[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 20th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 34982 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 2329)
---------------------------------------
Vector Time (GMT): 2013/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3476314
36 A = 6792638
53 meter
Y = 3521767
88 meter E =
0005436
Z = 4653319
26 I = 51
28280
XDOT = -2788
636513 Wp = 27
36585
YDOT = 6537
155914 meter/sec RA = 274
29505 deg
ZDOT = -2858
151190 TA = 91
23328
MA = 91
17100
Ha = 226
129 n
mi
Hp = 223
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11405230
83 X = 3414070
30
Y = 11554356
56 feet Y = 3560293
72 meter
Z = 15266795
47 Z = 4670056
02
XDOT = -9149
069923 XDOT = -2847
645100
YDOT = 21447
361921 feet/sec YDOT = 6505
641969 meter/sec
ZDOT = -9377
136449 ZDOT = -2871
840736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12235148
50 X = -3729273
26
Y = 10571045
50 feet Y = 3222054
67 meter
Z = 15336610
71 Z = 4674598
94
XDOT = -20070
336043 XDOT = -6117
438426
YDOT = -9511
460380 feet/sec YDOT = -2899
093124 meter/sec
ZDOT = -9435
792306 ZDOT = -2876
029495
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 13352
54324941
00016717 00000-0 10270-3 0 9003
2 25544 51
6495 274
8966 0004977 285
2503 74
8097 15
49829233 23305
Satellite: ISS
Catalog Number: 25544
Epoch time: 13352
54324941 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 274
8966 deg
Eccentricity:
0004977
Arg of perigee: 285
2503 deg
Mean anomaly: 74
8097 deg
Mean motion: 15
49829233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 332
Coasting Arc #2 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2013/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658104
74 A = 6793061
00 meter
Y = -3530211
84 meter E =
0004699
Z = -4510464
08 I = 51
28346
XDOT = 2440
568367 Wp = 111
81972
YDOT = -6541
902149 meter/sec RA = 269
31601 deg
ZDOT = 3141
728547 TA = 189
90422
MA = 189
91349
Ha = 226
181 n
mi
Hp = 223
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12001655
98 X = -3596446
77
Y = -11582059
86 feet Y = -3570773
91 meter
Z = -14798110
51 Z = -4528085
30
XDOT = 8007
114065 XDOT = 2498
278405
YDOT = -21462
933561 feet/sec YDOT = -6514
287789 meter/sec
ZDOT = 10307
508356 ZDOT = 3153
724079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12106030
31 X = 3689918
04
Y = -11377426
02 feet Y = -3467839
45 meter
Z = -14871655
55 Z = -4532880
61
XDOT = 20254
386240 XDOT = 6173
536926
YDOT = 8014
954700 feet/sec YDOT = 2442
958193 meter/sec
ZDOT = 10359
031916 ZDOT = 3157
432928
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 13353
51044327
00016717 00000-0 10270-3 0 9019
2 25544 51
6496 270
1061 0005002 288
9807 71
0801 15
49875396 23457
Satellite: ISS
Catalog Number: 25544
Epoch time: 13353
51044327 = yrday
fracday
Element set: 901
Inclination: 51
6496 deg
RA of node: 270
1061 deg
Eccentricity:
0005002
Arg of perigee: 288
9807 deg
Mean anomaly: 71
0801 deg
Mean motion: 15
49875396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 300
Coasting Arc #3 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2013/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3842966
36 A = 6793618
83 meter
Y = 3548355
56 meter E =
0006679
Z = 4334334
40 I = 51
28648
XDOT = -2123
457047 Wp = 42
17181
YDOT = 6508
278318 meter/sec RA = 264
33798 deg
ZDOT = -3437
395328 TA = 82
97094
MA = 82
89499
Ha = 226
259 n
mi
Hp = 223
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12608157
36 X = 3781947
39
Y = 11641586
49 feet Y = 3590988
52 meter
Z = 14220257
22 Z = 4352855
13
XDOT = -6966
722596 XDOT = -2179
378437
YDOT = 21352
619153 feet/sec YDOT = 6484
220084 meter/sec
ZDOT = -11277
543728 ZDOT = -3447
846090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11984873
99 X = -3652989
59
Y = 12192188
57 feet Y = 3716179
08 meter
Z = 14297594
79 Z = 4357906
89
XDOT = -20263
519643 XDOT = -6176
320787
YDOT = -6610
722595 feet/sec YDOT = -2014
948247 meter/sec
ZDOT = -11322
554606 ZDOT = -3451
114644
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 13354
54209187
00016717 00000-0 10270-3 0 9021
2 25544 51
6492 264
9970 0004991 292
6300 67
4322 15
49906866 23611
Satellite: ISS
Catalog Number: 25544
Epoch time: 13354
54209187 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 264
9970 deg
Eccentricity:
0004991
Arg of perigee: 292
6300 deg
Mean anomaly: 67
4322 deg
Mean motion: 15
49906866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 326
Coasting Arc #4 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2013/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049161
69 A = 6794147
96 meter
Y = -3545814
11 meter E =
0002786
Z = -4148972
57 I = 51
29307
XDOT = 1825
534905 Wp = 97
45684
YDOT = -6438
239278 meter/sec RA = 259
35898 deg
ZDOT = 3722
463210 TA = 211
06546
MA = 211
08194
Ha = 226
287 n
mi
Hp = 222
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13284651
22 X = -3989056
26
Y = -11633248
41 feet Y = -3590758
06 meter
Z = -13612114
72 Z = -4168497
12
XDOT = 5989
287746 XDOT = 1879
310489
YDOT = -21122
832276 feet/sec YDOT = -6417
524567 meter/sec
ZDOT = 12212
805807 ZDOT = 3731
461583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11772119
29 X = 3588141
96
Y = -13076858
33 feet Y = -3985826
42 meter
Z = -13693687
51 Z = -4173835
95
XDOT = 20105
080342 XDOT = 6128
028488
YDOT = 5275
671436 feet/sec YDOT = 1608
024654 meter/sec
ZDOT = 12251
685577 ZDOT = 3734
313764
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 13355
50923810
00016717 00000-0 10270-3 0 9035
2 25544 51
6496 260
2061 0005042 296
2028 63
8604 15
49953150 23767
Satellite: ISS
Catalog Number: 25544
Epoch time: 13355
50923810 = yrday
fracday
Element set: 903
Inclination: 51
6496 deg
RA of node: 260
2061 deg
Eccentricity:
0005042
Arg of perigee: 296
2028 deg
Mean anomaly: 63
8604 deg
Mean motion: 15
49953150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 296
Coasting Arc #5 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2013/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258229
44 A = 6794818
52 meter
Y = 3550724
34 meter E =
0007864
Z = 3925843
04 I = 51
30163
XDOT = -1569
441695 Wp = 55
85282
YDOT = 6332
526744 meter/sec RA = 254
38121 deg
ZDOT = -4014
996916 TA = 76
37800
MA = 76
29044
Ha = 226
415 n
mi
Hp = 222
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13970569
02 X = 4199137
45
Y = 11649358
08 feet Y = 3598011
96 meter
Z = 12880062
47 Z = 3946385
63
XDOT = -5149
086926 XDOT = -1620
633170
YDOT = 20776
006379 feet/sec YDOT = 6314
690244 meter/sec
ZDOT = -13172
562061 ZDOT = -4022
745045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11556844
80 X = -3522526
30
Y = 13967976
54 feet Y = 4257439
25 meter
Z = 12965929
25 Z = 3952015
24
XDOT = -19789
914790 XDOT = -6031
966028
YDOT = -4084
404008 feet/sec YDOT = -1244
926342 meter/sec
ZDOT = -13206
155155 ZDOT = -4025
236091
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 13356
54083668
00016717 00000-0 10270-3 0 9049
2 25544 51
6490 255
0964 0005036 300
0952 59
9699 15
49983446 23927
Satellite: ISS
Catalog Number: 25544
Epoch time: 13356
54083668 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 255
0964 deg
Eccentricity:
0005036
Arg of perigee: 300
0952 deg
Mean anomaly: 59
9699 deg
Mean motion: 15
49983446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 340
Coasting Arc #6 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2013/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4484408
13 A = 6795436
89 meter
Y = -3524125
74 meter E =
0002162
Z = -3694030
56 I = 51
31385
XDOT = 1340
531571 Wp = 38
03330
YDOT = -6200
736201 meter/sec RA = 249
40319 deg
ZDOT = 4291
201053 TA = 277
82540
MA = 277
84993
Ha = 226
419 n
mi
Hp = 222
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14712625
11 X = -4426722
81
Y = -11562092
33 feet Y = -3573950
55 meter
Z = -12119522
82 Z = -3715675
29
XDOT = 4398
069460 XDOT = 1388
924608
YDOT = -20343
622707 feet/sec YDOT = -6185
475131 meter/sec
ZDOT = 14078
743611 ZDOT = 4297
830458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11209698
76 X = 3416716
18
Y = -14909180
83 feet Y = -4544318
32 meter
Z = -12210042
21 Z = -3721620
86
XDOT = 19352
522056 XDOT = 5898
648723
YDOT = 3004
961257 feet/sec YDOT = 915
912191 meter/sec
ZDOT = 14107
599832 ZDOT = 4299
996429
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 13357
50793638
00016717 00000-0 10270-3 0 9052
2 25544 51
6496 250
3050 0005152 303
3602 56
7055 15
50026186 24073
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
50793638 = yrday
fracday
Element set: 905
Inclination: 51
6496 deg
RA of node: 250
3050 deg
Eccentricity:
0005152
Arg of perigee: 303
3602 deg
Mean anomaly: 56
7055 deg
Mean motion: 15
50026186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 289
Coasting Arc #7 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2013/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711034
01 A = 6796168
60 meter
Y = 3502478
06 meter E =
0008865
Z = 3420535
23 I = 51
32799
XDOT = -1163
418818 Wp = 68
79462
YDOT = 6038
524603 meter/sec RA = 244
42681 deg
ZDOT = -4568
076545 TA = 71
05179
MA = 70
95573
Ha = 226
580 n
mi
Hp = 222
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15456148
34 X = 4654902
44
Y = 11491069
75 feet Y = 3554845
87 meter
Z = 11222228
43 Z = 3443284
68
XDOT = -3816
990873 XDOT = -1208
666106
YDOT = 19811
432424 feet/sec YDOT = 6025
261686 meter/sec
ZDOT = -14987
127772 ZDOT = -4573
837984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10849746
87 X = -3307002
85
Y = 15845341
18 feet Y = 4829659
99 meter
Z = 11317410
14 Z = 3449546
61
XDOT = -18791
044170 XDOT = -5727
510263
YDOT = -2114
699025 feet/sec YDOT = -644
560263 meter/sec
ZDOT = -15012
298741 ZDOT = -4575
748656
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 13358
53948633
00016717 00000-0 10270-3 0 9064
2 25544 51
6492 245
1947 0005122 307
5411 52
5273 15
50058492 24236
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
53948633 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 245
1947 deg
Eccentricity:
0005122
Arg of perigee: 307
5411 deg
Mean anomaly: 52
5273 deg
Mean motion: 15
50058492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 304
Coasting Arc #8 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2013/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4946861
42 A = 6796837
77 meter
Y = -3440251
45 meter E =
0004402
Z = -3140040
61 I = 51
34510
XDOT = 1019
163130 Wp = 5
39280
YDOT = -5863
484684 meter/sec RA = 239
45073 deg
ZDOT = 4823
323848 TA = 318
32347
MA = 318
35700
Ha = 226
575 n
mi
Hp = 222
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16229860
30 X = -4892770
67
Y = -11286914
20 feet Y = -3495267
86 meter
Z = -10301970
49 Z = -3163940
69
XDOT = 3343
711057 XDOT = 1061
223826
YDOT = -19237
154476 feet/sec YDOT = -5851
852743 meter/sec
ZDOT = 15824
553306 ZDOT = 4828
376801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10326259
80 X = 3147443
99
Y = -16795828
71 feet Y = -5119368
59 meter
Z = -10402013
75 Z = -3170533
79
XDOT = 18167
502466 XDOT = 5537
454752
YDOT = 1365
135891 feet/sec YDOT = 416
093420 meter/sec
ZDOT = 15846
709918 ZDOT = 4830
077183
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 13359
50654081
00016717 00000-0 10270-3 0 9074
2 25544 51
6496 240
4030 0005311 310
3971 49
6716 15
50094294 24389
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
50654081 = yrday
fracday
Element set: 907
Inclination: 51
6496 deg
RA of node: 240
4030 deg
Eccentricity:
0005311
Arg of perigee: 310
3971 deg
Mean anomaly: 49
6716 deg
Mean motion: 15
50094294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 297
Coasting Arc #9 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2013/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5178371
54 A = 6797557
26 meter
Y = 3381253
20 meter E =
0009534
Z = 2814881
31 I = 51
36425
XDOT = -934
638268 Wp = 81
20729
YDOT = 5665
852804 meter/sec RA = 234
47691 deg
ZDOT = -5070
264895 TA = 66
76489
MA = 66
66453
Ha = 226
746 n
mi
Hp = 222
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16989407
95 X = 5126502
82
Y = 11093350
38 feet Y = 3438870
92 meter
Z = 9235174
91 Z = 2839911
53
XDOT = -3066
398518 XDOT = -973
295651
YDOT = 18588
755920 feet/sec YDOT = 5655
185137 meter/sec
ZDOT = -16634
727346 ZDOT = -5074
898959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9784907
38 X = -2982439
77
Y = 17720354
86 feet Y = 5401164
16 meter
Z = 9339993
15 Z = 2846829
91
XDOT = -17465
725271 XDOT = -5323
553063
YDOT = -838
100388 feet/sec YDOT = -255
452998 meter/sec
ZDOT = -16655
086848 ZDOT = -5076
470471
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 13360
53804340
00016717 00000-0 10270-3 0 9085
2 25544 51
6495 235
2924 0005245 314
7788 45
2935 15
50131120 24545
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
53804340 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 235
2924 deg
Eccentricity:
0005245
Arg of perigee: 314
7788 deg
Mean anomaly: 45
2935 deg
Mean motion: 15
50131120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 294
Coasting Arc #10 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2013/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5408120
90 A = 6798211
44 meter
Y = -3275741
17 meter E =
0007423
Z = -2485647
64 I = 51
38516
XDOT = 885
463610 Wp = 2
78925
YDOT = -5470
720841 meter/sec RA = 229
50360 deg
ZDOT = 5291
052165 TA = 329
29042
MA = 329
33383
Ha = 226
743 n
mi
Hp = 222
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17743178
80 X = -5359014
26
Y = -10747182
30 feet Y = -3335943
52 meter
Z = -8155011
94 Z = -2511800
75
XDOT = 2905
064337 XDOT = 920
870070
YDOT = -17948
559189 feet/sec YDOT = -5460
621329 meter/sec
ZDOT = 17359
095030 ZDOT = 5295
439392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9063456
42 X = 2762541
52
Y = -18611205
52 feet Y = -5672695
44 meter
Z = -8264582
74 Z = -2519044
82
XDOT = 16771
811359 XDOT = 5112
048102
YDOT = 461
966597 feet/sec YDOT = 140
807419 meter/sec
ZDOT = 17378
383915 ZDOT = 5296
931417
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 13361
50505388
00016717 00000-0 10270-3 0 9094
2 25544 51
6493 230
5004 0005471 317
2815 42
7910 15
50159184 24691
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
50505388 = yrday
fracday
Element set: 909
Inclination: 51
6493 deg
RA of node: 230
5004 deg
Eccentricity:
0005471
Arg of perigee: 317
2815 deg
Mean anomaly: 42
7910 deg
Mean motion: 15
50159184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 299
Coasting Arc #11 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2013/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5626757
28 A = 6798827
79 meter
Y = 3173514
23 meter E =
0009714
Z = 2110059
51 I = 51
40822
XDOT = -900
608964 Wp = 93
08557
YDOT = 5263
042954 meter/sec RA = 224
53313 deg
ZDOT = -5492
544640 TA = 63
50833
MA = 63
40874
Ha = 226
904 n
mi
Hp = 221
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18460489
76 X = 5580602
02
Y = 10411792
10 feet Y = 3236178
00 meter
Z = 6922767
41 Z = 2137281
96
XDOT = -2954
753819 XDOT = -932
713192
YDOT = 17267
201293 feet/sec YDOT = 5252
792657 meter/sec
ZDOT = -18020
159581 ZDOT = -5496
997332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8328972
09 X = -2538670
69
Y = 19448149
91 feet Y = 5927796
09 meter
Z = 7036866
84 Z = 2144837
01
XDOT = -16055
108347 XDOT = -4893
597024
YDOT = -323
563134 feet/sec YDOT = -98
622043 meter/sec
ZDOT = -18039
692065 ZDOT = -5498
498141
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 13362
53650994
00016717 00000-0 10270-3 0 9104
2 25544 51
6491 225
3897 0005389 321
6606 38
4161 15
50201915 24854
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
53650994 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 225
3897 deg
Eccentricity:
0005389
Arg of perigee: 321
6606 deg
Mean anomaly: 38
4161 deg
Mean motion: 15
50201915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 312
Coasting Arc #12 (Orbit 2499)
---------------------------------------
Vector Time (GMT): 2013/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5830715
23 A = 6799378
71 meter
Y = -3023152
86 meter E =
0010439
Z = -1734571
85 I = 51
43182
XDOT = 949
901605 Wp = 7
76406
YDOT = -5073
959996 meter/sec RA = 219
56301 deg
ZDOT = 5664
368239 TA = 333
17436
MA = 333
22830
Ha = 226
910 n
mi
Hp = 221
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19129643
13 X = -5788050
22
Y = -9918480
51 feet Y = -3088116
92 meter
Z = -5690852
53 Z = -1762793
61
XDOT = 3116
475081 XDOT = 979
053175
YDOT = -16646
850380 feet/sec YDOT = -5063
175122 meter/sec
ZDOT = 18583
885297 ZDOT = 5669
053114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7417957
69 X = 2260993
50
Y = -20197337
72 feet Y = -6156148
54 meter
Z = -5809195
93 Z = -1770642
92
XDOT = 15418
567780 XDOT = 4699
579459
YDOT = 324
875257 feet/sec YDOT = 99
021978 meter/sec
ZDOT = 18604
367137 ZDOT = 5670
611103
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 13363
50347721
00016717 00000-0 10270-3 0 9114
2 25544 51
6480 220
5971 0005589 324
0492 36
0282 15
50223730 25009
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
50347721 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 220
5971 deg
Eccentricity:
0005589
Arg of perigee: 324
0492 deg
Mean anomaly: 36
0282 deg
Mean motion: 15
50223730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2500
Checksum: 277
Coasting Arc #13 (Orbit 2515)
---------------------------------------
Vector Time (GMT): 2013/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6015465
70 A = 6799787
44 meter
Y = 2878751
13 meter E =
0009270
Z = 1312748
73 I = 51
45765
XDOT = -1063
421275 Wp = 104
05930
YDOT = 4883
713655 meter/sec RA = 214
59611 deg
ZDOT = -5804
288513 TA = 61
64427
MA = 61
55082
Ha = 227
048 n
mi
Hp = 221
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19735779
84 X = 5976450
82
Y = 9444721
55 feet Y = 2945801
61 meter
Z = 4306918
42 Z = 1341876
78
XDOT = -3488
914943 XDOT = -1089
757449
YDOT = 16022
682596 feet/sec YDOT = 4871
675190 meter/sec
ZDOT = -19042
941314 ZDOT = -5809
517928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6512067
42 X = -1984878
15
Y = 20862147
98 feet Y = 6358782
70 meter
Z = 4429116
95 Z = 1349994
85
XDOT = -14817
920690 XDOT = -4516
502226
YDOT = -555
753597 feet/sec YDOT = -169
393696 meter/sec
ZDOT = -19065
687836 ZDOT = -5811
221652
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 13364
53488695
00016717 00000-0 10270-3 0 9125
2 25544 51
6476 215
4860 0005537 328
3060 31
7756 15
50273956 25165
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
53488695 = yrday
fracday
Element set: 912
Inclination: 51
6476 deg
RA of node: 215
4860 deg
Eccentricity:
0005537
Arg of perigee: 328
3060 deg
Mean anomaly: 31
7756 deg
Mean motion: 15
50273956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2516
Checksum: 324
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