[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 935)
---------------------------------------
Vector Time (GMT): 2014/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4584399
41 A = 6791260
14 meter
Y = 2210429
65 meter E =
0013619
Z = -4510203
73 I = 51
74496
XDOT = -5315
376235 Wp = 68
50617
YDOT = 4464
061534 meter/sec RA = 161
41591 deg
ZDOT = -3217
970474 TA = 169
12282
MA = 169
09335
Ha = 228
095 n
mi
Hp = 218
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15040680
49 X = 4581250
34
Y = 7252065
77 feet Y = 2261678
08 meter
Z = -14797256
33 Z = -4487940
78
XDOT = -17438
898410 XDOT = -5349
267426
YDOT = 14645
871176 feet/sec YDOT = 4404
432327 meter/sec
ZDOT = -10557
645912 ZDOT = -3243
873882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11566915
51 X = 3525595
85
Y = -12157051
29 feet Y = -3705469
23 meter
Z = -14703261
27 Z = -4481554
04
XDOT = 7682
656095 XDOT = 2341
673578
YDOT = 20200
329564 feet/sec YDOT = 6157
060451 meter/sec
ZDOT = -10668
104216 ZDOT = -3251
638165
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 14155
52202338
00016717 00000-0 10270-3 0 9008
2 25544 51
6443 162
3796 0004243 64
9629 295
1962 15
50562656 9361
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
52202338 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 162
3796 deg
Eccentricity:
0004243
Arg of perigee: 64
9629 deg
Mean anomaly: 295
1962 deg
Mean motion: 15
50562656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 936
Checksum: 313
Coasting Arc #2 (Orbit 951)
---------------------------------------
Vector Time (GMT): 2014/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4296316
20 A = 6790225
31 meter
Y = -2217919
11 meter E =
0010988
Z = 4759087
00 I = 51
76997
XDOT = 5428
663963 Wp = 100
41848
YDOT = -4690
923418 meter/sec RA = 156
46331 deg
ZDOT = 2707
381524 TA = 322
83535
MA = 322
91137
Ha = 228
220 n
mi
Hp = 218
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14095525
60 X = -4294313
83
Y = -7276637
49 feet Y = -2265952
40 meter
Z = 15613802
50 Z = 4738220
72
XDOT = 17810
577306 XDOT = 5467
563816
YDOT = -15390
168693 feet/sec YDOT = -4629
999287 meter/sec
ZDOT = 8882
485314 ZDOT = 2733
847502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11104858
30 X = -3384760
81
Y = 11448069
59 feet Y = 3489371
61 meter
Z = 15525718
93 Z = 4732239
13
XDOT = -8695
360000 XDOT = -2650
345728
YDOT = -20666
525127 feet/sec YDOT = -6299
156859 meter/sec
ZDOT = 8995
375952 ZDOT = 2741
790590
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 14156
55321970
00016717 00000-0 10270-3 0 9017
2 25544 51
6435 157
2662 0004254 67
2972 292
8629 15
50567395 9523
Satellite: ISS
Catalog Number: 25544
Epoch time: 14156
55321970 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 157
2662 deg
Eccentricity:
0004254
Arg of perigee: 67
2972 deg
Mean anomaly: 292
8629 deg
Mean motion: 15
50567395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 952
Checksum: 324
Coasting Arc #3 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4006121
63 A = 6789303
16 meter
Y = 2296615
98 meter E =
0016641
Z = -4992419
46 I = 51
79493
XDOT = -5475
629605 Wp = 73
57080
YDOT = 4892
161558 meter/sec RA = 151
51179 deg
ZDOT = -2144
726717 TA = 175
53293
MA = 175
51806
Ha = 228
116 n
mi
Hp = 218
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13143443
66 X = 4004394
34
Y = 7534829
33 feet Y = 2341405
66 meter
Z = -16379328
93 Z = -4972962
20
XDOT = -17964
664058 XDOT = -5519
509440
YDOT = 16050
398813 feet/sec YDOT = 4830
684335 meter/sec
ZDOT = -7036
504978 ZDOT = -2171
433022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10893261
00 X = 3320265
95
Y = -10655682
63 feet Y = -3247852
07 meter
Z = -16297222
86 Z = -4967393
53
XDOT = 9710
279687 XDOT = 2959
693249
YDOT = 20856
152875 feet/sec YDOT = 6356
955396 meter/sec
ZDOT = -7150
459396 ZDOT = -2179
460024
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 14157
51996031
00016717 00000-0 10270-3 0 9021
2 25544 51
6433 152
4726 0004271 70
7608 289
4005 15
50573469 9678
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51996031 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 152
4726 deg
Eccentricity:
0004271
Arg of perigee: 70
7608 deg
Mean anomaly: 289
4005 deg
Mean motion: 15
50573469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 313
Coasting Arc #4 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2014/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3711148
47 A = 6788542
06 meter
Y = -2399340
04 meter E =
0008234
Z = 5146551
11 I = 51
81884
XDOT = 5494
337748 Wp = 101
41693
YDOT = -5112
271416 meter/sec RA = 146
56136 deg
ZDOT = 1574
854971 TA = 333
41673
MA = 333
45893
Ha = 228
208 n
mi
Hp = 218
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12175683
95 X = -3709043
22
Y = -7871850
54 feet Y = -2440829
04 meter
Z = 16885010
20 Z = 5128527
66
XDOT = 18026
042480 XDOT = 5543
445762
YDOT = -16772
544017 feet/sec YDOT = -5050
555720 meter/sec
ZDOT = 5166
847019 ZDOT = 1601
664916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10783887
19 X = -3286928
81
Y = 9822546
33 feet Y = 2993912
12 meter
Z = 16808992
85 Z = 5123381
02
XDOT = -10820
594936 XDOT = -3298
117336
YDOT = -20938
299935 feet/sec YDOT = -6381
993820 meter/sec
ZDOT = 5281
290488 ZDOT = 1609
737341
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 14158
55114457
00016717 00000-0 10270-3 0 9031
2 25544 51
6427 147
3592 0004219 72
7028 287
4585 15
50583959 9839
Satellite: ISS
Catalog Number: 25544
Epoch time: 14158
55114457 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 147
3592 deg
Eccentricity:
0004219
Arg of perigee: 72
7028 deg
Mean anomaly: 287
4585 deg
Mean motion: 15
50583959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 983
Checksum: 334
Coasting Arc #5 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2014/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3436667
80 A = 6788027
78 meter
Y = 2567168
90 meter E =
0018572
Z = -5277080
60 I = 51
84245
XDOT = -5441
836528 Wp = 81
22969
YDOT = 5286
212282 meter/sec RA = 141
61176 deg
ZDOT = -972
523940 TA = 179
46565
MA = 179
46366
Ha = 228
116 n
mi
Hp = 218
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11275156
81 X = 3433340
39
Y = 8422470
13 feet Y = 2605581
69 meter
Z = -17313256
57 Z = -5260393
44
XDOT = -17853
794384 XDOT = -5495
819437
YDOT = 17343
216148 feet/sec YDOT = 5225
056402 meter/sec
ZDOT = -3190
695340 ZDOT = -999
090694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10929790
28 X = 3331400
08
Y = -9002064
53 feet Y = -2743829
27 meter
Z = -17242927
14 Z = -5255644
19
XDOT = 11844
980853 XDOT = 3610
350164
YDOT = 20709
327711 feet/sec YDOT = 6312
203086 meter/sec
ZDOT = -3304
152652 ZDOT = -1007
105728
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 14159
51787389
00016717 00000-0 10270-3 0 9049
2 25544 51
6426 142
5652 0004273 76
3187 283
8439 15
50587154 9983
Satellite: ISS
Catalog Number: 25544
Epoch time: 14159
51787389 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 142
5652 deg
Eccentricity:
0004273
Arg of perigee: 76
3187 deg
Mean anomaly: 283
8439 deg
Mean motion: 15
50587154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 346
Coasting Arc #6 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2014/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3167484
11 A = 6787684
40 meter
Y = -2759781
97 meter E =
0006629
Z = 5325630
47 I = 51
86507
XDOT = 5370
995992 Wp = 89
80648
YDOT = -5460
919246 meter/sec RA = 136
66372 deg
ZDOT = 364
207026 TA = 356
72951
MA = 356
73384
Ha = 228
188 n
mi
Hp = 218
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10392008
23 X = -3162258
75
Y = -9054402
78 feet Y = -2795174
06 meter
Z = 17472540
91 Z = 5310255
51
XDOT = 17621
377925 XDOT = 5429
892820
YDOT = -17916
401725 feet/sec YDOT = -5400
528038 meter/sec
ZDOT = 1194
904941 ZDOT = 390
441525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11189796
01 X = -3410649
82
Y = 8186732
02 feet Y = 2495315
92 meter
Z = 17407803
27 Z = 5305898
44
XDOT = -12880
723572 XDOT = -3926
044545
YDOT = -20387
359554 feet/sec YDOT = -6214
067192 meter/sec
ZDOT = 1307
001134 ZDOT = 398
373946
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 14160
54904583
00016717 00000-0 10270-3 0 9052
2 25544 51
6423 137
4517 0004205 78
4203 281
7420 15
50601173 10145
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
54904583 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 137
4517 deg
Eccentricity:
0004205
Arg of perigee: 78
4203 deg
Mean anomaly: 281
7420 deg
Mean motion: 15
50601173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 271
Coasting Arc #7 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2014/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2940057
91 A = 6787656
24 meter
Y = 3004090
53 meter E =
0019002
Z = -5345919
84 I = 51
88727
XDOT = -5233
711181 Wp = 89
81004
YDOT = 5571
874852 meter/sec RA = 131
71652 deg
ZDOT = 253
556812 TA = 182
59979
MA = 182
60969
Ha = 228
088 n
mi
Hp = 218
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9645859
28 X = 2932216
12
Y = 9855940
04 feet Y = 3036924
88 meter
Z = -17539107
07 Z = -5331655
95
XDOT = -17170
968442 XDOT = -5296
859885
YDOT = 18280
429303 feet/sec YDOT = 5512
995018 meter/sec
ZDOT = 831
879306 ZDOT = 227
979025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11675334
93 X = 3558642
09
Y = -7481269
40 feet Y = -2280290
91 meter
Z = -17479118
82 Z = -5327635
42
XDOT = 13742
520062 XDOT = 4188
720115
YDOT = 19765
058505 feet/sec YDOT = 6024
389832 meter/sec
ZDOT = 722
527698 ZDOT = 220
226442
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 14161
51576330
00016717 00000-0 10270-3 0 9066
2 25544 51
6426 132
6575 0004233 81
8074 278
3557 15
50604813 10297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14161
51576330 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 132
6575 deg
Eccentricity:
0004233
Arg of perigee: 81
8074 deg
Mean anomaly: 278
3557 deg
Mean motion: 15
50604813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 297
Coasting Arc #8 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2014/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2725792
23 A = 6787809
16 meter
Y = -3268818
29 meter E =
0007327
Z = 5281831
98 I = 51
90841
XDOT = 5091
824463 Wp = 73
98390
YDOT = -5666
330293 meter/sec RA = 126
77133 deg
ZDOT = -876
064609 TA = 24
38009
MA = 24
34545
Ha = 228
149 n
mi
Hp = 218
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8942887
91 X = -2714694
76
Y = -10724469
46 feet Y = -3299238
50 meter
Z = 17328845
07 Z = 5268616
81
XDOT = 16705
460835 XDOT = 5159
063915
YDOT = -18590
322484 feet/sec YDOT = -5609
014168 meter/sec
ZDOT = -2874
227719 ZDOT = -851
166332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12261998
29 X = -3737457
08
Y = 6822994
34 feet Y = 2079648
67 meter
Z = 17273346
72 Z = 5264916
08
XDOT = -14534
297838 XDOT = -4430
053981
YDOT = -19088
765266 feet/sec YDOT = -5818
255653 meter/sec
ZDOT = -2767
718589 ZDOT = -843
600626
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 14162
54692274
00016717 00000-0 10270-3 0 9077
2 25544 51
6430 127
5441 0004182 84
4697 275
6930 15
50621406 10450
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
54692274 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 127
5441 deg
Eccentricity:
0004182
Arg of perigee: 84
4697 deg
Mean anomaly: 275
6930 deg
Mean motion: 15
50621406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 301
Coasting Arc #9 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2014/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2570387
99 A = 6788274
59 meter
Y = 3565696
42 meter E =
0017813
Z = -5188734
62 I = 51
92854
XDOT = -4896
904201 Wp = 98
14399
YDOT = 5686
023743 meter/sec RA = 121
82727 deg
ZDOT = 1483
515109 TA = 186
10713
MA = 186
12887
Ha = 228
035 n
mi
Hp = 218
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8433031
46 X = 2555529
97
Y = 11698479
06 feet Y = 3594357
84 meter
Z = -17023407
55 Z = -5176283
48
XDOT = -16065
958665 XDOT = -4967
329170
YDOT = 18654
933540 feet/sec YDOT = 5630
869427 meter/sec
ZDOT = 4867
175553 ZDOT = 1459
556186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13012135
38 X = 3966098
86
Y = -6358427
01 feet Y = -1938048
55 meter
Z = -16971198
41 Z = -5172821
27
XDOT = 15083
310833 XDOT = 4597
393142
YDOT = 18166
602900 feet/sec YDOT = 5537
180564 meter/sec
ZDOT = 4764
623005 ZDOT = 1452
257092
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 14163
51362827
00016717 00000-0 10270-3 0 9084
2 25544 51
6437 122
7500 0004153 87
4765 272
6861 15
50626003 10602
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
51362827 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 122
7500 deg
Eccentricity:
0004153
Arg of perigee: 87
4765 deg
Mean anomaly: 272
6861 deg
Mean motion: 15
50626003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 290
Coasting Arc #10 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2432184
14 A = 6788918
76 meter
Y = -3874225
29 meter E =
0009763
Z = 5009495
61 I = 51
94744
XDOT = 4714
010084 Wp = 70
59942
YDOT = -5674
352290 meter/sec RA = 116
88547 deg
ZDOT = -2093
214633 TA = 39
71919
MA = 39
64774
Ha = 228
086 n
mi
Hp = 218
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7979606
77 X = -2413015
54
Y = -12710712
89 feet Y = -3901317
13 meter
Z = 16435353
05 Z = 4997726
30
XDOT = 15465
912349 XDOT = 4787
279834
YDOT = -18616
641370 feet/sec YDOT = -5621
227201 meter/sec
ZDOT = -6867
502077 ZDOT = -2070
137441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13828043
32 X = -4214787
60
Y = 5969802
00 feet Y = 1819595
65 meter
Z = 16386087
33 Z = 4994479
42
XDOT = -15493
483024 XDOT = -4722
413626
YDOT = -17250
738684 feet/sec YDOT = -5258
025151 meter/sec
ZDOT = -6768
668718 ZDOT = -2063
090225
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 14164
54477511
00016717 00000-0 10270-3 0 9096
2 25544 51
6446 117
6370 0004132 90
7334 269
4290 15
50644457 10766
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54477511 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 117
6370 deg
Eccentricity:
0004132
Arg of perigee: 90
7334 deg
Mean anomaly: 269
4290 deg
Mean motion: 15
50644457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 306
Coasting Arc #11 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2014/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2363477
27 A = 6789803
50 meter
Y = 4191460
05 meter E =
0015216
Z = -4804648
06 I = 51
96419
XDOT = -4497
607463 Wp = 104
71881
YDOT = 5586
158603 meter/sec RA = 111
94494 deg
ZDOT = 2664
082039 TA = 191
50265
MA = 191
53746
Ha = 227
970 n
mi
Hp = 218
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7754190
51 X = 2339771
16
Y = 13751509
34 feet Y = 4217758
15 meter
Z = -15763281
05 Z = -4793223
57
XDOT = -14755
929997 XDOT = -4572
680129
YDOT = 18327
292004 feet/sec YDOT = 5535
443307 meter/sec
ZDOT = 8740
426636 ZDOT = 2642
051811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14721306
70 X = 4487054
28
Y = -5832470
51 feet Y = -1777737
01 meter
Z = -15715531
36 Z = -4790093
96
XDOT = 15627
538050 XDOT = 4763
273598
YDOT = 16176
849989 feet/sec YDOT = 4930
703877 meter/sec
ZDOT = 8646
029431 ZDOT = 2635
309770
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 14165
51146886
00016717 00000-0 10270-3 0 9104
2 25544 51
6451 112
8432 0004074 93
5620 266
5997 15
50649605 10911
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
51146886 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 112
8432 deg
Eccentricity:
0004074
Arg of perigee: 93
5620 deg
Mean anomaly: 266
5997 deg
Mean motion: 15
50649605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 309
Coasting Arc #12 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2014/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2310824
04 A = 6790846
89 meter
Y = -4508572
07 meter E =
0012680
Z = 4512867
43 I = 51
97945
XDOT = 4311
512633 Wp = 77
23801
YDOT = -5455
670461 meter/sec RA = 107
00655 deg
ZDOT = -3232
400926 TA = 45
16284
MA = 45
05987
Ha = 228
012 n
mi
Hp = 218
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7581443
70 X = -2282158
36
Y = -14791903
13 feet Y = -4534253
54 meter
Z = 14805995
52 Z = 4501710
83
XDOT = 14145
382653 XDOT = 4387
900624
YDOT = -17899
181302 feet/sec YDOT = -5407
028797 meter/sec
ZDOT = -10604
989914 ZDOT = -3211
271524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15629035
46 X = -4763730
01
Y = 5778277
05 feet Y = 1761218
85 meter
Z = 14759436
13 Z = 4498676
13
XDOT = -15575
566397 XDOT = -4747
432638
YDOT = -15184
641540 feet/sec YDOT = -4628
278741 meter/sec
ZDOT = -10514
420196 ZDOT = -3204
795276
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 14166
54260294
00016717 00000-0 10270-3 0 9119
2 25544 51
6459 107
7303 0004076 97
1501 263
0113 15
50667657 11076
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
54260294 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 107
7303 deg
Eccentricity:
0004076
Arg of perigee: 97
1501 deg
Mean anomaly: 263
0113 deg
Mean motion: 15
50667657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 289
Coasting Arc #13 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2014/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2330451
04 A = 6791996
73 meter
Y = 4810045
37 meter E =
0011786
Z = -4202934
39 I = 51
99159
XDOT = -4113
901874 Wp = 106
48321
YDOT = 5257
279743 meter/sec RA = 102
06922 deg
ZDOT = 3741
040630 TA = 201
84149
MA = 201
89178
Ha = 227
906 n
mi
Hp = 218
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7645836
74 X = 2296907
17
Y = 15780988
76 feet Y = 4835918
92 meter
Z = -13789154
82 Z = -4191694
36
XDOT = -13497
053394 XDOT = -4190
556860
YDOT = 17248
293121 feet/sec YDOT = 5210
846398 meter/sec
ZDOT = 12273
755348 ZDOT = 3720
870456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16517031
61 X = 5034391
23
Y = -5998020
11 feet Y = -1828196
53 meter
Z = -13742293
76 Z = -4188651
14
XDOT = 15259
277898 XDOT = 4651
027903
YDOT = 14138
449354 feet/sec YDOT = 4309
399363 meter/sec
ZDOT = 12187
276327 ZDOT = 3714
681824
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 14167
50928485
00016717 00000-0 10270-3 0 9120
2 25544 51
6459 102
9365 0004027 100
1310 260
0295 15
50674404 11223
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
50928485 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 102
9365 deg
Eccentricity:
0004027
Arg of perigee: 100
1310 deg
Mean anomaly: 260
0295 deg
Mean motion: 15
50674404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 277
Coasting Arc #14 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2014/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2359069
77 A = 6793271
61 meter
Y = -5098428
72 meter E =
0015329
Z = 3806753
21 I = 52
00195
XDOT = 3964
776073 Wp = 88
41201
YDOT = -5011
015069 meter/sec RA = 97
13364 deg
ZDOT = -4239
204899 TA = 46
20168
MA = 46
07499
Ha = 227
938 n
mi
Hp = 218
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7739730
22 X = -2320374
50
Y = -16727128
35 feet Y = -5124593
38 meter
Z = 12489347
79 Z = 3795386
73
XDOT = 13007
795516 XDOT = 4041
108264
YDOT = -16440
338154 feet/sec YDOT = -4966
251174 meter/sec
ZDOT = -13908
152557 ZDOT = -4219
759803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17361546
69 X = -5291799
43
Y = 6281507
52 feet Y = 1914603
49 meter
Z = 12442002
04 Z = 3792322
22
XDOT = -14738
757180 XDOT = -4492
373189
YDOT = -13254
874083 feet/sec YDOT = -4040
085621 meter/sec
ZDOT = -13824
781977 ZDOT = -4213
793547
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 14168
54040598
00016717 00000-0 10270-3 0 9136
2 25544 51
6462 97
8232 0004036 103
7346 256
4254 15
50687311 11382
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
54040598 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 97
8232 deg
Eccentricity:
0004036
Arg of perigee: 103
7346 deg
Mean anomaly: 256
4254 deg
Mean motion: 15
50687311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 302
Coasting Arc #15 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2014/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2454768
93 A = 6794471
87 meter
Y = 5349171
46 meter E =
0008694
Z = -3403444
89 I = 52
00901
XDOT = -3824
590046 Wp = 96
96259
YDOT = 4715
261637 meter/sec RA = 92
19889 deg
ZDOT = 4661
595303 TA = 223
60325
MA = 223
67200
Ha = 227
838 n
mi
Hp = 218
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8053703
84 X = 2411303
59
Y = 17549775
14 feet Y = 5376379
53 meter
Z = -11166157
76 Z = -3391625
14
XDOT = -12547
867606 XDOT = -3899
677346
YDOT = 15470
018494 feet/sec YDOT = 4672
072381 meter/sec
ZDOT = 15293
947843 ZDOT = 4642
834087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18093766
92 X = 5514980
16
Y = -6824159
41 feet Y = -2080003
79 meter
Z = -11116936
59 Z = -3388442
27
XDOT = 14011
951788 XDOT = 4270
842905
YDOT = 12417
256337 feet/sec YDOT = 3784
779731 meter/sec
ZDOT = 15213
521251 ZDOT = 4637
081277
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 14169
50707577
00016717 00000-0 10270-3 0 9141
2 25544 51
6462 93
0290 0003998 106
9791 253
1799 15
50699157 11535
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
50707577 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 93
0290 deg
Eccentricity:
0003998
Arg of perigee: 106
9791 deg
Mean anomaly: 253
1799 deg
Mean motion: 15
50699157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 340
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