[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 31215 34 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 54)
---------------------------------------
Vector Time (GMT): 2014/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514538
61 A = 6781901
75 meter
Y = 2449561
60 meter E =
0017558
Z = -5271551
60 I = 51
29695
XDOT = -3706
872052 Wp = 108
14451
YDOT = -6666
630798 meter/sec RA = 244
74029 deg
ZDOT = -633
560588 TA = 155
80821
MA = 155
72567
Ha = 225
123 n
mi
Hp = 215
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11530638
48 X = -3516061
60
Y = 8036619
42 feet Y = 2410251
81 meter
Z = -17295116
81 Z = -5288628
08
XDOT = -12161
653713 XDOT = -3628
971107
YDOT = -21872
148289 feet/sec YDOT = -6707
647807 meter/sec
ZDOT = -2078
610854 ZDOT = -651
379483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8061605
64 X = -2457177
40
Y = -11402333
30 feet Y = -3475431
19 meter
Z = -17368398
05 Z = -5293887
72
XDOT = 21012
507763 XDOT = 6404
612366
YDOT = -11611
346821 feet/sec YDOT = -3539
138511 meter/sec
ZDOT = -2153
418097 ZDOT = -656
361836
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 14356
51724710
00016717 00000-0 10270-3 0 9003
2 25544 51
6465 245
6004 0007031 162
5577 197
5818 15
52617019 550
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51724710 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 245
6004 deg
Eccentricity:
0007031
Arg of perigee: 162
5577 deg
Mean anomaly: 197
5818 deg
Mean motion: 15
52617019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 55
Checksum: 297
Coasting Arc #2 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2014/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4047842
53 A = 6781724
18 meter
Y = -1407957
85 meter E =
0006905
Z = 5251629
28 I = 51
31084
XDOT = 3331
600281 Wp = 142
14610
YDOT = 6870
170986 meter/sec RA = 239
73297 deg
ZDOT = -730
883398 TA = 314
83791
MA = 314
89400
Ha = 224
811 n
mi
Hp = 215
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13280323
26 X = 4037775
32
Y = -4619284
28 feet Y = -1362749
06 meter
Z = 17229754
85 Z = 5271268
35
XDOT = 10930
447115 XDOT = 3258
079173
YDOT = 22539
931056 feet/sec YDOT = 6907
016094 meter/sec
ZDOT = -2397
911411 ZDOT = -714
877002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4874052
04 X = 1485611
06
Y = 13078441
06 feet Y = 3986308
83 meter
Z = 17313787
04 Z = 5277242
29
XDOT = -21367
944225 XDOT = -6512
949400
YDOT = 11028
106067 feet/sec YDOT = 3361
366729 meter/sec
ZDOT = -2330
851528 ZDOT = -710
443546
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 14357
54707631
00016717 00000-0 10270-3 0 9011
2 25544 51
6460 240
4785 0006997 167
5557 192
5769 15
52681180 715
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
54707631 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 240
4785 deg
Eccentricity:
0006997
Arg of perigee: 167
5557 deg
Mean anomaly: 192
5769 deg
Mean motion: 15
52681180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 330
Coasting Arc #3 (Orbit 85)
---------------------------------------
Vector Time (GMT): 2014/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4617747
29 A = 6782915
91 meter
Y = 359189
68 meter E =
0016698
Z = -4970116
84 I = 51
33122
XDOT = -2780
020330 Wp = 127
84016
YDOT = -6819
330252 meter/sec RA = 234
72635 deg
ZDOT = 2084
861157 TA = 162
60773
MA = 162
55047
Ha = 224
761 n
mi
Hp = 215
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15150089
55 X = -4597277
73
Y = 1178443
82 feet Y = 307665
89 meter
Z = -16306157
60 Z = -4992499
16
XDOT = -9120
801606 XDOT = -2713
685819
YDOT = -22373
130749 feet/sec YDOT = -6850
047518 meter/sec
ZDOT = 6840
095658 ZDOT = 2071
516944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1728747
60 X = -526922
27
Y = -14993327
08 feet Y = -4569966
09 meter
Z = -16401716
18 Z = -4999243
09
XDOT = 20927
525058 XDOT = 6378
709638
YDOT = -9853
278061 feet/sec YDOT = -3003
279153 meter/sec
ZDOT = 6784
363604 ZDOT = 2067
874027
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 14358
51251170
00016717 00000-0 10270-3 0 9022
2 25544 51
6455 235
6757 0006932 171
3566 188
7707 15
52708976 864
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51251170 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 235
6757 deg
Eccentricity:
0006932
Arg of perigee: 171
3566 deg
Mean anomaly: 188
7707 deg
Mean motion: 15
52708976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 86
Checksum: 330
Coasting Arc #4 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2014/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5125814
97 A = 6784918
41 meter
Y = 617518
19 meter E =
0009887
Z = 4392148
04 I = 51
35754
XDOT = 2074
879900 Wp = 111
48034
YDOT = 6585
478173 meter/sec RA = 229
72490 deg
ZDOT = -3344
836809 TA = 12
46202
MA = 12
43759
Ha = 224
353 n
mi
Hp = 216
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16816978
25 X = 5097193
44
Y = 2025978
31 feet Y = 674678
07 meter
Z = 14409934
51 Z = 4416978
69
XDOT = 6807
348753 XDOT = 2017
333241
YDOT = 21605
899519 feet/sec YDOT = 6608
359274 meter/sec
ZDOT = -10973
874046 ZDOT = -3334
896843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1122681
48 X = -342193
31
Y = 16810511
38 feet Y = 5123843
87 meter
Z = 14515779
40 Z = 4424409
56
XDOT = -19976
910403 XDOT = -6088
962291
YDOT = 8113
193039 feet/sec YDOT = 2472
901238 meter/sec
ZDOT = -10932
607438 ZDOT = -3332
258747
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 14359
54227513
00016717 00000-0 10270-3 0 9031
2 25544 51
6454 230
5531 0006803 175
8272 184
2938 15
52789327 1022
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
54227513 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 230
5531 deg
Eccentricity:
0006803
Arg of perigee: 175
8272 deg
Mean anomaly: 184
2938 deg
Mean motion: 15
52789327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 307
Coasting Arc #5 (Orbit 116)
---------------------------------------
Vector Time (GMT): 2014/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5577007
34 A = 6787688
84 meter
Y = -1503513
22 meter E =
0009245
Z = -3576818
13 I = 51
38719
XDOT = -1181
018939 Wp = 145
25701
YDOT = -6138
767038 meter/sec RA = 224
72858 deg
ZDOT = 4420
098875 TA = 172
38397
MA = 172
36992
Ha = 224
375 n
mi
Hp = 216
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18297268
17 X = -5542405
41
Y = -4932786
15 feet Y = -1565685
30 meter
Z = -11734967
61 Z = -3603826
10
XDOT = -3874
734051 XDOT = -1133
757161
YDOT = -20140
311806 feet/sec YDOT = -6151
709900 meter/sec
ZDOT = 14501
636729 ZDOT = 4414
476249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3626143
75 X = 1105248
61
Y = -18527313
19 feet Y = -5647125
06 meter
Z = -11849962
61 Z = -3611868
60
XDOT = 18455
086156 XDOT = 5625
110260
YDOT = -5652
191901 feet/sec YDOT = -1722
788091 meter/sec
ZDOT = 14478
700794 ZDOT = 4413
108002
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 14360
50764950
00016717 00000-0 10270-3 0 9041
2 25544 51
6447 225
7496 0006835 180
1579 179
9572 15
52797497 1172
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50764950 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 225
7496 deg
Eccentricity:
0006835
Arg of perigee: 180
1579 deg
Mean anomaly: 179
9572 deg
Mean motion: 15
52797497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 117
Checksum: 347
Coasting Arc #6 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2014/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5871729
66 A = 6790242
20 meter
Y = 2265243
29 meter E =
0016277
Z = 2522138
81 I = 51
41951
XDOT = 121
375577 Wp = 128
16355
YDOT = 5572
183777 meter/sec RA = 219
74031 deg
ZDOT = -5273
867653 TA = 23
42141
MA = 23
34735
Ha = 224
056 n
mi
Hp = 216
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19264204
91 X = 5833711
18
Y = 7431900
55 feet Y = 2330692
13 meter
Z = 8274733
63 Z = 2550570
26
XDOT = 398
213836 XDOT = 84
675560
YDOT = 18281
442839 feet/sec YDOT = 5573
336050 meter/sec
ZDOT = -17302
715396 ZDOT = -5273
366991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5708727
05 X = -1740020
01
Y = 19792343
06 feet Y = 6032706
16 meter
Z = 8395686
11 Z = 2559005
13
XDOT = -16720
506257 XDOT = -5096
410307
YDOT = 2534
676736 feet/sec YDOT = 772
569469 meter/sec
ZDOT = -17301
530682 ZDOT = -5273
506552
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 14361
53734927
00016717 00000-0 10270-3 0 9057
2 25544 51
6449 220
6265 0006747 183
4603 176
6504 15
52861607 1330
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
53734927 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 220
6265 deg
Eccentricity:
0006747
Arg of perigee: 183
4603 deg
Mean anomaly: 176
6504 deg
Mean motion: 15
52861607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 311
Coasting Arc #7 (Orbit 147)
---------------------------------------
Vector Time (GMT): 2014/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6006830
94 A = 6792146
70 meter
Y = -2880404
83 meter E =
0004322
Z = -1327726
52 I = 51
44991
XDOT = 1065
085441 Wp = 87
63802
YDOT = -4887
525547 meter/sec RA = 214
75714 deg
ZDOT = 5801
084589 TA = 257
88855
MA = 257
93698
Ha = 223
969 n
mi
Hp = 216
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19707450
60 X = -5967725
52
Y = -9450147
07 feet Y = -2947358
42 meter
Z = -4356058
13 Z = -1356811
72
XDOT = 3494
374808 XDOT = 1091
480161
YDOT = -16035
188801 feet/sec YDOT = -4875
467665 meter/sec
ZDOT = 19032
429753 ZDOT = 5806
322543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7324782
02 X = 2232593
56
Y = -20565599
92 feet Y = -6268394
86 meter
Z = -4479709
73 Z = -1365415
53
XDOT = 14799
992395 XDOT = 4511
037682
YDOT = 1131
977049 feet/sec YDOT = 345
026605 meter/sec
ZDOT = 19055
615861 ZDOT = 5808
151715
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 14362
50266236
00016717 00000-0 10270-3 0 9069
2 25544 51
6440 215
8224 0006744 188
4866 171
6173 15
52886178 1488
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
50266236 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 215
8224 deg
Eccentricity:
0006744
Arg of perigee: 188
4866 deg
Mean anomaly: 171
6173 deg
Mean motion: 15
52886178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 148
Checksum: 321
Coasting Arc #8 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5890664
81 A = 6792840
26 meter
Y = 3361895
95 meter E =
0016841
Z = 9812
15 I = 51
47875
XDOT = -2356
025997 Wp = 154
46873
YDOT = 4156
886908 meter/sec RA = 209
78007 deg
ZDOT = -6002
315618 TA = 25
42533
MA = 25
34257
Ha = 223
818 n
mi
Hp = 216
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19326328
11 X = 5852585
83
Y = 11029842
35 feet Y = 3427556
28 meter
Z = 32192
08 Z = 38335
65
XDOT = -7729
744084 XDOT = -2373
177009
YDOT = 13638
080406 feet/sec YDOT = 4130
444622 meter/sec
ZDOT = -19692
636541 ZDOT = -6013
802303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8580673
82 X = -2615389
38
Y = 20530804
39 feet Y = 6257789
18 meter
Z = 153378
31 Z = 46749
71
XDOT = -12967
686964 XDOT = -3952
550987
YDOT = -5252
550215 feet/sec YDOT = -1600
977306 meter/sec
ZDOT = -19742
371033 ZDOT = -6017
474691
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 14363
53229845
00016717 00000-0 10270-3 0 9079
2 25544 51
6439 210
6992 0006824 192
0051 168
0939 15
52923011 1643
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
53229845 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 210
6992 deg
Eccentricity:
0006824
Arg of perigee: 192
0051 deg
Mean anomaly: 168
0939 deg
Mean motion: 15
52923011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 306
Coasting Arc #9 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2014/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5545171
29 A = 6791917
06 meter
Y = -3697997
68 meter E =
0009848
Z = 1295894
26 I = 51
50306
XDOT = 3642
810052 Wp = 87
08725
YDOT = -3411
435122 meter/sec RA = 204
80294 deg
ZDOT = 5814
938429 TA = 287
02720
MA = 287
13509
Ha = 223
557 n
mi
Hp = 216
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18192819
19 X = -5509702
30
Y = -12132538
32 feet Y = -3759809
13 meter
Z = 4251621
59 Z = 1269042
66
XDOT = 11951
476549 XDOT = 3652
439780
YDOT = -11192
372447 feet/sec YDOT = -3370
645305 meter/sec
ZDOT = 19077
881986 ZDOT = 5832
657841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9472104
52 X = 2887097
46
Y = -19733545
48 feet Y = -6014784
66 meter
Z = 4137615
41 Z = 1261145
18
XDOT = 11292
477148 XDOT = 3441
947035
YDOT = 9463
229070 feet/sec YDOT = 2884
392221 meter/sec
ZDOT = 19154
102149 ZDOT = 5838
170335
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 14364
56189923
00016717 00000-0 10270-3 0 9086
2 25544 51
6428 205
5742 0006815 196
7561 163
3367 15
53007169 1803
Satellite: ISS
Catalog Number: 25544
Epoch time: 14364
56189923 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 205
5742 deg
Eccentricity:
0006815
Arg of perigee: 196
7561 deg
Mean anomaly: 163
3367 deg
Mean motion: 15
53007169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 323
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