[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 17th 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) : 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
028/18:41:29
095 0
8 -1
3 1
4
N/A 0
6 0
2 220
6
000/00:02:58
190 -0
9 -0
0 216
6
Coasting Arc #1 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2015/016/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4853568
62 A = 6788059
80 meter
Y = -3740051
18 meter E =
0003673
Z = -2915270
45 I = 51
96292
XDOT = 1285
690501 Wp = 213
83805
YDOT = 5612
896612 meter/sec RA = 120
53081 deg
ZDOT = -5060
276082 TA = 359
21955
MA = 359
22012
Ha = 220
292 n
mi
Hp = 218
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15923781
57 X = 4909191
27
Y = -12270509
11 feet Y = -3685464
26 meter
Z = -9564535
60 Z = -2891557
92
XDOT = 4218
144688 XDOT = 1247
411068
YDOT = 18415
015132 feet/sec YDOT = 5627
060266 meter/sec
ZDOT = -16601
955648 ZDOT = -5054
123154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14832217
02 X = 4520859
75
Y = 13641113
72 feet Y = 4157811
46 meter
Z = -9462447
33 Z = -2884153
95
XDOT = -16403
781976 XDOT = -4999
872746
YDOT = 6337
186442 feet/sec YDOT = 1931
574427 meter/sec
ZDOT = -16576
617807 ZDOT = -5052
553108
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 15016
48505772
00016717 00000-0 10270-3 0 9008
2 25544 51
6451 121
3586 0006259 260
6614 99
3831 15
53352923 4439
Satellite: ISS
Catalog Number: 25544
Epoch time: 15016
48505772 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 121
3586 deg
Eccentricity:
0006259
Arg of perigee: 260
6614 deg
Mean anomaly: 99
3831 deg
Mean motion: 15
53352923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 443
Checksum: 301
Coasting Arc #2 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2015/017/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4765465
64 A = 6784648
65 meter
Y = 2671338
18 meter E =
0005207
Z = 4021265
76 I = 51
96834
XDOT = -312
003735 Wp = 120
39491
YDOT = -6548
305697 meter/sec RA = 115
57522 deg
ZDOT = 3973
925494 TA = 288
42092
MA = 288
47752
Ha = 219
990 n
mi
Hp = 218
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15634729
79 X = -4814516
67
Y = 8764232
89 feet Y = 2617773
14 meter
Z = 13193129
14 Z = 3997997
23
XDOT = -1023
634300 XDOT = -258
059572
YDOT = -21483
942575 feet/sec YDOT = -6551
493357 meter/sec
ZDOT = 13037
813299 ZDOT = 3972
540461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11571428
73 X = -3526971
48
Y = -13783601
40 feet Y = -4201241
71 meter
Z = 13093111
92 Z = 3990780
51
XDOT = 19883
895384 XDOT = 6060
611313
YDOT = -4292
454968 feet/sec YDOT = -1308
340274 meter/sec
ZDOT = 13033
044791 ZDOT = 3972
472052
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 15017
51439040
00016717 00000-0 10270-3 0 9018
2 25544 51
6461 116
2332 0006238 265
1024 94
9416 15
53418104 4595
Satellite: ISS
Catalog Number: 25544
Epoch time: 15017
51439040 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 116
2332 deg
Eccentricity:
0006238
Arg of perigee: 265
1024 deg
Mean anomaly: 94
9416 deg
Mean motion: 15
53418104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 459
Checksum: 277
Coasting Arc #3 (Orbit 473)
---------------------------------------
Vector Time (GMT): 2015/018/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4557568
28 A = 6781648
16 meter
Y = -1374867
67 meter E =
0005797
Z = -4835410
13 I = 51
97134
XDOT = -558
425644 Wp = 52
57747
YDOT = 7196
320594 meter/sec RA = 110
61361 deg
ZDOT = -2571
173445 TA = 192
20128
MA = 192
21532
Ha = 219
850 n
mi
Hp = 218
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14952651
84 X = 4596092
00
Y = -4510720
69 feet Y = -1323686
26 meter
Z = -15864206
48 Z = -4813177
12
XDOT = -1832
105132 XDOT = -626
365427
YDOT = 23609
975703 feet/sec YDOT = 7189
696213 meter/sec
ZDOT = -8435
608415 ZDOT = -2574
050680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7507608
24 X = 2288318
99
Y = 13805110
70 feet Y = 4207797
74 meter
Z = -15768835
79 Z = -4806341
15
XDOT = -22464
506103 XDOT = -6847
181460
YDOT = 2560
794379 feet/sec YDOT = 780
530127 meter/sec
ZDOT = -8449
200735 ZDOT = -2575
316384
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 15018
47937232
00016717 00000-0 10270-3 0 9021
2 25544 51
6464 111
4290 0006264 269
7357 90
3078 15
53407250 4747
Satellite: ISS
Catalog Number: 25544
Epoch time: 15018
47937232 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 111
4290 deg
Eccentricity:
0006264
Arg of perigee: 269
7357 deg
Mean anomaly: 90
3078 deg
Mean motion: 15
53407250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 474
Checksum: 302
Coasting Arc #4 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2015/019/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263184
78 A = 6779537
51 meter
Y = -69460
83 meter E =
0003460
Z = 5273832
60 I = 51
97581
XDOT = 1315
144768 Wp = 246
00931
YDOT = -7489
807735 meter/sec RA = 105
64575 deg
ZDOT = 963
599130 TA = 194
80299
MA = 194
81312
Ha = 219
943 n
mi
Hp = 217
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13986826
70 X = -4287709
09
Y = -227889
85 feet Y = -117271
96 meter
Z = 17302600
40 Z = 5253063
64
XDOT = 4314
779424 XDOT = 1394
119084
YDOT = -24572
860023 feet/sec YDOT = -7474
659416 meter/sec
ZDOT = 3161
414469 ZDOT = 970
179128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2911362
04 X = -887383
15
Y = -13793995
18 feet Y = -4204409
73 meter
Z = 17213741
71 Z = 5246748
47
XDOT = 23906
697070 XDOT = 7286
761267
YDOT = -1060
172527 feet/sec YDOT = -323
140586 meter/sec
ZDOT = 3190
913466 ZDOT = 972
590425
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 15019
50866295
00016717 00000-0 10270-3 0 9037
2 25544 51
6469 106
3034 0006195 274
4511 85
5933 15
53484397 4900
Satellite: ISS
Catalog Number: 25544
Epoch time: 15019
50866295 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 106
3034 deg
Eccentricity:
0006195
Arg of perigee: 274
4511 deg
Mean anomaly: 85
5933 deg
Mean motion: 15
53484397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 490
Checksum: 321
Coasting Arc #5 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2015/020/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3924104
14 A = 6779370
87 meter
Y = 1576128
47 meter E =
0008506
Z = -5306139
72 I = 51
98280
XDOT = -1970
862186 Wp = 92
87725
YDOT = 7367
301304 meter/sec RA = 100
67679 deg
ZDOT = 731
434443 TA = 184
07962
MA = 184
08656
Ha = 220
027 n
mi
Hp = 218
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12874357
43 X = 3931962
58
Y = 5171025
18 feet Y = 1620054
51 meter
Z = -17408594
87 Z = -5287058
41
XDOT = -6466
083289 XDOT = -2056
651563
YDOT = 24170
936036 feet/sec YDOT = 7344
782136 meter/sec
ZDOT = 2399
719301 ZDOT = 721
652495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1917388
09 X = -584419
89
Y = 13843365
41 feet Y = 4219457
78 meter
Z = -17327221
73 Z = -5281337
18
XDOT = -24010
142838 XDOT = -7318
291537
YDOT = -378
414155 feet/sec YDOT = -115
340634 meter/sec
ZDOT = 2356
530483 ZDOT = 718
270491
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 15020
47360525
00016717 00000-0 10270-3 0 9041
2 25544 51
6468 101
4992 0006127 279
4437 80
6023 15
53493461 5050
Satellite: ISS
Catalog Number: 25544
Epoch time: 15020
47360525 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 101
4992 deg
Eccentricity:
0006127
Arg of perigee: 279
4437 deg
Mean anomaly: 80
6023 deg
Mean motion: 15
53493461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 295
Coasting Arc #6 (Orbit 520)
---------------------------------------
Vector Time (GMT): 2015/021/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3550936
60 A = 6780918
59 meter
Y = -3047844
11 meter E =
0004997
Z = 4909308
91 I = 51
99339
XDOT = 2554
104951 Wp = 358
87836
YDOT = -6822
979540 meter/sec RA = 95
70844 deg
ZDOT = -2383
685306 TA = 114
39236
MA = 114
34020
Ha = 220
181 n
mi
Hp = 217
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11650054
46 X = -3540438
03
Y = -9999488
55 feet Y = -3087494
37 meter
Z = 16106656
52 Z = 4892084
98
XDOT = 8379
609418 XDOT = 2641
790076
YDOT = -22385
103477 feet/sec YDOT = -6793
927563 meter/sec
ZDOT = -7820
489848 ZDOT = -2371
065371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6662203
56 X = 2030639
64
Y = -13916897
52 feet Y = -4241870
37 meter
Z = 16033494
05 Z = 4887008
99
XDOT = 22781
809587 XDOT = 6943
895562
YDOT = 1941
402758 feet/sec YDOT = 591
739561 meter/sec
ZDOT = -7765
245265 ZDOT = -2366
846757
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 15021
50285476
00016717 00000-0 10270-3 0 9058
2 25544 51
6468 96
3730 0006134 284
1409 75
9062 15
53540883 5211
Satellite: ISS
Catalog Number: 25544
Epoch time: 15021
50285476 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 96
3730 deg
Eccentricity:
0006134
Arg of perigee: 284
1409 deg
Mean anomaly: 75
9062 deg
Mean motion: 15
53540883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 521
Checksum: 303
Coasting Arc #7 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2015/022/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3162005
90 A = 6783828
73 meter
Y = 4365410
17 meter E =
0001383
Z = -4120379
48 I = 52
00484
XDOT = -3083
651063 Wp = 114
34054
YDOT = 5866
453698 meter/sec RA = 90
74677 deg
ZDOT = 3849
365254 TA = 195
24933
MA = 195
25350
Ha = 220
357 n
mi
Hp = 217
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10374035
12 X = 3132970
68
Y = 14322211
84 feet Y = 4400607
40 meter
Z = -13518305
37 Z = -4105089
96
XDOT = -10116
965431 XDOT = -3167
720310
YDOT = 19246
895336 feet/sec YDOT = 5831
500279 meter/sec
ZDOT = 12629
151097 ZDOT = 3834
181565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10933342
53 X = -3332482
80
Y = 13962520
72 feet Y = 4255776
31 meter
Z = -13453660
21 Z = -4100675
63
XDOT = -20278
576891 XDOT = -6180
910236
YDOT = -3775
343546 feet/sec YDOT = -1150
724713 meter/sec
ZDOT = 12563
099978 ZDOT = 3829
232873
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 15022
46775760
00016717 00000-0 10270-3 0 9065
2 25544 51
6460 91
5681 0006034 287
6735 72
3760 15
53570026 5368
Satellite: ISS
Catalog Number: 25544
Epoch time: 15022
46775760 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 91
5681 deg
Eccentricity:
0006034
Arg of perigee: 287
6735 deg
Mean anomaly: 72
3760 deg
Mean motion: 15
53570026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 307
Coasting Arc #8 (Orbit 551)
---------------------------------------
Vector Time (GMT): 2015/023/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2732363
08 A = 6787177
33 meter
Y = -5449767
45 meter E =
0007534
Z = 2977658
73 I = 52
01545
XDOT = 3593
223973 Wp = 85
03493
YDOT = -4548
893442 meter/sec RA = 85
79202 deg
ZDOT = -5016
731206 TA = 61
12842
MA = 61
05283
Ha = 220
501 n
mi
Hp = 217
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8964445
80 X = -2685683
50
Y = -17879814
48 feet Y = -5480061
44 meter
Z = 9769221
55 Z = 2964499
21
XDOT = 11788
792563 XDOT = 3668
192646
YDOT = -14924
191083 feet/sec YDOT = -4508
292629 meter/sec
ZDOT = -16459
091883 ZDOT = -4999
094152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14511789
20 X = 4423193
35
Y = -13803441
38 feet Y = -4207288
93 meter
Z = 9713893
38 Z = 2960794
70
XDOT = 16717
018989 XDOT = 5095
347388
YDOT = 6019
084260 feet/sec YDOT = 1834
616883 meter/sec
ZDOT = -16382
773820 ZDOT = -4993
469460
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
49696598
00016717 00000-0 10270-3 0 9071
2 25544 51
6457 86
4416 0006066 293
3248 66
7266 15
53591630 5521
Satellite: ISS
Catalog Number: 25544
Epoch time: 15023
49696598 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 86
4416 deg
Eccentricity:
0006066
Arg of perigee: 293
3248 deg
Mean anomaly: 66
7266 deg
Mean motion: 15
53591630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 552
Checksum: 336
Coasting Arc #9 (Orbit 566)
---------------------------------------
Vector Time (GMT): 2015/024/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2257533
08 A = 6789886
34 meter
Y = 6195848
15 meter E =
0009277
Z = -1592032
80 I = 52
02065
XDOT = -4085
068550 Wp = 356
58579
YDOT = 2969
462700 meter/sec RA = 80
84437 deg
ZDOT = 5771
082126 TA = 346
09274
MA = 346
11828
Ha = 220
829 n
mi
Hp = 217
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7406604
59 X = 2195815
24
Y = 20327585
80 feet Y = 6220748
22 meter
Z = -5223204
72 Z = -1581216
43
XDOT = -13402
455873 XDOT = -4146
003485
YDOT = 9742
331694 feet/sec YDOT = 2923
440295 meter/sec
ZDOT = 18933
996478 ZDOT = 5751
089865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17087749
63 X = -5208346
09
Y = 13287100
00 feet Y = 4049908
08 meter
Z = -5178048
82 Z = -1578269
28
XDOT = -12436
397699 XDOT = -3790
614019
YDOT = -8657
987386 feet/sec YDOT = -2638
954555 meter/sec
ZDOT = 18847
882081 ZDOT = 5744
834458
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
46182939
00016717 00000-0 10270-3 0 9089
2 25544 51
6452 81
6354 0006187 297
9687 62
0839 15
53573436 5670
Satellite: ISS
Catalog Number: 25544
Epoch time: 15024
46182939 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 81
6354 deg
Eccentricity:
0006187
Arg of perigee: 297
9687 deg
Mean anomaly: 62
0839 deg
Mean motion: 15
53573436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 567
Checksum: 343
Coasting Arc #10 (Orbit 582)
---------------------------------------
Vector Time (GMT): 2015/025/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1690278
58 A = 6790723
68 meter
Y = -6573115
10 meter E =
0006409
Z = 48925
26 I = 52
01816
XDOT = 4557
371038 Wp = 144
87470
YDOT = -1219
778244 meter/sec RA = 75
90131 deg
ZDOT = -6041
713386 TA = 34
60130
MA = 34
55961
Ha = 220
824 n
mi
Hp = 217
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5545533
40 X = -1616888
50
Y = -21565338
26 feet Y = -6591606
55 meter
Z = 160515
95 Z = 40892
78
XDOT = 14952
004717 XDOT = 4600
020192
YDOT = -4001
897127 feet/sec YDOT = -1168
576484 meter/sec
ZDOT = -19821
894311 ZDOT = -6019
471207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18637711
14 X = 5680774
36
Y = -12184499
36 feet Y = -3713835
40 meter
Z = 127354
86 Z = 38817
76
XDOT = 7749
430492 XDOT = 2362
026414
YDOT = 11630
817765 feet/sec YDOT = 3545
073255 meter/sec
ZDOT = -19726
469831 ZDOT = -6012
628004
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
49099702
00016717 00000-0 10270-3 0 9099
2 25544 51
6451 76
5087 0006009 302
5602 57
4969 15
53647844 5833
Satellite: ISS
Catalog Number: 25544
Epoch time: 15025
49099702 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 76
5087 deg
Eccentricity:
0006009
Arg of perigee: 302
5602 deg
Mean anomaly: 57
4969 deg
Mean motion: 15
53647844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 583
Checksum: 326
Coasting Arc #11 (Orbit 598)
---------------------------------------
Vector Time (GMT): 2015/026/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1021317
90 A = 6789791
56 meter
Y = 6535753
79 meter E =
0012675
Z = 1494043
34 I = 52
00643
XDOT = -4985
926201 Wp = 35
99890
YDOT = -550
977882 meter/sec RA = 70
95736 deg
ZDOT = 5803
712674 TA = 340
23427
MA = 340
28335
Ha = 221
094 n
mi
Hp = 217
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3350780
51 X = 940900
23
Y = 21442761
78 feet Y = 6546725
22 meter
Z = 4901717
00 Z = 1498809
19
XDOT = -16358
025593 XDOT = -5007
586456
YDOT = -1807
670218 feet/sec YDOT = -606
854732 meter/sec
ZDOT = 19041
052079 ZDOT = 5779
439655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19062404
06 X = -5810220
76
Y = 10366106
64 feet Y = 3159589
31 meter
Z = 4920891
88 Z = 1499887
84
XDOT = -3108
999714 XDOT = -947
623113
YDOT = -14730
022816 feet/sec YDOT = -4489
710954 meter/sec
ZDOT = 18937
264731 ZDOT = 5772
078290
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
52014397
00016717 00000-0 10270-3 0 9103
2 25544 51
6451 71
3816 0006012 307
9432 52
1176 15
53642924 5993
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
52014397 = yrday
fracday
Element set: 910
Inclination: 51
6451 deg
RA of node: 71
3816 deg
Eccentricity:
0006012
Arg of perigee: 307
9432 deg
Mean anomaly: 52
1176 deg
Mean motion: 15
53642924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 599
Checksum: 290
Coasting Arc #12 (Orbit 613)
---------------------------------------
Vector Time (GMT): 2015/027/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -216776
92 A = 6786914
69 meter
Y = -6119330
80 meter E =
0002104
Z = -2929792
21 I = 51
98681
XDOT = 5313
475688 Wp = 352
43084
YDOT = 2230
769663 meter/sec RA = 66
00837 deg
ZDOT = -5050
019421 TA = 220
78703
MA = 220
80278
Ha = 221
103 n
mi
Hp = 216
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -711210
36 X = -134101
31
Y = -20076544
61 feet Y = -6121292
70 meter
Z = -9612179
16 Z = -2930644
39
XDOT = 17432
663020 XDOT = 5312
666671
YDOT = 7318
798108 feet/sec YDOT = 2290
183833 meter/sec
ZDOT = -16568
305186 ZDOT = -5024
209807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18548375
00 X = 5653544
70
Y = -7712545
81 feet Y = -2350783
96 meter
Z = -9614669
70 Z = -2930551
32
XDOT = -1200
866288 XDOT = -366
024045
YDOT = 17639
254486 feet/sec YDOT = 5376
444767 meter/sec
ZDOT = -16458
259294 ZDOT = -5016
477433
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
48494844
00016717 00000-0 10270-3 0 9119
2 25544 51
6456 66
5752 0005945 311
6887 48
3756 15
53707634 6142
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
48494844 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 66
5752 deg
Eccentricity:
0005945
Arg of perigee: 311
6887 deg
Mean anomaly: 48
3756 deg
Mean motion: 15
53707634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 614
Checksum: 335
Coasting Arc #13 (Orbit 629)
---------------------------------------
Vector Time (GMT): 2015/028/11:00:35
460
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -713780
99 A = 6783331
43 meter
Y = 5346794
91 meter E =
0006410
Z = 4106275
92 I = 51
96118
XDOT = -5498
532366 Wp = 73
02566
YDOT = -3700
957031 meter/sec RA = 61
05036 deg
ZDOT = 3860
097614 TA = 337
24382
MA = 337
27222
Ha = 221
288 n
mi
Hp = 216
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2341801
16 X = -793463
61
Y = 17541978
07 feet Y = 5338367
41 meter
Z = 13472033
87 Z = 4102615
02
XDOT = -18039
804349 XDOT = -5475
489456
YDOT = -12142
247476 feet/sec YDOT = -3762
316367 meter/sec
ZDOT = 12664
362252 ZDOT = 3833
443032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17196744
19 X = -5241567
63
Y = 4233961
12 feet Y = 1290511
35 meter
Z = 13455344
14 Z = 4101188
89
XDOT = 4886
695891 XDOT = 1489
464908
YDOT = -20071
329892 feet/sec YDOT = -6117
741351 meter/sec
ZDOT = 12550
983511 ZDOT = 3825
539774
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
51405285
00016717 00000-0 10270-3 0 9126
2 25544 51
6453 61
4481 0005926 316
1337 43
9345 15
53736942 6308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
51405285 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 61
4481 deg
Eccentricity:
0005926
Arg of perigee: 316
1337 deg
Mean anomaly: 43
9345 deg
Mean motion: 15
53736942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 630
Checksum: 298
Coasting Arc #14 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:42:58
190
Vector Time (MET): N/A
Weight (LBS) : 949942
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -323876
76 A = 6783150
79 meter
Y = 5510568
83 meter E =
0006381
Z = 3935306
46 I = 51
95802
XDOT = -5623
959065 Wp = 72
42610
YDOT = -3247
577174 meter/sec RA = 59
45803 deg
ZDOT = 4081
141865 TA = 335
05723
MA = 335
08806
Ha = 220
594 n
mi
Hp = 216
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1062587
80 X = -404589
21
Y = 18079294
06 feet Y = 5506495
72 meter
Z = 12911110
43 Z = 3933537
14
XDOT = -18451
309269 XDOT = -5607
050362
YDOT = -10654
780754 feet/sec YDOT = -3310
373425 meter/sec
ZDOT = 13389
573049 ZDOT = 4053
863098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12584421
67 X = 3835731
73
Y = 13032460
00 feet Y = 3972293
81 meter
Z = 12902482
58 Z = 3932676
69
XDOT = -19413
321780 XDOT = -5917
180479
YDOT = 5593
311555 feet/sec YDOT = 1704
841362 meter/sec
ZDOT = 13273
437512 ZDOT = 4045
743754
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
83563388
00016717 00000-0 10270-3 0 9131
2 25544 51
6451 59
8459 0006141 308
2839 51
7761 15
53996366 6353
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83563388 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 59
8459 deg
Eccentricity:
0006141
Arg of perigee: 308
2839 deg
Mean anomaly: 51
7761 deg
Mean motion: 15
53996366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 338
Coasting Arc #15 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2015/029/18:42:58
190
Vector Time (MET): N/A
Weight (LBS) : 949942
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471033
58 A = 6779611
53 meter
Y = -4497280
24 meter E =
0010221
Z = -4864034
19 I = 51
93031
XDOT = 5640
874141 Wp = 40
55987
YDOT = 4545
011312 meter/sec RA = 54
48854 deg
ZDOT = -2491
715461 TA = 205
01204
MA = 205
06160
Ha = 220
670 n
mi
Hp = 216
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4826225
65 X = 1544841
24
Y = -14754856
43 feet Y = -4480417
44 meter
Z = -15958117
43 Z = -4856709
08
XDOT = 18506
804923 XDOT = 5601
735176
YDOT = 14911
454436 feet/sec YDOT = 4607
872431 meter/sec
ZDOT = -8174
919492 ZDOT = -2464
408552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7811649
29 X = -2380990
70
Y = -13453761
91 feet Y = -4100706
63 meter
Z = -15925896
52 Z = -4854213
26
XDOT = 22476
034283 XDOT = 6850
695249
YDOT = -3492
509012 feet/sec YDOT = -1064
516747 meter/sec
ZDOT = -8058
917423 ZDOT = -2456
358030
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
80023855
00016717 00000-0 10270-3 0 9140
2 25544 51
6456 55
0382 0006149 312
9606 47
1031 15
54040752 6509
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
80023855 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 55
0382 deg
Eccentricity:
0006149
Arg of perigee: 312
9606 deg
Mean anomaly: 47
1031 deg
Mean motion: 15
54040752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 283
Coasting Arc #16 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/18:42:58
190
Vector Time (MET): N/A
Weight (LBS) : 949942
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2693293
68 A = 6777578
31 meter
Y = 3249621
72 meter E =
0003651
Z = 5304199
84 I = 51
90467
XDOT = -5334
996051 Wp = 331
35357
YDOT = -5469
605928 meter/sec RA = 49
51039 deg
ZDOT = 645
331911 TA = 112
52673
MA = 112
48809
Ha = 220
794 n
mi
Hp = 216
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8836265
35 X = -2755196
93
Y = 10661488
57 feet Y = 3219157
35 meter
Z = 17402230
45 Z = 5290966
25
XDOT = -17503
267884 XDOT = -5276
571854
YDOT = -17944
901339 feet/sec YDOT = -5528
938666 meter/sec
ZDOT = 2117
230680 ZDOT = 619
557787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2319825
67 X = 707082
86
Y = 13724265
26 feet Y = 4183156
05 meter
Z = 17344956
05 Z = 5286742
60
XDOT = -24017
758547 XDOT = -7320
612805
YDOT = 1535
783529 feet/sec YDOT = 468
106820 meter/sec
ZDOT = 2007
973225 ZDOT = 612
030239
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
82912761
00016717 00000-0 10270-3 0 9158
2 25544 51
6454 49
9100 0006226 315
4533 44
6119 15
54091120 6661
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82912761 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 49
9100 deg
Eccentricity:
0006226
Arg of perigee: 315
4533 deg
Mean anomaly: 44
6119 deg
Mean motion: 15
54091120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 283
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