[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 31st 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 33368 12 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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 3888)
---------------------------------------
Vector Time (GMT): 2014/087/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3733892
48 A = 6798675
76 meter
Y = -5426325
12 meter E =
0010708
Z = 1666901
58 I = 51
90970
XDOT = 4842
099809 Wp = 106
58438
YDOT = 1563
896984 meter/sec RA = 135
97311 deg
ZDOT = -5727
927453 TA = 55
25314
MA = 55
15236
Ha = 226
326 n
mi
Hp = 221
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12250303
41 X = 3786196
11
Y = -17802903
95 feet Y = -5384277
65 meter
Z = 5468837
20 Z = 1685168
11
XDOT = 15886
154228 XDOT = 4852
076449
YDOT = 5130
895617 feet/sec YDOT = 1618
099379 meter/sec
ZDOT = -18792
412903 ZDOT = -5704
381279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11026490
75 X = -3360874
38
Y = 18562616
43 feet Y = 5657885
49 meter
Z = 5546825
74 Z = 1690672
49
XDOT = -14950
785080 XDOT = -4556
999292
YDOT = -3268
656986 feet/sec YDOT = -996
286649 meter/sec
ZDOT = -18693
060108 ZDOT = -5697
644721
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 14088
03072105
00016717 00000-0 10270-3 0 9006
2 25544 51
6484 136
8410 0003789 323
8688 36
2206 15
50505546 38891
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
03072105 = yrday
fracday
Element set: 900
Inclination: 51
6484 deg
RA of node: 136
8410 deg
Eccentricity:
0003789
Arg of perigee: 323
8688 deg
Mean anomaly: 36
2206 deg
Mean motion: 15
50505546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 311
Coasting Arc #2 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3656005
82 A = 6799091
56 meter
Y = 5602790
06 meter E =
0011134
Z = -1175559
03 I = 51
93241
XDOT = -4581
015937 Wp = 18
46242
YDOT = -1759
432848 meter/sec RA = 131
03583 deg
ZDOT = 5886
944407 TA = 328
83885
MA = 328
90482
Ha = 226
321 n
mi
Hp = 220
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11994769
76 X = -3712675
26
Y = 18381857
14 feet Y = 5561589
22 meter
Z = -3856820
97 Z = -1193457
93
XDOT = -15029
579846 XDOT = -4589
598041
YDOT = -5772
417481 feet/sec YDOT = -1810
707799 meter/sec
ZDOT = 19314
122071 ZDOT = 5864
669855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10413179
49 X = 3173937
11
Y = -19306402
23 feet Y = -5884591
40 meter
Z = -3933289
59 Z = -1198866
67
XDOT = 14166
726799 XDOT = 4318
018328
YDOT = 3742
006675 feet/sec YDOT = 1140
563634 meter/sec
ZDOT = 19220
170779 ZDOT = 5858
308054
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 14088
99748235
00016717 00000-0 10270-3 0 9016
2 25544 51
6475 132
0469 0004003 327
0543 33
0358 15
50567704 39044
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99748235 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 132
0469 deg
Eccentricity:
0004003
Arg of perigee: 327
0543 deg
Mean anomaly: 33
0358 deg
Mean motion: 15
50567704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 304
Coasting Arc #3 (Orbit 3919)
---------------------------------------
Vector Time (GMT): 2014/089/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3578955
67 A = 6799427
69 meter
Y = -5742431
61 meter E =
0009693
Z = 628440
09 I = 51
95297
XDOT = 4321
690429 Wp = 119
34554
YDOT = 2030
773418 meter/sec RA = 126
10138 deg
ZDOT = -5990
716089 TA = 53
91054
MA = 53
82082
Ha = 226
372 n
mi
Hp = 220
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11741980
55 X = 3639850
06
Y = -18839998
73 feet Y = -5702068
86 meter
Z = 2061811
33 Z = 645975
02
XDOT = 14178
774373 XDOT = 4327
761833
YDOT = 6662
642447 feet/sec YDOT = 2079
134403 meter/sec
ZDOT = -19654
580346 ZDOT = -5969
707342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9793534
10 X = -2985069
19
Y = 19914608
13 feet Y = 6069972
56 meter
Z = 2136772
81 Z = 651288
35
XDOT = -13441
752266 XDOT = -4097
046091
YDOT = -4488
937980 feet/sec YDOT = -1368
228296 meter/sec
ZDOT = -19566
018792 ZDOT = -5963
722528
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 14090
02866439
00016717 00000-0 10270-3 0 9021
2 25544 51
6470 126
9339 0003860 331
0460 29
0476 15
50599116 39206
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
02866439 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 126
9339 deg
Eccentricity:
0003860
Arg of perigee: 331
0460 deg
Mean anomaly: 29
0476 deg
Mean motion: 15
50599116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3920
Checksum: 301
Coasting Arc #4 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3455620
54 A = 6799409
17 meter
Y = 5845771
15 meter E =
0013731
Z = -87540
90 I = 51
96986
XDOT = -4102
712752 Wp = 29
04764
YDOT = -2340
937075 meter/sec RA = 121
16638 deg
ZDOT = 6037
405178 TA = 330
01470
MA = 330
09327
Ha = 226
374 n
mi
Hp = 220
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11337337
74 X = -3520307
19
Y = 19179039
22 feet Y = 5806766
49 meter
Z = -287207
68 Z = -104485
88
XDOT = -13460
343673 XDOT = -4105
559004
YDOT = -7680
239748 feet/sec YDOT = -2386
831349 meter/sec
ZDOT = 19807
759770 ZDOT = 6017
467986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9019094
04 X = 2749019
86
Y = -20371053
39 feet Y = -6209097
07 meter
Z = -359703
75 Z = -109637
70
XDOT = 12901
992361 XDOT = 3932
527272
YDOT = 5382
817603 feet/sec YDOT = 1640
682805 meter/sec
ZDOT = 19723
773906 ZDOT = 6011
806287
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 14090
99536575
00016717 00000-0 10270-3 0 9033
2 25544 51
6458 122
1388 0003983 334
3353 25
7600 15
50666011 39354
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99536575 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 122
1388 deg
Eccentricity:
0003983
Arg of perigee: 334
3353 deg
Mean anomaly: 25
7600 deg
Mean motion: 15
50666011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 311
Coasting Arc #5 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2014/091/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3341809
69 A = 6799206
03 meter
Y = -5896922
40 meter E =
0007501
Z = -500093
08 I = 51
98447
XDOT = 3899
202890 Wp = 128
28438
YDOT = 2713
710369 meter/sec RA = 116
23393 deg
ZDOT = -6008
697611 TA = 57
07465
MA = 57
00252
Ha = 226
394 n
mi
Hp = 220
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10963942
54 X = 3409931
35
Y = -19346858
26 feet Y = -5859171
31 meter
Z = -1640725
32 Z = -483692
72
XDOT = 12792
660400 XDOT = 3897
756419
YDOT = 8903
249242 feet/sec YDOT = 2757
304977 meter/sec
ZDOT = -19713
574838 ZDOT = -5989
759451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8286800
33 X = -2525816
74
Y = 20641302
85 feet Y = 6291469
11 meter
Z = -1570508
63 Z = -478691
03
XDOT = -12485
445263 XDOT = -3805
563716
YDOT = -6489
265683 feet/sec YDOT = -1977
928180 meter/sec
ZDOT = -19633
868690 ZDOT = -5984
403177
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 14092
02648300
00016717 00000-0 10270-3 0 9040
2 25544 51
6455 117
0252 0003909 338
2003 21
8981 15
50702398 39513
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
02648300 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 117
0252 deg
Eccentricity:
0003909
Arg of perigee: 338
2003 deg
Mean anomaly: 21
8981 deg
Mean motion: 15
50702398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 287
Coasting Arc #6 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2014/092/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3194712
97 A = 6798654
29 meter
Y = 5895247
99 meter E =
0015053
Z = 1068580
20 I = 51
99528
XDOT = -3750
604168 Wp = 42
16939
YDOT = -3112
076212 meter/sec RA = 111
30019 deg
ZDOT = 5918
565467 TA = 329
35177
MA = 329
43962
Ha = 226
399 n
mi
Hp = 220
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10481341
77 X = -3265588
40
Y = 19341364
80 feet Y = 5859126
47 meter
Z = 3505840
55 Z = 1052887
85
XDOT = -12305
131786 XDOT = -3744
276276
YDOT = -10210
223794 feet/sec YDOT = -3153
981929 meter/sec
ZDOT = 19417
865704 ZDOT = 5900
361033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7465788
52 X = 2275572
34
Y = -20704488
84 feet Y = -6310728
20 meter
Z = 3438601
34 Z = 1048085
69
XDOT = 12314
141372 XDOT = 3753
350290
YDOT = 7673
278232 feet/sec YDOT = 2338
815205 meter/sec
ZDOT = 19341
322638 ZDOT = 5895
235140
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 14093
05756565
00016717 00000-0 10270-3 0 9058
2 25544 51
6447 111
9098 0003878 341
8026 18
2986 15
50768799 39674
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
05756565 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 111
9098 deg
Eccentricity:
0003878
Arg of perigee: 341
8026 deg
Mean anomaly: 18
2986 deg
Mean motion: 15
50768799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 356
Coasting Arc #7 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2014/093/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3071243
14 A = 6797825
12 meter
Y = -5829385
10 meter E =
0004556
Z = -1669225
39 I = 52
00328
XDOT = 3627
198527 Wp = 121
65754
YDOT = 3549
358220 meter/sec RA = 106
36826 deg
ZDOT = -5735
370981 TA = 76
49997
MA = 76
44920
Ha = 226
406 n
mi
Hp = 220
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10076257
03 X = 3144309
01
Y = -19125279
20 feet Y = -5794632
09 meter
Z = -5476461
24 Z = -1654127
66
XDOT = 11900
257635 XDOT = 3615
100063
YDOT = 11644
876049 feet/sec YDOT = 3589
851783 meter/sec
ZDOT = -18816
833927 ZDOT = -5717
780070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6757596
46 X = -2059715
40
Y = 20551081
66 feet Y = 6263969
69 meter
Z = -5411729
91 Z = -1649495
28
XDOT = -12302
557413 XDOT = -3749
819499
YDOT = -8968
837246 feet/sec YDOT = -2733
701592 meter/sec
ZDOT = -18742
952896 ZDOT = -5712
852043
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 14094
02417565
00016717 00000-0 10270-3 0 9061
2 25544 51
6445 107
1155 0003895 346
3440 13
7605 15
50814949 39826
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
02417565 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 107
1155 deg
Eccentricity:
0003895
Arg of perigee: 346
3440 deg
Mean anomaly: 13
7605 deg
Mean motion: 15
50814949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 311
Coasting Arc #8 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2014/094/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2933631
31 A = 6796736
51 meter
Y = 5699031
64 meter E =
0014836
Z = 2234868
62 I = 52
00763
XDOT = -3565
542047 Wp = 57
00292
YDOT = -3994
854728 meter/sec RA = 101
43445 deg
ZDOT = 5488
284209 TA = 327
68988
MA = 327
78066
Ha = 226
408 n
mi
Hp = 219
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9624774
65 X = -3007997
48
Y = 18697610
37 feet Y = 5665810
24 meter
Z = 7332246
13 Z = 2220436
34
XDOT = -11697
972596 XDOT = -3547
266178
YDOT = -13106
478767 feet/sec YDOT = -4034
624340 meter/sec
ZDOT = 18006
181789 ZDOT = 5471
007865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6049780
64 X = 1843973
14
Y = -20162865
80 feet Y = -6145641
50 meter
Z = 7270333
60 Z = 2215997
68
XDOT = 12557
820114 XDOT = 3827
623571
YDOT = 10256
467218 feet/sec YDOT = 3126
171208 meter/sec
ZDOT = 17933
700984 ZDOT = 5466
192060
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 14095
05519240
00016717 00000-0 10270-3 0 9079
2 25544 51
6441 101
9999 0003716 349
5913 10
5161 15
50873658 39983
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
05519240 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 101
9999 deg
Eccentricity:
0003716
Arg of perigee: 349
5913 deg
Mean anomaly: 10
5161 deg
Mean motion: 15
50873658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 326
Coasting Arc #9 (Orbit 4012)
---------------------------------------
Vector Time (GMT): 2014/095/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2837674
16 A = 6795351
87 meter
Y = -5499334
46 meter E =
0004036
Z = -2812648
24 I = 52
00894
XDOT = 3530
884661 Wp = 69
95210
YDOT = 4446
558274 meter/sec RA = 96
50115 deg
ZDOT = -5136
308228 TA = 141
71789
MA = 141
68923
Ha = 226
408 n
mi
Hp = 219
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9309954
60 X = 2912621
05
Y = -18042435
90 feet Y = -5467182
91 meter
Z = -9227848
55 Z = -2798680
74
XDOT = 11584
267260 XDOT = 3505
850456
YDOT = 14588
445782 feet/sec YDOT = 4485
902565 meter/sec
ZDOT = -16851
404948 ZDOT = -5119
216732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5537390
95 X = -1687796
76
Y = 19561301
15 feet Y = 5962284
59 meter
Z = -9167918
81 Z = -2794381
65
XDOT = -12963
987996 XDOT = -3951
423541
YDOT = -11526
952784 feet/sec YDOT = -3513
415208 meter/sec
ZDOT = -16779
777972 ZDOT = -5114
476326
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 14096
02173978
00016717 00000-0 10270-3 0 9082
2 25544 51
6443 97
2052 0003786 355
6338 4
4780 15
50927700 40134
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
02173978 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 97
2052 deg
Eccentricity:
0003786
Arg of perigee: 355
6338 deg
Mean anomaly: 4
4780 deg
Mean motion: 15
50927700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4013
Checksum: 310
Coasting Arc #10 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2014/096/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2750212
74 A = 6793836
11 meter
Y = 5230600
79 meter E =
0013045
Z = 3336702
95 I = 52
00664
XDOT = -3554
584708 Wp = 72
65499
YDOT = -4887
199645 meter/sec RA = 91
56541 deg
ZDOT = 4719
974095 TA = 325
94502
MA = 326
02866
Ha = 226
399 n
mi
Hp = 219
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9023007
68 X = -2824706
76
Y = 17160763
74 feet Y = 5199429
87 meter
Z = 10947188
17 Z = 3323161
45
XDOT = -11662
023319 XDOT = -3522
598918
YDOT = -16034
119570 feet/sec YDOT = -4926
770098 meter/sec
ZDOT = 15485
479315 ZDOT = 4702
784445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5123137
29 X = 1561532
25
Y = -18733088
01 feet Y = -5709845
23 meter
Z = 10889090
24 Z = 3318994
70
XDOT = 13610
824011 XDOT = 4148
579158
YDOT = 12703
616269 feet/sec YDOT = 3872
062239 meter/sec
ZDOT = 15413
508584 ZDOT = 4698
037417
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 14097
05268841
00016717 00000-0 10270-3 0 9091
2 25544 51
6439 92
0895 0003535 358
1039 2
0098 15
50981772 40297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
05268841 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 92
0895 deg
Eccentricity:
0003535
Arg of perigee: 358
1039 deg
Mean anomaly: 2
0098 deg
Mean motion: 15
50981772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 322
Coasting Arc #11 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2014/097/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2723070
01 A = 6792150
62 meter
Y = -4897349
14 meter E =
0008099
Z = -3848199
71 I = 52
00200
XDOT = 3596
018657 Wp = 50
94958
YDOT = 5296
175628 meter/sec RA = 86
62901 deg
ZDOT = -4196
431703 TA = 174
97157
MA = 174
96343
Ha = 226
388 n
mi
Hp = 219
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8933956
74 X = 2796324
23
Y = -16067418
44 feet Y = -4866488
76 meter
Z = -12625327
15 Z = -3834793
08
XDOT = 11797
961474 XDOT = 3556
913297
YDOT = 17375
904291 feet/sec YDOT = 5336
169616 meter/sec
ZDOT = -13767
820548 ZDOT = -4179
058164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4980912
48 X = -1518182
12
Y = 17737425
56 feet Y = 5406367
31 meter
Z = -12567841
88 Z = -3830678
21
XDOT = -14343
438407 XDOT = -4371
880026
YDOT = -13729
273823 feet/sec YDOT = -4184
682661 meter/sec
ZDOT = -13695
139837 ZDOT = -4174
278622
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 14098
01917132
00016717 00000-0 10270-3 0 9104
2 25544 51
6445 87
2945 0003611 5
2631 354
8557 15
51034480 40440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
01917132 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 87
2945 deg
Eccentricity:
0003611
Arg of perigee: 5
2631 deg
Mean anomaly: 354
8557 deg
Mean motion: 15
51034480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 288
Coasting Arc #12 (Orbit 4059)
---------------------------------------
Vector Time (GMT): 2014/098/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2726680
00 A = 6790468
61 meter
Y = 4498990
64 meter E =
0009926
Z = 4284694
55 I = 51
99366
XDOT = -3680
600848 Wp = 86
96616
YDOT = -5675
699981 meter/sec RA = 81
68932 deg
ZDOT = 3610
636473 TA = 326
30405
MA = 326
36712
Ha = 226
375 n
mi
Hp = 219
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8945800
54 X = -2797599
76
Y = 14760467
98 feet Y = 4468103
02 meter
Z = 14057396
81 Z = 4271276
03
XDOT = -12075
462101 XDOT = -3634
399663
YDOT = -18621
062929 feet/sec YDOT = -5716
600157 meter/sec
ZDOT = 11845
920186 ZDOT = 3592
869374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5024359
40 X = 1531424
75
Y = -16561018
50 feet Y = -5047798
44 meter
Z = 13999915
92 Z = 4267174
37
XDOT = 15239
888391 XDOT = 4645
117981
YDOT = 14593
351552 feet/sec YDOT = 4448
053553 meter/sec
ZDOT = 11771
639369 ZDOT = 3587
995680
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 14099
05004949
00016717 00000-0 10270-3 0 9113
2 25544 51
6439 82
1783 0003384 6
9376 353
1821 15
51091212 40608
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
05004949 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 82
1783 deg
Eccentricity:
0003384
Arg of perigee: 6
9376 deg
Mean anomaly: 353
1821 deg
Mean motion: 15
51091212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4060
Checksum: 295
Coasting Arc #13 (Orbit 4074)
---------------------------------------
Vector Time (GMT): 2014/099/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2805017
56 A = 6788869
96 meter
Y = -4052792
38 meter E =
0012712
Z = -4681080
81 I = 51
98434
XDOT = 3761
556858 Wp = 57
27275
YDOT = 5986
730004 meter/sec RA = 76
74872 deg
ZDOT = -2928
278408 TA = 183
66530
MA = 183
67462
Ha = 226
334 n
mi
Hp = 219
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9202813
53 X = 2872867
55
Y = -13296562
93 feet Y = -4021045
99 meter
Z = -15357876
69 Z = -4667289
19
XDOT = 12341
065807 XDOT = 3708
556981
YDOT = 19641
502638 feet/sec YDOT = 6028
497502 meter/sec
ZDOT = -9607
212625 ZDOT = -2910
134630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5387160
21 X = -1642006
43
Y = 15306125
17 feet Y = 4665306
95 meter
Z = -15298881
53 Z = -4663099
09
XDOT = -16102
658650 XDOT = -4908
090357
YDOT = -15197
369092 feet/sec YDOT = -4632
158099 meter/sec
ZDOT = -9531
394147 ZDOT = -2905
168936
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 14100
01646560
00016717 00000-0 10270-3 0 9124
2 25544 51
6449 77
3832 0003435 14
2997 345
8251 15
51139830 40758
Satellite: ISS
Catalog Number: 25544
Epoch time: 14100
01646560 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 77
3832 deg
Eccentricity:
0003435
Arg of perigee: 14
2997 deg
Mean anomaly: 345
8251 deg
Mean motion: 15
51139830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4075
Checksum: 296
Coasting Arc #14 (Orbit 4090)
---------------------------------------
Vector Time (GMT): 2014/100/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2931152
09 A = 6787448
43 meter
Y = 3553891
18 meter E =
0006202
Z = 4979473
99 I = 51
97171
XDOT = -3858
375026 Wp = 91
97438
YDOT = -6253
905330 meter/sec RA = 71
80383 deg
ZDOT = 2189
687128 TA = 336
75542
MA = 336
78345
Ha = 226
346 n
mi
Hp = 218
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9616640
71 X = -2994863
42
Y = 11659747
96 feet Y = 3520757
49 meter
Z = 16336856
92 Z = 4965079
66
XDOT = -12658
710715 XDOT = -3798
792513
YDOT = -20518
062105 feet/sec YDOT = -6296
718760 meter/sec
ZDOT = 7184
012886 ZDOT = 2171
089066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5992094
13 X = 1826390
29
Y = -13947365
24 feet Y = -4251156
93 meter
Z = 16275386
51 Z = 4960737
81
XDOT = 17007
177928 XDOT = 5183
787833
YDOT = 15608
951179 feet/sec YDOT = 4757
608319 meter/sec
ZDOT = 7106
323569 ZDOT = 2166
007424
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 14101
04727156
00016717 00000-0 10270-3 0 9130
2 25544 51
6445 72
2662 0003289 15
7467 344
3786 15
51196326 40912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14101
04727156 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 72
2662 deg
Eccentricity:
0003289
Arg of perigee: 15
7467 deg
Mean anomaly: 344
3786 deg
Mean motion: 15
51196326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4091
Checksum: 306
Coasting Arc #15 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2014/101/23:53:01
116
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3136479
05 A = 6786357
72 meter
Y = -3035210
61 meter E =
0015923
Z = -5210588
87 I = 51
95911
XDOT = 3920
415935 Wp = 69
45202
YDOT = 6424
560765 meter/sec RA = 66
85876 deg
ZDOT = -1380
470016 TA = 187
29392
MA = 187
31711
Ha = 226
246 n
mi
Hp = 218
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10290285
61 X = 3195497
88
Y = -9958040
05 feet Y = -2999807
13 meter
Z = -17095107
85 Z = -5195208
48
XDOT = 12862
257006 XDOT = 3854
989592
YDOT = 21077
955265 feet/sec YDOT = 6468
035385 meter/sec
ZDOT = -4529
101102 ZDOT = -1361
584775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6911086
00 X = -2106499
01
Y = 12630389
03 feet Y = 3849742
58 meter
Z = -17029545
37 Z = -5190605
43
XDOT = -17723
635401 XDOT = -5402
164070
YDOT = -15707
227810 feet/sec YDOT = -4787
563037 meter/sec
ZDOT = -4450
234864 ZDOT = -1356
431586
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 14102
01361856
00016717 00000-0 10270-3 0 9140
2 25544 51
6456 67
4711 0003295 22
5315 337
5980 15
51251757 41067
Satellite: ISS
Catalog Number: 25544
Epoch time: 14102
01361856 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 67
4711 deg
Eccentricity:
0003295
Arg of perigee: 22
5315 deg
Mean anomaly: 337
5980 deg
Mean motion: 15
51251757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 291
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