[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 17th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29062 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 640)
---------------------------------------
Vector Time (GMT): 2014/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4124857
93 A = 6794406
38 meter
Y = -3824056
35 meter E =
0006238
Z = -3815393
27 I = 51
29789
XDOT = 1870
613811 Wp = 76
73913
YDOT = -6154
477276 meter/sec RA = 255
75366 deg
ZDOT = 4153
272812 TA = 237
26279
MA = 237
32293
Ha = 227
374 n
mi
Hp = 220
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13532998
47 X = -4063255
62
Y = -12546116
65 feet Y = -3869838
42 meter
Z = -12517694
45 Z = -3835282
27
XDOT = 6137
184420 XDOT = 1919
119929
YDOT = -20191
854580 feet/sec YDOT = -6133
287991 meter/sec
ZDOT = 13626
223137 ZDOT = 4162
477476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18100734
78 X = -5517103
96
Y = 3288421
40 feet Y = 1002310
84 meter
Z = -12601168
60 Z = -3840836
19
XDOT = -12331
610879 XDOT = -3758
674996
YDOT = -15598
873258 feet/sec YDOT = -4754
536569 meter/sec
ZDOT = 13666
160420 ZDOT = 4165
445696
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 14136
50826173
00016717 00000-0 10270-3 0 9004
2 25544 51
6480 256
6293 0002983 1
3050 358
8108 15
50249387 6418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
50826173 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 256
6293 deg
Eccentricity:
0002983
Arg of perigee: 1
3050 deg
Mean anomaly: 358
8108 deg
Mean motion: 15
50249387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 296
Coasting Arc #2 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2014/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4318664
81 A = 6795320
95 meter
Y = 3919024
85 meter E =
0013003
Z = 3480348
86 I = 51
30980
XDOT = -1749
316129 Wp = 75
59356
YDOT = 5945
769835 meter/sec RA = 250
77426 deg
ZDOT = -4507
149256 TA = 63
36857
MA = 63
23543
Ha = 227
402 n
mi
Hp = 220
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14168847
79 X = 4257613
78
Y = 12857693
08 feet Y = 3966977
28 meter
Z = 11418467
38 Z = 3501180
64
XDOT = -5739
226146 XDOT = -1793
778502
YDOT = 19507
118882 feet/sec YDOT = 5925
959645 meter/sec
ZDOT = -14787
235093 ZDOT = -4515
754781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18669587
77 X = 5690490
35
Y = -3939299
90 feet Y = -1200698
61 meter
Z = 11505925
65 Z = 3507006
14
XDOT = 12253
836692 XDOT = 3734
969424
YDOT = 14609
843007 feet/sec YDOT = 4453
080149 meter/sec
ZDOT = -14824
601470 ZDOT = -4518
538528
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 14137
53964626
00016717 00000-0 10270-3 0 9015
2 25544 51
6480 251
5179 0002949 7
8040 352
3157 15
50290012 6578
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
53964626 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 251
5179 deg
Eccentricity:
0002949
Arg of perigee: 7
8040 deg
Mean anomaly: 352
3157 deg
Mean motion: 15
50290012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 657
Checksum: 297
Coasting Arc #3 (Orbit 671)
---------------------------------------
Vector Time (GMT): 2014/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4539034
67 A = 6796143
26 meter
Y = -3963322
63 meter E =
0006389
Z = -3142094
07 I = 51
32423
XDOT = 1661
068305 Wp = 49
78938
YDOT = -5715
270157 meter/sec RA = 245
79606 deg
ZDOT = 4820
029396 TA = 273
89482
MA = 273
96785
Ha = 227
390 n
mi
Hp = 220
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14891846
03 X = -4479115
14
Y = -13003027
01 feet Y = -4013745
74 meter
Z = -10308707
59 Z = -3163999
04
XDOT = 5449
699163 XDOT = 1701
439951
YDOT = -18750
886343 feet/sec YDOT = -5696
469695 meter/sec
ZDOT = 15813
744739 ZDOT = 4828
196286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19134278
44 X = -5832128
07
Y = 4777008
77 feet Y = 1456032
27 meter
Z = -10400712
37 Z = -3170137
13
XDOT = -12012
653164 XDOT = -3661
456684
YDOT = -13683
752260 feet/sec YDOT = -4170
807689 meter/sec
ZDOT = 15849
213943 ZDOT = 4830
840410
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 14138
50653973
00016717 00000-0 10270-3 0 9024
2 25544 51
6482 246
7260 0003221 7
5977 352
5222 15
50332276 6728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
50653973 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 246
7260 deg
Eccentricity:
0003221
Arg of perigee: 7
5977 deg
Mean anomaly: 352
5222 deg
Mean motion: 15
50332276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 672
Checksum: 296
Coasting Arc #4 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747149
75 A = 6797020
89 meter
Y = 4016485
50 meter E =
0014000
Z = 2733000
67 I = 51
34065
XDOT = -1650
203729 Wp = 87
87492
YDOT = 5453
286572 meter/sec RA = 240
81923 deg
ZDOT = -5124
596192 TA = 61
10958
MA = 60
96919
Ha = 227
430 n
mi
Hp = 220
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15574638
30 X = 4688607
58
Y = 13177445
87 feet Y = 4069243
66 meter
Z = 8966537
64 Z = 2755919
87
XDOT = -5414
054230 XDOT = -1686
167202
YDOT = 17891
360145 feet/sec YDOT = 5434
632213 meter/sec
ZDOT = -16812
979634 ZDOT = -5132
699660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19578159
76 X = 5967423
10
Y = -5583353
06 feet Y = -1701806
01 meter
Z = 9062839
73 Z = 2762353
55
XDOT = 11519
898531 XDOT = 3511
265072
YDOT = 12924
170812 feet/sec YDOT = 3939
287264 meter/sec
ZDOT = -16848
132692 ZDOT = -5135
310844
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 14139
53786497
00016717 00000-0 10270-3 0 9037
2 25544 51
6476 241
6144 0003175 14
6416 345
4826 15
50383129 6882
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53786497 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 241
6144 deg
Eccentricity:
0003175
Arg of perigee: 14
6416 deg
Mean anomaly: 345
4826 deg
Mean motion: 15
50383129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 323
Coasting Arc #5 (Orbit 702)
---------------------------------------
Vector Time (GMT): 2014/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4968005
51 A = 6797801
47 meter
Y = -4009472
29 meter E =
0008812
Z = -2326510
30 I = 51
35977
XDOT = 1676
683403 Wp = 34
21140
YDOT = -5189
465608 meter/sec RA = 235
84336 deg
ZDOT = 5380
177830 TA = 299
78936
MA = 299
87697
Ha = 227
422 n
mi
Hp = 220
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16299230
66 X = -4911499
96
Y = -13154436
66 feet Y = -4064711
66 meter
Z = -7632907
81 Z = -2350507
23
XDOT = 5500
929801 XDOT = 1708
453291
YDOT = -17025
805799 feet/sec YDOT = -5170
538507 meter/sec
ZDOT = 17651
502067 ZDOT = 5388
399847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19856367
92 X = -6052220
94
Y = 6548176
48 feet Y = 1995884
19 meter
Z = -7733785
85 Z = -2357257
93
XDOT = -10922
534172 XDOT = -3329
188416
YDOT = -12296
839345 feet/sec YDOT = -3748
076632 meter/sec
ZDOT = 17687
108650 ZDOT = 5391
030717
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 14140
50470365
00016717 00000-0 10270-3 0 9041
2 25544 51
6479 236
8217 0003442 14
1925 345
9322 15
50413053 7033
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
50470365 = yrday
fracday
Element set: 904
Inclination: 51
6479 deg
RA of node: 236
8217 deg
Eccentricity:
0003442
Arg of perigee: 14
1925 deg
Mean anomaly: 345
9322 deg
Mean motion: 15
50413053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 703
Checksum: 278
Coasting Arc #6 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2014/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5164290
09 A = 6798482
46 meter
Y = 4008569
00 meter E =
0014194
Z = 1847936
88 I = 51
38006
XDOT = -1787
108547 Wp = 99
75515
YDOT = 4904
326122 meter/sec RA = 230
86959 deg
ZDOT = -5609
673407 TA = 59
87068
MA = 59
73008
Ha = 227
461 n
mi
Hp = 219
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16943208
96 X = 5110104
81
Y = 13151473
11 feet Y = 4066016
38 meter
Z = 6062785
05 Z = 1872892
94
XDOT = -5863
217019 XDOT = -1814
566883
YDOT = 16090
308800 feet/sec YDOT = 4884
188202 meter/sec
ZDOT = -18404
440311 ZDOT = -5618
421490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20082423
97 X = 6121122
83
Y = -7446222
09 feet Y = -2269608
49 meter
Z = 6167735
52 Z = 1879925
79
XDOT = 10108
158097 XDOT = 3080
966588
YDOT = 11893
572185 feet/sec YDOT = 3625
160802 meter/sec
ZDOT = -18442
222347 ZDOT = -5621
189371
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 14141
53597120
00016717 00000-0 10270-3 0 9055
2 25544 51
6472 231
7095 0003402 21
0643 339
0648 15
50474597 7196
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
53597120 = yrday
fracday
Element set: 905
Inclination: 51
6472 deg
RA of node: 231
7095 deg
Eccentricity:
0003402
Arg of perigee: 21
0643 deg
Mean anomaly: 339
0648 deg
Mean motion: 15
50474597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 295
Coasting Arc #7 (Orbit 733)
---------------------------------------
Vector Time (GMT): 2014/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5356605
09 A = 6799075
34 meter
Y = -3943899
84 meter E =
0012077
Z = -1380291
14 I = 51
40300
XDOT = 1933
776888 Wp = 33
00011
YDOT = -4639
063070 meter/sec RA = 225
89690 deg
ZDOT = 5784
471446 TA = 311
93196
MA = 312
03485
Ha = 227
466 n
mi
Hp = 219
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17574163
67 X = -5305400
32
Y = -12939303
93 feet Y = -4003514
50 meter
Z = -4528514
25 Z = -1406188
72
XDOT = 6344
412361 XDOT = 1957
408891
YDOT = -15220
023195 feet/sec YDOT = -4617
306354 meter/sec
ZDOT = 18977
924692 ZDOT = 5793
922816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20096859
30 X = -6125522
71
Y = 8449518
46 feet Y = 2575413
23 meter
Z = -4637471
35 Z = -1413501
27
XDOT = -9271
059978 XDOT = -2825
819081
YDOT = -11672
125500 feet/sec YDOT = -3557
663852 meter/sec
ZDOT = 19018
637360 ZDOT = 5796
880667
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 14142
50275677
00016717 00000-0 10270-3 0 9064
2 25544 51
6476 226
9164 0003651 20
8844 339
2456 15
50491616 7346
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
50275677 = yrday
fracday
Element set: 906
Inclination: 51
6476 deg
RA of node: 226
9164 deg
Eccentricity:
0003651
Arg of perigee: 20
8844 deg
Mean anomaly: 339
2456 deg
Mean motion: 15
50491616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 734
Checksum: 314
Coasting Arc #8 (Orbit 749)
---------------------------------------
Vector Time (GMT): 2014/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5509471
17 A = 6799381
96 meter
Y = 3886531
11 meter E =
0013348
Z = 843531
51 I = 51
42631
XDOT = -2163
379418 Wp = 110
24351
YDOT = 4365
642712 meter/sec RA = 220
92665 deg
ZDOT = -5912
783451 TA = 60
61994
MA = 60
48673
Ha = 227
489 n
mi
Hp = 219
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18075692
80 X = 5461503
96
Y = 12751086
32 feet Y = 3947873
33 meter
Z = 2767491
83 Z = 870179
66
XDOT = -7097
701502 XDOT = -2183
313495
YDOT = 14322
974778 feet/sec YDOT = 4341
339116 meter/sec
ZDOT = -19398
895837 ZDOT = -5923
341270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20039828
32 X = 6108139
67
Y = -9332352
77 feet Y = -2844501
12 meter
Z = 2879645
23 Z = 877715
86
XDOT = 8279
691831 XDOT = 2523
650070
YDOT = 11709
773925 feet/sec YDOT = 3569
139092 meter/sec
ZDOT = -19444
246499 ZDOT = -5926
606333
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 14143
53396847
00016717 00000-0 10270-3 0 9072
2 25544 51
6470 221
8038 0003636 27
0600 333
0740 15
50565232 7508
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
53396847 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 221
8038 deg
Eccentricity:
0003636
Arg of perigee: 27
0600 deg
Mean anomaly: 333
0740 deg
Mean motion: 15
50565232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 284
Coasting Arc #9 (Orbit 764)
---------------------------------------
Vector Time (GMT): 2014/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5640954
17 A = 6799638
70 meter
Y = -3768886
39 meter E =
0015093
Z = -328254
87 I = 51
45155
XDOT = 2422
507766 Wp = 39
24365
YDOT = -4132
800766 meter/sec RA = 215
95759 deg
ZDOT = 5983
510870 TA = 317
21349
MA = 317
33087
Ha = 227
526 n
mi
Hp = 219
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18507067
47 X = -5596795
79
Y = -12365112
82 feet Y = -3831720
25 meter
Z = -1076951
68 Z = -355551
13
XDOT = 7947
860125 XDOT = 2439
475216
YDOT = -13559
057631 feet/sec YDOT = -4105
616079 meter/sec
ZDOT = 19630
941175 ZDOT = 5995
320314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19751056
05 X = -6020121
88
Y = 10249029
31 feet Y = 3123904
13 meter
Z = -1191876
53 Z = -363283
97
XDOT = -7359
671663 XDOT = -2243
227923
YDOT = -11950
125550 feet/sec YDOT = -3642
398268 meter/sec
ZDOT = 19681
553508 ZDOT = 5998
937509
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 14144
50070270
00016717 00000-0 10270-3 0 9080
2 25544 51
6473 217
0104 0003862 27
8868 332
2489 15
50569622 7651
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
50070270 = yrday
fracday
Element set: 908
Inclination: 51
6473 deg
RA of node: 217
0104 deg
Eccentricity:
0003862
Arg of perigee: 27
8868 deg
Mean anomaly: 332
2489 deg
Mean motion: 15
50569622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 765
Checksum: 305
Coasting Arc #10 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2014/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5717870
49 A = 6799425
84 meter
Y = 3665023
00 meter E =
0011421
Z = -248354
54 I = 51
47681
XDOT = -2753
945345 Wp = 117
29269
YDOT = 3905
540236 meter/sec RA = 210
99074 deg
ZDOT = -5986
748634 TA = 65
38452
MA = 65
26559
Ha = 227
521 n
mi
Hp = 219
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18759417
61 X = 5677668
85
Y = 12024353
66 feet Y = 3728739
13 meter
Z = -814811
47 Z = -220674
89
XDOT = -9035
253756 XDOT = -2768
331088
YDOT = 12813
452217 feet/sec YDOT = 3874
663732 meter/sec
ZDOT = -19641
563761 ZDOT = -6000
161886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19393694
50 X = 5911198
08
Y = -10980064
94 feet Y = -3346723
79 meter
Z = -698237
32 Z = -212822
74
XDOT = 6368
511657 XDOT = 1941
122353
YDOT = 12448
190942 feet/sec YDOT = 3794
208599 meter/sec
ZDOT = -19698
932105 ZDOT = -6004
234506
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 14145
53186015
00016717 00000-0 10270-3 0 9090
2 25544 51
6467 211
8973 0003875 33
2684 326
8710 15
50653858 7810
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
53186015 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 211
8973 deg
Eccentricity:
0003875
Arg of perigee: 33
2684 deg
Mean anomaly: 326
8710 deg
Mean motion: 15
50653858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 324
Coasting Arc #11 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5757852
94 A = 6799220
82 meter
Y = -3511495
01 meter E =
0017195
Z = 790968
23 I = 51
50284
XDOT = 3103
248835 Wp = 49
40429
YDOT = -3735
521162 meter/sec RA = 206
02503 deg
ZDOT = 5932
372800 TA = 319
15511
MA = 319
28385
Ha = 227
599 n
mi
Hp = 219
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18890593
63 X = -5722001
00
Y = -11520652
93 feet Y = -3575682
62 meter
Z = 2595040
13 Z = 763083
71
XDOT = 10181
262581 XDOT = 3115
971550
YDOT = -12255
646857 feet/sec YDOT = -3700
747926 meter/sec
ZDOT = 19463
165355 ZDOT = 5947
478861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18816672
82 X = -5735321
88
Y = 11666563
68 feet Y = 3555968
61 meter
Z = 2477563
45 Z = 755161
34
XDOT = -5540
153345 XDOT = -1688
638740
YDOT = -13136
486834 feet/sec YDOT = -4004
001187 meter/sec
ZDOT = 19527
678369 ZDOT = 5952
036367
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 14146
56299086
00016717 00000-0 10270-3 0 9109
2 25544 51
6464 206
7841 0004080 35
6853 324
4570 15
50651236 7970
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56299086 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 206
7841 deg
Eccentricity:
0004080
Arg of perigee: 35
6853 deg
Mean anomaly: 324
4570 deg
Mean motion: 15
50651236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 313
Coasting Arc #12 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2014/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5730935
50 A = 6798430
92 meter
Y = 3383726
21 meter E =
0008820
Z = -1382112
65 I = 51
52928
XDOT = -3503
854669 Wp = 115
75046
YDOT = 3582
118209 meter/sec RA = 201
06082 deg
ZDOT = -5791
544891 TA = 79
30228
MA = 79
20298
Ha = 227
548 n
mi
Hp = 218
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18802281
82 X = 5699385
94
Y = 11101463
96 feet Y = 3447636
93 meter
Z = -4534490
33 Z = -1354348
42
XDOT = -11495
586186 XDOT = -3515
516358
YDOT = 11752
356329 feet/sec YDOT = 3542
871166 meter/sec
ZDOT = -19001
131533 ZDOT = -5808
594432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18202627
24 X = 5548160
78
Y = -12102894
30 feet Y = -3688962
18 meter
Z = -4417489
89 Z = -1346450
92
XDOT = 4729
582831 XDOT = 1441
576847
YDOT = 14034
976945 feet/sec YDOT = 4277
860973 meter/sec
ZDOT = -19073
855855 ZDOT = -5813
711265
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 14147
52964864
00016717 00000-0 10270-3 0 9110
2 25544 51
6463 201
9901 0004088 40
0257 320
1194 15
50738340 8124
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
52964864 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 201
9901 deg
Eccentricity:
0004088
Arg of perigee: 40
0257 deg
Mean anomaly: 320
1194 deg
Mean motion: 15
50738340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 288
Coasting Arc #13 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2014/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5655924
06 A = 6797702
91 meter
Y = -3222916
06 meter E =
0017934
Z = 1925136
73 I = 51
55515
XDOT = 3907
307128 Wp = 61
79317
YDOT = -3495
782020 meter/sec RA = 196
09765 deg
ZDOT = 5595
548305 TA = 319
43539
MA = 319
56889
Ha = 227
665 n
mi
Hp = 218
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18556181
31 X = -5628816
16
Y = -10573871
57 feet Y = -3286012
86 meter
Z = 6316065
38 Z = 1897726
13
XDOT = 12819
249106 XDOT = 3918
925560
YDOT = -11469
101117 feet/sec YDOT = -3452
023623 meter/sec
ZDOT = 18358
098112 ZDOT = 5614
557606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17414140
73 X = -5307830
09
Y = 12423064
44 feet Y = 3786550
04 meter
Z = 6200522
50 Z = 1889919
26
XDOT = -4154
281853 XDOT = -1266
225109
YDOT = -15079
046260 feet/sec YDOT = -4596
093300 meter/sec
ZDOT = 18439
116093 ZDOT = 5620
242585
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 14148
56072660
00016717 00000-0 10270-3 0 9120
2 25544 51
6454 196
8764 0004282 43
5401 316
6088 15
50737057 8281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
56072660 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 196
8764 deg
Eccentricity:
0004282
Arg of perigee: 43
5401 deg
Mean anomaly: 316
6088 deg
Mean motion: 15
50737057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 315
Coasting Arc #14 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2014/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5507778
19 A = 6796400
17 meter
Y = 3104066
82 meter E =
0007182
Z = -2498991
97 I = 51
58228
XDOT = -4331
690569 Wp = 96
03727
YDOT = 3430
889050 meter/sec RA = 191
13526 deg
ZDOT = -5299
323067 TA = 111
94313
MA = 111
86677
Ha = 227
555 n
mi
Hp = 218
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18070138
41 X = 5484797
91
Y = 10183946
26 feet Y = 3165530
13 meter
Z = -8198792
54 Z = -2472291
08
XDOT = -14211
583231 XDOT = -4343
990877
YDOT = 11256
197672 feet/sec YDOT = 3382
381139 meter/sec
ZDOT = -17386
230535 ZDOT = -5320
395561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16649156
12 X = 5074662
79
Y = -12445139
71 feet Y = -3793278
58 meter
Z = -8086220
41 Z = -2464679
98
XDOT = 3672
270693 XDOT = 1119
308107
YDOT = 16237
788873 feet/sec YDOT = 4949
278048 meter/sec
ZDOT = -17475
986218 ZDOT = -5326
680599
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 14149
52733538
00016717 00000-0 10270-3 0 9136
2 25544 51
6459 192
0817 0004248 47
0643 313
0864 15
50818440 8438
Satellite: ISS
Catalog Number: 25544
Epoch time: 14149
52733538 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 192
0817 deg
Eccentricity:
0004248
Arg of perigee: 47
0643 deg
Mean anomaly: 313
0864 deg
Mean motion: 15
50818440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 308
Coasting Arc #15 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2014/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903421
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5306744
85 A = 6795206
23 meter
Y = -2972620
59 meter E =
0017082
Z = 3009549
28 I = 51
60766
XDOT = 4742
925988 Wp = 75
27236
YDOT = -3433
850346 meter/sec RA = 186
17363 deg
ZDOT = 4952
214624 TA = 319
18604
MA = 319
31386
Ha = 227
694 n
mi
Hp = 218
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17410580
23 X = -5287729
48
Y = -9752692
23 feet Y = -3031858
06 meter
Z = 9873849
36 Z = 2983815
45
XDOT = 15560
780799 XDOT = 4756
915087
YDOT = -11265
913210 feet/sec YDOT = -3380
734277 meter/sec
ZDOT = 16247
423308 ZDOT = 4975
288877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15782642
41 X = -4810549
41
Y = 12299700
24 feet Y = 3748948
63 meter
Z = 9765335
80 Z = 2976474
35
XDOT = -3463
605713 XDOT = -1055
707021
YDOT = -17472
818621 feet/sec YDOT = -5325
715116 meter/sec
ZDOT = 16345
669634 ZDOT = 4982
160105
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 14150
55836103
00016717 00000-0 10270-3 0 9144
2 25544 51
6446 186
9674 0004429 51
0972 309
0574 15
50825611 8596
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
55836103 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 186
9674 deg
Eccentricity:
0004429
Arg of perigee: 51
0972 deg
Mean anomaly: 309
0574 deg
Mean motion: 15
50825611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 314
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