[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 24th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
028/18:42:08
283 1
2 -1
9 1
9
N/A 0
9 0
3 220
3
000/00:04:12
566 -1
2 -0
0 216
7
Coasting Arc #1 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2015/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -727392
70 A = 6789964
81 meter
Y = 6558570
91 meter E =
0011196
Z = 1569431
26 I = 52
02376
XDOT = -4669
795875 Wp = 37
73357
YDOT = -1903
904340 meter/sec RA = 85
62907 deg
ZDOT = 5778
898520 TA = 339
33603
MA = 339
38127
Ha = 220
652 n
mi
Hp = 217
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2386458
99 X = -808301
68
Y = 21517621
08 feet Y = 6549984
38 meter
Z = 5149052
70 Z = 1565701
11
XDOT = -15320
852608 XDOT = -4676
230090
YDOT = -6246
405316 feet/sec YDOT = -1956
160859 meter/sec
ZDOT = 18959
640815 ZDOT = 5756
198415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19583286
76 X = -5968985
80
Y = 9239834
20 feet Y = 2816301
46 meter
Z = 5131889
62 Z = 1564199
96
XDOT = -2119
045564 XDOT = -645
885088
YDOT = -14991
702956 feet/sec YDOT = -4569
471061 meter/sec
ZDOT = 18862
830949 ZDOT = 5749
390873
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 15023
56127426
00016717 00000-0 10270-3 0 9001
2 25544 51
6451 86
1253 0006010 294
3336 65
7188 15
53554402 5538
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
56127426 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 86
1253 deg
Eccentricity:
0006010
Arg of perigee: 294
3336 deg
Mean anomaly: 65
7188 deg
Mean motion: 15
53554402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 553
Checksum: 283
Coasting Arc #2 (Orbit 567)
---------------------------------------
Vector Time (GMT): 2015/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1373325
01 A = 6787133
38 meter
Y = -5947312
02 meter E =
0001489
Z = -2968386
10 I = 52
01147
XDOT = 4560
475555 Wp = 314
96982
YDOT = 3561
899453 meter/sec RA = 80
68155 deg
ZDOT = -5023
981044 TA = 258
73459
MA = 258
75132
Ha = 220
687 n
mi
Hp = 217
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4505659
48 X = 1454146
27
Y = -19512178
53 feet Y = -5931502
81 meter
Z = -9738799
54 Z = -2961518
35
XDOT = 14962
190140 XDOT = 4544
710854
YDOT = 11686
021826 feet/sec YDOT = 3612
809341 meter/sec
ZDOT = -16482
877440 ZDOT = -5001
865896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18892669
39 X = 5758485
63
Y = -6684760
84 feet Y = -2037515
10 meter
Z = -9708311
41 Z = -2959093
32
XDOT = -2194
412908 XDOT = -668
857054
YDOT = 17611
966351 feet/sec YDOT = 5368
127344 meter/sec
ZDOT = -16388
877798 ZDOT = -4995
329953
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 15024
52613793
00016717 00000-0 10270-3 0 9016
2 25544 51
6450 81
3191 0005954 298
1839 61
8712 15
53607961 5686
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
52613793 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 81
3191 deg
Eccentricity:
0005954
Arg of perigee: 298
1839 deg
Mean anomaly: 61
8712 deg
Mean motion: 15
53607961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 568
Checksum: 316
Coasting Arc #3 (Orbit 583)
---------------------------------------
Vector Time (GMT): 2015/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2051702
97 A = 6783614
81 meter
Y = 4982139
49 meter E =
0005294
Z = 4116370
17 I = 51
99382
XDOT = -4373
547649 Wp = 81
46848
YDOT = -4985
571810 meter/sec RA = 75
72572 deg
ZDOT = 3850
818035 TA = 328
92747
MA = 328
95877
Ha = 220
931 n
mi
Hp = 217
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6731308
95 X = -2127257
48
Y = 16345601
99 feet Y = 4958773
69 meter
Z = 13505151
46 Z = 4106219
84
XDOT = -14348
909608 XDOT = -4336
178367
YDOT = -16356
862894 feet/sec YDOT = -5034
270600 meter/sec
ZDOT = 12633
917438 ZDOT = 3829
663373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17385294
80 X = -5299037
86
Y = 3381889
46 feet Y = 1030799
91 meter
Z = 13460783
36 Z = 4102846
77
XDOT = 5868
668346 XDOT = 1788
770112
YDOT = -19805
618322 feet/sec YDOT = -6036
752464 meter/sec
ZDOT = 12544
298364 ZDOT = 3823
502141
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 15025
55530739
00016717 00000-0 10270-3 0 9029
2 25544 51
6448 76
1921 0005945 302
6273 57
4305 15
53638614 5845
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
55530739 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 76
1921 deg
Eccentricity:
0005945
Arg of perigee: 302
6273 deg
Mean anomaly: 57
4305 deg
Mean motion: 15
53638614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 584
Checksum: 308
Coasting Arc #4 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2770608
53 A = 6780525
01 meter
Y = -3755104
59 meter E =
0009793
Z = -4927593
05 I = 51
97573
XDOT = 4053
425741 Wp = 43
88666
YDOT = 6064
777444 meter/sec RA = 70
76097 deg
ZDOT = -2338
518826 TA = 203
29021
MA = 203
33461
Ha = 221
007 n
mi
Hp = 217
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9089922
99 X = 2836329
24
Y = -12319896
93 feet Y = -3723754
48 meter
Z = -16166643
86 Z = -4913974
39
XDOT = 13298
640884 XDOT = 3996
666253
YDOT = 19897
563792 feet/sec YDOT = 6109
788075 meter/sec
ZDOT = -7672
305859 ZDOT = -2318
966261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15362127
47 X = 4682376
45
Y = 561716
54 feet Y = 171211
20 meter
Z = -16107651
86 Z = -4909612
29
XDOT = -8746
250351 XDOT = -2665
857107
YDOT = 21169
049352 feet/sec YDOT = 6452
326243 meter/sec
ZDOT = -7589
754947 ZDOT = -2313
357308
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 15026
52013794
00016717 00000-0 10270-3 0 9035
2 25544 51
6456 71
3856 0005942 306
7437 53
3170 15
53649189 5992
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
52013794 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 71
3856 deg
Eccentricity:
0005942
Arg of perigee: 306
7437 deg
Mean anomaly: 53
3170 deg
Mean motion: 15
53649189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 321
Coasting Arc #5 (Orbit 614)
---------------------------------------
Vector Time (GMT): 2015/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3507148
06 A = 6778721
85 meter
Y = 2334743
92 meter E =
0003277
Z = 5311645
96 I = 51
95837
XDOT = -3568
263549 Wp = 327
22758
YDOT = -6758
011044 meter/sec RA = 65
78953 deg
ZDOT = 617
320494 TA = 116
92135
MA = 116
88786
Ha = 221
242 n
mi
Hp = 216
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11506391
28 X = -3558796
81
Y = 7659921
01 feet Y = 2295235
98 meter
Z = 17426659
97 Z = 5294483
60
XDOT = -11706
901407 XDOT = -3495
427366
YDOT = -22171
952243 feet/sec YDOT = -6797
506432 meter/sec
ZDOT = 2025
329706 ZDOT = 600
163691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12993151
45 X = -3960312
56
Y = -4981925
09 feet Y = -1518490
77 meter
Z = 17352761
91 Z = 5289121
83
XDOT = 10836
322101 XDOT = 3302
910976
YDOT = -21491
392816 feet/sec YDOT = -6550
576530 meter/sec
ZDOT = 1953
175114 ZDOT = 595
327775
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 15027
54927095
00016717 00000-0 10270-3 0 9047
2 25544 51
6451 66
2589 0005907 312
0159 48
0490 15
53696331 6151
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
54927095 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 66
2589 deg
Eccentricity:
0005907
Arg of perigee: 312
0159 deg
Mean anomaly: 48
0490 deg
Mean motion: 15
53696331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 615
Checksum: 312
Coasting Arc #6 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4218420
33 A = 6779055
21 meter
Y = -865007
79 meter E =
0010018
Z = -5243752
97 I = 51
94690
XDOT = 2873
450328 Wp = 77
87832
YDOT = 7006
351263 meter/sec RA = 60
81522 deg
ZDOT = 1159
740326 TA = 203
18299
MA = 203
22821
Ha = 221
348 n
mi
Hp = 216
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13839961
71 X = 4253251
46
Y = -2837952
08 feet Y = -817639
90 meter
Z = -17203913
96 Z = -5223176
31
XDOT = 9427
330474 XDOT = 2789
256573
YDOT = 22986
716741 feet/sec YDOT = 7038
013295 meter/sec
ZDOT = 3804
922330 ZDOT = 1173
494378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10596311
63 X = 3229755
78
Y = 9504994
27 feet Y = 2897122
25 meter
Z = -17115677
94 Z = -5216858
63
XDOT = -12154
537972 XDOT = -3704
703174
YDOT = 20481
960769 feet/sec YDOT = 6242
901643 meter/sec
ZDOT = 3862
453607 ZDOT = 1177
275860
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 15028
51406702
00016717 00000-0 10270-3 0 9053
2 25544 51
6463 61
4525 0005988 315
7285 44
3398 15
53700219 6304
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
51406702 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 61
4525 deg
Eccentricity:
0005988
Arg of perigee: 315
7285 deg
Mean anomaly: 44
3398 deg
Mean motion: 15
53700219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 301
Coasting Arc #7 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -743823
99 A = 6781886
27 meter
Y = 5247891
49 meter E =
0004536
Z = 4226553
04 I = 51
95465
XDOT = -5572
412532 Wp = 81
04684
YDOT = -3763
041256 meter/sec RA = 59
45672 deg
ZDOT = 3689
014700 TA = 331
29520
MA = 331
32015
Ha = 220
271 n
mi
Hp = 216
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2440367
41 X = -822982
66
Y = 17217491
77 feet Y = 5239130
94 meter
Z = 13866643
85 Z = 4222747
49
XDOT = -18282
193345 XDOT = -5547
838832
YDOT = -12345
935879 feet/sec YDOT = -3825
218220 meter/sec
ZDOT = 12103
066601 ZDOT = 3662
004948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11090001
19 X = 3380232
36
Y = 13412254
85 feet Y = 4088055
28 meter
Z = 13849350
92 Z = 4221282
16
XDOT = -20485
943554 XDOT = -6244
115595
YDOT = 4550
968098 feet/sec YDOT = 1387
135076 meter/sec
ZDOT = 11988
181167 ZDOT = 3653
997620
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 15028
83564677
00016717 00000-0 10270-3 0 9065
2 25544 51
6450 59
8499 0006270 303
4095 56
6458 15
54087731 6355
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83564677 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 59
8499 deg
Eccentricity:
0006270
Arg of perigee: 303
4095 deg
Mean anomaly: 56
6458 deg
Mean motion: 15
54087731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 334
Coasting Arc #8 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2015/029/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1913853
05 A = 6778636
96 meter
Y = -4117169
88 meter E =
0010368
Z = -5042110
81 I = 51
92776
XDOT = 5469
338790 Wp = 46
45460
YDOT = 4982
501478 meter/sec RA = 54
48398 deg
ZDOT = -1988
079571 TA = 204
27391
MA = 204
32279
Ha = 220
373 n
mi
Hp = 216
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6279045
43 X = 1984242
33
Y = -13507775
20 feet Y = -4095374
29 meter
Z = -16542358
29 Z = -5032642
89
XDOT = 17944
024902 XDOT = 5422
874015
YDOT = 16346
789626 feet/sec YDOT = 5043
403409 meter/sec
ZDOT = -6522
570772 ZDOT = -1961
623724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5989398
72 X = -1825568
73
Y = -13688638
78 feet Y = -4172297
10 meter
Z = -16501039
09 Z = -5029516
72
XDOT = 23141
399612 XDOT = 7053
498602
YDOT = -2380
647024 feet/sec YDOT = -725
621213 meter/sec
ZDOT = -6410
295862 ZDOT = -1953
858179
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 15029
80019911
00016717 00000-0 10270-3 0 9070
2 25544 51
6455 55
0417 0006268 308
2246 51
8342 15
54122941 6505
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
80019911 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 55
0417 deg
Eccentricity:
0006268
Arg of perigee: 308
2246 deg
Mean anomaly: 51
8342 deg
Mean motion: 15
54122941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 289
Coasting Arc #9 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3129288
41 A = 6777222
70 meter
Y = 2775585
12 meter E =
0004756
Z = 5334458
02 I = 51
90417
XDOT = -5021
885194 Wp = 329
06288
YDOT = -5793
271781 meter/sec RA = 49
50380 deg
ZDOT = 72
387262 TA = 120
27329
MA = 120
22621
Ha = 220
516 n
mi
Hp = 216
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10266694
27 X = -3186005
45
Y = 9106250
38 feet Y = 2740274
17 meter
Z = 17501502
70 Z = 5319119
08
XDOT = -16476
001292 XDOT = -4957
081856
YDOT = -19006
797181 feet/sec YDOT = -5849
067432 meter/sec
ZDOT = 237
491017 ZDOT = 48
149633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 284853
20 X = 86823
26
Y = 13804356
76 feet Y = 4207567
94 meter
Z = 17435308
92 Z = 5314282
16
XDOT = -24145
342784 XDOT = -7359
500480
YDOT = 344
542586 feet/sec YDOT = 105
016580 meter/sec
ZDOT = 134
873043 ZDOT = 41
109303
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 15030
82903438
00016717 00000-0 10270-3 0 9081
2 25544 51
6453 49
9132 0006383 310
9987 49
0613 15
54171464 6660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82903438 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 49
9132 deg
Eccentricity:
0006383
Arg of perigee: 310
9987 deg
Mean anomaly: 49
0613 deg
Mean motion: 15
54171464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 315
Coasting Arc #10 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2015/031/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4277757
71 A = 6778397
09 meter
Y = -1382206
02 meter E =
0008361
Z = -5079871
80 I = 51
88729
XDOT = 4180
933403 Wp = 80
31759
YDOT = 6148
874377 meter/sec RA = 44
52116 deg
ZDOT = 1851
645711 TA = 207
54612
MA = 207
59045
Ha = 220
682 n
mi
Hp = 216
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14034638
17 X = 4317571
56
Y = -4534796
66 feet Y = -1334146
69 meter
Z = -16666246
07 Z = -5058995
01
XDOT = 13716
973107 XDOT = 4102
870087
YDOT = 20173
472367 feet/sec YDOT = 6195
191799 meter/sec
ZDOT = 6074
953120 ZDOT = 1871
765929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5398431
85 X = 1645442
03
Y = -13833722
93 feet Y = -4216518
75 meter
Z = -16576617
59 Z = -5052553
04
XDOT = 23273
568705 XDOT = 7093
783741
YDOT = 1716
632200 feet/sec YDOT = 523
229495 meter/sec
ZDOT = 6159
873340 ZDOT = 1877
529394
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 15031
79355161
00016717 00000-0 10270-3 0 9093
2 25544 51
6457 45
1046 0006318 315
7036 44
3602 15
54168604 6817
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
79355161 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 45
1046 deg
Eccentricity:
0006318
Arg of perigee: 315
7036 deg
Mean anomaly: 44
3602 deg
Mean motion: 15
54168604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 294
Coasting Arc #11 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2015/032/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5264725
64 A = 6781499
87 meter
Y = 3882
39 meter E =
0009430
Z = 4274646
26 I = 51
87436
XDOT = -2939
825706 Wp = 35
89361
YDOT = -6094
803237 meter/sec RA = 39
54332 deg
ZDOT = -3603
734489 TA = 90
85423
MA = 90
74618
Ha = 220
777 n
mi
Hp = 215
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17272721
92 X = -5285141
93
Y = 12737
50 feet Y = -55105
35 meter
Z = 14024429
99 Z = 4249022
23
XDOT = -9645
097459 XDOT = -2853
948493
YDOT = -19996
073612 feet/sec YDOT = -6127
198115 meter/sec
ZDOT = -11823
275881 ZDOT = -3617
806684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10706001
17 X = -3263189
16
Y = 13667222
07 feet Y = 4165769
29 meter
Z = 13914751
20 Z = 4241216
17
XDOT = -20643
278423 XDOT = -6292
071263
YDOT = -4034
456763 feet/sec YDOT = -1229
702421 meter/sec
ZDOT = -11882
315568 ZDOT = -3621
729785
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 15032
82234986
00016717 00000-0 10270-3 0 9101
2 25544 51
6453 39
9756 0006303 319
9407 40
1280 15
54198849 6971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
82234986 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 39
9756 deg
Eccentricity:
0006303
Arg of perigee: 319
9407 deg
Mean anomaly: 40
1280 deg
Mean motion: 15
54198849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 326
Coasting Arc #12 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2015/033/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5946850
60 A = 6785223
24 meter
Y = 1213505
89 meter E =
0006704
Z = -3025388
07 I = 51
86301
XDOT = 1365
439832 Wp = 3
43734
YDOT = 5679
100918 meter/sec RA = 34
57293 deg
ZDOT = 4968
995313 TA = 322
00823
MA = 322
05550
Ha = 220
900 n
mi
Hp = 215
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19510664
69 X = 5947534
75
Y = 3981318
55 feet Y = 1280011
23 meter
Z = -9925813
88 Z = -2996498
49
XDOT = 4479
789475 XDOT = 1277
696380
YDOT = 18632
220860 feet/sec YDOT = 5693
879630 meter/sec
ZDOT = 16302
478062 ZDOT = 4975
414990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14989100
66 X = 4568677
88
Y = -13201460
86 feet Y = -4023805
27 meter
Z = -9802398
05 Z = -2987770
93
XDOT = 16534
657067 XDOT = 5039
763474
YDOT = 6666
589203 feet/sec YDOT = 2031
976389 meter/sec
ZDOT = 16328
841982 ZDOT = 4977
031036
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 15033
78682908
00016717 00000-0 10270-3 0 9119
2 25544 51
6461 35
1663 0006319 323
2046 36
8672 15
54237172 7127
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
78682908 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 35
1663 deg
Eccentricity:
0006319
Arg of perigee: 323
2046 deg
Mean anomaly: 36
8672 deg
Mean motion: 15
54237172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 300
Coasting Arc #13 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2015/034/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237966
55 A = 6788221
86 meter
Y = -2261150
28 meter E =
0008767
Z = 1421093
84 I = 51
84643
XDOT = 474
951948 Wp = 100
51598
YDOT = -4979
313238 meter/sec RA = 29
61133 deg
ZDOT = -5809
085220 TA = 64
03826
MA = 63
94797
Ha = 220
906 n
mi
Hp = 215
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20465769
52 X = -6219121
19
Y = -7418472
06 feet Y = -2330801
87 meter
Z = 4662381
38 Z = 1390837
62
XDOT = 1558
241298 XDOT = 558
814152
YDOT = -16336
329521 feet/sec YDOT = -4973
533308 meter/sec
ZDOT = -19058
678544 ZDOT = -5806
574201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18079393
19 X = -5510599
04
Y = 12173896
38 feet Y = 3710603
62 meter
Z = 4533325
33 Z = 1381757
56
XDOT = -11314
860048 XDOT = -3448
769343
YDOT = -9674
683586 feet/sec YDOT = -2948
843557 meter/sec
ZDOT = -19046
954098 ZDOT = -5805
511609
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 15034
81558832
00016717 00000-0 10270-3 0 9123
2 25544 51
6460 30
0369 0006204 326
8041 33
2722 15
54230690 7282
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
81558832 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 30
0369 deg
Eccentricity:
0006204
Arg of perigee: 326
8041 deg
Mean anomaly: 33
2722 deg
Mean motion: 15
54230690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 279
Coasting Arc #14 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2015/035/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6043309
53 A = 6788804
72 meter
Y = 3054319
51 meter E =
0015355
Z = 324524
88 I = 51
82162
XDOT = -2403
208767 Wp = 24
45665
YDOT = 4105
966454 meter/sec RA = 24
65255 deg
ZDOT = 6020
687771 TA = 339
03473
MA = 339
09762
Ha = 220
995 n
mi
Hp = 215
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19827131
02 X = 6007129
88
Y = 10020733
32 feet Y = 3121697
46 meter
Z = 1064714
16 Z = 353793
35
XDOT = -7884
543198 XDOT = -2478
189570
YDOT = 13471
018549 feet/sec YDOT = 4078
673273 meter/sec
ZDOT = 19752
912634 ZDOT = 6008
831411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19606476
17 X = 5976053
94
Y = -10432415
84 feet Y = -3179800
35 meter
Z = 1189381
78 Z = 362523
57
XDOT = 5640
988826 XDOT = 1719
373394
YDOT = 12877
126241 feet/sec YDOT = 3924
948078 meter/sec
ZDOT = 19701
362769 ZDOT = 6004
975372
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 15035
84432483
00016717 00000-0 10270-3 0 9131
2 25544 51
6465 24
9069 0006402 330
6277 29
4515 15
54291933 7442
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
84432483 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 24
9069 deg
Eccentricity:
0006402
Arg of perigee: 330
6277 deg
Mean anomaly: 29
4515 deg
Mean motion: 15
54291933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 307
Coasting Arc #15 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2015/036/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5345399
48 A = 6786988
05 meter
Y = -3638867
47 meter E =
0001544
Z = -2063949
59 I = 51
78684
XDOT = 4264
115436 Wp = 59
92735
YDOT = -3116
285459 meter/sec RA = 19
69123 deg
ZDOT = -5551
734867 TA = 142
84021
MA = 142
82952
Ha = 221
044 n
mi
Hp = 215
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17537399
86 X = -5294285
86
Y = -11938541
58 feet Y = -3698357
55 meter
Z = -6771488
15 Z = -2089791
52
XDOT = 13989
880039 XDOT = 4325
613195
YDOT = -10224
033659 feet/sec YDOT = -3068
257857 meter/sec
ZDOT = -18214
353239 ZDOT = -5530
871519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19704643
51 X = -6005975
34
Y = 7766337
01 feet Y = 2367179
52 meter
Z = -6881370
08 Z = -2097441
60
XDOT = 29
932719 XDOT = 9
123493
YDOT = -15976
521521 feet/sec YDOT = -4869
643760 meter/sec
ZDOT = -18124
453440 ZDOT = -5524
333408
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 15036
80874764
00016717 00000-0 10270-3 0 9141
2 25544 51
6467 20
0981 0006319 332
7431 27
3389 15
54291164 7594
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
80874764 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 20
0981 deg
Eccentricity:
0006319
Arg of perigee: 332
7431 deg
Mean anomaly: 27
3389 deg
Mean motion: 15
54291164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 319
Coasting Arc #16 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2015/037/18:44:14
566
Vector Time (MET): N/A
Weight (LBS) : 949887
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154635
15 A = 6783272
09 meter
Y = 3995627
29 meter E =
0010997
Z = 3562423
70 I = 51
74482
XDOT = -5867
223801 Wp = 60
60365
YDOT = 2106
618123 meter/sec RA = 14
71888 deg
ZDOT = 4474
683030 TA = 341
42421
MA = 341
46432
Ha = 221
147 n
mi
Hp = 214
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13630692
75 X = 4092341
75
Y = 13109013
42 feet Y = 4041739
10 meter
Z = 11687741
80 Z = 3582454
10
XDOT = -19249
421918 XDOT = -5912
080339
YDOT = 6911
476780 feet/sec YDOT = 2040
756542 meter/sec
ZDOT = 14680
718604 ZDOT = 4446
072657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18392354
92 X = 5605989
78
Y = -4167814
98 feet Y = -1270350
01 meter
Z = 11772677
05 Z = 3588311
97
XDOT = -5107
381293 XDOT = -1556
729818
YDOT = 18629
473156 feet/sec YDOT = 5678
263418 meter/sec
ZDOT = 14557
869933 ZDOT = 4437
238756
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 15037
83744489
00016717 00000-0 10270-3 0 9156
2 25544 51
6467 14
9678 0006455 338
6203 21
4679 15
54331062 7759
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
83744489 = yrday
fracday
Element set: 915
Inclination: 51
6467 deg
RA of node: 14
9678 deg
Eccentricity:
0006455
Arg of perigee: 338
6203 deg
Mean anomaly: 21
4679 deg
Mean motion: 15
54331062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 329
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