[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 28th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
090/14:15:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
2
091/16:23:58
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
1
093/17:58:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
0
094/18:43:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
9
098/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2016/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3728422
79 A = 6782848
33 meter
Y = -4201710
43 meter E =
0007021
Z = -3809783
13 I = 52
00212
XDOT = 2355
625309 Wp = 58
59795
YDOT = 5930
962282 meter/sec RA = 99
59030 deg
ZDOT = -4237
970236 TA = 166
82223
MA = 166
80388
Ha = 221
007 n
mi
Hp = 214
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12232358
23 X = 3793636
69
Y = -13785139
20 feet Y = -4159652
50 meter
Z = -12499288
49 Z = -3791512
40
XDOT = 7728
429493 XDOT = 2309
715140
YDOT = 19458
537669 feet/sec YDOT = 5957
047301 meter/sec
ZDOT = -13904
101823 ZDOT = -4226
639248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10937958
53 X = 3333889
76
Y = -14900282
82 feet Y = -4541606
20 meter
Z = -12419158
53 Z = -3785359
52
XDOT = 8555
593276 XDOT = 2607
744830
YDOT = 17823
111328 feet/sec YDOT = 5432
484333 meter/sec
ZDOT = -13855
876173 ZDOT = -4223
271057
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 16088
52407929
00016717 00000-0 10270-3 0 9008
2 25544 51
6400 100
3457 0002302 3
7173 356
3996 15
54270295 32439
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
52407929 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 100
3457 deg
Eccentricity:
0002302
Arg of perigee: 3
7173 deg
Mean anomaly: 356
3996 deg
Mean motion: 15
54270295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 291
Coasting Arc #2 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2016/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3986660
59 A = 6779169
94 meter
Y = 2612044
08 meter E =
0006898
Z = 4815545
86 I = 51
99378
XDOT = -1473
133581 Wp = 100
22232
YDOT = -7063
601323 meter/sec RA = 94
62306 deg
ZDOT = 2607
511719 TA = 324
20274
MA = 324
24895
Ha = 221
206 n
mi
Hp = 214
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13079595
12 X = -4038964
83
Y = 8569698
43 feet Y = 2567170
60 meter
Z = 15799034
99 Z = 4796052
25
XDOT = -4833
115422 XDOT = -1406
703401
YDOT = -23174
545022 feet/sec YDOT = -7079
703201 meter/sec
ZDOT = 8554
828473 ZDOT = 2600
517579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12130775
66 X = -3697460
42
Y = 10002206
11 feet Y = 3048672
42 meter
Z = 15713853
80 Z = 4789582
64
XDOT = -6739
585134 XDOT = -2054
225549
YDOT = -21590
538644 feet/sec YDOT = -6580
796179 meter/sec
ZDOT = 8525
660797 ZDOT = 2598
621411
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 16089
55281383
00016717 00000-0 10270-3 0 9017
2 25544 51
6395 95
2158 0002376 7
4533 352
6655 15
54270530 32594
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
55281383 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 95
2158 deg
Eccentricity:
0002376
Arg of perigee: 7
4533 deg
Mean anomaly: 352
6655 deg
Mean motion: 15
54270530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3259
Checksum: 315
Coasting Arc #3 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2016/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148610
91 A = 6777076
07 meter
Y = -787985
80 meter E =
0015521
Z = -5313980
87 I = 51
98909
XDOT = 575
491878 Wp = 76
25804
YDOT = 7605
670745 meter/sec RA = 89
64850 deg
ZDOT = -676
595242 TA = 187
29164
MA = 187
31424
Ha = 221
123 n
mi
Hp = 214
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13610928
19 X = 4182927
18
Y = -2585255
26 feet Y = -741401
87 meter
Z = -17434320
42 Z = -5293744
45
XDOT = 1888
096714 XDOT = 493
687227
YDOT = 24952
988007 feet/sec YDOT = 7611
648821 meter/sec
ZDOT = -2219
800662 ZDOT = -673
998991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13270904
04 X = 4044971
55
Y = -4346043
58 feet Y = -1324674
08 meter
Z = -17346222
95 Z = -5287128
76
XDOT = 4808
010577 XDOT = 1465
481624
YDOT = 23527
079338 feet/sec YDOT = 7171
053782 meter/sec
ZDOT = -2209
857806 ZDOT = -673
564659
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 16090
51724511
00016717 00000-0 10270-3 0 9021
2 25544 51
6402 90
4077 0002407 11
9889 348
1320 15
54277262 32744
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
51724511 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 90
4077 deg
Eccentricity:
0002407
Arg of perigee: 11
9889 deg
Mean anomaly: 348
1320 deg
Mean motion: 15
54277262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 289
Coasting Arc #4 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2016/090/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 904351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3897838
73 A = 6778139
84 meter
Y = 2326863
95 meter E =
0005261
Z = 5029234
91 I = 51
99299
XDOT = -1684
675196 Wp = 98
76495
YDOT = -7205
580710 meter/sec RA = 89
19212 deg
ZDOT = 2025
523422 TA = 331
64412
MA = 331
67274
Ha = 221
139 n
mi
Hp = 214
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12788184
81 X = -3947998
56
Y = 7634068
09 feet Y = 2282995
70 meter
Z = 16500114
54 Z = 5010178
08
XDOT = -5527
149594 XDOT = -1613
814553
YDOT = -23640
356660 feet/sec YDOT = -7224
023487 meter/sec
ZDOT = 6645
418051 ZDOT = 2017
512395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4616147
31 X = -1407001
70
Y = 14256505
45 feet Y = 4345382
86 meter
Z = 16416871
88 Z = 5003862
55
XDOT = -18777
809382 XDOT = -5723
476300
YDOT = -13703
714728 feet/sec YDOT = -4176
892249 meter/sec
ZDOT = 6611
870238 ZDOT = 2015
298048
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 16090
64583525
00016717 00000-0 10270-3 0 9034
2 25544 51
6401 89
7665 0002499 5
9867 354
1315 15
54317633 32767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
64583525 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 89
7665 deg
Eccentricity:
0002499
Arg of perigee: 5
9867 deg
Mean anomaly: 354
1315 deg
Mean motion: 15
54317633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 325
Coasting Arc #5 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2016/091/14:15:30
000
Vector Time (MET): N/A
Weight (LBS) : 904351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4153102
32 A = 6776877
30 meter
Y = -474730
73 meter E =
0015611
Z = -5347344
70 I = 51
98671
XDOT = 807
761850 Wp = 80
37227
YDOT = 7614
599497 meter/sec RA = 84
21506 deg
ZDOT = -46
230540 TA = 189
17439
MA = 189
20295
Ha = 221
131 n
mi
Hp = 214
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13625663
77 X = 4184077
34
Y = -1557515
51 feet Y = -428115
24 meter
Z = -17543781
84 Z = -5327094
67
XDOT = 2650
137302 XDOT = 722
778037
YDOT = 24982
281814 feet/sec YDOT = 7623
157250 meter/sec
ZDOT = -151
674999 ZDOT = -42
513688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9091741
10 X = 2771162
69
Y = -10416740
76 feet Y = -3175022
58 meter
Z = -17455675
42 Z = -5320489
87
XDOT = 18046
881560 XDOT = 5500
689500
YDOT = 15994
094120 feet/sec YDOT = 4874
999888 meter/sec
ZDOT = -136
878048 ZDOT = -41
720429
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 16091
61026130
00016717 00000-0 10270-3 0 9047
2 25544 51
6397 84
9574 0002566 11
6824 348
4387 15
54293909 32910
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
61026130 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 84
9574 deg
Eccentricity:
0002566
Arg of perigee: 11
6824 deg
Mean anomaly: 348
4387 deg
Mean motion: 15
54293909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 321
Coasting Arc #6 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 904351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2651324
05 A = 6781967
44 meter
Y = 4756871
17 meter E =
0011160
Z = 4032147
02 I = 52
00502
XDOT = -3702
493283 Wp = 88
26767
YDOT = -5429
112752 meter/sec RA = 83
79827 deg
ZDOT = 3961
266915 TA = 320
76494
MA = 320
84577
Ha = 221
203 n
mi
Hp = 214
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8698569
72 X = -2723905
97
Y = 15606532
71 feet Y = 4726816
81 meter
Z = 13228828
81 Z = 4019090
84
XDOT = -12147
287674 XDOT = -3660
750571
YDOT = -17812
049711 feet/sec YDOT = -5470
282761 meter/sec
ZDOT = 12996
282530 ZDOT = 3943
382956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12718257
47 X = 3876524
88
Y = 12609345
69 feet Y = 3843328
57 meter
Z = 13171226
91 Z = 4014589
96
XDOT = -19497
897599 XDOT = -5942
959188
YDOT = 6139
787621 feet/sec YDOT = 1871
407267 meter/sec
ZDOT = 12919
515191 ZDOT = 3937
868230
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 16091
73885115
00016717 00000-0 10270-3 0 9057
2 25544 51
6411 84
3172 0002541 12
6633 347
4583 15
54306441 32932
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
73885115 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 84
3172 deg
Eccentricity:
0002541
Arg of perigee: 12
6633 deg
Mean anomaly: 347
4583 deg
Mean motion: 15
54306441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 293
Coasting Arc #7 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 904351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3323074
51 A = 6778393
59 meter
Y = -3216391
15 meter E =
0013877
Z = -4968495
84 I = 51
98977
XDOT = 3089
808677 Wp = 64
50177
YDOT = 6641
753816 meter/sec RA = 78
82917 deg
ZDOT = -2232
074056 TA = 183
78099
MA = 183
79149
Ha = 221
127 n
mi
Hp = 214
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10902475
41 X = 3382928
81
Y = -10552464
40 feet Y = -3178896
10 meter
Z = -16300839
37 Z = -4952207
53
XDOT = 10137
167576 XDOT = 3026
151738
YDOT = 21790
530893 feet/sec YDOT = 6675
949985 meter/sec
ZDOT = -7323
077612 ZDOT = -2217
219760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7485280
94 X = -2281513
63
Y = -13285750
58 feet Y = -4049496
78 meter
Z = -16229455
94 Z = -4946738
17
XDOT = 22669
074435 XDOT = 6909
533888
YDOT = -3899
821876 feet/sec YDOT = -1188
665708 meter/sec
ZDOT = -7259
704885 ZDOT = -2212
758049
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 16092
70326991
00016717 00000-0 10270-3 0 9068
2 25544 51
6420 79
5084 0002611 15
4957 344
6275 15
54329990 33086
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
70326991 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 79
5084 deg
Eccentricity:
0002611
Arg of perigee: 15
4957 deg
Mean anomaly: 344
6275 deg
Mean motion: 15
54329990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 318
Coasting Arc #8 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 904351
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3923484
15 A = 6776680
32 meter
Y = 1439527
51 meter E =
0003712
Z = 5331780
49 I = 51
97729
XDOT = -2327
845533 Wp = 57
61727
YDOT = -7305
491811 meter/sec RA = 73
85242 deg
ZDOT = 261
227708 TA = 29
91603
MA = 29
89482
Ha = 221
218 n
mi
Hp = 213
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12872323
32 X = -3965189
14
Y = 4722859
28 feet Y = 1395419
84 meter
Z = 17492718
15 Z = 5312619
79
XDOT = -7637
288495 XDOT = -2247
249624
YDOT = -23968
148985 feet/sec YDOT = -7331
072663 meter/sec
ZDOT = 857
046285 ZDOT = 250
116126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1583500
65 X = 482651
00
Y = 13726280
43 feet Y = 4183770
27 meter
Z = 17409165
60 Z = 5306313
68
XDOT = -24086
229173 XDOT = -7341
482652
YDOT = 1758
772696 feet/sec YDOT = 536
073918 meter/sec
ZDOT = 810
071758 ZDOT = 246
909872
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 16093
73197391
00016717 00000-0 10270-3 0 9073
2 25544 51
6420 74
3793 0002572 15
8542 344
2691 15
54363282 33244
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
73197391 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 74
3793 deg
Eccentricity:
0002572
Arg of perigee: 15
8542 deg
Mean anomaly: 344
2691 deg
Mean motion: 15
54363282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 311
Coasting Arc #9 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184992
74 A = 6776796
70 meter
Y = 478544
59 meter E =
0005051
Z = 5306121
54 I = 51
97852
XDOT = -1678
617320 Wp = 41
55970
YDOT = -7457
619887 meter/sec RA = 73
51839 deg
ZDOT = -647
328115 TA = 54
61271
MA = 54
56554
Ha = 221
206 n
mi
Hp = 214
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13730291
15 X = -4215807
71
Y = 1570028
19 feet Y = 431573
46 meter
Z = 17408535
25 Z = 5285717
05
XDOT = -5507
274673 XDOT = -1591
955166
YDOT = -24467
256847 feet/sec YDOT = -7475
906810 meter/sec
ZDOT = -2123
779906 ZDOT = -655
271160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4033254
49 X = 1229335
97
Y = 13334244
84 feet Y = 4064277
83 meter
Z = 17319750
45 Z = 5279059
94
XDOT = -22109
728312 XDOT = -6739
045189
YDOT = 9506
526084 feet/sec YDOT = 2897
589150 meter/sec
ZDOT = -2156
952619 ZDOT = -657
439158
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 16093
79626724
00016717 00000-0 10270-3 0 9087
2 25544 51
6434 74
0590 0002561 15
3761 344
7469 15
54365994 33258
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79626724 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 74
0590 deg
Eccentricity:
0002561
Arg of perigee: 15
3761 deg
Mean anomaly: 344
7469 deg
Mean motion: 15
54365994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 329
Coasting Arc #10 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4578908
04 A = 6778936
15 meter
Y = 1320910
93 meter E =
0011766
Z = -4831597
32 I = 51
97468
XDOT = 651
001647 Wp = 95
18712
YDOT = 7180
984670 meter/sec RA = 68
54172 deg
ZDOT = 2584
530879 TA = 200
15204
MA = 200
19853
Ha = 221
194 n
mi
Hp = 214
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15022664
17 X = 4587266
74
Y = 4333697
28 feet Y = 1372161
51 meter
Z = -15851697
25 Z = -4809334
03
XDOT = 2135
832175 XDOT = 558
099191
YDOT = 23559
660990 feet/sec YDOT = 7187
745452 meter/sec
ZDOT = 8479
432018 ZDOT = 2587
466800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1274552
96 X = 388483
74
Y = -15680819
14 feet Y = -4779513
67 meter
Z = -15755161
14 Z = -4802173
12
XDOT = 21548
077472 XDOT = 6567
854013
YDOT = -6765
205232 feet/sec YDOT = -2062
034555 meter/sec
ZDOT = 8490
880251 ZDOT = 2588
020301
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 16094
76067283
00016717 00000-0 10270-3 0 9095
2 25544 51
6426 69
2502 0002633 19
7103 340
4151 15
54345609 33405
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76067283 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 69
2502 deg
Eccentricity:
0002633
Arg of perigee: 19
7103 deg
Mean anomaly: 340
4151 deg
Mean motion: 15
54345609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 294
Coasting Arc #11 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4450779
71 A = 6777726
37 meter
Y = -424797
58 meter E =
0007702
Z = 5090848
64 I = 51
97036
XDOT = -1378
987927 Wp = 43
36316
YDOT = -7326
173372 meter/sec RA = 68
39428 deg
ZDOT = -1809
857770 TA = 64
10483
MA = 64
02546
Ha = 221
231 n
mi
Hp = 213
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14602295
64 X = -4470427
83
Y = -1393692
86 feet Y = -474678
43 meter
Z = 16702259
31 Z = 5069180
24
XDOT = -4524
238607 XDOT = -1288
170851
YDOT = -24036
001877 feet/sec YDOT = -7341
086553 meter/sec
ZDOT = -5937
853576 ZDOT = -1816
335103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4324541
98 X = 1318120
40
Y = 14128083
11 feet Y = 4306239
73 meter
Z = 16608145
23 Z = 5062162
67
XDOT = -19477
162155 XDOT = -5936
639025
YDOT = 13001
013889 feet/sec YDOT = 3962
709033 meter/sec
ZDOT = -5964
669388 ZDOT = -1818
031229
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 16094
82496478
00016717 00000-0 10270-3 0 9106
2 25544 51
6424 68
9294 0002614 18
1341 341
9904 15
54375007 33411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82496478 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 68
9294 deg
Eccentricity:
0002614
Arg of perigee: 18
1341 deg
Mean anomaly: 341
9904 deg
Mean motion: 15
54375007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 311
Coasting Arc #12 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2016/095/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4812063
16 A = 6780982
71 meter
Y = 2120028
62 meter E =
0008659
Z = -4289195
40 I = 51
96810
XDOT = 229
367528 Wp = 92
53992
YDOT = 6757
385408 meter/sec RA = 63
42079 deg
ZDOT = 3603
200950 TA = 214
09345
MA = 214
14909
Ha = 221
197 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15787608
79 X = 4808833
90
Y = 6955474
46 feet Y = 2173821
69 meter
Z = -14072163
39 Z = -4265827
73
XDOT = 752
518135 XDOT = 136
284914
YDOT = 22169
899632 feet/sec YDOT = 6759
430364 meter/sec
ZDOT = 11821
525428 ZDOT = 3604
088190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 72966
58 X = 22240
21
Y = -17333766
35 feet Y = -5283331
98 meter
Z = -13970977
73 Z = -4258354
01
XDOT = 18812
939855 XDOT = 5734
184068
YDOT = -9435
354709 feet/sec YDOT = -2875
896115 meter/sec
ZDOT = 11824
136989 ZDOT = 3603
996954
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 16095
78936416
00016717 00000-0 10270-3 0 9114
2 25544 51
6421 64
1201 0002592 21
1859 338
9401 15
54356913 33566
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
78936416 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 64
1201 deg
Eccentricity:
0002592
Arg of perigee: 21
1859 deg
Mean anomaly: 338
9401 deg
Mean motion: 15
54356913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 304
Coasting Arc #13 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2016/096/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4928115
34 A = 6784890
19 meter
Y = -3584475
91 meter E =
0014191
Z = 2972071
07 I = 51
96729
XDOT = 1106
154983 Wp = 86
84472
YDOT = -5697
005180 meter/sec RA = 58
45671 deg
ZDOT = -5015
386270 TA = 59
33872
MA = 59
19891
Ha = 221
212 n
mi
Hp = 213
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16168357
41 X = -4902103
67
Y = -11760091
57 feet Y = -3639439
52 meter
Z = 9750889
35 Z = 2948195
12
XDOT = 3629
117397 XDOT = 1194
140784
YDOT = -18690
961876 feet/sec YDOT = -5684
144167 meter/sec
ZDOT = -16454
679363 ZDOT = -5009
798316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4004939
39 X = -1220705
53
Y = 19638643
33 feet Y = 5985858
49 meter
Z = 9647773
15 Z = 2940641
26
XDOT = -17133
917920 XDOT = -5222
418182
YDOT = 4611
773205 feet/sec YDOT = 1405
668473 meter/sec
ZDOT = -16429
332566 ZDOT = -5007
660566
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 16096
81804705
00016717 00000-0 10270-3 0 9125
2 25544 51
6431 58
9899 0002749 22
9754 337
1521 15
54394567 33727
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
81804705 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 58
9899 deg
Eccentricity:
0002749
Arg of perigee: 22
9754 deg
Mean anomaly: 337
1521 deg
Mean motion: 15
54394567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 336
Coasting Arc #14 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2016/097/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4753041
20 A = 6787926
58 meter
Y = 4646590
68 meter E =
0011494
Z = -1350924
55 I = 51
95812
XDOT = -2526
598618 Wp = 34
91340
YDOT = 4273
928174 meter/sec RA = 53
50159 deg
ZDOT = 5844
617184 TA = 310
43791
MA = 310
53810
Ha = 221
302 n
mi
Hp = 213
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15593967
18 X = 4707290
87
Y = 15244720
09 feet Y = 4699486
36 meter
Z = -4432167
16 Z = -1327947
05
XDOT = -8289
365544 XDOT = -2602
593846
YDOT = 14022
074063 feet/sec YDOT = 4245
249975 meter/sec
ZDOT = 19175
253227 ZDOT = 5832
158311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7076078
31 X = 2156788
67
Y = -20648733
50 feet Y = -6293733
97 meter
Z = -4333166
18 Z = -1320749
05
XDOT = 14770
386196 XDOT = 4502
013712
YDOT = 1072
917984 feet/sec YDOT = 327
025402 meter/sec
ZDOT = 19120
300518 ZDOT = 5827
867598
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 16097
78243157
00016717 00000-0 10270-3 0 9131
2 25544 51
6417 54
1802 0002704 26
9507 333
1786 15
54355408 33870
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
78243157 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 54
1802 deg
Eccentricity:
0002704
Arg of perigee: 26
9507 deg
Mean anomaly: 333
1786 deg
Mean motion: 15
54355408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 315
Coasting Arc #15 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2016/098/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3245477
26 A = 6776582
20 meter
Y = -2648227
68 meter E =
0016416
Z = -5340899
16 I = 51
90512
XDOT = 4946
201440 Wp = 82
90659
YDOT = 5844
004893 meter/sec RA = 49
10978 deg
ZDOT = 110
208209 TA = 188
12802
MA = 188
15465
Ha = 221
240 n
mi
Hp = 213
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10647891
28 X = 3300793
31
Y = -8688411
01 feet Y = -2611626
00 meter
Z = -17522635
06 Z = -5324998
55
XDOT = 16227
695013 XDOT = 4879
949357
YDOT = 19173
244399 feet/sec YDOT = 5898
946185 meter/sec
ZDOT = 361
575488 ZDOT = 134
074233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5720493
32 X = -1743606
36
Y = -12592721
87 feet Y = -3838261
63 meter
Z = -17453026
27 Z = -5319682
41
XDOT = 21705
428283 XDOT = 6615
814541
YDOT = -10493
155521 feet/sec YDOT = -3198
313803 meter/sec
ZDOT = 464
199286 ZDOT = 141
487942
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 16098
68251916
00016717 00000-0 10270-3 0 9144
2 25544 51
6436 49
6932 0002646 32
8507 327
2810 15
54397043 34015
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
68251916 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 49
6932 deg
Eccentricity:
0002646
Arg of perigee: 32
8507 deg
Mean anomaly: 327
2810 deg
Mean motion: 15
54397043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 313
Coasting Arc #16 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2016/099/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4436813
29 A = 6777961
87 meter
Y = 1148992
83 meter E =
0008692
Z = 4989613
38 I = 51
88941
XDOT = -3997
918465 Wp = 49
82914
YDOT = -6195
028526 meter/sec RA = 44
12616 deg
ZDOT = -2120
517570 TA = 60
78035
MA = 60
69346
Ha = 221
287 n
mi
Hp = 213
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14556474
06 X = -4473569
63
Y = 3769661
51 feet Y = 1099172
46 meter
Z = 16370122
64 Z = 4967970
72
XDOT = -13116
530397 XDOT = -3918
046259
YDOT = -20324
896739 feet/sec YDOT = -6239
289550 meter/sec
ZDOT = -6957
078642 ZDOT = -2139
744068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 242272
33 X = 73844
61
Y = 15136725
08 feet Y = 4613673
80 meter
Z = 16275842
79 Z = 4960876
88
XDOT = -21712
688399 XDOT = -6618
027424
YDOT = 7944
760803 feet/sec YDOT = 2421
563093 meter/sec
ZDOT = -7039
454416 ZDOT = -2145
625706
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 16099
71117998
00016717 00000-0 10270-3 0 9151
2 25544 51
6446 44
5638 0002590 32
9400 327
1914 15
54441848 34178
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
71117998 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 44
5638 deg
Eccentricity:
0002590
Arg of perigee: 32
9400 deg
Mean anomaly: 327
1914 deg
Mean motion: 15
54441848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 323
Coasting Arc #17 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2016/100/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5408205
61 A = 6781540
85 meter
Y = 263662
59 meter E =
0008427
Z = -4090351
93 I = 51
87715
XDOT = 2630
462797 Wp = 90
58335
YDOT = 6063
109294 meter/sec RA = 39
14822 deg
ZDOT = 3875
590441 TA = 219
40207
MA = 219
46340
Ha = 221
308 n
mi
Hp = 213
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17743456
74 X = 5424724
80
Y = 865034
73 feet Y = 324232
76 meter
Z = -13419789
80 Z = -4064039
72
XDOT = 8630
127287 XDOT = 2543
641856
YDOT = 19892
090859 feet/sec YDOT = 6092
039762 meter/sec
ZDOT = 12715
191734 ZDOT = 3888
157371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4708955
26 X = 1435289
56
Y = -17217983
77 feet Y = -5248041
45 meter
Z = -13305490
44 Z = -4055513
49
XDOT = 20017
850074 XDOT = 6101
440702
YDOT = -4375
090032 feet/sec YDOT = -1333
527442 meter/sec
ZDOT = 12768
634948 ZDOT = 3891
879932
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 16100
67554318
00016717 00000-0 10270-3 0 9161
2 25544 51
6444 39
7548 0002662 37
0809 323
0527 15
54410150 34325
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
67554318 = yrday
fracday
Element set: 916
Inclination: 51
6444 deg
RA of node: 39
7548 deg
Eccentricity:
0002662
Arg of perigee: 37
0809 deg
Mean anomaly: 323
0527 deg
Mean motion: 15
54410150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 290
Coasting Arc #18 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2016/101/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941215
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030248
11 A = 6785495
54 meter
Y = -1547034
44 meter E =
0015167
Z = 2684961
20 I = 51
86447
XDOT = -904
448122 Wp = 93
03442
YDOT = -5557
745250 meter/sec RA = 34
18032 deg
ZDOT = -5209
077937 TA = 56
73440
MA = 56
58917
Ha = 221
385 n
mi
Hp = 213
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19784278
56 X = -6025543
16
Y = -5075572
30 feet Y = -1614442
21 meter
Z = 8808927
82 Z = 2655678
90
XDOT = -2967
349483 XDOT = -816
929012
YDOT = -18234
072344 feet/sec YDOT = -5567
370372 meter/sec
ZDOT = -17090
150712 ZDOT = -5213
258651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8940174
43 X = -2724965
17
Y = 18424790
76 feet Y = 5615876
22 meter
Z = 8681974
91 Z = 2646265
95
XDOT = -17095
110051 XDOT = -5210
589544
YDOT = -195
354502 feet/sec YDOT = -59
544052 meter/sec
ZDOT = -17107
234731 ZDOT = -5214
285146
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 16101
70418855
00016717 00000-0 10270-3 0 9172
2 25544 51
6438 34
6256 0002762 43
1076 317
0293 15
54426482 34488
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
70418855 = yrday
fracday
Element set: 917
Inclination: 51
6438 deg
RA of node: 34
6256 deg
Eccentricity:
0002762
Arg of perigee: 43
1076 deg
Mean anomaly: 317
0293 deg
Mean motion: 15
54426482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 304
Coasting Arc #19 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2016/102/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941215
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6198716
74 A = 6788015
44 meter
Y = 2563642
97 meter E =
0012449
Z = -1003706
98 I = 51
84615
XDOT = -1018
585686 Wp = 39
43025
YDOT = 4762
781939 meter/sec RA = 29
21968 deg
ZDOT = 5923
954947 TA = 309
72270
MA = 309
83236
Ha = 221
302 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20336997
16 X = 6174464
36
Y = 8410902
13 feet Y = 2632825
49 meter
Z = -3293001
92 Z = -973653
90
XDOT = -3341
816556 XDOT = -1100
544915
YDOT = 15625
924996 feet/sec YDOT = 4750
933471 meter/sec
ZDOT = 19435
547725 ZDOT = 5918
807553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11996058
76 X = 3656398
71
Y = -18473527
03 feet Y = -5630731
04 meter
Z = -3162904
20 Z = -964053
20
XDOT = 13381
569123 XDOT = 4078
702269
YDOT = 5394
893559 feet/sec YDOT = 1644
363557 meter/sec
ZDOT = 19412
241882 ZDOT = 5916
851326
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 16102
66853438
00016717 00000-0 10270-3 0 9189
2 25544 51
6438 29
8163 0002611 43
7580 316
3780 15
54443946 34634
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
66853438 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 29
8163 deg
Eccentricity:
0002611
Arg of perigee: 43
7580 deg
Mean anomaly: 316
3780 deg
Mean motion: 15
54443946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 317
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