
MA = 155
36498
Ha = 226
378 n
mi
Hp = 220
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14321473
59 X = -4366823
70
Y = 7289468
35 feet Y = 2173006
03 meter
Z = -15454714
47 Z = -4731806
12
XDOT = -2179
387156 XDOT = -571
329164
YDOT = -23344
191511 feet/sec YDOT = -7122
218515 meter/sec
ZDOT = -9005
681576 ZDOT = -2747
932169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15952321
45 X = -4862267
58
Y = 989710
71 feet Y = 301663
82 meter
Z = -15544551
04 Z = -4737979
16
XDOT = 7464
643716 XDOT = 2275
223405
YDOT = -21081
831313 feet/sec YDOT = -6425
742184 meter/sec
ZDOT = -9017
232962 ZDOT = -2748
452607
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 14058
52101520
00016717 00000-0 10270-3 0 9102
2 25544 51
6480 283
2279 0003196 192
4066 167
7007 15
50752167 34314
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
52101520 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 283
2279 deg
Eccentricity:
0003196
Arg of perigee: 192
4066 deg
Mean anomaly: 167
7007 deg
Mean motion: 15
50752167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 290
Coasting Arc #12 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2014/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251215
36 A = 6788702
95 meter
Y = -1883473
91 meter E =
0007840
Z = 4944534
87 I = 51
27836
XDOT = 749
926224 Wp = 144
84024
YDOT = 7321
995561 meter/sec RA = 277
60904 deg
ZDOT = 2136
330327 TA = 284
18309
MA = 284
27018
Ha = 226
265 n
mi
Hp = 220
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13947556
97 X = 4247942
40
Y = -6179376
36 feet Y = -1835951
80 meter
Z = 16222227
27 Z = 4965178
49
XDOT = 2460
387874 XDOT = 657
616913
YDOT = 24022
295149 feet/sec YDOT = 7329
865847 meter/sec
ZDOT = 7008
957766 ZDOT = 2139
748180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15156783
90 X = 4619787
73
Y = -384509
49 feet Y = -117198
49 meter
Z = 16309621
37 Z = 4971172
59
XDOT = -7026
273348 XDOT = -2141
608116
YDOT = 22002
374168 feet/sec YDOT = 6706
323647 meter/sec
ZDOT = 7022
255692 ZDOT = 2140
383535
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 14059
55208067
00016717 00000-0 10270-3 0 9111
2 25544 51
6477 278
1140 0003127 194
1482 165
9582 15
50757105 34477
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
55208067 = yrday
fracday
Element set: 911
Inclination: 51
6477 deg
RA of node: 278
1140 deg
Eccentricity:
0003127
Arg of perigee: 194
1482 deg
Mean anomaly: 165
9582 deg
Mean motion: 15
50757105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 312
Coasting Arc #13 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2014/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4193024
49 A = 6787728
41 meter
Y = 1482728
42 meter E =
0012341
Z = -5138378
41 I = 51
27085
XDOT = -840
121198 Wp = 91
30029
YDOT = -7464
097155 meter/sec RA = 272
61838 deg
ZDOT = -1471
633410 TA = 164
45037
MA = 164
41242
Ha = 226
115 n
mi
Hp = 220
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13756642
02 X = -4184332
92
Y = 4864594
56 feet Y = 1435887
21 meter
Z = -16858196
89 Z = -5158726
25
XDOT = -2756
303144 XDOT = -749
444958
YDOT = -24488
507725 feet/sec YDOT = -7472
985134 meter/sec
ZDOT = -4828
193602 ZDOT = -1475
493238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14482547
70 X = -4414280
54
Y = -505496
00 feet Y = -154075
18 meter
Z = -16944278
33 Z = -5164616
03
XDOT = 6446
680994 XDOT = 1964
948367
YDOT = -22715
775418 feet/sec YDOT = -6923
768347 meter/sec
ZDOT = -4843
350798 ZDOT = -1476
253323
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 14060
51868264
00016717 00000-0 10270-3 0 9121
2 25544 51
6460 273
3185 0003159 200
8667 159
2355 15
50818593 34620
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
51868264 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 273
3185 deg
Eccentricity:
0003159
Arg of perigee: 200
8667 deg
Mean anomaly: 159
2355 deg
Mean motion: 15
50818593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 315
Coasting Arc #14 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2014/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4167689
81 A = 6787214
19 meter
Y = -1074080
12 meter E =
0004703
Z = 5247298
92 I = 51
26878
XDOT = 948
093907 Wp = 160
62093
YDOT = 7564
081459 meter/sec RA = 267
62775 deg
ZDOT = 790
716120 TA = 281
75279
MA = 281
80554
Ha = 225
960 n
mi
Hp = 220
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13673523
00 X = 4153901
32
Y = -3523884
90 feet Y = -1027550
65 meter
Z = 17215547
63 Z = 5267511
35
XDOT = 3110
544313 XDOT = 859
599192
YDOT = 24816
540220 feet/sec YDOT = 7574
188968 meter/sec
ZDOT = 2594
212991 ZDOT = 795
105694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13937005
53 X = 4247999
28
Y = 1481068
64 feet Y = 451429
72 meter
Z = 17300993
87 Z = 5273342
93
XDOT = -5736
534789 XDOT = -1748
495804
YDOT = 23300
091525 feet/sec YDOT = 7101
867897 meter/sec
ZDOT = 2611
604153 ZDOT = 796
016946
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 14061
54970665
00016717 00000-0 10270-3 0 9135
2 25544 51
6461 268
2041 0003143 203
8682 156
2324 15
50817613 34780
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
54970665 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 268
2041 deg
Eccentricity:
0003143
Arg of perigee: 203
8682 deg
Mean anomaly: 156
2324 deg
Mean motion: 15
50817613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 299
Coasting Arc #15 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4205650
97 A = 6786826
83 meter
Y = 629158
80 meter E =
0013596
Z = -5300974
99 I = 51
26892
XDOT = -1041
650010 Wp = 101
12224
YDOT = -7581
859263 meter/sec RA = 262
63479 deg
ZDOT = -76
193999 TA = 168
16254
MA = 168
13054
Ha = 225
872 n
mi
Hp = 220
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13798067
49 X = -4186623
60
Y = 2064169
29 feet Y = 582234
13 meter
Z = -17391650
22 Z = -5321359
13
XDOT = -3417
486908 XDOT = -956
420416
YDOT = -24874
866347 feet/sec YDOT = -7593
031126 meter/sec
ZDOT = -249
980312 ZDOT = -81
046014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13586136
86 X = -4141054
51
Y = -2657434
49 feet Y = -809986
03 meter
Z = -17477754
02 Z = -5327219
43
XDOT = 4948
258868 XDOT = 1508
229303
YDOT = -23585
441355 feet/sec YDOT = -7188
842525 meter/sec
ZDOT = -269
331336 ZDOT = -82
092191
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 14062
51626999
00016717 00000-0 10270-3 0 9142
2 25544 51
6447 263
4078 0003155 208
5158 151
5820 15
50882091 34932
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51626999 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 263
4078 deg
Eccentricity:
0003155
Arg of perigee: 208
5158 deg
Mean anomaly: 151
5820 deg
Mean motion: 15
50882091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 318
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