[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 25th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
There are no maneuvers
Coasting Arc #1 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2016/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928850
74 A = 6778101
44 meter
Y = 3802974
42 meter E =
0012430
Z = -4797201
54 I = 51
62149
XDOT = -6908
314125 Wp = 77
55902
YDOT = 2048
185350 meter/sec RA = 180
07209 deg
ZDOT = -2597
131736 TA = 166
82817
MA = 166
79568
Ha = 220
707 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9609090
34 X = 2909410
32
Y = 12476950
21 feet Y = 3835618
54 meter
Z = -15738850
18 Z = -4783020
56
XDOT = -22665
072587 XDOT = -6918
088072
YDOT = 6719
768210 feet/sec YDOT = 1970
877584 meter/sec
ZDOT = -8520
773413 ZDOT = -2630
714638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15632308
98 X = 4764727
78
Y = -2357462
78 feet Y = -718554
66 meter
Z = -15677805
78 Z = -4778595
20
XDOT = -5385
072754 XDOT = -1641
370176
YDOT = 21863
703734 feet/sec YDOT = 6664
056898 meter/sec
ZDOT = -8667
198092 ZDOT = -2641
761978
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 16144
52075979
00016717 00000-0 10270-3 0 9007
2 25544 51
6405 181
0912 0001653 119
2160 240
9158 15
54665633 1149
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
52075979 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 181
0912 deg
Eccentricity:
0001653
Arg of perigee: 119
2160 deg
Mean anomaly: 240
9158 deg
Mean motion: 15
54665633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 290
Coasting Arc #2 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2016/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -962322
05 A = 6775825
80 meter
Y = -4118628
90 meter E =
0004563
Z = 5290230
03 I = 51
64577
XDOT = 7577
665287 Wp = 115
33295
YDOT = -1079
383206 meter/sec RA = 175
06854 deg
ZDOT = 535
810606 TA = 329
54488
MA = 329
57137
Ha = 220
721 n
mi
Hp = 213
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3157224
58 X = -941892
94
Y = -13512562
02 feet Y = -4129276
54 meter
Z = 17356397
74 Z = 5285604
46
XDOT = 24861
106584 XDOT = 7586
569263
YDOT = -3541
283484 feet/sec YDOT = -994
594980 meter/sec
ZDOT = 1757
908813 ZDOT = 572
642953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13443766
42 X = -4097660
01
Y = -3535050
49 feet Y = -1077483
39 meter
Z = 17336969
29 Z = 5284308
24
XDOT = 8418
961136 XDOT = 2566
099354
YDOT = -22572
578436 feet/sec YDOT = -6880
121907 meter/sec
ZDOT = 1918
329701 ZDOT = 584
706893
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 16145
54922732
00016717 00000-0 10270-3 0 9019
2 25544 51
6400 175
9601 0001690 116
7792 243
3534 15
54689208 1302
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
54922732 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 175
9601 deg
Eccentricity:
0001690
Arg of perigee: 116
7792 deg
Mean anomaly: 243
3534 deg
Mean motion: 15
54689208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 295
Coasting Arc #3 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2016/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1083793
09 A = 6776575
83 meter
Y = 4307084
29 meter E =
0015066
Z = -5131747
35 I = 51
68148
XDOT = -7488
169277 Wp = 104
00787
YDOT = 25
395187 meter/sec RA = 170
06488 deg
ZDOT = 1603
159791 TA = 181
46555
MA = 181
46997
Ha = 220
638 n
mi
Hp = 213
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3555751
60 X = -1106947
41
Y = 14130853
98 feet Y = 4294835
65 meter
Z = -16836441
42 Z = -5137067
99
XDOT = -24567
484504 XDOT = -7495
684237
YDOT = 83
317544 feet/sec YDOT = -58
384683 meter/sec
ZDOT = 5259
710602 ZDOT = 1566
765587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10966429
80 X = 3342567
80
Y = 9552862
19 feet Y = 2911712
40 meter
Z = -16860320
43 Z = -5139025
67
XDOT = -10530
480700 XDOT = -3209
690517
YDOT = 21090
074481 feet/sec YDOT = 6428
254702 meter/sec
ZDOT = 5101
349483 ZDOT = 1554
891323
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 16146
51341058
00016717 00000-0 10270-3 0 9024
2 25544 51
6413 171
1498 0001509 119
6802 240
4501 15
54672133 1458
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
51341058 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 171
1498 deg
Eccentricity:
0001509
Arg of perigee: 119
6802 deg
Mean anomaly: 240
4501 deg
Mean motion: 15
54672133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 276
Coasting Arc #4 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2016/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990169
34 A = 6779700
58 meter
Y = -4303705
70 meter E =
0010900
Z = 4293395
84 I = 51
72212
XDOT = 6711
007600 Wp = 78
95341
YDOT = 1110
625593 meter/sec RA = 165
06992 deg
ZDOT = -3550
963073 TA = 47
21378
MA = 47
12217
Ha = 220
538 n
mi
Hp = 213
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9810266
88 X = 3017216
65
Y = -14119769
37 feet Y = -4270116
81 meter
Z = 14085944
35 Z = 4307986
70
XDOT = 22017
741471 XDOT = 6715
338668
YDOT = 3643
784754 feet/sec YDOT = 1185
697093 meter/sec
ZDOT = -11650
141316 ZDOT = -3518
351879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8334310
05 X = -2540297
70
Y = -14977818
20 feet Y = -4565238
99 meter
Z = 14150169
24 Z = 4312971
58
XDOT = 11981
742135 XDOT = 3652
035003
YDOT = -17569
502006 feet/sec YDOT = -5355
184211 meter/sec
ZDOT = -11508
411880 ZDOT = -3507
763941
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 16147
54186817
00016717 00000-0 10270-3 0 9039
2 25544 51
6395 166
0189 0001619 119
9961 240
1353 15
54721576 1614
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
54186817 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 166
0189 deg
Eccentricity:
0001619
Arg of perigee: 119
9961 deg
Mean anomaly: 240
1353 deg
Mean motion: 15
54721576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 317
Coasting Arc #5 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4543306
00 A = 6783888
84 meter
Y = 4100745
12 meter E =
0005601
Z = -2930057
26 I = 51
76826
XDOT = -5307
506419 Wp = 81
72990
YDOT = -2292
494868 meter/sec RA = 160
08912 deg
ZDOT = 5030
301971 TA = 244
92239
MA = 244
98053
Ha = 220
557 n
mi
Hp = 213
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14905859
57 X = -4574590
88
Y = 13453888
20 feet Y = 4049764
17 meter
Z = -9613048
75 Z = -2952203
23
XDOT = -17413
078803 XDOT = -5305
911826
YDOT = -7521
308621 feet/sec YDOT = -2351
838433 meter/sec
ZDOT = 16503
615390 ZDOT = 5004
523025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5793341
10 X = 1765810
37
Y = 19176887
24 feet Y = 5845115
23 meter
Z = -9710131
72 Z = -2959648
15
XDOT = -12903
916899 XDOT = -3933
113871
YDOT = 12183
383177 feet/sec YDOT = 3713
495192 meter/sec
ZDOT = 16391
803435 ZDOT = 4996
221687
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 16148
50604291
00016717 00000-0 10270-3 0 9048
2 25544 51
6408 161
2089 0001607 123
9822 236
1484 15
54721117 1760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
50604291 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 161
2089 deg
Eccentricity:
0001607
Arg of perigee: 123
9822 deg
Mean anomaly: 236
1484 deg
Mean motion: 15
54721117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 176
Checksum: 292
Coasting Arc #6 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5623314
42 A = 6787012
29 meter
Y = -3607389
39 meter E =
0015298
Z = 1152811
79 I = 51
80754
XDOT = 3460
992045 Wp = 122
46133
YDOT = 3498
727898 meter/sec RA = 155
12150 deg
ZDOT = -5885
371010 TA = 45
04379
MA = 44
91983
Ha = 220
571 n
mi
Hp = 213
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18449194
28 X = 5657635
33
Y = -11835267
02 feet Y = -3544313
92 meter
Z = 3782190
92 Z = 1180211
66
XDOT = 11354
960779 XDOT = 3450
199858
YDOT = 11478
766071 feet/sec YDOT = 3537
371077 meter/sec
ZDOT = -19308
960007 ZDOT = -5868
584291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3169937
95 X = -966197
09
Y = -21667408
73 feet Y = -6604226
18 meter
Z = 3902073
25 Z = 1189351
93
XDOT = 13613
075974 XDOT = 4149
265557
YDOT = -5483
821916 feet/sec YDOT = -1671
468920 meter/sec
ZDOT = -19236
482008 ZDOT = -5863
279716
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 16149
53449022
00016717 00000-0 10270-3 0 9052
2 25544 51
6399 156
0773 0001584 122
6648 237
4658 15
54720513 1921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
53449022 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 156
0773 deg
Eccentricity:
0001584
Arg of perigee: 122
6648 deg
Mean anomaly: 237
4658 deg
Mean motion: 15
54720513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 192
Checksum: 317
Coasting Arc #7 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6114572
52 A = 6787282
53 meter
Y = 2838426
26 meter E =
0013526
Z = 738166
95 I = 51
83660
XDOT = -1406
908855 Wp = 59
45648
YDOT = -4603
118033 meter/sec RA = 150
16228 deg
ZDOT = 5971
482694 TA = 308
50114
MA = 308
62237
Ha = 220
447 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20060933
45 X = -6149443
78
Y = 9312422
11 feet Y = 2769854
02 meter
Z = 2421807
58 Z = 708379
20
XDOT = -4615
842699 XDOT = -1384
338107
YDOT = -15102
093285 feet/sec YDOT = -4618
725163 meter/sec
ZDOT = 19591
478655 ZDOT = 5964
702808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 571346
85 X = 174146
52
Y = 22123501
78 feet Y = 6743243
34 meter
Z = 2291645
73 Z = 698493
62
XDOT = -14128
165529 XDOT = -4306
264853
YDOT = -1688
293475 feet/sec YDOT = -514
591851 meter/sec
ZDOT = 19562
746208 ZDOT = 5962
725044
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 16150
56293079
00016717 00000-0 10270-3 0 9067
2 25544 51
6390 150
9470 0001560 135
0261 225
1019 15
54762471 2084
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
56293079 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 150
9470 deg
Eccentricity:
0001560
Arg of perigee: 135
0261 deg
Mean anomaly: 225
1019 deg
Mean motion: 15
54762471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 285
Coasting Arc #8 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6032923
73 A = 6784871
98 meter
Y = -1729174
51 meter E =
0006727
Z = -2576070
48 I = 51
85507
XDOT = -668
496688 Wp = 130
13331
YDOT = 5515
830646 meter/sec RA = 145
20000 deg
ZDOT = -5281
349631 TA = 78
73763
MA = 78
66204
Ha = 220
561 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19793056
86 X = 6064324
95
Y = -5673144
71 feet Y = -1661534
63 meter
Z = -8451674
81 Z = -2546687
63
XDOT = -2193
230604 XDOT = -704
471679
YDOT = 18096
557237 feet/sec YDOT = 5508
154187 meter/sec
ZDOT = -17327
262568 ZDOT = -5284
684150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2324509
83 X = 708510
60
Y = -20510906
90 feet Y = -6251724
42 meter
Z = -8323450
59 Z = -2536987
74
XDOT = 14437
620668 XDOT = 4400
586780
YDOT = 8656
001050 feet/sec YDOT = 2638
349120 meter/sec
ZDOT = -17342
723610 ZDOT = -5286
062156
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 16151
52709334
00016717 00000-0 10270-3 0 9071
2 25544 51
6385 146
1356 0001497 130
3957 229
7327 15
54721445 2232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52709334 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 146
1356 deg
Eccentricity:
0001497
Arg of perigee: 130
3957 deg
Mean anomaly: 229
7327 deg
Mean motion: 15
54721445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 307
Coasting Arc #9 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5420953
29 A = 6780661
07 meter
Y = 377246
06 meter E =
0011920
Z = 4048122
13 I = 51
86719
XDOT = 2513
380054 Wp = 105
63309
YDOT = -6096
743529 meter/sec RA = 140
22984 deg
ZDOT = 3921
181102 TA = 303
78680
MA = 303
90027
Ha = 220
478 n
mi
Hp = 213
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17785279
81 X = -5444433
11
Y = 1237683
91 feet Y = 316493
85 meter
Z = 13281240
58 Z = 4021731
18
XDOT = 8245
997552 XDOT = 2562
320941
YDOT = -20002
439401 feet/sec YDOT = -6068
363798 meter/sec
ZDOT = 12864
767395 ZDOT = 3933
509171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5377290
36 X = -1638998
10
Y = 17087236
56 feet Y = 5208189
70 meter
Z = 13166263
17 Z = 4013077
02
XDOT = -14388
821546 XDOT = -4385
712807
YDOT = -14515
416986 feet/sec YDOT = -4424
299097 meter/sec
ZDOT = 12919
496581 ZDOT = 3937
862558
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 16152
55552381
00016717 00000-0 10270-3 0 9084
2 25544 51
6386 141
0047 0001327 138
5232 221
6022 15
54757905 2392
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
55552381 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 141
0047 deg
Eccentricity:
0001327
Arg of perigee: 138
5232 deg
Mean anomaly: 221
6022 deg
Mean motion: 15
54757905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 239
Checksum: 290
Coasting Arc #10 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4400474
45 A = 6776993
09 meter
Y = 1191574
98 meter E =
0013417
Z = -5026443
44 I = 51
87807
XDOT = -3998
585794 Wp = 80
10801
YDOT = 6208
633209 meter/sec RA = 135
24738 deg
ZDOT = -2031
158297 TA = 170
20478
MA = 170
17860
Ha = 220
436 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14437252
15 X = 4411239
56
Y = 3909366
74 feet Y = 1240844
52 meter
Z = -16490956
18 Z = -5005040
50
XDOT = -13118
719796 XDOT = -4057
848465
YDOT = 20369
531525 feet/sec YDOT = 6163
587130 meter/sec
ZDOT = -6663
905174 ZDOT = -2050
726266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8742542
79 X = 2664727
04
Y = -12261477
37 feet Y = -3737298
30 meter
Z = -16397961
82 Z = -4998098
76
XDOT = 13623
030291 XDOT = 4152
299633
YDOT = 18730
328992 feet/sec YDOT = 5709
004277 meter/sec
ZDOT = -6750
195703 ZDOT = -2057
459650
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 16153
51967469
00016717 00000-0 10270-3 0 9099
2 25544 51
6378 136
1933 0001352 134
2807 225
8457 15
54734768 2548
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51967469 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 136
1933 deg
Eccentricity:
0001352
Arg of perigee: 134
2807 deg
Mean anomaly: 225
8457 deg
Mean motion: 15
54734768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 331
Coasting Arc #11 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3109523
94 A = 6775566
57 meter
Y = -2794887
74 meter E =
0003312
Z = 5329001
99 I = 51
89546
XDOT = 5023
561288 Wp = 105
01476
YDOT = -5798
153742 meter/sec RA = 130
25911 deg
ZDOT = -110
425681 TA = 346
02868
MA = 346
03784
Ha = 220
475 n
mi
Hp = 213
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10201850
19 X = -3103926
11
Y = -9169579
20 feet Y = -2829629
64 meter
Z = 17483602
32 Z = 5313909
82
XDOT = 16481
500289 XDOT = 5088
560741
YDOT = -19022
814113 feet/sec YDOT = -5741
613493 meter/sec
ZDOT = -362
288980 ZDOT = -85
864666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12080783
91 X = -3682222
93
Y = 6670113
59 feet Y = 2033050
62 meter
Z = 17418367
45 Z = 5309118
40
XDOT = -11957
078428 XDOT = -3644
517505
YDOT = -20999
044481 feet/sec YDOT = -6400
508758 meter/sec
ZDOT = -254
305191 ZDOT = -77
512222
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 16154
54809701
00016717 00000-0 10270-3 0 9109
2 25544 51
6376 131
0619 0001273 141
6179 218
5065 15
54740267 2700
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54809701 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 131
0619 deg
Eccentricity:
0001273
Arg of perigee: 141
6179 deg
Mean anomaly: 218
5065 deg
Mean motion: 15
54740267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 293
Coasting Arc #12 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1713288
63 A = 6777184
25 meter
Y = 4304963
07 meter E =
0013336
Z = -4958290
42 I = 51
92205
XDOT = -5540
230097 Wp = 109
48807
YDOT = 4788
519350 meter/sec RA = 125
27231 deg
ZDOT = 2243
765646 TA = 182
35832
MA = 182
36462
Ha = 220
330 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5621025
68 X = 1689107
74
Y = 14123894
58 feet Y = 4323987
51 meter
Z = -16267357
02 Z = -4950025
84
XDOT = -18176
607929 XDOT = -5604
264179
YDOT = 15710
365320 feet/sec YDOT = 4726
206541 meter/sec
ZDOT = 7361
435845 ZDOT = 2216
697117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15209003
61 X = 4635704
30
Y = -954699
05 feet Y = -290992
27 meter
Z = -16232128
36 Z = -4947552
72
XDOT = 9055
796861 XDOT = 2760
206883
YDOT = 21154
492754 feet/sec YDOT = 6447
889391 meter/sec
ZDOT = 7242
686343 ZDOT = 2207
570797
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 16155
51223639
00016717 00000-0 10270-3 0 9118
2 25544 51
6387 126
2510 0001205 142
3829 217
7408 15
54742432 2857
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51223639 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 126
2510 deg
Eccentricity:
0001205
Arg of perigee: 142
3829 deg
Mean anomaly: 217
7408 deg
Mean motion: 15
54742432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 289
Coasting Arc #13 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -324508
94 A = 6780941
11 meter
Y = -5519775
65 meter E =
0011658
Z = 3915996
76 I = 51
95274
XDOT = 5613
962444 Wp = 85
60035
YDOT = -3247
237938 meter/sec RA = 120
29575 deg
ZDOT = -4100
570286 TA = 47
18416
MA = 47
08622
Ha = 220
265 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1064661
87 X = -281783
79
Y = -18109500
17 feet Y = -5523166
12 meter
Z = 12847758
39 Z = 3914523
44
XDOT = 18418
511956 XDOT = 5669
775700
YDOT = -10653
667775 feet/sec YDOT = -3184
146293 meter/sec
ZDOT = -13453
314588 ZDOT = -4073
163527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17615831
18 X = -5369305
34
Y = -4348477
43 feet Y = -1325415
92 meter
Z = 12842337
51 Z = 3914344
47
XDOT = -4917
292884 XDOT = -1498
790871
YDOT = -19567
147318 feet/sec YDOT = -5964
066503 meter/sec
ZDOT = -13333
345581 ZDOT = -4064
003733
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 16156
54064653
00016717 00000-0 10270-3 0 9122
2 25544 51
6387 121
1194 0001089 144
6315 215
4911 15
54775174 3016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54064653 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 121
1194 deg
Eccentricity:
0001089
Arg of perigee: 144
6315 deg
Mean anomaly: 215
4911 deg
Mean motion: 15
54775174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 292
Coasting Arc #14 (Orbit 315)
---------------------------------------
Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -912296
10 A = 6785053
15 meter
Y = 6285634
66 meter E =
0005466
Z = -2385515
41 I = 51
98210
XDOT = -5281
627813 Wp = 58
07974
YDOT = 1280
362778 meter/sec RA = 115
33345 deg
ZDOT = 5405
371731 TA = 275
41382
MA = 275
47617
Ha = 220
234 n
mi
Hp = 213
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2993097
44 X = -970927
93
Y = 20622160
96 feet Y = 6275105
26 meter
Z = -7826494
11 Z = -2390088
69
XDOT = -17328
175238 XDOT = -5321
809809
YDOT = 4200
665282 feet/sec YDOT = 1221
074679 meter/sec
ZDOT = 17734
159224 ZDOT = 5379
617248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18935518
27 X = 5771545
97
Y = 8680323
49 feet Y = 2645762
60 meter
Z = -7847566
33 Z = -2391938
22
XDOT = -293
557884 XDOT = -89
476443
YDOT = 16536
452616 feet/sec YDOT = 5040
310757 meter/sec
ZDOT = 17621
726486 ZDOT = 5371
102233
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 16157
50477706
00016717 00000-0 10270-3 0 9137
2 25544 51
6390 116
3091 0001104 149
0756 211
0462 15
54763208 3162
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50477706 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 116
3091 deg
Eccentricity:
0001104
Arg of perigee: 149
0756 deg
Mean anomaly: 211
0462 deg
Mean motion: 15
54763208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 283
Coasting Arc #15 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1980815
28 A = 6787316
83 meter
Y = -6464880
36 meter E =
0013944
Z = 505385
83 I = 52
00466
XDOT = 4661
684257 Wp = 131
53978
YDOT = 950
244829 meter/sec RA = 110
38209 deg
ZDOT = -6017
720552 TA = 43
03296
MA = 42
92400
Ha = 220
174 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6498737
80 X = 2050505
02
Y = -21210237
42 feet Y = -6442339
98 meter
Z = 1658089
98 Z = 515176
51
XDOT = 15294
239687 XDOT = 4679
943522
YDOT = 3117
601145 feet/sec YDOT = 1002
477844 meter/sec
ZDOT = -19743
177664 ZDOT = -5995
030675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18700538
05 X = -5699924
00
Y = -11926872
91 feet Y = -3635310
86 meter
Z = 1701941
77 Z = 518751
85
XDOT = 6258
911724 XDOT = 1907
716293
YDOT = -12661
410115 feet/sec YDOT = -3859
197803 meter/sec
ZDOT = -19644
493743 ZDOT = -5987
641693
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 16158
53317707
00016717 00000-0 10270-3 0 9146
2 25544 51
6410 111
1773 0001061 156
1162 204
0041 15
54782537 3326
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
53317707 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 111
1773 deg
Eccentricity:
0001061
Arg of perigee: 156
1162 deg
Mean anomaly: 204
0041 deg
Mean motion: 15
54782537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 266
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