[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 24th 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) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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
116/10:27:43
751 1
5 1
6 1
6
N/A -0
4 0
1 226
6
000/00:07:27
501 -0
5 0
2 222
1
119/08:06:35
451 2
1 2
3 2
3
N/A -0
9 0
1 226
9
000/00:11:10
901 -0
4 0
5 223
2
Coasting Arc #1 (Orbit 287)
---------------------------------------
Vector Time (GMT): 2014/113/17:26:51
399
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3755656
55 A = 6793116
14 meter
Y = -3887958
49 meter E =
0007093
Z = -4121806
50 I = 51
70155
XDOT = 6312
011084 Wp = 38
54694
YDOT = -2052
594844 meter/sec RA = 8
96751 deg
ZDOT = -3813
288397 TA = 192
04221
MA = 192
05917
Ha = 226
454 n
mi
Hp = 221
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12321707
85 X = -3691878
89
Y = -12755769
33 feet Y = -3929600
30 meter
Z = -13522987
21 Z = -4139895
89
XDOT = 20708
697783 XDOT = 6353
018355
YDOT = -6734
235053 feet/sec YDOT = -1981
780830 meter/sec
ZDOT = -12510
788704 ZDOT = -3782
525670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7083919
95 X = -2159178
80
Y = 16195545
23 feet Y = 4936402
19 meter
Z = -13598812
87 Z = -4144918
16
XDOT = -13015
888606 XDOT = -3967
242847
YDOT = -16093
558524 feet/sec YDOT = -4905
316638 meter/sec
ZDOT = -12380
308799 ZDOT = -3773
518122
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 14113
75009039
00016717 00000-0 10270-3 0 9000
2 25544 51
6459 9
3723 0004042 318
3209 41
7634 15
50343197 2883
Satellite: ISS
Catalog Number: 25544
Epoch time: 14113
75009039 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 9
3723 deg
Eccentricity:
0004042
Arg of perigee: 318
3209 deg
Mean anomaly: 41
7634 deg
Mean motion: 15
50343197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 288
Checksum: 287
Coasting Arc #2 (Orbit 303)
---------------------------------------
Vector Time (GMT): 2014/114/17:26:51
399
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3592354
66 A = 6792016
06 meter
Y = 3730699
49 meter E =
0006088
Z = 4388895
32 I = 51
66719
XDOT = -6491
273744 Wp = 90
61647
YDOT = 2242
139804 meter/sec RA = 4
01190 deg
ZDOT = 3403
133654 TA = 324
88926
MA = 324
92937
Ha = 226
324 n
mi
Hp = 221
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11785940
50 X = 3529050
14
Y = 12239827
72 feet Y = 3770517
87 meter
Z = 14399262
84 Z = 4406192
56
XDOT = -21296
829869 XDOT = -6532
394862
YDOT = 7356
101718 feet/sec YDOT = 2169
320537 meter/sec
ZDOT = 11165
136659 ZDOT = 3371
499690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6547677
25 X = 1995732
02
Y = -15612705
97 feet Y = -4758752
78 meter
Z = 14471761
52 Z = 4410992
91
XDOT = 14143
607493 XDOT = 4310
971564
YDOT = 16168
946804 feet/sec YDOT = 4928
294986 meter/sec
ZDOT = 11030
946066 ZDOT = 3362
232361
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 14114
78143299
00016717 00000-0 10270-3 0 9012
2 25544 51
6456 4
2593 0004086 318
5061 41
5779 15
50383738 3047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14114
78143299 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 4
2593 deg
Eccentricity:
0004086
Arg of perigee: 318
5061 deg
Mean anomaly: 41
5779 deg
Mean motion: 15
50383738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 304
Checksum: 303
Coasting Arc #3 (Orbit 318)
---------------------------------------
Vector Time (GMT): 2014/115/17:26:51
399
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3396259
06 A = 6790954
40 meter
Y = -3620613
82 meter E =
0010145
Z = -4643803
08 I = 51
63402
XDOT = 6630
137327 Wp = 47
75575
YDOT = -2440
176492 meter/sec RA = 359
05482 deg
ZDOT = -2943
917733 TA = 192
85325
MA = 192
87913
Ha = 226
491 n
mi
Hp = 221
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11142582
21 X = -3332961
76
Y = -11878654
25 feet Y = -3658239
40 meter
Z = -15235574
41 Z = -4660147
79
XDOT = 21752
419052 XDOT = 6671
231932
YDOT = -8005
828387 feet/sec YDOT = -2365
804487 meter/sec
ZDOT = -9658
522747 ZDOT = -2911
609099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6219023
68 X = -1895558
42
Y = 14983051
26 feet Y = 4566834
02 meter
Z = -15304058
67 Z = -4664677
08
XDOT = -15249
820222 XDOT = -4648
145204
YDOT = -16063
642162 feet/sec YDOT = -4896
198131 meter/sec
ZDOT = -9521
452832 ZDOT = -2902
138823
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 14115
74829269
00016717 00000-0 10270-3 0 9028
2 25544 51
6466 359
4675 0003973 324
6309 35
4578 15
50424091 3194
Satellite: ISS
Catalog Number: 25544
Epoch time: 14115
74829269 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 359
4675 deg
Eccentricity:
0003973
Arg of perigee: 324
6309 deg
Mean anomaly: 35
4578 deg
Mean motion: 15
50424091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 319
Checksum: 326
Coasting Arc #4 (Orbit 329)
---------------------------------------
Vector Time (GMT): 2014/116/10:31:27
501
Vector Time (MET): N/A
Weight (LBS) : 923924
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2113675
11 A = 6789748
99 meter
Y = -3917300
75 meter E =
0011491
Z = -5137085
45 I = 51
60860
XDOT = 7259
777088 Wp = 58
50166
YDOT = -1830
524792 meter/sec RA = 355
52270 deg
ZDOT = -1587
956449 TA = 196
13004
MA = 196
16665
Ha = 226
595 n
mi
Hp = 222
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6934629
62 X = -2044759
20
Y = -12852036
58 feet Y = -3940552
26 meter
Z = -16853954
88 Z = -5147185
85
XDOT = 23818
166299 XDOT = 7287
420757
YDOT = -6005
658767 feet/sec YDOT = -1749
186852 meter/sec
ZDOT = -5209
830870 ZDOT = -1552
621696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9232950
37 X = -2814203
27
Y = -11251593
86 feet Y = -3429485
81 meter
Z = -16895975
57 Z = -5149893
35
XDOT = 21373
906871 XDOT = 6514
766814
YDOT = -9924
843111 feet/sec YDOT = -3025
092180 meter/sec
ZDOT = -5060
078139 ZDOT = -1542
311817
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 14116
45730873
00016717 00000-0 10270-3 0 9030
2 25544 51
6500 355
9573 0004705 312
3578 47
7174 15
50151030 3308
Satellite: ISS
Catalog Number: 25544
Epoch time: 14116
45730873 = yrday
fracday
Element set: 903
Inclination: 51
6500 deg
RA of node: 355
9573 deg
Eccentricity:
0004705
Arg of perigee: 312
3578 deg
Mean anomaly: 47
7174 deg
Mean motion: 15
50151030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 330
Checksum: 282
Coasting Arc #5 (Orbit 345)
---------------------------------------
Vector Time (GMT): 2014/117/10:31:27
501
Vector Time (MET): N/A
Weight (LBS) : 923924
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1966924
20 A = 6789259
44 meter
Y = 3870421
69 meter E =
0001263
Z = 5219647
05 I = 51
57621
XDOT = -7267
053605 Wp = 350
74412
YDOT = 2136
943126 meter/sec RA = 350
56180 deg
ZDOT = 1155
143227 TA = 88
16847
MA = 88
15400
Ha = 226
602 n
mi
Hp = 222
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6453163
38 X = 1898142
25
Y = 12698233
88 feet Y = 3892032
83 meter
Z = 17124826
28 Z = 5229034
96
XDOT = -23842
039386 XDOT = -7296
020695
YDOT = 7010
968262 feet/sec YDOT = 2055
516373 meter/sec
ZDOT = 3789
839985 ZDOT = 1119
769780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8920241
39 X = 2718889
58
Y = 11044460
25 feet Y = 3366351
48 meter
Z = 17163837
79 Z = 5231537
76
XDOT = -21002
616828 XDOT = -6401
597609
YDOT = 11312
894405 feet/sec YDOT = 3448
170215 meter/sec
ZDOT = 3639
878840 ZDOT = 1109
435070
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 14117
48878425
00016717 00000-0 10270-3 0 9041
2 25544 51
6497 350
8463 0004771 314
7971 45
2791 15
50184535 3462
Satellite: ISS
Catalog Number: 25544
Epoch time: 14117
48878425 = yrday
fracday
Element set: 904
Inclination: 51
6497 deg
RA of node: 350
8463 deg
Eccentricity:
0004771
Arg of perigee: 314
7971 deg
Mean anomaly: 45
2791 deg
Mean motion: 15
50184535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 346
Checksum: 327
Coasting Arc #6 (Orbit 360)
---------------------------------------
Vector Time (GMT): 2014/118/10:31:27
501
Vector Time (MET): N/A
Weight (LBS) : 923924
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1819962
12 A = 6788871
92 meter
Y = -3866360
58 meter E =
0012370
Z = -5285512
44 I = 51
54493
XDOT = 7222
498806 Wp = 65
84481
YDOT = -2432
070921 meter/sec RA = 345
59819 deg
ZDOT = -704
219393 TA = 197
38618
MA = 197
42858
Ha = 226
685 n
mi
Hp = 221
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5971004
33 X = -1750916
49
Y = -12684910
03 feet Y = -3886326
75 meter
Z = -17340920
09 Z = -5294185
86
XDOT = 23695
862224 XDOT = 7252
578918
YDOT = -7979
235305 feet/sec YDOT = -2351
136147 meter/sec
ZDOT = -2310
431079 ZDOT = -669
059618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8635410
61 X = -2632073
15
Y = -10988181
82 feet Y = -3349197
82 meter
Z = -17376906
77 Z = -5296481
18
XDOT = 20422
740781 XDOT = 6224
851390
YDOT = -12613
035887 feet/sec YDOT = -3844
453338 meter/sec
ZDOT = -2161
328716 ZDOT = -658
772993
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 14118
45576842
00016717 00000-0 10270-3 0 9058
2 25544 51
6498 346
0547 0004895 318
6572 41
4207 15
50230390 3618
Satellite: ISS
Catalog Number: 25544
Epoch time: 14118
45576842 = yrday
fracday
Element set: 905
Inclination: 51
6498 deg
RA of node: 346
0547 deg
Eccentricity:
0004895
Arg of perigee: 318
6572 deg
Mean anomaly: 41
4207 deg
Mean motion: 15
50230390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 361
Checksum: 310
Coasting Arc #7 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2014/119/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1636723
15 A = 6789959
36 meter
Y = -3906443
52 meter E =
0010713
Z = -5315847
31 I = 51
51639
XDOT = 7171
803267 Wp = 69
35562
YDOT = -2662
457413 meter/sec RA = 341
11175 deg
ZDOT = -248
322807 TA = 198
24979
MA = 198
28827
Ha = 226
912 n
mi
Hp = 223
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5369826
61 X = -1567095
54
Y = -12816415
75 feet Y = -3924357
25 meter
Z = -17440443
93 Z = -5323629
21
XDOT = 23529
538277 XDOT = 7202
248737
YDOT = -8735
096500 feet/sec YDOT = -2582
087482 meter/sec
ZDOT = -814
707372 ZDOT = -213
408424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -422229
29 X = -128695
49
Y = -13848929
14 feet Y = -4221153
60 meter
Z = -17472650
60 Z = -5325663
90
XDOT = 24092
958569 XDOT = 7343
533772
YDOT = 120
058781 feet/sec YDOT = 36
593916 meter/sec
ZDOT = -666
606591 ZDOT = -203
181689
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 14119
35826836
00016717 00000-0 10270-3 0 9060
2 25544 51
6487 341
5820 0005789 304
6852 55
3753 15
49813461 3758
Satellite: ISS
Catalog Number: 25544
Epoch time: 14119
35826836 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 341
5820 deg
Eccentricity:
0005789
Arg of perigee: 304
6852 deg
Mean anomaly: 55
3753 deg
Mean motion: 15
49813461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 332
Coasting Arc #8 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2014/120/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1627875
48 A = 6789758
51 meter
Y = 3903706
94 meter E =
0004505
Z = 5313569
48 I = 51
48698
XDOT = -7030
093143 Wp = 328
58076
YDOT = 3041
363806 meter/sec RA = 336
14790 deg
ZDOT = -76
904445 TA = 122
17625
MA = 122
13255
Ha = 226
957 n
mi
Hp = 223
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5340798
80 X = 1558290
20
Y = 12807437
48 feet Y = 3921521
87 meter
Z = 17432970
74 Z = 5321308
58
XDOT = -23064
610049 XDOT = -7063
206280
YDOT = 9978
227711 feet/sec YDOT = 2962
563645 meter/sec
ZDOT = -252
311170 ZDOT = -111
136817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 636086
17 X = 193879
06
Y = 13821447
95 feet Y = 4212777
34 meter
Z = 17464994
31 Z = 5323330
27
XDOT = -24065
059462 XDOT = -7335
030124
YDOT = 1625
368991 feet/sec YDOT = 495
412468 meter/sec
ZDOT = -397
592396 ZDOT = -121
186162
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 14120
38995938
00016717 00000-0 10270-3 0 9076
2 25544 51
6483 336
4724 0005962 307
5047 52
5561 15
49877362 3915
Satellite: ISS
Catalog Number: 25544
Epoch time: 14120
38995938 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 336
4724 deg
Eccentricity:
0005962
Arg of perigee: 307
5047 deg
Mean anomaly: 52
5561 deg
Mean motion: 15
49877362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 335
Coasting Arc #9 (Orbit 405)
---------------------------------------
Vector Time (GMT): 2014/121/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1633879
71 A = 6789782
68 meter
Y = -3923329
93 meter E =
0010747
Z = -5303928
32 I = 51
45978
XDOT = 6847
135035 Wp = 72
95747
YDOT = -3396
930675 meter/sec RA = 331
18120 deg
ZDOT = 407
220434 TA = 200
92067
MA = 200
96467
Ha = 227
099 n
mi
Hp = 222
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5360497
74 X = -1564121
45
Y = -12871817
34 feet Y = -3941210
93 meter
Z = -17401339
63 Z = -5311696
22
XDOT = 22464
353788 XDOT = 6882
633200
YDOT = -11144
785680 feet/sec YDOT = -3320
163139 meter/sec
ZDOT = 1336
025047 ZDOT = 440
569676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -872061
63 X = -265804
39
Y = -13875824
77 feet Y = -4229351
39 meter
Z = -17433480
26 Z = -5313724
78
XDOT = 23825
264623 XDOT = 7261
940657
YDOT = -3338
345741 feet/sec YDOT = -1017
527782 meter/sec
ZDOT = 1477
633772 ZDOT = 450
382774
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 14121
35714847
00016717 00000-0 10270-3 0 9083
2 25544 51
6489 331
6816 0005941 312
0134 48
0511 15
49891639 4060
Satellite: ISS
Catalog Number: 25544
Epoch time: 14121
35714847 = yrday
fracday
Element set: 908
Inclination: 51
6489 deg
RA of node: 331
6816 deg
Eccentricity:
0005941
Arg of perigee: 312
0134 deg
Mean anomaly: 48
0511 deg
Mean motion: 15
49891639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 406
Checksum: 307
Coasting Arc #10 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2014/122/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1614812
36 A = 6789741
32 meter
Y = 3972064
44 meter E =
0006068
Z = 5266567
38 I = 51
43337
XDOT = -6652
362964 Wp = 345
19223
YDOT = 3721
049054 meter/sec RA = 326
21243 deg
ZDOT = -761
156447 TA = 112
14106
MA = 112
07664
Ha = 227
156 n
mi
Hp = 222
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5297940
81 X = 1544692
12
Y = 13031707
49 feet Y = 3989730
14 meter
Z = 17278764
36 Z = 5274241
80
XDOT = -21825
337809 XDOT = -6689
780642
YDOT = 12208
166189 feet/sec YDOT = 3646
448864 meter/sec
ZDOT = -2497
232439 ZDOT = -793
564020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1003346
18 X = 305819
92
Y = 13992466
24 feet Y = 4264903
71 meter
Z = 17310501
43 Z = 5276240
84
XDOT = -23460
262502 XDOT = -7150
688011
YDOT = 4964
478187 feet/sec YDOT = 1513
172951 meter/sec
ZDOT = -2634
915974 ZDOT = -803
122389
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 14122
38878948
00016717 00000-0 10270-3 0 9091
2 25544 51
6487 326
5715 0006118 314
9221 45
1432 15
49955229 4228
Satellite: ISS
Catalog Number: 25544
Epoch time: 14122
38878948 = yrday
fracday
Element set: 909
Inclination: 51
6487 deg
RA of node: 326
5715 deg
Eccentricity:
0006118
Arg of perigee: 314
9221 deg
Mean anomaly: 45
1432 deg
Mean motion: 15
49955229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 323
Coasting Arc #11 (Orbit 436)
---------------------------------------
Vector Time (GMT): 2014/123/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1623196
47 A = 6789928
30 meter
Y = -4038498
86 meter E =
0010259
Z = -5219642
43 I = 51
40946
XDOT = 6421
305862 Wp = 75
74770
YDOT = -4015
152299 meter/sec RA = 321
24160 deg
ZDOT = 1114
001075 TA = 204
95797
MA = 205
00761
Ha = 227
280 n
mi
Hp = 222
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5325447
74 X = -1552560
75
Y = -13249668
16 feet Y = -4056255
40 meter
Z = -17124811
13 Z = -5227356
33
XDOT = 21067
276451 XDOT = 6460
315425
YDOT = -13173
071847 feet/sec YDOT = -3943
127049 meter/sec
ZDOT = 3654
859171 ZDOT = 1145
289937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1208806
00 X = -368444
07
Y = -14190120
17 feet Y = -4325148
63 meter
Z = -17156705
22 Z = -5229363
75
XDOT = 22898
296829 XDOT = 6979
400873
YDOT = -6513
279911 feet/sec YDOT = -1985
247717 meter/sec
ZDOT = 3787
862966 ZDOT = 1154
540632
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 14123
35593144
00016717 00000-0 10270-3 0 9103
2 25544 51
6493 321
7806 0006145 319
0568 41
0114 15
49969010 4374
Satellite: ISS
Catalog Number: 25544
Epoch time: 14123
35593144 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 321
7806 deg
Eccentricity:
0006145
Arg of perigee: 319
0568 deg
Mean anomaly: 41
0114 deg
Mean motion: 15
49969010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 437
Checksum: 291
Coasting Arc #12 (Orbit 452)
---------------------------------------
Vector Time (GMT): 2014/124/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1611161
95 A = 6790075
27 meter
Y = 4138053
43 meter E =
0007719
Z = 5138455
26 I = 51
38704
XDOT = -6183
892322 Wp = 359
83255
YDOT = 4268
230915 meter/sec RA = 316
26884 deg
ZDOT = -1490
730905 TA = 104
63167
MA = 104
54607
Ha = 227
349 n
mi
Hp = 222
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5285964
40 X = 1539808
33
Y = 13576290
79 feet Y = 4155671
41 meter
Z = 16858449
02 Z = 5146108
92
XDOT = -20288
360638 XDOT = -6223
919476
YDOT = 14003
382266 feet/sec YDOT = 4198
854889 meter/sec
ZDOT = -4890
849427 ZDOT = -1520
868832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1328252
48 X = 404851
36
Y = 14471542
20 feet Y = 4410926
06 meter
Z = 16890074
20 Z = 5148094
61
XDOT = -22226
962793 XDOT = -6774
778259
YDOT = 7926
804375 feet/sec YDOT = 2416
089973 meter/sec
ZDOT = -5019
028491 ZDOT = -1529
799884
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 14124
38752260
00016717 00000-0 10270-3 0 9114
2 25544 51
6494 316
6702 0006316 322
1759 37
8947 15
50033996 4532
Satellite: ISS
Catalog Number: 25544
Epoch time: 14124
38752260 = yrday
fracday
Element set: 911
Inclination: 51
6494 deg
RA of node: 316
6702 deg
Eccentricity:
0006316
Arg of perigee: 322
1759 deg
Mean anomaly: 37
8947 deg
Mean motion: 15
50033996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 453
Checksum: 310
Coasting Arc #13 (Orbit 467)
---------------------------------------
Vector Time (GMT): 2014/125/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1637908
37 A = 6790451
72 meter
Y = -4246799
51 meter E =
0009254
Z = -5046278
93 I = 51
36674
XDOT = 5918
258796 Wp = 76
55430
YDOT = -4486
042742 meter/sec RA = 311
29439 deg
ZDOT = 1859
381423 TA = 211
53279
MA = 211
58828
Ha = 227
456 n
mi
Hp = 222
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5373715
12 X = -1565784
55
Y = -13933069
26 feet Y = -4264712
32 meter
Z = -16556033
23 Z = -5054060
60
XDOT = 19416
859567 XDOT = 5958
950525
YDOT = -14717
988000 feet/sec YDOT = -4419
633477 meter/sec
ZDOT = 6100
332752 ZDOT = 1888
230522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1573459
94 X = -479590
59
Y = -14814378
43 feet Y = -4515422
55 meter
Z = -16588185
10 Z = -5056078
82
XDOT = 21390
780205 XDOT = 6519
909807
YDOT = -9221
862907 feet/sec YDOT = -2810
823814 meter/sec
ZDOT = 6223
096030 ZDOT = 1896
799670
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 14125
35461761
00016717 00000-0 10270-3 0 9126
2 25544 51
6495 311
8791 0006374 325
8676 34
2064 15
50045478 4685
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
35461761 = yrday
fracday
Element set: 912
Inclination: 51
6495 deg
RA of node: 311
8791 deg
Eccentricity:
0006374
Arg of perigee: 325
8676 deg
Mean anomaly: 34
2064 deg
Mean motion: 15
50045478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 468
Checksum: 315
Coasting Arc #14 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2014/126/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649049
49 A = 6790806
17 meter
Y = 4390207
62 meter E =
0009355
Z = 4912657
97 I = 51
34890
XDOT = -5653
938293 Wp = 13
80293
YDOT = 4652
937363 meter/sec RA = 306
31847 deg
ZDOT = -2250
426049 TA = 98
34676
MA = 98
24068
Ha = 227
533 n
mi
Hp = 221
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5410267
36 X = 1575970
33
Y = 14403568
32 feet Y = 4408239
73 meter
Z = 16117644
25 Z = 4920491
39
XDOT = -18549
666315 XDOT = -5694
616342
YDOT = 15265
542529 feet/sec YDOT = 4589
483958 meter/sec
ZDOT = -7383
287562 ZDOT = -2277
991096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1755068
39 X = 534944
84
Y = 15251544
67 feet Y = 4648670
81 meter
Z = 16149995
35 Z = 4922518
58
XDOT = -20473
901687 XDOT = -6240
445234
YDOT = 10332
520670 feet/sec YDOT = 3149
352300 meter/sec
ZDOT = -7500
644552 ZDOT = -2286
196459
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 14126
38615844
00016717 00000-0 10270-3 0 9134
2 25544 51
6496 306
7686 0006539 329
1953 30
8813 15
50112289 4847
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
38615844 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 306
7686 deg
Eccentricity:
0006539
Arg of perigee: 329
1953 deg
Mean anomaly: 30
8813 deg
Mean motion: 15
50112289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 325
Coasting Arc #15 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2014/127/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1707778
85 A = 6791379
35 meter
Y = -4530833
57 meter E =
0007900
Z = -4767721
87 I = 51
33263
XDOT = 5372
369341 Wp = 73
03794
YDOT = -4781
933615 meter/sec RA = 301
34087 deg
ZDOT = 2625
859852 TA = 222
98646
MA = 223
04822
Ha = 227
621 n
mi
Hp = 221
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5602948
99 X = -1633826
86
Y = -14864939
54 feet Y = -4549517
59 meter
Z = -15642132
13 Z = -4775838
44
XDOT = 17625
883666 XDOT = 5412
687028
YDOT = -15688
758578 feet/sec YDOT = -4721
630885 meter/sec
ZDOT = 8615
025762 ZDOT = 2652
056245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2106753
57 X = -642138
49
Y = -15712128
23 feet Y = -4789056
69 meter
Z = -15675661
97 Z = -4777941
77
XDOT = 19441
321539 XDOT = 5925
714805
YDOT = -11293
926692 feet/sec YDOT = -3442
388856 meter/sec
ZDOT = 8726
610839 ZDOT = 2659
870984
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 14127
35320615
00016717 00000-0 10270-3 0 9142
2 25544 51
6490 301
9769 0006586 332
5779 27
5023 15
50120893 4998
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
35320615 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 301
9769 deg
Eccentricity:
0006586
Arg of perigee: 332
5779 deg
Mean anomaly: 27
5023 deg
Mean motion: 15
50120893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 314
Coasting Arc #16 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2014/128/08:12:10
901
Vector Time (MET): N/A
Weight (LBS) : 923683
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1755024
60 A = 6791940
49 meter
Y = 4704840
94 meter E =
0010866
Z = 4573780
46 I = 51
31986
XDOT = -5102
157884 Wp = 27
66969
YDOT = 4850
840206 meter/sec RA = 296
36252 deg
ZDOT = -3019
721082 TA = 92
72158
MA = 92
59720
Ha = 227
704 n
mi
Hp = 221
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5757954
74 X = 1680065
40
Y = 15435829
85 feet Y = 4724047
70 meter
Z = 15005841
41 Z = 4582124
06
XDOT = -16739
363138 XDOT = -5141
352896
YDOT = 15914
830073 feet/sec YDOT = 4793
565402 meter/sec
ZDOT = -9907
221399 ZDOT = -3044
602163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2416671
34 X = 736601
42
Y = 16264778
34 feet Y = 4957504
44 meter
Z = 15040307
43 Z = 4584285
70
XDOT = -18370
848244 XDOT = -5599
434545
YDOT = 12026
389966 feet/sec YDOT = 3665
643662 meter/sec
ZDOT = -10013
249026 ZDOT = -3052
038303
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 14128
38469628
00016717 00000-0 10270-3 0 9155
2 25544 51
6490 296
8661 0006758 335
9370 24
1464 15
50188947 5151
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
38469628 = yrday
fracday
Element set: 915
Inclination: 51
6490 deg
RA of node: 296
8661 deg
Eccentricity:
0006758
Arg of perigee: 335
9370 deg
Mean anomaly: 24
1464 deg
Mean motion: 15
50188947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 340
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