[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 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 3138)
---------------------------------------
Vector Time (GMT): 2014/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -367220
93 A = 6787026
42 meter
Y = 4223703
10 meter E =
0012121
Z = -5310354
28 I = 51
63648
XDOT = -7638
516212 Wp = 86
71143
YDOT = -50
971195 meter/sec RA = 177
47586 deg
ZDOT = 489
321726 TA = 187
95551
MA = 187
97475
Ha = 225
381 n
mi
Hp = 220
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1204793
08 X = -388627
36
Y = 13857293
65 feet Y = 4219476
49 meter
Z = -17422422
19 Z = -5312190
57
XDOT = -25060
748728 XDOT = -7639
755556
YDOT = -167
228331 feet/sec YDOT = -136
396924 meter/sec
ZDOT = 1605
386240 ZDOT = 452
210861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6410094
38 X = -1953796
77
Y = -12332562
35 feet Y = -3758965
01 meter
Z = -17430877
90 Z = -5312931
58
XDOT = 20454
165036 XDOT = 6234
429503
YDOT = -12669
568694 feet/sec YDOT = -3861
684538 meter/sec
ZDOT = 1447
382621 ZDOT = 441
162223
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 14297
51536800
00016717 00000-0 10270-3 0 9008
2 25544 51
6462 178
5197 0003116 302
4915 57
5934 15
50834477 31392
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
51536800 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 178
5197 deg
Eccentricity:
0003116
Arg of perigee: 302
4915 deg
Mean anomaly: 57
5934 deg
Mean motion: 15
50834477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 314
Coasting Arc #2 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2014/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 797708
49 A = 6787203
84 meter
Y = -4266171
64 meter E =
0004043
Z = 5218334
32 I = 51
66868
XDOT = 7570
135977 Wp = 9
21276
YDOT = -45
678591 meter/sec RA = 172
51164 deg
ZDOT = -1190
537222 TA = 92
23315
MA = 92
18686
Ha = 225
272 n
mi
Hp = 220
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2617153
82 X = 820004
82
Y = -13996626
12 feet Y = -4257126
17 meter
Z = 17120519
42 Z = 5222264
00
XDOT = 24836
404125 XDOT = 7575
867539
YDOT = -149
864144 feet/sec YDOT = 39
007550 meter/sec
ZDOT = -3905
962015 ZDOT = -1153
747617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5510609
50 X = 1679633
78
Y = 13106973
46 feet Y = 3995005
51 meter
Z = 17137901
03 Z = 5223632
23
XDOT = -19819
851561 XDOT = -6041
090756
YDOT = 13252
539390 feet/sec YDOT = 4039
374006 meter/sec
ZDOT = -3749
294374 ZDOT = -1142
784925
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 14298
54638240
00016717 00000-0 10270-3 0 9014
2 25544 51
6460 173
4055 0003216 304
9838 55
1011 15
50897795 31559
Satellite: ISS
Catalog Number: 25544
Epoch time: 14298
54638240 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 173
4055 deg
Eccentricity:
0003216
Arg of perigee: 304
9838 deg
Mean anomaly: 55
1011 deg
Mean motion: 15
50897795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 307
Coasting Arc #3 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2014/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1217903
59 A = 6787794
00 meter
Y = 4363976
71 meter E =
0010208
Z = -5063466
16 I = 51
70097
XDOT = -7418
945099 Wp = 96
47461
YDOT = 113
848735 meter/sec RA = 167
54877 deg
ZDOT = 1884
728554 TA = 191
79629
MA = 191
82023
Ha = 225
314 n
mi
Hp = 220
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3995746
69 X = -1242014
72
Y = 14317508
90 feet Y = 4350222
30 meter
Z = -16612421
77 Z = -5069441
47
XDOT = -24340
371060 XDOT = -7428
822435
YDOT = 373
519471 feet/sec YDOT = 30
830137 meter/sec
ZDOT = 6183
492630 ZDOT = 1848
663402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4768334
10 X = -1453388
23
Y = -14048191
43 feet Y = -4281888
75 meter
Z = -16638537
11 Z = -5071426
11
XDOT = 18988
706282 XDOT = 5787
757675
YDOT = -13578
682155 feet/sec YDOT = -4138
782321 meter/sec
ZDOT = 6029
880634 ZDOT = 1837
907617
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 14299
51292801
00016717 00000-0 10270-3 0 9022
2 25544 51
6451 168
6098 0003283 308
4714 51
6142 15
50931764 31706
Satellite: ISS
Catalog Number: 25544
Epoch time: 14299
51292801 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 168
6098 deg
Eccentricity:
0003283
Arg of perigee: 308
4714 deg
Mean anomaly: 51
6142 deg
Mean motion: 15
50931764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 302
Coasting Arc #4 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2014/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1647124
77 A = 6788593
25 meter
Y = -4494758
60 meter E =
0006921
Z = 4812519
77 I = 51
73473
XDOT = 7214
318879 Wp = 33
31658
YDOT = -128
301702 meter/sec RA = 162
58903 deg
ZDOT = -2581
581183 TA = 82
13021
MA = 82
05166
Ha = 225
209 n
mi
Hp = 220
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5403952
66 X = 1673885
54
Y = -14746583
34 feet Y = -4476189
62 meter
Z = 15789106
85 Z = 4820586
59
XDOT = 23669
025195 XDOT = 7227
758185
YDOT = -420
937342 feet/sec YDOT = -47
551447 meter/sec
ZDOT = -8469
754538 ZDOT = -2546
501542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4096430
62 X = 1248592
05
Y = 15125328
74 feet Y = 4610200
20 meter
Z = 15824158
94 Z = 4823203
65
XDOT = -18101
861019 XDOT = -5517
447239
YDOT = 13632
686512 feet/sec YDOT = 4155
242849 meter/sec
ZDOT = -8320
317546 ZDOT = -2536
032788
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 14300
54387486
00016717 00000-0 10270-3 0 9033
2 25544 51
6451 163
4950 0003412 311
5264 48
5594 15
51004973 31862
Satellite: ISS
Catalog Number: 25544
Epoch time: 14300
54387486 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 163
4950 deg
Eccentricity:
0003412
Arg of perigee: 311
5264 deg
Mean anomaly: 48
5594 deg
Mean motion: 15
51004973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 299
Coasting Arc #5 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2014/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2036016
28 A = 6789775
49 meter
Y = 4668505
01 meter E =
0006607
Z = -4496271
22 I = 51
76738
XDOT = -6936
903843 Wp = 98
69442
YDOT = 93
394798 meter/sec RA = 157
63100 deg
ZDOT = 3241
262494 TA = 203
89719
MA = 203
92787
Ha = 225
271 n
mi
Hp = 220
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6679843
43 X = -2066227
37
Y = 15316617
50 feet Y = 4645567
94 meter
Z = -14751546
01 Z = -4506235
59
XDOT = -22758
870875 XDOT = -6953
177971
YDOT = 306
413378 feet/sec YDOT = 15
730923 meter/sec
ZDOT = 10634
063302 ZDOT = 3207
523766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3652032
02 X = -1113139
36
Y = -16266720
18 feet Y = -4958096
31 meter
Z = -14794717
52 Z = -4509429
90
XDOT = 17117
267254 XDOT = 5217
343059
YDOT = -13374
805316 feet/sec YDOT = -4076
640660 meter/sec
ZDOT = 10490
323375 ZDOT = 3197
450565
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 14301
51035790
00016717 00000-0 10270-3 0 9040
2 25544 51
6440 158
6986 0003412 314
4878 45
5993 15
51028300 32016
Satellite: ISS
Catalog Number: 25544
Epoch time: 14301
51035790 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 158
6986 deg
Eccentricity:
0003412
Arg of perigee: 314
4878 deg
Mean anomaly: 45
5993 deg
Mean motion: 15
51028300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 290
Coasting Arc #6 (Orbit 3216)
---------------------------------------
Vector Time (GMT): 2014/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2416878
22 A = 6791043
95 meter
Y = -4860310
64 meter E =
0009347
Z = 4077742
41 I = 51
80139
XDOT = 6608
801202 Wp = 57
92173
YDOT = 21
818024 meter/sec RA = 152
67711 deg
ZDOT = -3879
677691 TA = 72
23478
MA = 72
13280
Ha = 225
191 n
mi
Hp = 220
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7929390
47 X = 2451239
01
Y = -15945901
05 feet Y = -4833091
33 meter
Z = 13378419
99 Z = 4089567
04
XDOT = 21682
418643 XDOT = 6626
912587
YDOT = 71
581445 feet/sec YDOT = 95
823098 meter/sec
ZDOT = -12728
601349 ZDOT = -3847
528537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3303293
40 X = 1006843
83
Y = 17460365
96 feet Y = 5321919
54 meter
Z = 13429556
52 Z = 4093328
83
XDOT = -16169
647567 XDOT = -4928
508578
YDOT = 12772
440589 feet/sec YDOT = 3893
039891 meter/sec
ZDOT = -12591
632352 ZDOT = -3837
929541
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 14302
54123778
00016717 00000-0 10270-3 0 9059
2 25544 51
6444 153
5833 0003596 317
8471 42
2404 15
51108503 32176
Satellite: ISS
Catalog Number: 25544
Epoch time: 14302
54123778 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 153
5833 deg
Eccentricity:
0003596
Arg of perigee: 317
8471 deg
Mean anomaly: 42
2404 deg
Mean motion: 15
51108503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3217
Checksum: 289
Coasting Arc #7 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2014/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2732240
91 A = 6792548
87 meter
Y = 5071808
62 meter E =
0003682
Z = -3599540
07 I = 51
83269
XDOT = -6231
116907 Wp = 58
41877
YDOT = -201
943556 meter/sec RA = 147
72521 deg
ZDOT = 4450
434311 TA = 259
20636
MA = 259
24781
Ha = 225
250 n
mi
Hp = 220
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8964044
97 X = -2771266
33
Y = 16639792
06 feet Y = 5041036
61 meter
Z = -11809514
68 Z = -3612908
05
XDOT = -20443
296938 XDOT = -6250
014689
YDOT = -662
544476 feet/sec YDOT = -271
729461 meter/sec
ZDOT = 14601
162439 ZDOT = 4420
118115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3205179
61 X = -976938
75
Y = -18590216
23 feet Y = -5666297
91 meter
Z = -11867270
25 Z = -3617143
97
XDOT = 15255
234398 XDOT = 4649
795445
YDOT = -11857
660130 feet/sec YDOT = -3614
214808 meter/sec
ZDOT = 14472
014812 ZDOT = 4411
070115
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 14303
50765858
00016717 00000-0 10270-3 0 9068
2 25544 51
6431 148
7863 0003496 320
6277 39
4620 15
51124306 32320
Satellite: ISS
Catalog Number: 25544
Epoch time: 14303
50765858 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 148
7863 deg
Eccentricity:
0003496
Arg of perigee: 320
6277 deg
Mean anomaly: 39
4620 deg
Mean motion: 15
51124306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 302
Coasting Arc #8 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2014/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3025998
10 A = 6793920
97 meter
Y = -5276034
45 meter E =
0010914
Z = 3019805
49 I = 51
86457
XDOT = 5814
632417 Wp = 82
00765
YDOT = 481
510795 meter/sec RA = 142
77794 deg
ZDOT = -4968
454853 TA = 63
56354
MA = 63
45160
Ha = 225
204 n
mi
Hp = 219
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9927815
29 X = 3070101
62
Y = -17309824
30 feet Y = -5241949
03 meter
Z = 9907498
33 Z = 3034612
93
XDOT = 19076
878009 XDOT = 5832
951347
YDOT = 1579
759827 feet/sec YDOT = 546
635969 meter/sec
ZDOT = -16300
704898 ZDOT = -4940
163370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3185614
71 X = 970975
36
Y = 19666532
57 feet Y = 5994359
13 meter
Z = 9971429
82 Z = 3039291
81
XDOT = -14486
644874 XDOT = -4415
529358
YDOT = 10578
168832 feet/sec YDOT = 3224
225860 meter/sec
ZDOT = -16180
215480 ZDOT = -4931
729678
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 14304
53847152
00016717 00000-0 10270-3 0 9071
2 25544 51
6436 143
6707 0003742 324
2765 35
8135 15
51211718 32484
Satellite: ISS
Catalog Number: 25544
Epoch time: 14304
53847152 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 143
6707 deg
Eccentricity:
0003742
Arg of perigee: 324
2765 deg
Mean anomaly: 35
8135 deg
Mean motion: 15
51211718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 299
Coasting Arc #9 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2014/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3239228
85 A = 6795330
09 meter
Y = 5468205
85 meter E =
0007082
Z = -2394999
51 I = 51
89224
XDOT = -5381
379705 Wp = 17
93722
YDOT = -831
162485 meter/sec RA = 137
83234 deg
ZDOT = 5391
400474 TA = 315
43786
MA = 315
49478
Ha = 225
258 n
mi
Hp = 219
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10627391
23 X = -3288500
56
Y = 17940307
92 feet Y = 5431707
05 meter
Z = -7857609
94 Z = -2410855
47
XDOT = -17655
445228 XDOT = -5397
875529
YDOT = -2726
911040 feet/sec YDOT = -891
432443 meter/sec
ZDOT = 17688
321766 ZDOT = 5365
218137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3380840
21 X = -1030480
10
Y = -20549593
01 feet Y = -6263515
95 meter
Z = -7926050
29 Z = -2415860
13
XDOT = 13884
947023 XDOT = 4232
131853
YDOT = -9050
285193 feet/sec YDOT = -2758
526927 meter/sec
ZDOT = 17576
865871 ZDOT = 5357
428718
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 14305
50482977
00016717 00000-0 10270-3 0 9080
2 25544 51
6422 138
8733 0003546 327
3182 32
7749 15
51219182 32630
Satellite: ISS
Catalog Number: 25544
Epoch time: 14305
50482977 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 138
8733 deg
Eccentricity:
0003546
Arg of perigee: 327
3182 deg
Mean anomaly: 32
7749 deg
Mean motion: 15
51219182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 314
Coasting Arc #10 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2014/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3425055
42 A = 6796291
20 meter
Y = -5619999
36 meter E =
0011033
Z = 1679063
13 I = 51
91914
XDOT = 4928
981987 Wp = 104
26224
YDOT = 1284
934126 meter/sec RA = 132
89109 deg
ZDOT = -5724
824225 TA = 57
43420
MA = 57
32770
Ha = 225
241 n
mi
Hp = 219
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11237058
47 X = 3479488
52
Y = -18438318
11 feet Y = -5581393
69 meter
Z = 5508737
31 Z = 1695834
47
XDOT = 16171
200745 XDOT = 4942
057017
YDOT = 4215
663142 feet/sec YDOT = 1340
125868 meter/sec
ZDOT = -18782
231708 ZDOT = -5700
847888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3587371
32 X = 1093430
78
Y = 21273720
36 feet Y = 6484229
97 meter
Z = 5581114
01 Z = 1701123
55
XDOT = -13526
279845 XDOT = -4122
810097
YDOT = 7206
119159 feet/sec YDOT = 2196
425120 meter/sec
ZDOT = -18680
243001 ZDOT = -5693
738067
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 14306
53557509
00016717 00000-0 10270-3 0 9099
2 25544 51
6424 133
7571 0003836 331
5381 28
5560 15
51317527 32799
Satellite: ISS
Catalog Number: 25544
Epoch time: 14306
53557509 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 133
7571 deg
Eccentricity:
0003836
Arg of perigee: 331
5381 deg
Mean anomaly: 28
5560 deg
Mean motion: 15
51317527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 312
Coasting Arc #11 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2014/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3529249
34 A = 6797120
30 meter
Y = 5724256
71 meter E =
0011844
Z = -941782
20 I = 51
94125
XDOT = -4495
734414 Wp = 23
42882
YDOT = -1800
171977 meter/sec RA = 127
95062 deg
ZDOT = 5941
904402 TA = 326
42587
MA = 326
50087
Ha = 225
299 n
mi
Hp = 219
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11578902
04 X = -3588422
04
Y = 18780369
78 feet Y = 5684459
43 meter
Z = -3089836
63 Z = -959071
31
XDOT = -14749
784824 XDOT = -4504
134769
YDOT = -5906
076041 feet/sec YDOT = -1850
492700 meter/sec
ZDOT = 19494
437013 ZDOT = 5920
044066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3915035
05 X = -1193302
68
Y = -21702053
20 feet Y = -6614785
82 meter
Z = -3164449
31 Z = -964524
15
XDOT = 13436
253131 XDOT = 4095
369954
YDOT = -5236
002585 feet/sec YDOT = -1595
933588 meter/sec
ZDOT = 19401
545940 ZDOT = 5913
591203
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 14307
50186969
00016717 00000-0 10270-3 0 9107
2 25544 51
6411 128
9591 0003571 334
9928 25
1050 15
51316903 32944
Satellite: ISS
Catalog Number: 25544
Epoch time: 14307
50186969 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 128
9591 deg
Eccentricity:
0003571
Arg of perigee: 334
9928 deg
Mean anomaly: 25
1050 deg
Mean motion: 15
51316903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 305
Coasting Arc #12 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2014/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3611207
95 A = 6797197
03 meter
Y = -5752915
56 meter E =
0009109
Z = 135769
72 I = 51
96099
XDOT = 4066
585614 Wp = 122
12227
YDOT = 2403
444205 meter/sec RA = 123
01329 deg
ZDOT = -6032
199839 TA = 56
42374
MA = 56
33680
Ha = 225
297 n
mi
Hp = 219
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11847795
12 X = 3674610
45
Y = -18874394
88 feet Y = -5712178
18 meter
Z = 445438
73 Z = 153467
28
XDOT = 13341
816320 XDOT = 4068
710686
YDOT = 7885
315632 feet/sec YDOT = 2448
930860 meter/sec
ZDOT = -19790
681886 ZDOT = -6012
439480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4142385
45 X = 1262599
08
Y = 21894743
71 feet Y = 6673517
88 meter
Z = 521811
73 Z = 159048
22
XDOT = -13639
097554 XDOT = -4157
196934
YDOT = 3069
534350 feet/sec YDOT = 935
594070 meter/sec
ZDOT = -19706
838479 ZDOT = -6006
644368
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 14308
53254645
00016717 00000-0 10270-3 0 9119
2 25544 51
6411 123
8421 0003862 340
0056 20
0944 15
51421219 33105
Satellite: ISS
Catalog Number: 25544
Epoch time: 14308
53254645 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 123
8421 deg
Eccentricity:
0003862
Arg of perigee: 340
0056 deg
Mean anomaly: 20
0944 deg
Mean motion: 15
51421219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 258
Coasting Arc #13 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2014/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625506
26 A = 6797033
20 meter
Y = 5701264
78 meter E =
0014814
Z = 659425
21 I = 51
97624
XDOT = -3687
321166 Wp = 39
05575
YDOT = -3045
187385 meter/sec RA = 118
07579 deg
ZDOT = 5993
452806 TA = 328
02747
MA = 328
11728
Ha = 225
350 n
mi
Hp = 219
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11894705
59 X = -3692193
03
Y = 18704936
93 feet Y = 5660349
18 meter
Z = 2163468
54 Z = 641650
25
XDOT = -12097
510387 XDOT = -3682
110167
YDOT = -9990
772260 feet/sec YDOT = -3086
391934 meter/sec
ZDOT = 19663
559074 ZDOT = 5975
552667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4355514
76 X = -1327560
90
Y = -21741992
06 feet Y = -6626959
18 meter
Z = 2086757
12 Z = 636043
57
XDOT = 14149
022872 XDOT = 4312
622171
YDOT = -934
249630 feet/sec YDOT = -284
759287 meter/sec
ZDOT = 19587
751834 ZDOT = 5970
346759
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 14309
56319006
00016717 00000-0 10270-3 0 9127
2 25544 51
6406 118
7238 0003583 343
5953 16
5081 15
51425006 33269
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
56319006 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 118
7238 deg
Eccentricity:
0003583
Arg of perigee: 343
5953 deg
Mean anomaly: 16
5081 deg
Mean motion: 15
51425006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 290
Coasting Arc #14 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2014/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3634434
55 A = 6796027
02 meter
Y = -5545134
49 meter E =
0005241
Z = -1487891
12 I = 51
98803
XDOT = 3332
151887 Wp = 123
57863
YDOT = 3735
032574 meter/sec RA = 113
13950 deg
ZDOT = -5797
996529 TA = 72
55761
MA = 72
50032
Ha = 225
348 n
mi
Hp = 218
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11923997
88 X = 3703399
31
Y = -18192698
45 feet Y = -5504106
34 meter
Z = -4881532
54 Z = -1470067
34
XDOT = 10932
256848 XDOT = 3318
303826
YDOT = 12254
043879 feet/sec YDOT = 3772
217219 meter/sec
ZDOT = -19022
298325 ZDOT = -5781
842722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4335168
54 X = 1321359
37
Y = 21333244
00 feet Y = 6502372
77 meter
Z = -4804620
34 Z = -1464448
28
XDOT = -14919
904134 XDOT = -4547
586780
YDOT = -1223
755923 feet/sec YDOT = -373
000805 meter/sec
ZDOT = -18954
053967 ZDOT = -5777
195649
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 14310
52938306
00016717 00000-0 10270-3 0 9136
2 25544 51
6409 113
9260 0003828 348
8289 11
2777 15
51514636 33415
Satellite: ISS
Catalog Number: 25544
Epoch time: 14310
52938306 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 113
9260 deg
Eccentricity:
0003828
Arg of perigee: 348
8289 deg
Mean anomaly: 11
2777 deg
Mean motion: 15
51514636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 305
Coasting Arc #15 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2014/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602472
43 A = 6794736
59 meter
Y = 5285594
52 meter E =
0014894
Z = 2266629
10 I = 51
99568
XDOT = -3043
957037 Wp = 57
93220
YDOT = -4428
705548 meter/sec RA = 108
20198 deg
ZDOT = 5470
932432 TA = 327
14774
MA = 327
24024
Ha = 225
389 n
mi
Hp = 218
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11819135
26 X = -3672320
29
Y = 17341189
36 feet Y = 5244918
83 meter
Z = 7436447
18 Z = 2248958
57
XDOT = -9986
735687 XDOT = -3020
784753
YDOT = -14529
873844 feet/sec YDOT = -4462
615398 meter/sec
ZDOT = 17949
253386 ZDOT = 5456
201264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4153283
07 X = -1265920
68
Y = -20598229
51 feet Y = -6278340
36 meter
Z = 7360212
91 Z = 2243392
90
XDOT = 15953
667449 XDOT = 4862
677838
YDOT = 3196
659126 feet/sec YDOT = 974
341702 meter/sec
ZDOT = 17887
196721 ZDOT = 5452
017560
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 14311
55995508
00016717 00000-0 10270-3 0 9148
2 25544 51
6412 108
8078 0003623 351
6919 8
4172 15
51541188 33570
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
55995508 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 108
8078 deg
Eccentricity:
0003623
Arg of perigee: 351
6919 deg
Mean anomaly: 8
4172 deg
Mean motion: 15
51541188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 312
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