[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 11th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 215
7
322/07:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 216
8
322/20:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 217
1
324/22:00:36
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 217
3
326/13:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 217
4
328/20:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 217
7
Coasting Arc #1 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2016/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3092465
82 A = 6790087
85 meter
Y = 5875558
36 meter E =
0010607
Z = 1412762
69 I = 51
95833
XDOT = -4853
205060 Wp = 91
25838
YDOT = 1145
976076 meter/sec RA = 52
65728 deg
ZDOT = 5819
522908 TA = 284
06424
MA = 284
18212
Ha = 222
899 n
mi
Hp = 215
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10145885
22 X = 3019671
28
Y = 19276766
26 feet Y = 5909733
42 meter
Z = 4635048
19 Z = 1427608
30
XDOT = -15922
588779 XDOT = -4893
928123
YDOT = 3759
764030 feet/sec YDOT = 1091
476812 meter/sec
ZDOT = 19092
922926 ZDOT = 5795
847935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21116301
13 X = -6436248
59
Y = -5295095
51 feet Y = -1613945
11 meter
Z = 4698953
74 Z = 1432241
10
XDOT = 7496
164397 XDOT = 2284
830908
YDOT = -12933
999721 feet/sec YDOT = -3942
283115 meter/sec
ZDOT = 18989
004327 ZDOT = 5787
848519
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 16314
56153551
00016717 00000-0 10270-3 0 9003
2 25544 51
6431 53
0198 0007169 192
3487 167
7491 15
53568793 27595
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
56153551 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 53
0198 deg
Eccentricity:
0007169
Arg of perigee: 192
3487 deg
Mean anomaly: 167
7491 deg
Mean motion: 15
53568793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 332
Coasting Arc #2 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5356296
95 A = 6787748
97 meter
Y = -3077932
12 meter E =
0014626
Z = 2790023
97 I = 51
94020
XDOT = 566
116835 Wp = 127
43651
YDOT = -5661
398690 meter/sec RA = 50
59173 deg
ZDOT = -5148
998043 TA = 21
04629
MA = 20
98616
Ha = 222
797 n
mi
Hp = 215
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17573152
73 X = -5335033
59
Y = -10098202
50 feet Y = -3137710
82 meter
Z = 9153621
94 Z = 2764055
78
XDOT = 1857
338696 XDOT = 654
393990
YDOT = -18574
142684 feet/sec YDOT = -5654
574630 meter/sec
ZDOT = -16893
038199 ZDOT = -5146
033279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19743943
54 X = -6017953
99
Y = -4798418
74 feet Y = -1462558
03 meter
Z = 9040467
71 Z = 2755534
56
XDOT = -3623
971706 XDOT = -1104
586576
YDOT = -16950
575352 feet/sec YDOT = -5166
535367 meter/sec
ZDOT = -16878
969499 ZDOT = -5144
709903
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 16314
94748814
00016717 00000-0 10270-3 0 9018
2 25544 51
6410 51
1000 0006644 194
4954 165
6009 15
53564963 27656
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94748814 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 51
1000 deg
Eccentricity:
0006644
Arg of perigee: 194
4954 deg
Mean anomaly: 165
6009 deg
Mean motion: 15
53564963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 308
Coasting Arc #3 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5362433
42 A = 6790166
91 meter
Y = 3927135
71 meter E =
0003341
Z = -1389237
39 I = 51
92749
XDOT = -1871
711961 Wp = 78
12062
YDOT = 4611
891593 meter/sec RA = 45
64007 deg
ZDOT = 5824
741400 TA = 266
81598
MA = 266
85421
Ha = 222
534 n
mi
Hp = 215
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17593285
49 X = 5324869
08
Y = 12884303
51 feet Y = 3986891
94 meter
Z = -4557865
45 Z = -1363278
96
XDOT = -6140
787274 XDOT = -1951
438843
YDOT = 15130
877930 feet/sec YDOT = 4590
515360 meter/sec
ZDOT = 19110
043963 ZDOT = 5815
455036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20634814
87 X = 6289491
57
Y = 7123913
72 feet Y = 2171368
90 meter
Z = -4444927
18 Z = -1354813
80
XDOT = -1011
590854 XDOT = -308
332892
YDOT = 14801
582309 feet/sec YDOT = 4511
522288 meter/sec
ZDOT = 19068
482138 ZDOT = 5812
073356
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 16315
91236307
00016717 00000-0 10270-3 0 9026
2 25544 51
6413 46
2943 0006566 198
2712 161
8205 15
53570735 27804
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91236307 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 46
2943 deg
Eccentricity:
0006566
Arg of perigee: 198
2712 deg
Mean anomaly: 161
8205 deg
Mean motion: 15
53570735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 304
Coasting Arc #4 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5062098
79 A = 6790937
83 meter
Y = -4509682
98 meter E =
0015577
Z = -151758
12 I = 51
90742
XDOT = 3246
664739 Wp = 158
15448
YDOT = -3448
398253 meter/sec RA = 40
69152 deg
ZDOT = -6035
867107 TA = 23
47497
MA = 23
40394
Ha = 222
404 n
mi
Hp = 216
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16607935
65 X = -5010556
94
Y = -14795547
85 feet Y = -4566002
59 meter
Z = -497894
10 Z = -176223
72
XDOT = 10651
787202 XDOT = 3314
304646
YDOT = -11313
642562 feet/sec YDOT = -3411
713939 meter/sec
ZDOT = -19802
713607 ZDOT = -6019
930804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20380877
00 X = -6212091
31
Y = -8901376
00 feet Y = -2713139
40 meter
Z = -604168
54 Z = -184150
57
XDOT = 6079
501709 XDOT = 1853
032121
YDOT = -12619
506324 feet/sec YDOT = -3846
425528 meter/sec
ZDOT = -19732
248126 ZDOT = -6014
389229
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 16316
94155882
00016717 00000-0 10270-3 0 9039
2 25544 51
6419 41
1683 0006523 202
1018 157
9854 15
53571885 27962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94155882 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 41
1683 deg
Eccentricity:
0006523
Arg of perigee: 202
1018 deg
Mean anomaly: 157
9854 deg
Mean motion: 15
53571885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 325
Coasting Arc #5 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4478672
54 A = 6789689
22 meter
Y = 4823894
37 meter E =
0009630
Z = 1655762
36 I = 51
87849
XDOT = -4561
193263 Wp = 88
45722
YDOT = 2257
942478 meter/sec RA = 35
74109 deg
ZDOT = 5730
795887 TA = 289
60700
MA = 289
71093
Ha = 222
229 n
mi
Hp = 216
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14693807
56 X = 4416354
45
Y = 15826425
11 feet Y = 4873629
50 meter
Z = 5432291
21 Z = 1677367
72
XDOT = -14964
544826 XDOT = -4613
941649
YDOT = 7407
947762 feet/sec YDOT = 2206
641380 meter/sec
ZDOT = 18801
823775 ZDOT = 5708
509962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19029384
46 X = 5800156
38
Y = 10160696
41 feet Y = 3096980
26 meter
Z = 5525963
78 Z = 1684313
76
XDOT = -11091
022428 XDOT = -3380
543636
YDOT = 10549
580163 feet/sec YDOT = 3215
512034 meter/sec
ZDOT = 18703
781510 ZDOT = 5700
912604
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 16317
97074930
00016717 00000-0 10270-3 0 9048
2 25544 51
6419 36
0428 0006565 206
5273 153
5544 15
53591667 28126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16317
97074930 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 36
0428 deg
Eccentricity:
0006565
Arg of perigee: 206
5273 deg
Mean anomaly: 153
5544 deg
Mean motion: 15
53591667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 318
Coasting Arc #6 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3555518
02 A = 6786835
86 meter
Y = -4906728
48 meter E =
0006931
Z = -3049206
11 I = 51
84377
XDOT = 5752
816358 Wp = 170
67361
YDOT = -1098
530680 meter/sec RA = 30
78339 deg
ZDOT = -4948
555705 TA = 44
19184
MA = 44
13650
Ha = 221
991 n
mi
Hp = 216
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11665085
38 X = -3485573
32
Y = -16098190
54 feet Y = -4946097
59 meter
Z = -10003957
04 Z = -3066308
52
XDOT = 18874
069415 XDOT = 5788
711491
YDOT = -3604
103281 feet/sec YDOT = -1033
998138 meter/sec
ZDOT = -16235
418980 ZDOT = -4920
521964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16422432
34 X = -5005557
38
Y = -11137556
35 feet Y = -3394727
18 meter
Z = -10077880
08 Z = -3071737
85
XDOT = 15774
989693 XDOT = 4808
216858
YDOT = -8705
217875 feet/sec YDOT = -2653
350408 meter/sec
ZDOT = -16112
435285 ZDOT = -4911
070275
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 16318
93560984
00016717 00000-0 10270-3 0 9055
2 25544 51
6432 31
2371 0006419 210
4666 149
6114 15
53609569 28279
Satellite: ISS
Catalog Number: 25544
Epoch time: 16318
93560984 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 31
2371 deg
Eccentricity:
0006419
Arg of perigee: 210
4666 deg
Mean anomaly: 149
6114 deg
Mean motion: 15
53609569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2827
Checksum: 318
Coasting Arc #7 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2385892
88 A = 6783445
80 meter
Y = 4793914
39 meter E =
0010206
Z = 4164131
74 I = 51
80369
XDOT = -6681
776300 Wp = 140
78429
YDOT = 51
152519 meter/sec RA = 25
81654 deg
ZDOT = 3756
776900 TA = 270
57825
MA = 270
69520
Ha = 221
882 n
mi
Hp = 216
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7827732
54 X = 2311880
66
Y = 15728065
58 feet Y = 4820181
12 meter
Z = 13661849
54 Z = 4175542
48
XDOT = -21921
838256 XDOT = -6700
101002
YDOT = 167
823224 feet/sec YDOT = -23
670141 meter/sec
ZDOT = 12325
383529 ZDOT = 3724
273093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12875735
71 X = 3924524
24
Y = 11896190
44 feet Y = 3625958
85 meter
Z = 13710859
19 Z = 4179069
88
XDOT = -19602
548545 XDOT = -5974
856796
YDOT = 7127
166167 feet/sec YDOT = 2172
360248 meter/sec
ZDOT = 12183
036035 ZDOT = 3713
389384
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 16319
96478918
00016717 00000-0 10270-3 0 9065
2 25544 51
6427 26
1116 0006400 213
7720 146
3025 15
53608101 28434
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
96478918 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 26
1116 deg
Eccentricity:
0006400
Arg of perigee: 213
7720 deg
Mean anomaly: 146
3025 deg
Mean motion: 15
53608101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 293
Coasting Arc #8 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -966066
24 A = 6780377
93 meter
Y = -4540035
15 meter E =
0008193
Z = -4948918
49 I = 51
76456
XDOT = 7274
986256 Wp = 100
80636
YDOT = 884
154972 meter/sec RA = 20
83893 deg
ZDOT = -2235
876372 TA = 147
41001
MA = 147
35941
Ha = 221
709 n
mi
Hp = 216
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3169508
68 X = -891186
32
Y = -14895128
46 feet Y = -4550419
45 meter
Z = -16236609
21 Z = -4953429
84
XDOT = 23868
065143 XDOT = 7275
419894
YDOT = 2900
770904 feet/sec YDOT = 965
511278 meter/sec
ZDOT = -7335
552401 ZDOT = -2200
534370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8433003
74 X = -2570379
54
Y = -12656340
10 feet Y = -3857652
46 meter
Z = -16255448
90 Z = -4954660
83
XDOT = 22331
459309 XDOT = 6806
628797
YDOT = -5676
091019 feet/sec YDOT = -1730
072543 meter/sec
ZDOT = -7180
967140 ZDOT = -2188
758784
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 16320
92964074
00016717 00000-0 10270-3 0 9077
2 25544 51
6431 21
3060 0006340 217
7527 142
3182 15
53632349 28583
Satellite: ISS
Catalog Number: 25544
Epoch time: 16320
92964074 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 21
3060 deg
Eccentricity:
0006340
Arg of perigee: 217
7527 deg
Mean anomaly: 142
3182 deg
Mean motion: 15
53632349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2858
Checksum: 294
Coasting Arc #9 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -553255
77 A = 6778804
54 meter
Y = 4190737
20 meter E =
0006063
Z = 5301421
25 I = 51
72890
XDOT = -7461
484400 Wp = 197
26108
YDOT = -1675
708118 meter/sec RA = 15
85380 deg
ZDOT = 540
460645 TA = 247
55498
MA = 247
61920
Ha = 221
508 n
mi
Hp = 216
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1815143
60 X = -625829
04
Y = 13749137
80 feet Y = 4184144
24 meter
Z = 17393114
34 Z = 5298557
58
XDOT = -24479
935695 XDOT = -7444
817019
YDOT = -5497
730046 feet/sec YDOT = -1759
054282 meter/sec
ZDOT = 1773
164846 ZDOT = 504
254336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3607114
83 X = 1099448
60
Y = 13408499
84 feet Y = 4086910
75 meter
Z = 17379724
32 Z = 5297339
97
XDOT = -23711
332531 XDOT = -7227
214156
YDOT = 4262
101763 feet/sec YDOT = 1299
088617 meter/sec
ZDOT = 1614
957601 ZDOT = 492
239077
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 16321
95880930
00016717 00000-0 10270-3 0 9080
2 25544 51
6430 16
1801 0006512 222
8367 137
2279 15
53656483 28740
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
95880930 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 16
1801 deg
Eccentricity:
0006512
Arg of perigee: 222
8367 deg
Mean anomaly: 137
2279 deg
Mean motion: 15
53656483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 314
Coasting Arc #10 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4574517
27 A = 6782847
74 meter
Y = 2426477
73 meter E =
0005247
Z = 4375570
95 I = 51
72907
XDOT = -5474
045053 Wp = 113
81757
YDOT = -4136
622545 meter/sec RA = 13
86534 deg
ZDOT = -3427
790625 TA = 10
88648
MA = 10
87512
Ha = 221
873 n
mi
Hp = 216
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15008258
76 X = -4622565
76
Y = 7960884
93 feet Y = 2375053
50 meter
Z = 14355547
74 Z = 4353232
15
XDOT = -17959
465397 XDOT = -5410
730433
YDOT = -13571
596277 feet/sec YDOT = -4197
482784 meter/sec
ZDOT = -11246
032235 ZDOT = -3454
229054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16652126
76 X = 5075568
24
Y = -3760748
92 feet Y = -1146276
27 meter
Z = 14257233
69 Z = 4345604
83
XDOT = 13466
494589 XDOT = 4104
587551
YDOT = 16543
089289 feet/sec YDOT = 5042
333615 meter/sec
ZDOT = -11360
965123 ZDOT = -3462
822169
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 16322
34474799
00016717 00000-0 10270-3 0 9097
2 25544 51
6426 14
2527 0006776 219
9846 140
0808 15
53601903 28804
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34474799 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 14
2527 deg
Eccentricity:
0006776
Arg of perigee: 219
9846 deg
Mean anomaly: 140
0808 deg
Mean motion: 15
53601903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 325
Coasting Arc #11 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3322861
32 A = 6780645
34 meter
Y = -3298718
45 meter E =
0010508
Z = -4913389
32 I = 51
70461
XDOT = 6578
538727 Wp = 138
27664
YDOT = 3165
082913 meter/sec RA = 11
16525 deg
ZDOT = 2319
226648 TA = 154
44198
MA = 154
39000
Ha = 221
405 n
mi
Hp = 217
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10901775
99 X = 3383368
93
Y = -10822567
08 feet Y = -3261221
40 meter
Z = -16120043
71 Z = -4897100
68
XDOT = 21583
132308 XDOT = 6531
391068
YDOT = 10384
130292 feet/sec YDOT = 3238
384805 meter/sec
ZDOT = 7609
011312 ZDOT = 2351
069639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10715785
73 X = 3266171
49
Y = -11111465
37 feet Y = -3386774
64 meter
Z = -16048045
39 Z = -4891444
23
XDOT = 20990
335834 XDOT = 6397
854362
YDOT = 9030
029545 feet/sec YDOT = 2752
353005 meter/sec
ZDOT = 7747
806397 ZDOT = 2361
531390
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 16322
85932908
00016717 00000-0 10270-3 0 9106
2 25544 51
6423 11
6933 0006293 225
8448 134
2188 15
53634216 28888
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
85932908 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 11
6933 deg
Eccentricity:
0006293
Arg of perigee: 225
8448 deg
Mean anomaly: 134
2188 deg
Mean motion: 15
53634216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 318
Coasting Arc #12 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4634083
24 A = 6783735
06 meter
Y = 2762230
68 meter E =
0005840
Z = 4106670
76 I = 51
68276
XDOT = -5562
012801 Wp = 107
02577
YDOT = -3641
977387 meter/sec RA = 6
18282 deg
ZDOT = -3823
842562 TA = 22
44112
MA = 22
41558
Ha = 221
342 n
mi
Hp = 217
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15203685
18 X = -4684575
43
Y = 9062436
61 feet Y = 2710126
76 meter
Z = 13473329
27 Z = 4084036
80
XDOT = -18248
073494 XDOT = -5502
299131
YDOT = -11948
744707 feet/sec YDOT = -3703
841505 meter/sec
ZDOT = -12545
415230 ZDOT = -3850
716816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14880494
78 X = -4535574
81
Y = 9722479
99 feet Y = 2963411
90 meter
Z = 13373655
45 Z = 4076290
18
XDOT = -17961
699594 XDOT = -5474
726036
YDOT = -10060
429210 feet/sec YDOT = -3066
418823 meter/sec
ZDOT = -12662
352736 ZDOT = -3859
485114
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 16323
88849050
00016717 00000-0 10270-3 0 9116
2 25544 51
6420 6
5680 0006301 229
6913 130
3689 15
53628304 29049
Satellite: ISS
Catalog Number: 25544
Epoch time: 16323
88849050 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 6
5680 deg
Eccentricity:
0006301
Arg of perigee: 229
6913 deg
Mean anomaly: 130
3689 deg
Mean motion: 15
53628304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 299
Coasting Arc #13 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2016/324/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5692823
48 A = 6787117
16 meter
Y = -2219012
29 meter E =
0002100
Z = -2956727
36 I = 51
66268
XDOT = 4172
524736 Wp = 206
74526
YDOT = 4040
919877 meter/sec RA = 1
20471 deg
ZDOT = 4997
785362 TA = 119
52064
MA = 119
49969
Ha = 221
044 n
mi
Hp = 217
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18677242
39 X = 5731576
56
Y = -7280224
05 feet Y = -2155134
55 meter
Z = -9700549
08 Z = -2928978
76
XDOT = 13689
385617 XDOT = 4102
750743
YDOT = 13257
611145 feet/sec YDOT = 4087
189586 meter/sec
ZDOT = 16396
933603 ZDOT = 5017
885240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18262129
15 X = 5566296
96
Y = -8407549
07 feet Y = -2562620
96 meter
Z = -9578593
62 Z = -2919555
33
XDOT = 13751
102352 XDOT = 4191
335997
YDOT = 11076
634680 feet/sec YDOT = 3376
158250 meter/sec
ZDOT = 16484
123783 ZDOT = 5024
360929
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 16324
85332567
00016717 00000-0 10270-3 0 9125
2 25544 51
6426 1
7614 0006365 233
6946 126
3619 15
53647171 29197
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
85332567 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 1
7614 deg
Eccentricity:
0006365
Arg of perigee: 233
6946 deg
Mean anomaly: 126
3619 deg
Mean motion: 15
53647171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 316
Coasting Arc #14 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2016/324/22:00:36
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6777399
98 A = 6790673
68 meter
Y = -161055
21 meter E =
0005359
Z = -335186
95 I = 51
67373
XDOT = 407
505531 Wp = 28
62011
YDOT = 4750
800519 meter/sec RA =
87864 deg
ZDOT = 6001
277912 TA = 327
77085
MA = 327
80359
Ha = 221
003 n
mi
Hp = 217
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22235564
26 X = 6780325
44
Y = -528396
36 feet Y = -85249
41 meter
Z = -1099694
73 Z = -302256
68
XDOT = 1336
960402 XDOT = 325
198725
YDOT = 15586
615877 feet/sec YDOT = 4754
897160 meter/sec
ZDOT = 19689
231996 ZDOT = 6003
057696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19265227
85 X = 5872041
45
Y = -11128653
28 feet Y = -3392013
52 meter
Z = -955469
02 Z = -291226
96
XDOT = 7724
154480 XDOT = 2354
322285
YDOT = 11694
910930 feet/sec YDOT = 3564
608851 meter/sec
ZDOT = 19696
058786 ZDOT = 6003
358718
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 16324
91764714
00016717 00000-0 10270-3 0 9136
2 25544 51
6438 1
4416 0006438 234
7466 125
3085 15
53652230 29207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16324
91764714 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 1
4416 deg
Eccentricity:
0006438
Arg of perigee: 234
7466 deg
Mean anomaly: 125
3085 deg
Mean motion: 15
53652230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 297
Coasting Arc #15 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2016/325/22:00:36
000
Vector Time (MET): N/A
Weight (LBS) : 909067
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6653478
02 A = 6790145
18 meter
Y = -495440
66 meter E =
0010564
Z = -1223637
95 I = 51
63996
XDOT = 1427
875754 Wp = 179
49046
YDOT = -4746
248771 meter/sec RA = 355
91236 deg
ZDOT = -5853
005840 TA = 13
80991
MA = 13
78104
Ha = 220
876 n
mi
Hp = 217
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21828996
12 X = -6641499
42
Y = -1625461
49 feet Y = -569777
33 meter
Z = -4014560
20 Z = -1255930
04
XDOT = 4684
631739 XDOT = 1509
274998
YDOT = -15571
682319 feet/sec YDOT = -4729
826110 meter/sec
ZDOT = -19202
775064 ZDOT = -5845
871866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19754101
07 X = -6021050
01
Y = 9368472
50 feet Y = 2855510
42 meter
Z = -4155851
77 Z = -1266703
62
XDOT = -2838
224640 XDOT = -865
090870
YDOT = -14473
606757 feet/sec YDOT = -4411
555340 meter/sec
ZDOT = -19170
575207 ZDOT = -5843
191323
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 16325
94680042
00016717 00000-0 10270-3 0 9142
2 25544 51
6444 356
3157 0006499 237
8600 122
1922 15
53614239 29368
Satellite: ISS
Catalog Number: 25544
Epoch time: 16325
94680042 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 356
3157 deg
Eccentricity:
0006499
Arg of perigee: 237
8600 deg
Mean anomaly: 122
1922 deg
Mean motion: 15
53614239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 314
Coasting Arc #16 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2016/326/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6425298
09 A = 6790119
97 meter
Y = 1796294
05 meter E =
0012266
Z = 1219583
51 I = 51
61680
XDOT = -2336
780443 Wp = 148
24915
YDOT = -4374
172953 meter/sec RA = 352
70644 deg
ZDOT = -5851
995584 TA = 18
48913
MA = 18
44459
Ha = 220
821 n
mi
Hp = 217
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21080374
30 X = -6450831
42
Y = 5893353
19 feet Y = 1724299
28 meter
Z = 4001258
22 Z = 1188308
74
XDOT = -7666
602502 XDOT = -2259
266936
YDOT = -14350
961133 feet/sec YDOT = -4399
870976 meter/sec
ZDOT = -19199
460577 ZDOT = -5863
158917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2183652
80 X = -665577
37
Y = -21804250
12 feet Y = -6645935
44 meter
Z = 3863961
29 Z = 1177735
40
XDOT = 13844
228690 XDOT = 4219
720905
YDOT = -4807
318002 feet/sec YDOT = -1465
270527 meter/sec
ZDOT = -19247
451365 ZDOT = -5866
623176
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 16326
59001795
00016717 00000-0 10270-3 0 9157
2 25544 51
6416 353
1103 0006133 238
6444 121
4109 15
53655336 29466
Satellite: ISS
Catalog Number: 25544
Epoch time: 16326
59001795 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 353
1103 deg
Eccentricity:
0006133
Arg of perigee: 238
6444 deg
Mean anomaly: 121
4109 deg
Mean motion: 15
53655336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 297
Coasting Arc #17 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2016/327/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6674442
52 A = 6790520
48 meter
Y = -1184829
27 meter E =
0006698
Z = 327754
93 I = 51
58601
XDOT = 545
331884 Wp = 36
63925
YDOT = 4746
413581 meter/sec RA = 347
73655 deg
ZDOT = 5994
969983 TA = 326
89442
MA = 326
93633
Ha = 220
607 n
mi
Hp = 217
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21897777
30 X = 6685603
42
Y = -3887235
15 feet Y = -1110128
77 meter
Z = 1075311
44 Z = 360205
15
XDOT = 1789
146600 XDOT = 463
094459
YDOT = 15572
223035 feet/sec YDOT = 4752
052053 meter/sec
ZDOT = 19668
536689 ZDOT = 5997
419332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 454623
09 X = 138569
12
Y = 22228141
13 feet Y = 6775137
42 meter
Z = 1217621
67 Z = 371131
08
XDOT = -14022
703850 XDOT = -4274
120133
YDOT = -800
356474 feet/sec YDOT = -243
948653 meter/sec
ZDOT = 19678
300616 ZDOT = 5997
946028
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 16327
61916337
00016717 00000-0 10270-3 0 9169
2 25544 51
6409 347
9844 0006357 241
9595 118
0915 15
53698461 29624
Satellite: ISS
Catalog Number: 25544
Epoch time: 16327
61916337 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 347
9844 deg
Eccentricity:
0006357
Arg of perigee: 241
9595 deg
Mean anomaly: 118
0915 deg
Mean motion: 15
53698461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 347
Coasting Arc #18 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2016/328/13:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6506671
04 A = 6789162
40 meter
Y = 472097
30 meter E =
0007955
Z = -1860495
06 I = 51
54941
XDOT = 1239
928595 Wp = 188
24116
YDOT = -5061
566706 meter/sec RA = 342
76217 deg
ZDOT = -5625
459283 TA = 12
25799
MA = 12
23865
Ha = 220
303 n
mi
Hp = 217
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21347345
94 X = -6502428
96
Y = 1548875
66 feet Y = 399359
04 meter
Z = -6103986
42 Z = -1892092
95
XDOT = 4068
007202 XDOT = 1323
762590
YDOT = -16606
189979 feet/sec YDOT = -5047
232277 meter/sec
ZDOT = -18456
231245 ZDOT = -5619
232291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1399392
20 X = 426534
74
Y = -21317618
16 feet Y = -6497610
01 meter
Z = -6242411
59 Z = -1902687
05
XDOT = 14318
853738 XDOT = 4364
386619
YDOT = 6331
759646 feet/sec YDOT = 1929
920340 meter/sec
ZDOT = -18427
949644 ZDOT = -5616
839051
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 16328
58398768
00016717 00000-0 10270-3 0 9179
2 25544 51
6404 343
1779 0006146 247
0059 113
0446 15
53657894 29777
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
58398768 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 343
1779 deg
Eccentricity:
0006146
Arg of perigee: 247
0059 deg
Mean anomaly: 113
0446 deg
Mean motion: 15
53657894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 350
Coasting Arc #19 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2016/328/20:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 895793
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480772
27 A = 6786747
82 meter
Y = -4078073
52 meter E =
0001823
Z = -3057496
36 I = 51
53628
XDOT = 5426
818507 Wp = 247
44272
YDOT = 2281
126346 meter/sec RA = 341
32770 deg
ZDOT = 4907
440261 TA = 77
43068
MA = 77
41029
Ha = 220
219 n
mi
Hp = 217
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14700696
42 X = 4540893
51
Y = -13379506
31 feet Y = -4027630
37 meter
Z = -10031156
03 Z = -3035583
54
XDOT = 17804
522662 XDOT = 5377
068473
YDOT = 7484
010323 feet/sec YDOT = 2341
534531 meter/sec
ZDOT = 16100
525791 ZDOT = 4933
681903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14047729
97 X = 4281748
09
Y = -14132042
58 feet Y = -4307446
58 meter
Z = -9934405
40 Z = -3028006
77
XDOT = 17035
429379 XDOT = 5192
398875
YDOT = 5528
121026 feet/sec YDOT = 1684
971289 meter/sec
ZDOT = 16214
945012 ZDOT = 4942
315240
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 16328
84127326
00016717 00000-0 10270-3 0 9189
2 25544 51
6440 341
8972 0006341 250
0136 110
0334 15
53679988 29810
Satellite: ISS
Catalog Number: 25544
Epoch time: 16328
84127326 = yrday
fracday
Element set: 918
Inclination: 51
6440 deg
RA of node: 341
8972 deg
Eccentricity:
0006341
Arg of perigee: 250
0136 deg
Mean anomaly: 110
0334 deg
Mean motion: 15
53679988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 313
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