[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 19th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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
329/19:52:58
009 4
7 5
3 5
3
N/A 0
8 -0
6 219
9
000/00:13:56
017 2
3 -0
1 215
4
Coasting Arc #1 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2015/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3132505
44 A = 6774572
81 meter
Y = -2902781
11 meter E =
0018391
Z = -5274519
86 I = 51
82990
XDOT = 5935
144929 Wp = 111
91505
YDOT = 4752
018745 meter/sec RA = 33
31119 deg
ZDOT = 905
461925 TA = 166
76024
MA = 166
71191
Ha = 220
923 n
mi
Hp = 211
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10277248
81 X = 3190354
14
Y = -9523560
08 feet Y = -2867427
87 meter
Z = -17304855
19 Z = -5259162
11
XDOT = 19472
260265 XDOT = 5877
167138
YDOT = 15590
612679 feet/sec YDOT = 4818
065271 meter/sec
ZDOT = 2970
675607 ZDOT = 934
153230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2178230
79 X = 663924
74
Y = 13924400
01 feet Y = 4244157
12 meter
Z = -17237878
29 Z = -5254105
30
XDOT = -22739
464675 XDOT = -6930
988833
YDOT = 7404
042671 feet/sec YDOT = 2256
752206 meter/sec
ZDOT = 3093
712172 ZDOT = 942
963470
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 15322
51448052
00016717 00000-0 10270-3 0 9009
2 25544 51
6437 33
8512 0005821 152
3006 207
8458 15
55187796 12059
Satellite: ISS
Catalog Number: 25544
Epoch time: 15322
51448052 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 33
8512 deg
Eccentricity:
0005821
Arg of perigee: 152
3006 deg
Mean anomaly: 207
8458 deg
Mean motion: 15
55187796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 292
Coasting Arc #2 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2015/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4782052
00 A = 6777294
25 meter
Y = 1492765
20 meter E =
0010639
Z = 4554625
23 I = 51
81322
XDOT = -4621
812742 Wp = 99
38021
YDOT = -5276
657903 meter/sec RA = 28
31596 deg
ZDOT = -3118
687725 TA = 21
76477
MA = 21
71959
Ha = 220
820 n
mi
Hp = 211
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15689146
97 X = -4820513
95
Y = 4897523
61 feet Y = 1439074
11 meter
Z = 14942996
16 Z = 4531301
26
XDOT = -15163
427630 XDOT = -4547
314776
YDOT = -17311
869759 feet/sec YDOT = -5327
925538 meter/sec
ZDOT = -10231
915108 ZDOT = -3140
958859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4389100
22 X = 1337797
75
Y = -15933694
72 feet Y = -4856590
15 meter
Z = 14841879
13 Z = 4523804
76
XDOT = 21560
066444 XDOT = 6571
508252
YDOT = -3694
345581 feet/sec YDOT = -1126
036533 meter/sec
ZDOT = -10327
087281 ZDOT = -3147
696203
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 15323
54258921
00016717 00000-0 10270-3 0 9018
2 25544 51
6444 28
7171 0005711 155
8433 204
2989 15
55272220 12216
Satellite: ISS
Catalog Number: 25544
Epoch time: 15323
54258921 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 28
7171 deg
Eccentricity:
0005711
Arg of perigee: 155
8433 deg
Mean anomaly: 204
2989 deg
Mean motion: 15
55272220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 288
Coasting Arc #3 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2015/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6006334
79 A = 6781822
34 meter
Y = -115441
36 meter E =
0007825
Z = -3157646
49 I = 51
79923
XDOT = 2650
622627 Wp = 122
21782
YDOT = 5302
277580 meter/sec RA = 23
33232 deg
ZDOT = 4852
770484 TA = 201
47920
MA = 201
51206
Ha = 220
651 n
mi
Hp = 211
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19705822
81 X = 6022518
14
Y = -378744
62 feet Y = -48184
13 meter
Z = -10359732
57 Z = -3128429
19
XDOT = 8696
268462 XDOT = 2567
561012
YDOT = 17395
923820 feet/sec YDOT = 5331
454250 meter/sec
ZDOT = 15921
163004 ZDOT = 4865
445021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10053809
70 X = -3064401
20
Y = 17028937
23 feet Y = 5190420
07 meter
Z = -10233433
75 Z = -3119150
61
XDOT = -18077
522827 XDOT = -5510
028958
YDOT = -1082
329690 feet/sec YDOT = -329
894089 meter/sec
ZDOT = 15974
845994 ZDOT = 4869
133059
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 15324
50641885
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 23
9044 0005793 157
5591 202
5817 15
55291419 12365
Satellite: ISS
Catalog Number: 25544
Epoch time: 15324
50641885 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 23
9044 deg
Eccentricity:
0005793
Arg of perigee: 157
5591 deg
Mean anomaly: 202
5817 deg
Mean motion: 15
55291419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 310
Coasting Arc #4 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2015/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6561025
81 A = 6785224
51 meter
Y = -1156776
03 meter E =
0018476
Z = 1230343
99 I = 51
78208
XDOT = -236
381197 Wp = 132
21863
YDOT = -4945
406551 meter/sec RA = 18
36057 deg
ZDOT = -5866
169147 TA = 34
41675
MA = 34
29722
Ha = 220
501 n
mi
Hp = 211
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21525675
23 X = -6553579
47
Y = -3795196
94 feet Y = -1230104
09 meter
Z = 4036561
66 Z = 1198489
39
XDOT = -775
528861 XDOT = -152
566763
YDOT = -16225
087108 feet/sec YDOT = -4947
581407 meter/sec
ZDOT = -19245
961767 ZDOT = -5867
113777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14257619
06 X = 4345722
29
Y = -16600273
36 feet Y = -5059763
32 meter
Z = 3899136
71 Z = 1188456
87
XDOT = 13079
061167 XDOT = 3986
497844
YDOT = 6676
880619 feet/sec YDOT = 2035
113213 meter/sec
ZDOT = -19249
018892 ZDOT = -5867
100958
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 15325
53447673
00016717 00000-0 10270-3 0 9035
2 25544 51
6443 18
7701 0005604 159
7752 200
3624 15
55337166 12529
Satellite: ISS
Catalog Number: 25544
Epoch time: 15325
53447673 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 18
7701 deg
Eccentricity:
0005604
Arg of perigee: 159
7752 deg
Mean anomaly: 200
3624 deg
Mean motion: 15
55337166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 298
Coasting Arc #5 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2015/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353506
23 A = 6785536
52 meter
Y = 2211348
33 meter E =
0013007
Z = 861985
08 I = 51
75191
XDOT = -2300
975545 Wp = 78
14201
YDOT = 4266
544570 meter/sec RA = 13
39355 deg
ZDOT = 5941
395844 TA = 291
17123
MA = 291
31017
Ha = 220
442 n
mi
Hp = 211
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20844836
71 X = 6324118
90
Y = 7255079
83 feet Y = 2282233
13 meter
Z = 2828035
04 Z = 892778
39
XDOT = -7549
132366 XDOT = -2377
375727
YDOT = 13997
849639 feet/sec YDOT = 4240
386446 meter/sec
ZDOT = 19492
768516 ZDOT = 5930
032297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16617361
64 X = -5064971
83
Y = 14499622
78 feet Y = 4419485
02 meter
Z = 2960644
23 Z = 902404
36
XDOT = -7304
466732 XDOT = -2226
401460
YDOT = -12388
100508 feet/sec YDOT = -3775
893035 meter/sec
ZDOT = 19442
773959 ZDOT = 5926
157503
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 15326
56251058
00016717 00000-0 10270-3 0 9040
2 25544 51
6437 13
6360 0005493 161
5814 198
5539 15
55315223 12683
Satellite: ISS
Catalog Number: 25544
Epoch time: 15326
56251058 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 13
6360 deg
Eccentricity:
0005493
Arg of perigee: 161
5814 deg
Mean anomaly: 198
5539 deg
Mean motion: 15
55315223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 307
Coasting Arc #6 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2015/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5317255
00 A = 6782048
66 meter
Y = -3076435
96 meter E =
0009248
Z = -2868810
87 I = 51
71070
XDOT = 4670
336194 Wp = 142
11119
YDOT = -3356
785077 meter/sec RA = 8
41899 deg
ZDOT = -5072
397703 TA = 70
51087
MA = 70
41099
Ha = 220
202 n
mi
Hp = 211
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17445062
32 X = -5268522
42
Y = -10093293
84 feet Y = -3135624
53 meter
Z = -9412109
15 Z = -2894523
29
XDOT = 15322
625307 XDOT = 4732
165841
YDOT = -11013
074399 feet/sec YDOT = -3304
212573 meter/sec
ZDOT = -16641
724746 ZDOT = -5049
559426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17202654
09 X = 5243368
97
Y = -10401052
56 feet Y = -3170240
82 meter
Z = -9522571
94 Z = -2902479
93
XDOT = 1493
467985 XDOT = 455
209042
YDOT = 17568
358318 feet/sec YDOT = 5354
835615 meter/sec
ZDOT = -16542
335236 ZDOT = -5042
103780
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 15327
52626530
00016717 00000-0 10270-3 0 9059
2 25544 51
6445 8
8224 0005582 164
9151 195
2169 15
55401698 12839
Satellite: ISS
Catalog Number: 25544
Epoch time: 15327
52626530 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 8
8224 deg
Eccentricity:
0005582
Arg of perigee: 164
9151 deg
Mean anomaly: 195
2169 deg
Mean motion: 15
55401698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 312
Coasting Arc #7 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3615614
30 A = 6777290
85 meter
Y = 3689375
66 meter E =
0013214
Z = 4383511
94 I = 51
66218
XDOT = -6483
123370 Wp = 130
19925
YDOT = 2301
522641 meter/sec RA = 3
42787 deg
ZDOT = 3395
244665 TA = 285
37878
MA = 285
52474
Ha = 220
089 n
mi
Hp = 211
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11862251
63 X = 3552796
11
Y = 12104250
86 feet Y = 3729456
50 meter
Z = 14381600
85 Z = 4400923
81
XDOT = -21270
089797 XDOT = -6524
870932
YDOT = 7550
927301 feet/sec YDOT = 2228
790571 meter/sec
ZDOT = 11139
254150 ZDOT = 3363
648815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16190684
58 X = -4934920
66
Y = 4789614
24 feet Y = 1459874
42 meter
Z = 14456060
11 Z = 4406207
12
XDOT = 3588
885758 XDOT = 1093
892379
YDOT = -21224
079898 feet/sec YDOT = -6469
099553 meter/sec
ZDOT = 11002
246761 ZDOT = 3353
484813
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 15328
55424674
00016717 00000-0 10270-3 0 9069
2 25544 51
6433 3
6879 0005562 167
5303 192
5989 15
55432855 12997
Satellite: ISS
Catalog Number: 25544
Epoch time: 15328
55424674 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 3
6879 deg
Eccentricity:
0005562
Arg of perigee: 167
5303 deg
Mean anomaly: 192
5989 deg
Mean motion: 15
55432855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 340
Coasting Arc #8 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2015/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906699
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1394207
11 A = 6773887
15 meter
Y = -4099016
65 meter E =
0015301
Z = -5221965
93 I = 51
61991
XDOT = 7493
862272 Wp = 102
30727
YDOT = -1107
859031 meter/sec RA = 358
41884 deg
ZDOT = -1137
160738 TA = 156
81114
MA = 156
74202
Ha = 220
005 n
mi
Hp = 211
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4574170
32 X = -1322900
37
Y = -13448217
36 feet Y = -4114208
65 meter
Z = -17132434
14 Z = -5228565
86
XDOT = 24586
162311 XDOT = 7511
217682
YDOT = -3634
708106 feet/sec YDOT = -1023
960625 meter/sec
ZDOT = -3730
842316 ZDOT = -1100
714092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14020601
88 X = 4273479
45
Y = 2062061
60 feet Y = 628516
38 meter
Z = -17160084
75 Z = -5230393
83
XDOT = -7671
888692 XDOT = -2338
391673
YDOT = 22592
315391 feet/sec YDOT = 6886
137731 meter/sec
ZDOT = -3573
129900 ZDOT = -1089
089993
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 15329
51795629
00016717 00000-0 10270-3 0 9078
2 25544 51
6443 358
8738 0005516 171
7694 188
3551 15
55454417 13140
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
51795629 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 358
8738 deg
Eccentricity:
0005516
Arg of perigee: 171
7694 deg
Mean anomaly: 188
3551 deg
Mean motion: 15
55454417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 342
Coasting Arc #9 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5519699
21 A = 6784895
65 meter
Y = -2641729
66 meter E =
0001458
Z = -2932961
73 I = 51
63648
XDOT = 4444
448269 Wp = 137
82373
YDOT = 3720
396429 meter/sec RA = 356
72009 deg
ZDOT = 5013
664588 TA = 188
72461
MA = 188
72715
Ha = 219
913 n
mi
Hp = 215
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18109249
38 X = 5563076
97
Y = -8667092
07 feet Y = -2579762
05 meter
Z = -9622577
87 Z = -2906042
31
XDOT = 14581
523191 XDOT = 4378
160539
YDOT = 12206
025031 feet/sec YDOT = 3769
726275 meter/sec
ZDOT = 16449
030799 ZDOT = 5035
094508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17593332
64 X = 5362447
79
Y = -9786398
39 feet Y = -2982894
23 meter
Z = -9505706
51 Z = -2897339
34
XDOT = 14496
835773 XDOT = 4418
635544
YDOT = 9996
291941 feet/sec YDOT = 3046
869784 meter/sec
ZDOT = 16540
836930 ZDOT = 5041
647096
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 15329
83918772
00016717 00000-0 10270-3 0 9080
2 25544 51
6449 357
2682 0004424 226
0031 134
0757 15
54428727 13198
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83918772 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 357
2682 deg
Eccentricity:
0004424
Arg of perigee: 226
0031 deg
Mean anomaly: 134
0757 deg
Mean motion: 15
54428727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 322
Coasting Arc #10 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2015/330/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6376014
62 A = 6787820
13 meter
Y = 1931806
54 meter E =
0013114
Z = 1257314
53 I = 51
61454
XDOT = -2465
305966 Wp = 139
92566
YDOT = -4318
770507 meter/sec RA = 351
74227 deg
ZDOT = -5842
224521 TA = 26
38916
MA = 26
32243
Ha = 219
838 n
mi
Hp = 215
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20918683
14 X = -6403250
34
Y = 6337947
95 feet Y = 1860353
36 meter
Z = 4125047
68 Z = 1226274
53
XDOT = -8088
274167 XDOT = -2388
449360
YDOT = -14169
194576 feet/sec YDOT = -4345
909043 meter/sec
ZDOT = -19167
403285 ZDOT = -5854
014332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20373322
68 X = -6209788
75
Y = 7986260
40 feet Y = 2434212
17 meter
Z = 3990523
09 Z = 1216311
44
XDOT = -8486
405958 XDOT = -2586
656536
YDOT = -12005
960351 feet/sec YDOT = -3659
416715 meter/sec
ZDOT = -19217
427200 ZDOT = -5857
471811
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 15330
86781708
00016717 00000-0 10270-3 0 9093
2 25544 51
6449 352
1378 0004411 229
0596 131
0176 15
54432928 13357
Satellite: ISS
Catalog Number: 25544
Epoch time: 15330
86781708 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 352
1378 deg
Eccentricity:
0004411
Arg of perigee: 229
0596 deg
Mean anomaly: 131
0176 deg
Mean motion: 15
54432928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 314
Coasting Arc #11 (Orbit 1350)
---------------------------------------
Vector Time (GMT): 2015/331/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6668423
84 A = 6788146
60 meter
Y = -1114490
24 meter E =
0008786
Z = 556861
70 I = 51
58501
XDOT = 298
105956 Wp = 49
38245
YDOT = 4797
026775 meter/sec RA = 346
76684 deg
ZDOT = 5974
517854 TA = 316
63119
MA = 316
70030
Ha = 219
572 n
mi
Hp = 215
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21878030
97 X = 6677685
67
Y = -3656464
04 feet Y = -1039867
78 meter
Z = 1826974
10 Z = 589278
44
XDOT = 978
037912 XDOT = 215
419938
YDOT = 15738
276822 feet/sec YDOT = 4799
897602 meter/sec
ZDOT = 19601
436528 ZDOT = 5975
765548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21409414
11 X = 6525589
42
Y = -5755226
04 feet Y = -1754192
90 meter
Z = 1967273
08 Z = 599624
84
XDOT = 1952
191893 XDOT = 595
028089
YDOT = 14022
533176 feet/sec YDOT = 4274
068112 meter/sec
ZDOT = 19605
809126 ZDOT = 5975
850622
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 15331
89642116
00016717 00000-0 10270-3 0 9108
2 25544 51
6451 347
0068 0004321 234
9020 125
1728 15
54483067 13511
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
89642116 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 347
0068 deg
Eccentricity:
0004321
Arg of perigee: 234
9020 deg
Mean anomaly: 125
1728 deg
Mean motion: 15
54483067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1351
Checksum: 283
Coasting Arc #12 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2015/332/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6365822
27 A = 6785850
20 meter
Y = 142411
89 meter E =
0006299
Z = -2335187
25 I = 51
54731
XDOT = 1861
793967 Wp = 176
98990
YDOT = -5122
249954 meter/sec RA = 341
78716 deg
ZDOT = -5394
530852 TA = 29
09296
MA = 29
05787
Ha = 219
353 n
mi
Hp = 215
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20885243
68 X = -6355598
08
Y = 467230
62 feet Y = 71282
41 meter
Z = -7661375
48 Z = -2366086
59
XDOT = 6108
247922 XDOT = 1945
138671
YDOT = -16805
282000 feet/sec YDOT = -5100
963732 meter/sec
ZDOT = -17698
592035 ZDOT = -5385
284490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20647109
46 X = -6293238
96
Y = 2836302
57 feet Y = 864505
02 meter
Z = -7794911
20 Z = -2375888
93
XDOT = 4473
704903 XDOT = 1363
585254
YDOT = -15900
503154 feet/sec YDOT = -4846
473361 meter/sec
ZDOT = -17657
556293 ZDOT = -5382
023158
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 15332
86071545
00016717 00000-0 10270-3 0 9119
2 25544 51
6456 342
1969 0004475 237
8542 122
2177 15
54500860 13666
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
86071545 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 342
1969 deg
Eccentricity:
0004475
Arg of perigee: 237
8542 deg
Mean anomaly: 122
2177 deg
Mean motion: 15
54500860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 309
Coasting Arc #13 (Orbit 1381)
---------------------------------------
Vector Time (GMT): 2015/333/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5522023
93 A = 6781800
47 meter
Y = 938251
79 meter E =
0008290
Z = 3820042
36 I = 51
50431
XDOT = -3773
636819 Wp = 115
32846
YDOT = 5219
545497 meter/sec RA = 336
79522 deg
ZDOT = 4162
404752 TA = 290
71890
MA = 290
80773
Ha = 219
188 n
mi
Hp = 215
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18116876
39 X = 5492565
33
Y = 3078253
91 feet Y = 999837
75 meter
Z = 12532947
36 Z = 3846795
92
XDOT = -12380
698224 XDOT = -3851
942092
YDOT = 17124
493099 feet/sec YDOT = 5176
908103 meter/sec
ZDOT = 13656
183571 ZDOT = 4143
883199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18284245
96 X = 5573038
17
Y = 690973
36 feet Y = 210608
68 meter
Z = 12648341
10 Z = 3855214
37
XDOT = -10067
366618 XDOT = -3068
533345
YDOT = 17277
715148 feet/sec YDOT = 5266
247577 meter/sec
ZDOT = 13575
057270 ZDOT = 4137
677456
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 15333
88927311
00016717 00000-0 10270-3 0 9124
2 25544 51
6456 337
0657 0004229 242
3295 117
7429 15
54549679 13824
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
88927311 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 337
0657 deg
Eccentricity:
0004229
Arg of perigee: 242
3295 deg
Mean anomaly: 117
7429 deg
Mean motion: 15
54549679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1382
Checksum: 332
Coasting Arc #14 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2015/334/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226672
79 A = 6777795
98 meter
Y = -2125864
87 meter E =
0007663
Z = -4860447
63 I = 51
46256
XDOT = 5280
627478 Wp = 75
70007
YDOT = -5005
653808 meter/sec RA = 331
78918 deg
ZDOT = -2404
019049 TA = 170
66181
MA = 170
64755
Ha = 218
967 n
mi
Hp = 215
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13867036
72 X = -4178976
40
Y = -6974622
28 feet Y = -2172863
40 meter
Z = -15946350
50 Z = -4880864
31
XDOT = 17324
893302 XDOT = 5347
887318
YDOT = -16422
748713 feet/sec YDOT = -4946
226158 meter/sec
ZDOT = -7887
201604 ZDOT = -2378
203570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14645526
82 X = -4463956
58
Y = -4862289
68 feet Y = -1482025
89 meter
Z = -16034114
90 Z = -4887198
22
XDOT = 14398
634075 XDOT = 4388
703666
YDOT = -17745
991212 feet/sec YDOT = -5408
978121 meter/sec
ZDOT = -7774
613762 ZDOT = -2369
702275
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 15334
85352224
00016717 00000-0 10270-3 0 9138
2 25544 51
6456 332
2555 0004339 247
2681 112
8013 15
54613962 13971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
85352224 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 332
2555 deg
Eccentricity:
0004339
Arg of perigee: 247
2681 deg
Mean anomaly: 112
8013 deg
Mean motion: 15
54613962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 303
Coasting Arc #15 (Orbit 1412)
---------------------------------------
Vector Time (GMT): 2015/335/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2641773
41 A = 6775884
58 meter
Y = 3312123
86 meter E =
0002641
Z = 5289508
99 I = 51
42887
XDOT = -6251
767353 Wp = 216
17241
YDOT = 4427
280302 meter/sec RA = 326
77211 deg
ZDOT = 348
135000 TA = 230
48713
MA = 230
51047
Ha = 218
803 n
mi
Hp = 215
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8667235
60 X = 2578845
55
Y = 10866548
09 feet Y = 3341313
89 meter
Z = 17354032
12 Z = 5302189
52
XDOT = -20511
047747 XDOT = -6302
500754
YDOT = 14525
197841 feet/sec YDOT = 4357
085234 meter/sec
ZDOT = 1142
175198 ZDOT = 317
641949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10231772
81 X = 3118644
35
Y = 9307698
70 feet Y = 2836986
56 meter
Z = 17408125
72 Z = 5305996
72
XDOT = -17161
678046 XDOT = -5230
879468
YDOT = 16965
178021 feet/sec YDOT = 5170
986261 meter/sec
ZDOT = 1009
508335 ZDOT = 307
698140
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 15335
88203240
00016717 00000-0 10270-3 0 9146
2 25544 51
6458 327
1246 0004309 249
8021 110
2669 15
54641606 14130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15335
88203240 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 327
1246 deg
Eccentricity:
0004309
Arg of perigee: 249
8021 deg
Mean anomaly: 110
2669 deg
Mean motion: 15
54641606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1413
Checksum: 290
Coasting Arc #16 (Orbit 1427)
---------------------------------------
Vector Time (GMT): 2015/336/19:59:56
017
Vector Time (MET): N/A
Weight (LBS) : 906102
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -930421
13 A = 6776818
96 meter
Y = -4414586
92 meter E =
0009617
Z = -5065405
04 I = 51
40537
XDOT = 6622
328977 Wp = 116
04383
YDOT = -3424
833610 meter/sec RA = 321
75043 deg
ZDOT = 1766
877901 TA = 171
12499
MA = 171
10798
Ha = 218
719 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3052562
75 X = -856381
04
Y = -14483552
88 feet Y = -4424577
41 meter
Z = -16618782
95 Z = -5069745
13
XDOT = 21726
801105 XDOT = 6651
551249
YDOT = -11236
330740 feet/sec YDOT = -3350
615003 meter/sec
ZDOT = 5796
843507 ZDOT = 1799
118931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5532112
76 X = -1686187
97
Y = -13707446
24 feet Y = -4178029
62 meter
Z = -16636617
33 Z = -5070840
96
XDOT = 18283
748003 XDOT = 5572
886391
YDOT = -14590
598082 feet/sec YDOT = -4447
214295 meter/sec
ZDOT = 5936
843933 ZDOT = 1809
550031
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 15336
84623789
00016717 00000-0 10270-3 0 9158
2 25544 51
6451 322
3134 0004365 254
2544 105
8128 15
54684627 14284
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
84623789 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 322
3134 deg
Eccentricity:
0004365
Arg of perigee: 254
2544 deg
Mean anomaly: 105
8128 deg
Mean motion: 15
54684627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1428
Checksum: 316
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