[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 7th 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) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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
220/05:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
7
223/08:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
8
Coasting Arc #1 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2016/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6127751
15 A = 6785743
99 meter
Y = 2355798
35 meter E =
0008730
Z = -1707896
13 I = 51
70864
XDOT = -3139
899220 Wp = 49
19799
YDOT = -4052
082686 meter/sec RA = 170
82332 deg
ZDOT = 5700
983361 TA = 292
09182
MA = 292
18449
Ha = 220
425 n
mi
Hp = 212
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20104170
43 X = -6145342
80
Y = 7728997
23 feet Y = 2287175
36 meter
Z = -5603333
76 Z = -1737705
38
XDOT = -10301
506627 XDOT = -3122
046808
YDOT = -13294
234533 feet/sec YDOT = -4087
095221 meter/sec
ZDOT = 18704
013651 ZDOT = 5685
774254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19438278
60 X = 5924787
32
Y = 9197215
84 feet Y = 2803311
39 meter
Z = -5733843
57 Z = -1747675
52
XDOT = -1763
414602 XDOT = -537
488771
YDOT = 15297
448765 feet/sec YDOT = 4662
662384 meter/sec
ZDOT = 18638
262562 ZDOT = 5680
942429
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 16218
50342916
00016717 00000-0 10270-3 0 9005
2 25544 51
6399 171
9650 0001908 94
5658 265
5713 15
54914491 12655
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
50342916 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 171
9650 deg
Eccentricity:
0001908
Arg of perigee: 94
5658 deg
Mean anomaly: 265
5713 deg
Mean motion: 15
54914491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1265
Checksum: 324
Coasting Arc #2 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2016/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6619924
96 A = 6786992
83 meter
Y = -1445008
40 meter E =
0013125
Z = -274582
89 I = 51
74583
XDOT = 783
039634 Wp = 132
11478
YDOT = 4693
719400 meter/sec RA = 165
85553 deg
ZDOT = -6015
270933 TA = 50
84086
MA = 50
72431
Ha = 220
425 n
mi
Hp = 212
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21718913
93 X = 6636925
19
Y = -4740841
21 feet Y = -1370884
93 meter
Z = -900862
50 Z = -242384
17
XDOT = 2569
027669 XDOT = 759
714175
YDOT = 15399
341863 feet/sec YDOT = 4702
345288 meter/sec
ZDOT = -19735
140856 ZDOT = -6011
523969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18629762
37 X = -5678351
57
Y = -12138888
93 feet Y = -3699933
35 meter
Z = -760052
82 Z = -231664
10
XDOT = 8184
551413 XDOT = 2494
651271
YDOT = -11373
171818 feet/sec YDOT = -3466
542770 meter/sec
ZDOT = -19719
528283 ZDOT = -6010
512221
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 16219
53173433
00016717 00000-0 10270-3 0 9016
2 25544 51
6413 166
8328 0001803 99
2795 260
8562 15
54924671 12814
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
53173433 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 166
8328 deg
Eccentricity:
0001803
Arg of perigee: 99
2795 deg
Mean anomaly: 260
8562 deg
Mean motion: 15
54924671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 314
Coasting Arc #3 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4665339
60 A = 6778795
76 meter
Y = -2153979
04 meter E =
0011500
Z = 4413989
06 I = 51
74251
XDOT = 5252
787421 Wp = 109
01629
YDOT = -4473
863370 meter/sec RA = 162
14538 deg
ZDOT = 3357
906270 TA = 307
06319
MA = 307
16829
Ha = 220
568 n
mi
Hp = 212
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15306232
28 X = -4662347
47
Y = -7066860
36 feet Y = -2206133
12 meter
Z = 14481591
42 Z = 4391333
68
XDOT = 17233
554531 XDOT = 5286
113874
YDOT = -14678
029428 feet/sec YDOT = -4414
936749 meter/sec
ZDOT = 11016
752854 ZDOT = 3383
503697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15901642
74 X = -4846820
71
Y = 5848454
81 feet Y = 1782609
03 meter
Z = 14383013
83 Z = 4383942
61
XDOT = 2246
704466 XDOT = 684
795521
YDOT = -21349
004865 feet/sec YDOT = -6507
176683 meter/sec
ZDOT = 11129
231547 ZDOT = 3392
189776
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 16220
30295822
00016717 00000-0 10270-3 0 9021
2 25544 51
6421 162
9834 0002055 104
9262 255
2118 15
54942353 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30295822 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 162
9834 deg
Eccentricity:
0002055
Arg of perigee: 104
9262 deg
Mean anomaly: 255
2118 deg
Mean motion: 15
54942353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 285
Coasting Arc #4 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2927570
60 A = 6775591
65 meter
Y = 3219160
59 meter E =
0015697
Z = -5207533
87 I = 51
76315
XDOT = -6501
420773 Wp = 83
74929
YDOT = 3837
666738 meter/sec RA = 157
15073 deg
ZDOT = -1284
281548 TA = 173
93208
MA = 173
91304
Ha = 220
416 n
mi
Hp = 212
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9604890
43 X = 2916651
21
Y = 10561550
48 feet Y = 3251837
44 meter
Z = -17085084
88 Z = -5193339
25
XDOT = -21330
120646 XDOT = -6537
612923
YDOT = 12590
770137 feet/sec YDOT = 3764
761106 meter/sec
ZDOT = -4213
522140 ZDOT = -1315
951460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14343782
71 X = 4371984
97
Y = 390930
78 feet Y = 119155
70 meter
Z = -17023614
91 Z = -5188797
82
XDOT = -5786
123445 XDOT = -1763
610426
YDOT = 23006
098030 feet/sec YDOT = 7012
258679 meter/sec
ZDOT = -4352
428784 ZDOT = -1326
620293
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 16221
26698509
00016717 00000-0 10270-3 0 9037
2 25544 51
6430 158
1727 0001944 108
9588 251
1776 15
54935184 13085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26698509 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 158
1727 deg
Eccentricity:
0001944
Arg of perigee: 108
9588 deg
Mean anomaly: 251
1776 deg
Mean motion: 15
54935184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 326
Coasting Arc #5 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -976376
24 A = 6775199
02 meter
Y = -4160982
93 meter E =
0004984
Z = 5252954
03 I = 51
78973
XDOT = 7051
731105 Wp = 78
17341
YDOT = -2869
990957 meter/sec RA = 152
15206 deg
ZDOT = -960
899475 TA = 21
00670
MA = 20
98624
Ha = 220
452 n
mi
Hp = 212
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3203334
11 X = -955290
85
Y = -13651518
81 feet Y = -4171783
41 meter
Z = 17234101
15 Z = 5248262
39
XDOT = 23135
600739 XDOT = 7087
967562
YDOT = -9415
980831 feet/sec YDOT = -2790
931197 meter/sec
ZDOT = -3152
557332 ZDOT = -926
556184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12220710
20 X = -3724872
47
Y = -6925486
88 feet Y = -2110888
40 meter
Z = 17214279
88 Z = 5246912
51
XDOT = 8477
513859 XDOT = 2583
946224
YDOT = -22436
021029 feet/sec YDOT = -6838
499210 meter/sec
ZDOT = -3002
114583 ZDOT = -915
044525
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 16222
29527512
00016717 00000-0 10270-3 0 9047
2 25544 51
6412 153
0408 0002051 110
5891 249
5483 15
54960639 13248
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29527512 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 153
0408 deg
Eccentricity:
0002051
Arg of perigee: 110
5891 deg
Mean anomaly: 249
5483 deg
Mean motion: 15
54960639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 289
Coasting Arc #6 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -951915
50 A = 6778010
80 meter
Y = 4907867
27 meter E =
0011969
Z = -4588740
11 I = 51
82850
XDOT = -6844
553479 Wp = 110
80123
YDOT = 1543
031479 meter/sec RA = 147
15957 deg
ZDOT = 3072
543589 TA = 189
86717
MA = 189
89069
Ha = 220
347 n
mi
Hp = 212
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3123082
33 X = -984435
82
Y = 16101926
75 feet Y = 4897040
42 meter
Z = -15054921
62 Z = -4593443
29
XDOT = -22455
884117 XDOT = -6876
224317
YDOT = 5062
439234 feet/sec YDOT = 1466
314067 meter/sec
ZDOT = 10080
523587 ZDOT = 3039
217791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9894080
89 X = 3015715
86
Y = 13057182
77 feet Y = 3979829
31 meter
Z = -15076255
99 Z = -4595242
83
XDOT = -10425
738836 XDOT = -3177
765197
YDOT = 19362
263319 feet/sec YDOT = 5901
617860 meter/sec
ZDOT = 9934
721150 ZDOT = 3028
103006
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 16223
25929109
00016717 00000-0 10270-3 0 9053
2 25544 51
6426 148
2297 0001839 112
2711 247
8638 15
54946133 13390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
25929109 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 148
2297 deg
Eccentricity:
0001839
Arg of perigee: 112
2711 deg
Mean anomaly: 247
8638 deg
Mean motion: 15
54946133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 317
Coasting Arc #7 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5572292
22 A = 6780673
25 meter
Y = -27373
35 meter E =
0007817
Z = -3870856
29 I = 51
83795
XDOT = -2848
484140 Wp = 83
80476
YDOT = 5778
749420 meter/sec RA = 146
63281 deg
ZDOT = -4147
765684 TA = 142
71366
MA = 142
65937
Ha = 220
375 n
mi
Hp = 212
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18281798
63 X = 5590986
97
Y = -89807
58 feet Y = 35044
22 meter
Z = -12699659
73 Z = -3843742
30
XDOT = -9345
420406 XDOT = -2892
743977
YDOT = 18959
151642 feet/sec YDOT = 5746
648240 meter/sec
ZDOT = -13608
155132 ZDOT = -4161
710371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 98178
90 X = 29924
93
Y = -18363457
22 feet Y = -5597181
76 meter
Z = -12581231
41 Z = -3834759
33
XDOT = 17522
477553 XDOT = 5340
851158
YDOT = 9444
873612 feet/sec YDOT = 2878
797477 meter/sec
ZDOT = -13669
994591 ZDOT = -4166
614351
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 16223
38782706
00016717 00000-0 10270-3 0 9068
2 25544 51
6401 147
5875 0001873 110
3961 249
7394 15
54961503 13412
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
38782706 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 147
5875 deg
Eccentricity:
0001873
Arg of perigee: 110
3961 deg
Mean anomaly: 249
7394 deg
Mean motion: 15
54961503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 314
Coasting Arc #8 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4399385
97 A = 6776564
80 meter
Y = -1464455
14 meter E =
0008292
Z = 4937253
90 I = 51
85076
XDOT = 4477
696575 Wp = 120
70625
YDOT = -5806
867468 meter/sec RA = 141
64951 deg
ZDOT = 2260
555405 TA = 307
25535
MA = 307
33095
Ha = 220
340 n
mi
Hp = 212
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14433681
00 X = -4406665
95
Y = -4804642
86 feet Y = -1513692
71 meter
Z = 16198339
56 Z = 4915865
27
XDOT = 14690
605562 XDOT = 4531
316927
YDOT = -19051
402453 feet/sec YDOT = -5756
495056 meter/sec
ZDOT = 7416
520358 ZDOT = 2282
437016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4702707
73 X = -1433385
32
Y = 14570882
08 feet Y = 4441204
86 meter
Z = 16105150
74 Z = 4908849
94
XDOT = -18088
814566 XDOT = -5513
470680
YDOT = -14167
582986 feet/sec YDOT = -4318
279294 meter/sec
ZDOT = 7513
047256 ZDOT = 2289
976804
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 16224
41610263
00016717 00000-0 10270-3 0 9072
2 25544 51
6399 142
4560 0001669 115
2392 244
8934 15
54994990 13577
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
41610263 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 142
4560 deg
Eccentricity:
0001669
Arg of perigee: 115
2392 deg
Mean anomaly: 244
8934 deg
Mean motion: 15
54994990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 323
Coasting Arc #9 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2906562
56 A = 6774905
55 meter
Y = 3018183
06 meter E =
0016411
Z = -5337826
39 I = 51
86965
XDOT = -5548
618113 Wp = 92
56098
YDOT = 5277
661674 meter/sec RA = 136
65682 deg
ZDOT = -37
993848 TA = 177
08243
MA = 177
07284
Ha = 220
245 n
mi
Hp = 212
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9535966
41 X = 2898525
09
Y = 9902175
40 feet Y = 3050641
29 meter
Z = -17512553
78 Z = -5323726
66
XDOT = -18204
127666 XDOT = -5607
037320
YDOT = 17315
162974 feet/sec YDOT = 5215
286677 meter/sec
ZDOT = -124
651731 ZDOT = -65
089259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9665143
54 X = 2945935
75
Y = -9884787
75 feet Y = -3012883
31 meter
Z = -17451453
94 Z = -5319203
16
XDOT = 17028
042693 XDOT = 5190
147413
YDOT = 17075
516347 feet/sec YDOT = 5204
617383 meter/sec
ZDOT = -243
886782 ZDOT = -74
336691
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16225
38010699
00016717 00000-0 10270-3 0 9087
2 25544 51
6398 137
6440 0001710 117
3394 242
7933 15
54972079 13728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
38010699 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 137
6440 deg
Eccentricity:
0001710
Arg of perigee: 117
3394 deg
Mean anomaly: 242
7933 deg
Mean motion: 15
54972079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 319
Coasting Arc #10 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1271191
13 A = 6776360
21 meter
Y = -4427681
19 meter E =
0007151
Z = 4964863
96 I = 51
89890
XDOT = 6037
649685 Wp = 69
42643
YDOT = -4197
964580 meter/sec RA = 131
66640 deg
ZDOT = -2192
897283 TA = 41
89458
MA = 41
83988
Ha = 220
223 n
mi
Hp = 212
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4170574
58 X = -1245702
11
Y = -14526513
08 feet Y = -4441754
06 meter
Z = 16288923
76 Z = 4958750
73
XDOT = 19808
561958 XDOT = 6094
795693
YDOT = -13772
849671 feet/sec YDOT = -4130
127986 meter/sec
ZDOT = -7194
544891 ZDOT = -2163
429478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14336072
10 X = -4369634
78
Y = 4871947
65 feet Y = 1484969
64 meter
Z = 16262947
90 Z = 4956946
52
XDOT = -14226
385118 XDOT = -4336
202184
YDOT = -18223
528046 feet/sec YDOT = -5554
531348 meter/sec
ZDOT = -7065
103201 ZDOT = -2153
443456
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16226
40836990
00016717 00000-0 10270-3 0 9092
2 25544 51
6410 132
5120 0001630 121
4345 238
6967 15
54995132 13888
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
40836990 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 132
5120 deg
Eccentricity:
0001630
Arg of perigee: 121
4345 deg
Mean anomaly: 238
6967 deg
Mean motion: 15
54995132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 304
Coasting Arc #11 (Orbit 1402)
---------------------------------------
Vector Time (GMT): 2016/227/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -302859
43 A = 6780322
41 meter
Y = 5535451
13 meter E =
0008084
Z = -3912545
20 I = 51
93293
XDOT = -5931
680270 Wp = 109
40877
YDOT = 2576
290119 meter/sec RA = 126
68634 deg
ZDOT = 4108
365605 TA = 203
50263
MA = 203
53959
Ha = 220
154 n
mi
Hp = 212
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -993633
31 X = -345730
54
Y = 18160928
89 feet Y = 5531824
72 meter
Z = -12836434
38 Z = -3914120
41
XDOT = -19460
893273 XDOT = -5980
004542
YDOT = 8452
395402 feet/sec YDOT = 2509
687829 meter/sec
ZDOT = 13478
889780 ZDOT = 4079
434056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18181936
43 X = 5541854
22
Y = -152834
39 feet Y = -46583
92 meter
Z = -12844240
83 Z = -3914924
60
XDOT = 9571
068251 XDOT = 2917
261603
YDOT = 17693
983625 feet/sec YDOT = 5393
126209 meter/sec
ZDOT = 13352
042220 ZDOT = 4069
702469
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16227
37235917
00016717 00000-0 10270-3 0 9103
2 25544 51
6411 127
7006 0001587 121
6291 238
5017 15
54992067 14038
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
37235917 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 127
7006 deg
Eccentricity:
0001587
Arg of perigee: 121
6291 deg
Mean anomaly: 238
5017 deg
Mean motion: 15
54992067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1403
Checksum: 295
Coasting Arc #12 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2016/228/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1711690
97 A = 6784554
28 meter
Y = -6150866
39 meter E =
0015387
Z = 2273117
00 I = 51
96612
XDOT = 5358
776627 Wp = 109
71422
YDOT = -537
827056 meter/sec RA = 121
72185 deg
ZDOT = -5465
654849 TA = 45
08223
MA = 44
95748
Ha = 220
120 n
mi
Hp = 212
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5615784
04 X = 1769302
67
Y = -20180007
86 feet Y = -6131403
02 meter
Z = 7457732
93 Z = 2281571
68
XDOT = 17581
288147 XDOT = 5390
941822
YDOT = -1764
524461 feet/sec YDOT = -477
721720 meter/sec
ZDOT = -17931
938481 ZDOT = -5439
545573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20542637
16 X = -6261395
81
Y = -4025155
33 feet Y = -1226867
35 meter
Z = 7495712
83 Z = 2284693
27
XDOT = -3393
180257 XDOT = -1034
241342
YDOT = -16014
560841 feet/sec YDOT = -4881
238144 meter/sec
ZDOT = -17817
750238 ZDOT = -5430
850273
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16228
40060873
00016717 00000-0 10270-3 0 9116
2 25544 51
6415 122
5686 0001599 124
6795 235
4509 15
55010331 14199
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
40060873 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 122
5686 deg
Eccentricity:
0001599
Arg of perigee: 124
6795 deg
Mean anomaly: 235
4509 deg
Mean motion: 15
55010331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 299
Coasting Arc #13 (Orbit 1433)
---------------------------------------
Vector Time (GMT): 2016/229/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2810017
91 A = 6786662
63 meter
Y = 6163106
09 meter E =
0011497
Z = -341603
75 I = 51
98965
XDOT = -4425
638435 Wp = 50
52852
YDOT = -1691
452991 meter/sec RA = 116
76923 deg
ZDOT = 6030
324624 TA = 305
80620
MA = 305
91299
Ha = 220
040 n
mi
Hp = 212
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9219218
86 X = -2877067
14
Y = 20220164
34 feet Y = 6131307
70 meter
Z = -1120747
21 Z = -355416
72
XDOT = -14519
811137 XDOT = -4435
687406
YDOT = -5549
386455 feet/sec YDOT = -1740
999609 meter/sec
ZDOT = 19784
529607 ZDOT = 6008
801998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20987511
57 X = 6396993
53
Y = 7296024
98 feet Y = 2223828
41 meter
Z = -1182156
55 Z = -360321
32
XDOT = -3632
647982 XDOT = -1107
231105
YDOT = 13568
504418 feet/sec YDOT = 4135
680147 meter/sec
ZDOT = 19690
751894 ZDOT = 6001
741177
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16229
36458557
00016717 00000-0 10270-3 0 9123
2 25544 51
6417 117
7575 0001551 131
5058 228
6228 15
55026320 14345
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
36458557 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 117
7575 deg
Eccentricity:
0001551
Arg of perigee: 131
5058 deg
Mean anomaly: 228
6228 deg
Mean motion: 15
55026320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1434
Checksum: 302
Coasting Arc #14 (Orbit 1449)
---------------------------------------
Vector Time (GMT): 2016/230/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3612618
97 A = 6785524
36 meter
Y = -5487978
97 meter E =
0009252
Z = -1681972
47 I = 52
00047
XDOT = 3266
293045 Wp = 140
49304
YDOT = 3901
027907 meter/sec RA = 111
81894 deg
ZDOT = -5737
076087 TA = 57
85044
MA = 57
76072
Ha = 220
043 n
mi
Hp = 212
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11852424
43 X = 3681888
57
Y = -18005180
36 feet Y = -5447192
98 meter
Z = -5518282
38 Z = -1664255
27
XDOT = 10716
184530 XDOT = 3250
295665
YDOT = 12798
647989 feet/sec YDOT = 3937
464201 meter/sec
ZDOT = -18822
428108 ZDOT = -5721
248533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19203017
70 X = -5853079
80
Y = -9837143
02 feet Y = -2998361
19 meter
Z = -5439913
01 Z = -1658085
49
XDOT = 10811
121539 XDOT = 3295
229845
YDOT = -10778
006244 feet/sec YDOT = -3285
136303 meter/sec
ZDOT = -18753
911046 ZDOT = -5716
192087
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16230
39282028
00016717 00000-0 10270-3 0 9137
2 25544 51
6426 112
6248 0001473 130
9599 229
1682 15
55035226 14505
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
39282028 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 112
6248 deg
Eccentricity:
0001473
Arg of perigee: 130
9599 deg
Mean anomaly: 229
1682 deg
Mean motion: 15
55035226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1450
Checksum: 296
Coasting Arc #15 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2016/231/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070987
03 A = 6781762
95 meter
Y = 4193566
19 meter E =
0013528
Z = 3429462
53 I = 51
99827
XDOT = -2030
735171 Wp = 94
56184
YDOT = -5771
312000 meter/sec RA = 106
86184 deg
ZDOT = 4629
878246 TA = 305
39779
MA = 305
52408
Ha = 220
057 n
mi
Hp = 212
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13356256
66 X = -4134236
49
Y = 13758419
27 feet Y = 4147688
19 meter
Z = 11251517
50 Z = 3409533
31
XDOT = -6662
516965 XDOT = -1988
537456
YDOT = -18934
750657 feet/sec YDOT = -5793
784895 meter/sec
ZDOT = 15189
889258 ZDOT = 4620
116393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15353162
20 X = 4679643
84
Y = 11572932
24 feet Y = 3527429
75 meter
Z = 11163690
65 Z = 3402692
91
XDOT = -17077
804463 XDOT = -5205
314800
YDOT = 7990
351495 feet/sec YDOT = 2435
459136 meter/sec
ZDOT = 15148
203566 ZDOT = 4617
172447
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16231
42104961
00016717 00000-0 10270-3 0 9142
2 25544 51
6418 107
4931 0001494 135
6019 224
5255 15
55040923 14661
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
42104961 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 107
4931 deg
Eccentricity:
0001494
Arg of perigee: 135
6019 deg
Mean anomaly: 224
5255 deg
Mean motion: 15
55040923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 287
Coasting Arc #16 (Orbit 1480)
---------------------------------------
Vector Time (GMT): 2016/232/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4265470
18 A = 6777275
48 meter
Y = -2360499
31 meter E =
0011338
Z = -4718657
82 I = 51
99275
XDOT = 777
648111 Wp = 77
37099
YDOT = 7072
768401 meter/sec RA = 101
89056 deg
ZDOT = -2838
498097 TA = 164
59548
MA = 164
56094
Ha = 219
921 n
mi
Hp = 212
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13994324
73 X = 4314469
64
Y = -7744420
32 feet Y = -2312526
29 meter
Z = -15481160
82 Z = -4697818
47
XDOT = 2551
338948 XDOT = 712
288769
YDOT = 23204
620737 feet/sec YDOT = 7081
098961 meter/sec
ZDOT = -9312
657798 ZDOT = -2834
879732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9694859
96 X = -2954993
32
Y = -12831659
84 feet Y = -3911089
92 meter
Z = -15389662
35 Z = -4690769
09
XDOT = 21650
086224 XDOT = 6598
946281
YDOT = -5219
070022 feet/sec YDOT = -1590
772543 meter/sec
ZDOT = -9298
053586 ZDOT = -2834
046733
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16232
38500943
00016717 00000-0 10270-3 0 9159
2 25544 51
6426 102
6813 0001425 138
2951 221
8311 15
55068697 14812
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
38500943 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 102
6813 deg
Eccentricity:
0001425
Arg of perigee: 138
2951 deg
Mean anomaly: 221
8311 deg
Mean motion: 15
55068697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1481
Checksum: 295
Coasting Arc #17 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2016/233/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204192
50 A = 6774668
98 meter
Y = 230531
56 meter E =
0004178
Z = 5304636
14 I = 51
98991
XDOT = 410
045760 Wp = 125
56119
YDOT = -7633
984361 meter/sec RA = 96
90836 deg
ZDOT = 654
017227 TA = 318
21231
MA = 318
24421
Ha = 219
931 n
mi
Hp = 212
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13793282
49 X = -4232225
15
Y = 756337
12 feet Y = 183361
12 meter
Z = 17403661
88 Z = 5284145
44
XDOT = 1345
294489 XDOT = 492
203546
YDOT = -25045
880448 feet/sec YDOT = -7628
939534 meter/sec
ZDOT = 2145
725810 ZDOT = 656
209212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2987047
12 X = 910451
96
Y = 13602034
65 feet Y = 4145900
16 meter
Z = 17314050
29 Z = 5277322
53
XDOT = -23941
378398 XDOT = -7297
332136
YDOT = 2500
981133 feet/sec YDOT = 762
299049 meter/sec
ZDOT = 2156
625584 ZDOT = 657
339478
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16233
41322540
00016717 00000-0 10270-3 0 9160
2 25544 51
6424 97
5488 0001333 147
7421 212
3814 15
55097086 14979
Satellite: ISS
Catalog Number: 25544
Epoch time: 16233
41322540 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 97
5488 deg
Eccentricity:
0001333
Arg of perigee: 147
7421 deg
Mean anomaly: 212
3814 deg
Mean motion: 15
55097086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 303
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