[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 14th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 68 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
229/22:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 212
9
233/21:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 212
9
237/07:37:09
920 1
4 4
6 4
6
N/A 4
4 -0
5 219
8
000/00:14:15
840 0
4 -0
0 215
9
239/10:03:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
9
Coasting Arc #1 (Orbit 1373)
---------------------------------------
Vector Time (GMT): 2016/225/10:49:40
629
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5633400
16 A = 6782309
00 meter
Y = 1804050
29 meter E =
0014190
Z = 3306256
08 I = 51
89800
XDOT = 874
656997 Wp = 91
34957
YDOT = -5975
400815 meter/sec RA = 136
24748 deg
ZDOT = 4732
941964 TA = 306
96777
MA = 307
09760
Ha = 220
310 n
mi
Hp = 212
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18482283
99 X = -5669215
05
Y = 5918800
16 feet Y = 1740853
56 meter
Z = 10847296
85 Z = 3278803
70
XDOT = 2869
609570 XDOT = 918
420045
YDOT = -19604
333381 feet/sec YDOT = -5965
375165 meter/sec
ZDOT = 15528
024817 ZDOT = 4737
297031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15044411
65 X = 4585536
67
Y = 12364727
22 feet Y = 3768768
86 meter
Z = 10727071
58 Z = 3269611
42
XDOT = -17063
470159 XDOT = -5200
945705
YDOT = 7221
431897 feet/sec YDOT = 2201
092442 meter/sec
ZDOT = 15548
032532 ZDOT = 4739
040316
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 16225
50865708
00016717 00000-0 10270-3 0 9002
2 25544 51
6412 137
0030 0001691 117
7742 242
3582 15
54983006 13743
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
50865708 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 137
0030 deg
Eccentricity:
0001691
Arg of perigee: 117
7742 deg
Mean anomaly: 242
3582 deg
Mean motion: 15
54983006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1374
Checksum: 289
Coasting Arc #2 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2016/226/10:49:40
629
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4957295
94 A = 6777810
22 meter
Y = -145425
33 meter E =
0011335
Z = -4630636
07 I = 51
90718
XDOT = -2610
931598 Wp = 76
41420
YDOT = 6545
182559 meter/sec RA = 131
27139 deg
ZDOT = -3004
238326 TA = 163
71566
MA = 163
67921
Ha = 220
184 n
mi
Hp = 212
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16264094
29 X = 4981047
07
Y = -477117
22 feet Y = -89856
65 meter
Z = -15192375
57 Z = -4606497
35
XDOT = -8566
048549 XDOT = -2669
334300
YDOT = 21473
696060 feet/sec YDOT = 6515
658880 meter/sec
ZDOT = -9856
424954 ZDOT = -3017
063177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9516455
77 X = -2900615
72
Y = -13318392
91 feet Y = -4059446
16 meter
Z = -15086886
99 Z = -4598483
15
XDOT = 21595
925873 XDOT = 6582
438206
YDOT = -4214
487212 feet/sec YDOT = -1284
575702 meter/sec
ZDOT = -9913
542480 ZDOT = -3021
647748
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 16226
47265341
00016717 00000-0 10270-3 0 9017
2 25544 51
6425 132
1913 0001649 117
4648 242
6673 15
55009939 13893
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
47265341 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 132
1913 deg
Eccentricity:
0001649
Arg of perigee: 117
4648 deg
Mean anomaly: 242
6673 deg
Mean motion: 15
55009939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 314
Coasting Arc #3 (Orbit 1404)
---------------------------------------
Vector Time (GMT): 2016/227/10:49:40
629
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3908491
78 A = 6774957
50 meter
Y = -1661216
76 meter E =
0004934
Z = 5275380
68 I = 51
91857
XDOT = 3946
660048 Wp = 122
19825
YDOT = -6523
127706 meter/sec RA = 126
28586 deg
ZDOT = 866
767035 TA = 319
53255
MA = 319
56923
Ha = 220
192 n
mi
Hp = 212
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12823135
77 X = -3915250
32
Y = -5450186
21 feet Y = -1704962
01 meter
Z = 17307679
39 Z = 5256378
02
XDOT = 12948
359737 XDOT = 4015
099667
YDOT = -21401
337619 feet/sec YDOT = -6478
610863 meter/sec
ZDOT = 2843
723868 ZDOT = 886
104762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2921721
53 X = 890540
72
Y = 13728025
31 feet Y = 4184302
11 meter
Z = 17224922
96 Z = 5250156
52
XDOT = -23949
949256 XDOT = -7299
944533
YDOT = 1408
716397 feet/sec YDOT = 429
376758 meter/sec
ZDOT = 2929
310596 ZDOT = 892
853870
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 16227
50090779
00016717 00000-0 10270-3 0 9024
2 25544 51
6425 127
0597 0001537 124
7838 235
3460 15
55039461 14057
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
50090779 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 127
0597 deg
Eccentricity:
0001537
Arg of perigee: 124
7838 deg
Mean anomaly: 235
3460 deg
Mean motion: 15
55039461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1405
Checksum: 305
Coasting Arc #4 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2016/228/10:49:40
629
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2655674
79 A = 6775402
53 meter
Y = 3463595
79 meter E =
0015347
Z = -5195958
35 I = 51
93877
XDOT = -4808
350379 Wp = 103
16817
YDOT = 5792
977358 meter/sec RA = 121
29670 deg
ZDOT = 1404
077973 TA = 180
29664
MA = 180
29756
Ha = 220
099 n
mi
Hp = 212
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8712843
80 X = 2641985
91
Y = 11363503
25 feet Y = 3493216
84 meter
Z = -17047107
43 Z = -5183091
17
XDOT = -15775
427754 XDOT = -4879
591842
YDOT = 19005
831226 feet/sec YDOT = 5738
808819 meter/sec
ZDOT = 4606
555030 ZDOT = 1380
547640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4043849
74 X = 1232565
40
Y = -13805228
00 feet Y = -4207833
49 meter
Z = -16991459
16 Z = -5178996
75
XDOT = 23655
042240 XDOT = 7210
056875
YDOT = 1387
412351 feet/sec YDOT = 422
883284 meter/sec
ZDOT = 4502
753013 ZDOT = 1372
439118
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 16228
46489348
00016717 00000-0 10270-3 0 9035
2 25544 51
6431 122
2483 0001572 125
1874 234
9426 15
55014495 14203
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
46489348 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 122
2483 deg
Eccentricity:
0001572
Arg of perigee: 125
1874 deg
Mean anomaly: 234
9426 deg
Mean motion: 15
55014495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 302
Coasting Arc #5 (Orbit 1435)
---------------------------------------
Vector Time (GMT): 2016/229/10:49:40
629
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1318721
37 A = 6778695
55 meter
Y = -5017954
80 meter E =
0010501
Z = 4354922
24 I = 51
96595
XDOT = 5224
037384 Wp = 78
79712
YDOT = -4407
943076 meter/sec RA = 116
31583 deg
ZDOT = -3488
064058 TA = 46
49266
MA = 46
40543
Ha = 220
109 n
mi
Hp = 212
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4326513
68 X = -1283665
24
Y = -16463106
29 feet Y = -5032505
59 meter
Z = 14287802
62 Z = 4348601
51
XDOT = 17139
230264 XDOT = 5289
883039
YDOT = -14461
755498 feet/sec YDOT = -4349
156248 meter/sec
ZDOT = -11443
779717 ZDOT = -3462
527544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10527775
55 X = -3208865
99
Y = 13404587
94 feet Y = 4085718
40 meter
Z = 14261025
81 Z = 4346760
67
XDOT = -20916
808828 XDOT = -6375
443331
YDOT = -4340
591185 feet/sec YDOT = -1323
012193 meter/sec
ZDOT = -11331
428495 ZDOT = -3453
819405
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 16229
49313707
00016717 00000-0 10270-3 0 9045
2 25544 51
6432 117
1169 0001541 129
6795 230
4494 15
55023651 14362
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
49313707 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 117
1169 deg
Eccentricity:
0001541
Arg of perigee: 129
6795 deg
Mean anomaly: 230
4494 deg
Mean motion: 15
55023651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1436
Checksum: 301
Coasting Arc #6 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2016/229/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1459375
15 A = 6778791
94 meter
Y = 5030354
21 meter E =
0010015
Z = -4313756
96 I = 51
97411
XDOT = -5054
020150 Wp = 116
32490
YDOT = 4520
916262 meter/sec RA = 113
91674 deg
ZDOT = 3564
185082 TA = 189
86714
MA = 189
88682
Ha = 219
995 n
mi
Hp = 212
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4787976
20 X = 1423969
93
Y = 16503786
77 feet Y = 5046475
89 meter
Z = -14152745
92 Z = -4306753
89
XDOT = -16581
430939 XDOT = -5121
511477
YDOT = 14832
402433 feet/sec YDOT = 4464
021512 meter/sec
ZDOT = 11693
520610 ZDOT = 3539
470434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11657817
62 X = -3553302
81
Y = 12658450
04 feet Y = 3858295
57 meter
Z = -14122989
83 Z = -4304687
30
XDOT = -20357
119667 XDOT = -6204
850074
YDOT = -5830
460672 feet/sec YDOT = -1777
124413 meter/sec
ZDOT = 11584
736003 ZDOT = 3531
027534
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 16229
94298935
00016717 00000-0 10270-3 0 9051
2 25544 51
6439 114
8684 0001801 144
3045 215
8229 15
55052868 14439
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
94298935 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 114
8684 deg
Eccentricity:
0001801
Arg of perigee: 144
3045 deg
Mean anomaly: 215
8229 deg
Mean motion: 15
55052868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 324
Coasting Arc #7 (Orbit 1458)
---------------------------------------
Vector Time (GMT): 2016/230/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -214580
88 A = 6783315
27 meter
Y = -6157899
29 meter E =
0014692
Z = 2819453
88 I = 52
00075
XDOT = 5110
277894 Wp = 104
72858
YDOT = -2536
410060 meter/sec RA = 108
95054 deg
ZDOT = -5132
184037 TA = 43
39963
MA = 43
28405
Ha = 220
028 n
mi
Hp = 212
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -704005
51 X = -159401
15
Y = -20203081
66 feet Y = -6159990
25 meter
Z = 9250176
77 Z = 2818545
76
XDOT = 16766
003589 XDOT = 5163
190280
YDOT = -8321
555315 feet/sec YDOT = -2478
967843 meter/sec
ZDOT = -16837
874138 ZDOT = -5107
231510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16753358
25 X = 5106423
59
Y = -11315439
08 feet Y = -3448945
83 meter
Z = 9247255
18 Z = 2818563
38
XDOT = 15152
926562 XDOT = 4618
612016
YDOT = 8714
328587 feet/sec YDOT = 2656
127353 meter/sec
ZDOT = -16728
376114 ZDOT = -5098
809040
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 16230
97122333
00016717 00000-0 10270-3 0 9065
2 25544 51
6434 109
7364 0001752 144
3862 215
7408 15
55037908 14597
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
97122333 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 109
7364 deg
Eccentricity:
0001752
Arg of perigee: 144
3862 deg
Mean anomaly: 215
7408 deg
Mean motion: 15
55037908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1459
Checksum: 306
Coasting Arc #8 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2016/231/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -894376
59 A = 6786385
06 meter
Y = 6656227
32 meter E =
0009462
Z = -950595
95 I = 52
01971
XDOT = -4834
530275 Wp = 47
84651
YDOT = 193
642219 meter/sec RA = 103
99728 deg
ZDOT = 5948
446884 TA = 301
91198
MA = 302
00398
Ha = 219
972 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2934306
41 X = -964124
25
Y = 21838016
15 feet Y = 6645835
77 meter
Z = -3118753
13 Z = -955110
29
XDOT = -15861
319801 XDOT = -4865
230738
YDOT = 635
309118 feet/sec YDOT = 139
407935 meter/sec
ZDOT = 19515
901852 ZDOT = 5924
887841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19925465
83 X = -6073281
99
Y = 9399696
51 feet Y = 2865027
49 meter
Z = -3139624
42 Z = -956957
52
XDOT = -8523
233801 XDOT = -2597
881663
YDOT = -11631
188695 feet/sec YDOT = -3545
186314 meter/sec
ZDOT = 19412
887958 ZDOT = 5917
048250
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 16231
93518756
00016717 00000-0 10270-3 0 9071
2 25544 51
6428 104
9250 0001555 148
3892 211
7354 15
55006494 14748
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
93518756 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 104
9250 deg
Eccentricity:
0001555
Arg of perigee: 148
3892 deg
Mean anomaly: 211
7354 deg
Mean motion: 15
55006494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 313
Coasting Arc #9 (Orbit 1489)
---------------------------------------
Vector Time (GMT): 2016/232/22:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1887824
72 A = 6786150
11 meter
Y = -6420386
61 meter E =
0011159
Z = -1094707
97 I = 52
02574
XDOT = 4316
445042 Wp = 143
35951
YDOT = 2271
618658 meter/sec RA = 99
04942 deg
ZDOT = -5918
826769 TA = 48
45779
MA = 48
36213
Ha = 219
924 n
mi
Hp = 212
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6193650
64 X = 1964796
33
Y = -21064260
54 feet Y = -6398845
40 meter
Z = -3591561
59 Z = -1085350
15
XDOT = 14161
565098 XDOT = 4319
473044
YDOT = 7452
817119 feet/sec YDOT = 2319
904553 meter/sec
ZDOT = -19418
722997 ZDOT = -5897
851723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20957914
93 X = 6387972
47
Y = -6567357
59 feet Y = -2001730
59 meter
Z = -3549550
86 Z = -1081903
10
XDOT = 1288
708283 XDOT = 392
798285
YDOT = 14487
573127 feet/sec YDOT = 4415
812289 meter/sec
ZDOT = -19327
425460 ZDOT = -5890
999280
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 16232
96341100
00016717 00000-0 10270-3 0 9083
2 25544 51
6424 99
7924 0001664 152
4632 207
6609 15
55051047 14901
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
96341100 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 99
7924 deg
Eccentricity:
0001664
Arg of perigee: 152
4632 deg
Mean anomaly: 207
6609 deg
Mean motion: 15
55051047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1490
Checksum: 298
Coasting Arc #10 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3864061
92 A = 6775397
44 meter
Y = -2134265
61 meter E =
0004900
Z = 5136352
17 I = 51
99531
XDOT = 1832
594873 Wp = 72
99221
YDOT = -7268
730974 meter/sec RA = 94
31326 deg
ZDOT = -1638
978925 TA = 32
75118
MA = 32
72081
Ha = 219
901 n
mi
Hp = 212
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12677368
50 X = -3864858
70
Y = -7002183
78 feet Y = -2177480
19 meter
Z = 16851549
10 Z = 5117580
00
XDOT = 6012
450370 XDOT = 1921
700812
YDOT = -23847
542565 feet/sec YDOT = -7247
739578 meter/sec
ZDOT = -5377
227445 ZDOT = -1629
859763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3136478
02 X = 955998
50
Y = -14235704
66 feet Y = -4339042
78 meter
Z = 16769859
13 Z = 5111453
06
XDOT = 23548
950705 XDOT = 7177
720175
YDOT = -1107
999928 feet/sec YDOT = -337
718378 meter/sec
ZDOT = -5336
103960 ZDOT = -1626
444487
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 16233
92736331
00016717 00000-0 10270-3 0 9095
2 25544 51
6434 94
9792 0001555 157
6063 202
5159 15
55098493 15053
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
92736331 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 94
9792 deg
Eccentricity:
0001555
Arg of perigee: 157
6063 deg
Mean anomaly: 202
5159 deg
Mean motion: 15
55098493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 322
Coasting Arc #11 (Orbit 1519)
---------------------------------------
Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3357158
50 A = 6778995
75 meter
Y = 4100660
43 meter E =
0009213
Z = -4237017
77 I = 52
00750
XDOT = -2806
992484 Wp = 117
73803
YDOT = 6102
577914 meter/sec RA = 89
33623 deg
ZDOT = 3684
026474 TA = 189
85505
MA = 189
87314
Ha = 219
797 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11014299
55 X = 3331635
80
Y = 13453610
33 feet Y = 4138059
38 meter
Z = -13900976
94 Z = -4220772
00
XDOT = -9209
292928 XDOT = -2892
919693
YDOT = 20021
581082 feet/sec YDOT = 6070
708088 meter/sec
ZDOT = 12086
701030 ZDOT = 3670
181742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9551384
28 X = -2911261
93
Y = 14595718
00 feet Y = 4448774
85 meter
Z = -13830678
22 Z = -4215590
72
XDOT = -20812
382214 XDOT = -6343
614099
YDOT = -2230
785972 feet/sec YDOT = -679
943564 meter/sec
ZDOT = 12025
111704 ZDOT = 3665
254048
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 16234
89131443
00016717 00000-0 10270-3 0 9107
2 25544 51
6421 90
1683 0001690 157
8579 202
2648 15
55092883 15204
Satellite: ISS
Catalog Number: 25544
Epoch time: 16234
89131443 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 90
1683 deg
Eccentricity:
0001690
Arg of perigee: 157
8579 deg
Mean anomaly: 202
2648 deg
Mean motion: 15
55092883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1520
Checksum: 305
Coasting Arc #12 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2669871
18 A = 6783486
81 meter
Y = -5613311
95 meter E =
0014366
Z = 2698296
90 I = 52
02170
XDOT = 3672
501913 Wp = 107
08716
YDOT = -4263
638467 meter/sec RA = 84
37188 deg
ZDOT = -5217
195763 TA = 42
57030
MA = 42
45902
Ha = 219
783 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8759419
87 X = -2620010
37
Y = -18416377
79 feet Y = -5642889
26 meter
Z = 8852680
13 Z = 2685448
91
XDOT = 12048
890792 XDOT = 3745
248807
YDOT = -13988
315179 feet/sec YDOT = -4222
163709 meter/sec
ZDOT = -17116
784000 ZDOT = -5199
178771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14728799
39 X = 4489338
06
Y = -14139541
50 feet Y = -4309732
25 meter
Z = 8797510
30 Z = 2681481
14
XDOT = 16062
655622 XDOT = 4895
897434
YDOT = 6093
174416 feet/sec YDOT = 1857
199562 meter/sec
ZDOT = -17037
269042 ZDOT = -5192
959604
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 16235
91952284
00016717 00000-0 10270-3 0 9116
2 25544 51
6427 85
0353 0001516 161
8309 198
2898 15
55089167 15369
Satellite: ISS
Catalog Number: 25544
Epoch time: 16235
91952284 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 85
0353 deg
Eccentricity:
0001516
Arg of perigee: 161
8309 deg
Mean anomaly: 198
2898 deg
Mean motion: 15
55089167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 329
Coasting Arc #13 (Orbit 1550)
---------------------------------------
Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1842530
58 A = 6786417
40 meter
Y = 6478765
99 meter E =
0009696
Z = -796397
42 I = 52
02699
XDOT = -4378
134794 Wp = 45
94860
YDOT = 1973
643031 meter/sec RA = 79
41964 deg
ZDOT = 5978
123022 TA = 305
48528
MA = 305
57571
Ha = 219
766 n
mi
Hp = 213
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6045047
83 X = 1773814
98
Y = 21255793
94 feet Y = 6498986
15 meter
Z = -2612852
41 Z = -787614
16
XDOT = -14363
959298 XDOT = -4428
918223
YDOT = 6475
206795 feet/sec YDOT = 1924
400184 meter/sec
ZDOT = 19613
264509 ZDOT = 5956
731760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18072293
91 X = -5508435
18
Y = 12725437
52 feet Y = 3878713
36 meter
Z = -2575618
36 Z = -785048
48
XDOT = -9960
911634 XDOT = -3036
085866
YDOT = -10230
196300 feet/sec YDOT = -3118
163832 meter/sec
ZDOT = 19519
399546 ZDOT = 5949
512982
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 16236
88346333
00016717 00000-0 10270-3 0 9126
2 25544 51
6428 80
2234 0001273 162
5981 197
5216 15
55039291 15515
Satellite: ISS
Catalog Number: 25544
Epoch time: 16236
88346333 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 80
2234 deg
Eccentricity:
0001273
Arg of perigee: 162
5981 deg
Mean anomaly: 197
5216 deg
Mean motion: 15
55039291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1551
Checksum: 305
Coasting Arc #14 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2016/237/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4290425
23 A = 6780086
76 meter
Y = 2408648
88 meter E =
0007914
Z = -4672548
20 I = 51
99533
XDOT = -754
443863 Wp = 124
43907
YDOT = 7037
048426 meter/sec RA = 77
21797 deg
ZDOT = 2933
955874 TA = 174
64345
MA = 174
63498
Ha = 219
796 n
mi
Hp = 215
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14076198
26 X = 4285869
38
Y = 7902391
35 feet Y = 2456601
59 meter
Z = -15329882
55 Z = -4651717
64
XDOT = -2475
209525 XDOT = -847
329695
YDOT = 23087
429218 feet/sec YDOT = 7028
092515 meter/sec
ZDOT = 9625
839481 ZDOT = 2930
065041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8332181
89 X = 2539649
04
Y = -13925956
24 feet Y = -4244631
46 meter
Z = -15239256
32 Z = -4644925
33
XDOT = 21984
081592 XDOT = 6700
748069
YDOT = 2636
938660 feet/sec YDOT = 803
738903 meter/sec
ZDOT = 9607
562131 ZDOT = 2928
384938
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 16237
33330380
00016717 00000-0 10270-3 0 9133
2 25544 51
6435 77
9783 0003436 253
7683 106
3092 15
54165114 15580
Satellite: ISS
Catalog Number: 25544
Epoch time: 16237
33330380 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 77
9783 deg
Eccentricity:
0003436
Arg of perigee: 253
7683 deg
Mean anomaly: 106
3092 deg
Mean motion: 15
54165114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 307
Coasting Arc #15 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2016/238/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4201207
09 A = 6783868
92 meter
Y = -3928946
31 meter E =
0008714
Z = 3588696
86 I = 51
99945
XDOT = 1758
470260 Wp = 91
44296
YDOT = -5975
941199 meter/sec RA = 72
25498 deg
ZDOT = -4474
795560 TA = 46
35666
MA = 46
28443
Ha = 219
873 n
mi
Hp = 215
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13783487
81 X = -4174392
63
Y = -12890243
81 feet Y = -3975776
98 meter
Z = 11773939
84 Z = 3568353
81
XDOT = 5769
259384 XDOT = 1846
900583
YDOT = -19606
106295 feet/sec YDOT = -5955
782510 meter/sec
ZDOT = -14681
087796 ZDOT = -4466
038412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13074865
27 X = -3985218
93
Y = 13684308
46 feet Y = 4170977
22 meter
Z = 11685725
54 Z = 3561809
14
XDOT = -18528
708525 XDOT = -5647
550358
YDOT = -5174
435656 feet/sec YDOT = -1577
167988 meter/sec
ZDOT = -14641
715151 ZDOT = -4462
794778
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 16238
36211485
00016717 00000-0 10270-3 0 9142
2 25544 51
6431 72
8508 0003456 256
5397 103
5370 15
54155542 15740
Satellite: ISS
Catalog Number: 25544
Epoch time: 16238
36211485 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 72
8508 deg
Eccentricity:
0003456
Arg of perigee: 256
5397 deg
Mean anomaly: 103
5370 deg
Mean motion: 15
54155542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 306
Coasting Arc #16 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2016/239/07:44:17
840
Vector Time (MET): N/A
Weight (LBS) : 929483
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3942213
75 A = 6787248
83 meter
Y = 5090050
57 meter E =
0004325
Z = -2140876
48 I = 52
00171
XDOT = -2806
121868 Wp = 8
56493
YDOT = 4499
543669 meter/sec RA = 67
29974 deg
ZDOT = 5536
305412 TA = 327
83070
MA = 327
85708
Ha = 219
633 n
mi
Hp = 215
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12933772
15 X = 3895401
90
Y = 16699640
97 feet Y = 5133873
25 meter
Z = -7023872
98 Z = -2121840
16
XDOT = -9206
436574 XDOT = -2883
121129
YDOT = 14762
282380 feet/sec YDOT = 4467
733339 meter/sec
ZDOT = 18163
731668 ZDOT = 5522
486953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16650614
65 X = 5075107
35
Y = -13040958
95 feet Y = -3974884
29 meter
Z = -6941590
84 Z = -2115796
89
XDOT = 13847
533091 XDOT = 4220
728086
YDOT = 8054
524416 feet/sec YDOT = 2455
019042 meter/sec
ZDOT = 18102
492528 ZDOT = 5517
639723
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 16239
32661888
00016717 00000-0 10270-3 0 9156
2 25544 51
6444 68
0420 0003610 261
8515 98
2228 15
54190079 15899
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
32661888 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node: 68
0420 deg
Eccentricity:
0003610
Arg of perigee: 261
8515 deg
Mean anomaly: 98
2228 deg
Mean motion: 15
54190079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 319
Coasting Arc #17 (Orbit 1590)
---------------------------------------
Vector Time (GMT): 2016/239/10:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4008935
32 A = 6787141
92 meter
Y = -5010917
90 meter E =
0010666
Z = 2192582
73 I = 51
99963
XDOT = 2717
077009 Wp = 117
37162
YDOT = -4591
652686 meter/sec RA = 66
82142 deg
ZDOT = -5510
110731 TA = 38
40464
MA = 38
32876
Ha = 219
611 n
mi
Hp = 215
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13152674
93 X = -3963254
55
Y = -16440019
35 feet Y = -5055493
03 meter
Z = 7193512
89 Z = 2173219
55
XDOT = 8914
294650 XDOT = 2794
985625
YDOT = -15064
477315 feet/sec YDOT = -4560
833028 meter/sec
ZDOT = -18077
791112 ZDOT = -5496
722622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5901498
96 X = -1798776
88
Y = 20239489
81 feet Y = 6168996
49 meter
Z = 7109787
92 Z = 2167063
36
XDOT = -16045
861715 XDOT = -4890
778651
YDOT = 1669
169131 feet/sec YDOT = 508
762751 meter/sec
ZDOT = -18018
415449 ZDOT = -5492
013029
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 16239
45521784
00016717 00000-0 10270-3 0 9161
2 25544 51
6438 67
4008 0003662 265
1739 94
8995 15
54196414 15914
Satellite: ISS
Catalog Number: 25544
Epoch time: 16239
45521784 = yrday
fracday
Element set: 916
Inclination: 51
6438 deg
RA of node: 67
4008 deg
Eccentricity:
0003662
Arg of perigee: 265
1739 deg
Mean anomaly: 94
8995 deg
Mean motion: 15
54196414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1591
Checksum: 339
Coasting Arc #18 (Orbit 1605)
---------------------------------------
Vector Time (GMT): 2016/240/10:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 910045
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3543336
90 A = 6789083
68 meter
Y = 5761161
63 meter E =
0008941
Z = -523124
22 I = 51
99080
XDOT = -3792
344187 Wp = 23
80301
YDOT = 2874
488608 meter/sec RA = 61
87240 deg
ZDOT = 6013
233233 TA = 330
58040
MA = 330
63069
Ha = 219
600 n
mi
Hp = 215
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11625121
05 X = 3481191
86
Y = 18901448
92 feet Y = 5800438
11 meter
Z = -1716286
82 Z = -506062
86
XDOT = -12442
074105 XDOT = -3853
414946
YDOT = 9430
736904 feet/sec YDOT = 2831
738760 meter/sec
ZDOT = 19728
455490 ZDOT = 5994
662790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8462985
57 X = 2579518
00
Y = -20519089
44 feet Y = -6254218
46 meter
Z = -1642770
46 Z = -500716
43
XDOT = 13520
409286 XDOT = 4121
020750
YDOT = 4015
464074 feet/sec YDOT = 1223
913450 meter/sec
ZDOT = 19646
735171 ZDOT = 5988
324880
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 16240
41971780
00016717 00000-0 10270-3 0 9175
2 25544 51
6422 62
5918 0003675 268
5639 91
5093 15
54175725 16065
Satellite: ISS
Catalog Number: 25544
Epoch time: 16240
41971780 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 62
5918 deg
Eccentricity:
0003675
Arg of perigee: 268
5639 deg
Mean anomaly: 91
5093 deg
Mean motion: 15
54175725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1606
Checksum: 324
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