[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 19th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
027/19:27:44
185 2
4 2
8 2
8
N/A 1
4 -0
2 222
5
000/00:09:28
371 -0
4 0
0 213
2
Coasting Arc #1 (Orbit 2153)
---------------------------------------
Vector Time (GMT): 2016/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3168986
95 A = 6781630
30 meter
Y = 4542345
29 meter E =
0010110
Z = -3918677
94 I = 52
00786
XDOT = -3078
914987 Wp = 69
01422
YDOT = 5685
823805 meter/sec RA = 88
64565 deg
ZDOT = 4112
902595 TA = 243
85728
MA = 243
96131
Ha = 222
151 n
mi
Hp = 212
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10396938
81 X = 3136992
97
Y = 14902707
65 feet Y = 4577604
22 meter
Z = -12856554
94 Z = -3903361
44
XDOT = -10101
427124 XDOT = -3162
245065
YDOT = 18654
277574 feet/sec YDOT = 5650
927297 meter/sec
ZDOT = 13493
774918 ZDOT = 4097
743821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8661886
14 X = -2640142
89
Y = 16026234
74 feet Y = 4884796
35 meter
Z = -12790995
47 Z = -3898695
42
XDOT = -20072
504196 XDOT = -6118
099279
YDOT = -164
094941 feet/sec YDOT = -50
016138 meter/sec
ZDOT = 13426
949865 ZDOT = 4092
534319
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 16018
50841948
00016717 00000-0 10270-3 0 9002
2 25544 51
6416 89
4727 0006268 30
8239 329
3281 15
54559372 21545
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
50841948 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 89
4727 deg
Eccentricity:
0006268
Arg of perigee: 30
8239 deg
Mean anomaly: 329
3281 deg
Mean motion: 15
54559372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2154
Checksum: 321
Coasting Arc #2 (Orbit 2169)
---------------------------------------
Vector Time (GMT): 2016/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2536056
99 A = 6785589
31 meter
Y = -5809086
39 meter E =
0016835
Z = 2410462
71 I = 52
02020
XDOT = 3801
982341 Wp = 84
61358
YDOT = -3910
890726 meter/sec RA = 83
68681 deg
ZDOT = -5391
164289 TA = 68
58171
MA = 68
40219
Ha = 222
195 n
mi
Hp = 212
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8320396
96 X = -2482618
79
Y = -19058682
39 feet Y = -5837147
57 meter
Z = 7908342
22 Z = 2398272
80
XDOT = 12473
695343 XDOT = 3871
620102
YDOT = -12831
006320 feet/sec YDOT = -3867
984848 meter/sec
ZDOT = -17687
546879 ZDOT = -5372
526350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13045230
04 X = 3976186
12
Y = -16220362
79 feet Y = -4943966
58 meter
Z = 7856593
45 Z = 2394689
68
XDOT = 16009
978100 XDOT = 4879
841325
YDOT = 4294
243105 feet/sec YDOT = 1308
885298 meter/sec
ZDOT = -17605
959055 ZDOT = -5366
296320
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 16019
53697680
00016717 00000-0 10270-3 0 9019
2 25544 51
6423 84
3413 0006454 33
2300 326
9257 15
54579679 21708
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
53697680 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 84
3413 deg
Eccentricity:
0006454
Arg of perigee: 33
2300 deg
Mean anomaly: 326
9257 deg
Mean motion: 15
54579679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2170
Checksum: 311
Coasting Arc #3 (Orbit 2184)
---------------------------------------
Vector Time (GMT): 2016/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1814111
95 A = 6788007
61 meter
Y = 6499901
31 meter E =
0017291
Z = -652980
05 I = 52
02292
XDOT = -4414
931919 Wp = 38
89272
YDOT = 1825
362790 meter/sec RA = 78
73771 deg
ZDOT = 6003
280291 TA = 314
08913
MA = 314
23132
Ha = 222
400 n
mi
Hp = 212
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5951810
85 X = 1744465
49
Y = 21325135
52 feet Y = 6519798
52 meter
Z = -2142322
98 Z = -644336
46
XDOT = -14484
684772 XDOT = -4464
176510
YDOT = 5988
723065 feet/sec YDOT = 1775
716453 meter/sec
ZDOT = 19695
801480 ZDOT = 5981
714351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15903742
45 X = -4847460
70
Y = 15408125
46 feet Y = 4696396
64 meter
Z = -2106098
57 Z = -641938
84
XDOT = -11106
534548 XDOT = -3385
271730
YDOT = -8829
526730 feet/sec YDOT = -2691
239747 meter/sec
ZDOT = 19601
908052 ZDOT = 5974
661574
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 16020
50124035
00016717 00000-0 10270-3 0 9028
2 25544 51
6419 79
5314 0006611 36
4029 323
7573 15
54523240 21852
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
50124035 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 79
5314 deg
Eccentricity:
0006611
Arg of perigee: 36
4029 deg
Mean anomaly: 323
7573 deg
Mean motion: 15
54523240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2185
Checksum: 274
Coasting Arc #4 (Orbit 2200)
---------------------------------------
Vector Time (GMT): 2016/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -912885
78 A = 6787304
39 meter
Y = -6610394
60 meter E =
0010179
Z = -1240473
21 I = 52
01468
XDOT = 4900
452840 Wp = 102
15795
YDOT = 418
040377 meter/sec RA = 73
79089 deg
ZDOT = -5876
708560 TA = 91
24979
MA = 91
13317
Ha = 222
344 n
mi
Hp = 212
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2995032
09 X = -832873
27
Y = -21687646
33 feet Y = -6620155
65 meter
Z = -4069793
98 Z = -1244713
72
XDOT = 16077
601182 XDOT = 4923
960115
YDOT = 1371
523545 feet/sec YDOT = 472
972226 meter/sec
ZDOT = -19280
539895 ZDOT = -5852
846603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17425846
95 X = 5311398
15
Y = -13248571
08 feet Y = -4038164
47 meter
Z = -4086889
51 Z = -1245683
92
XDOT = 5806
692167 XDOT = 1769
879772
YDOT = 13510
251189 feet/sec YDOT = 4117
924562 meter/sec
ZDOT = -19177
119961 ZDOT = -5845
186164
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 16021
52977726
00016717 00000-0 10270-3 0 9035
2 25544 51
6424 74
4001 0006643 41
5355 318
6302 15
54596367 22011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
52977726 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 74
4001 deg
Eccentricity:
0006643
Arg of perigee: 41
5355 deg
Mean anomaly: 318
6302 deg
Mean motion: 15
54596367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2201
Checksum: 290
Coasting Arc #5 (Orbit 2216)
---------------------------------------
Vector Time (GMT): 2016/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -98521
90 A = 6784346
55 meter
Y = 6103237
14 meter E =
0019114
Z = 2937075
95 I = 51
99404
XDOT = -5205
685026 Wp = 69
73275
YDOT = -2522
458839 meter/sec RA = 68
83797 deg
ZDOT = 5047
016140 TA = 323
65315
MA = 323
78282
Ha = 222
499 n
mi
Hp = 212
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -323234
59 X = -181029
27
Y = 20023743
91 feet Y = 6101673
95 meter
Z = 9636075
96 Z = 2936397
25
XDOT = -17079
019114 XDOT = -5201
607161
YDOT = -8275
783592 feet/sec YDOT = -2580
649687 meter/sec
ZDOT = 16558
451902 ZDOT = 5021
738467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17460224
78 X = -5321876
51
Y = 9811998
74 feet Y = 2990697
22 meter
Z = 9631925
67 Z = 2935810
95
XDOT = -855
935034 XDOT = -260
888998
YDOT = -17735
063664 feet/sec YDOT = -5405
647405 meter/sec
ZDOT = 16449
302902 ZDOT = 5013
747524
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 16022
55830360
00016717 00000-0 10270-3 0 9042
2 25544 51
6416 69
2690 0006782 45
7646 314
4063 15
54584493 22173
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
55830360 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 69
2690 deg
Eccentricity:
0006782
Arg of perigee: 45
7646 deg
Mean anomaly: 314
4063 deg
Mean motion: 15
54584493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2217
Checksum: 309
Coasting Arc #6 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2016/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1265197
64 A = 6780065
65 meter
Y = -5086837
85 meter E =
0014965
Z = -4316182
09 I = 51
96848
XDOT = 5221
949812 Wp = 60
38218
YDOT = 4319
503770 meter/sec RA = 63
87265 deg
ZDOT = -3562
116213 TA = 173
42199
MA = 173
40232
Ha = 222
450 n
mi
Hp = 211
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4150910
91 X = 1342951
60
Y = -16689100
55 feet Y = -5072254
68 meter
Z = -14160702
41 Z = -4309847
53
XDOT = 17132
381274 XDOT = 5190
562812
YDOT = 14171
600295 feet/sec YDOT = 4377
723695 meter/sec
ZDOT = -11686
732981 ZDOT = -3536
825909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16454171
79 X = 5015231
56
Y = -5081574
92 feet Y = -1548864
04 meter
Z = -14132213
50 Z = -4307498
67
XDOT = -3492
469176 XDOT = -1064
504605
YDOT = 20871
361394 feet/sec YDOT = 6361
590953 meter/sec
ZDOT = -11577
885391 ZDOT = -3528
939467
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 16023
52253616
00016717 00000-0 10270-3 0 9054
2 25544 51
6424 64
4582 0006738 49
2816 310
8921 15
54615623 22328
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
52253616 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 64
4582 deg
Eccentricity:
0006738
Arg of perigee: 49
2816 deg
Mean anomaly: 310
8921 deg
Mean motion: 15
54615623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2232
Checksum: 296
Coasting Arc #7 (Orbit 2247)
---------------------------------------
Vector Time (GMT): 2016/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2478015
92 A = 6776724
04 meter
Y = 3662475
58 meter E =
0009625
Z = 5126617
46 I = 51
94139
XDOT = -4924
236833 Wp = 82
14336
YDOT = -5651
627530 meter/sec RA = 58
89473 deg
ZDOT = 1655
986763 TA = 351
94842
MA = 351
96386
Ha = 222
605 n
mi
Hp = 211
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8129973
48 X = -2543688
78
Y = 12015996
00 feet Y = 3634397
48 meter
Z = 16819611
10 Z = 5114420
71
XDOT = -16155
632653 XDOT = -4868
716849
YDOT = -18542
085073 feet/sec YDOT = -5706
383202 meter/sec
ZDOT = 5433
027437 ZDOT = 1632
201359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14560828
56 X = -4438140
54
Y = -514189
46 feet Y = -156724
95 meter
Z = 16765972
30 Z = 5110268
36
XDOT = 6939
591891 XDOT = 2115
187609
YDOT = -22543
972304 feet/sec YDOT = -6871
402758 meter/sec
ZDOT = 5330
975557 ZDOT = 1624
881350
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 16024
55104008
00016717 00000-0 10270-3 0 9069
2 25544 51
6412 59
3266 0006855 52
9773 307
2006 15
54640324 22487
Satellite: ISS
Catalog Number: 25544
Epoch time: 16024
55104008 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 59
3266 deg
Eccentricity:
0006855
Arg of perigee: 52
9773 deg
Mean anomaly: 307
2006 deg
Mean motion: 15
54640324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2248
Checksum: 290
Coasting Arc #8 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682467
34 A = 6775978
74 meter
Y = -2035514
73 meter E =
0020535
Z = -5328613
58 I = 51
92244
XDOT = 4199
027234 Wp = 81
72885
YDOT = 6382
745689 meter/sec RA = 53
90907 deg
ZDOT = 468
061357 TA = 192
70054
MA = 192
75236
Ha = 222
527 n
mi
Hp = 211
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12081585
76 X = 3730838
79
Y = -6678197
93 feet Y = -1994064
51 meter
Z = -17482328
00 Z = -5310607
99
XDOT = 13776
336068 XDOT = 4125
068132
YDOT = 20940
766697 feet/sec YDOT = 6429
288465 meter/sec
ZDOT = 1535
634374 ZDOT = 488
279041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12288119
00 X = 3745418
67
Y = 6504168
05 feet Y = 1982470
42 meter
Z = -17403814
63 Z = -5304682
70
XDOT = -9433
047453 XDOT = -2875
192864
YDOT = 22122
947441 feet/sec YDOT = 6743
074380 meter/sec
ZDOT = 1622
059406 ZDOT = 494
403707
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 16025
51525324
00016717 00000-0 10270-3 0 9075
2 25544 51
6422 54
5158 0006803 55
6717 304
5078 15
54630764 22639
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
51525324 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 54
5158 deg
Eccentricity:
0006803
Arg of perigee: 55
6717 deg
Mean anomaly: 304
5078 deg
Mean motion: 15
54630764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 298
Coasting Arc #9 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4737565
30 A = 6777919
75 meter
Y = 325064
13 meter E =
0014288
Z = 4828560
08 I = 51
90848
XDOT = -3063
319691 Wp = 59
85080
YDOT = -6558
274101 meter/sec RA = 48
92348 deg
ZDOT = -2551
461075 TA = 55
20259
MA = 55
06823
Ha = 222
661 n
mi
Hp = 211
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15543193
25 X = -4764302
69
Y = 1066483
38 feet Y = 271936
16 meter
Z = 15841732
54 Z = 4805481
73
XDOT = -10050
261452 XDOT = -2977
362157
YDOT = -21516
647312 feet/sec YDOT = -6592
049617 meter/sec
ZDOT = -8370
935287 ZDOT = -2566
132648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9715191
38 X = -2961190
33
Y = -12308823
10 feet Y = -3751729
28 meter
Z = 15741558
48 Z = 4798027
02
XDOT = 11216
830778 XDOT = 3418
890021
YDOT = -19691
746637 feet/sec YDOT = -6002
044375 meter/sec
ZDOT = -8433
261363 ZDOT = -2570
458063
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 16026
54373559
00016717 00000-0 10270-3 0 9081
2 25544 51
6409 49
3836 0006945 59
5210 300
6628 15
54685600 22791
Satellite: ISS
Catalog Number: 25544
Epoch time: 16026
54373559 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 49
3836 deg
Eccentricity:
0006945
Arg of perigee: 59
5210 deg
Mean anomaly: 300
6628 deg
Mean motion: 15
54685600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 326
Coasting Arc #10 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5517441
24 A = 6781859
97 meter
Y = 1228199
58 meter E =
0012042
Z = -3755736
59 I = 51
90092
XDOT = 1540
540443 Wp = 79
74422
YDOT = 6157
355516 meter/sec RA = 43
94693 deg
ZDOT = 4290
497669 TA = 235
56783
MA = 235
68170
Ha = 222
629 n
mi
Hp = 211
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18101841
35 X = 5521540
54
Y = 4029526
17 feet Y = 1289922
03 meter
Z = -12321970
45 Z = -3728924
87
XDOT = 5054
266546 XDOT = 1450
731904
YDOT = 20201
297625 feet/sec YDOT = 6174
080880 meter/sec
ZDOT = 14076
435921 ZDOT = 4297
762707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7237226
36 X = 2205906
59
Y = 17157587
25 feet Y = 5229632
59 meter
Z = -12205918
71 Z = -3720364
02
XDOT = -12350
985185 XDOT = -3764
580284
YDOT = 15212
860671 feet/sec YDOT = 4636
879933 meter/sec
ZDOT = 14106
709358 ZDOT = 4299
725012
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 16027
50792878
00016717 00000-0 10270-3 0 9098
2 25544 51
6419 44
5731 0006999 62
6587 297
5278 15
54679055 22943
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
50792878 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 44
5731 deg
Eccentricity:
0006999
Arg of perigee: 62
6587 deg
Mean anomaly: 297
5278 deg
Mean motion: 15
54679055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 365
Coasting Arc #11 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2016/027/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3268135
91 A = 6777363
29 meter
Y = -2669092
69 meter E =
0018629
Z = -5319427
39 I = 51
87463
XDOT = 5340
212905 Wp = 84
69992
YDOT = 5457
339048 meter/sec RA = 42
40471 deg
ZDOT = 545
931933 TA = 190
48210
MA = 190
52099
Ha = 222
531 n
mi
Hp = 213
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10722230
67 X = 3323578
46
Y = -8756865
77 feet Y = -2632236
45 meter
Z = -17452189
61 Z = -5303417
14
XDOT = 17520
383548 XDOT = 5276
138849
YDOT = 17904
655669 feet/sec YDOT = 5516
698610 meter/sec
ZDOT = 1791
115267 ZDOT = 571
716999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1877437
82 X = -572243
05
Y = -13804418
78 feet Y = -4207586
84 meter
Z = -17382206
43 Z = -5298096
52
XDOT = 23379
210103 XDOT = 7125
983239
YDOT = -5560
652431 feet/sec YDOT = -1694
886861 meter/sec
ZDOT = 1901
859677 ZDOT = 579
686829
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 16027
82932665
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 42
9689 0004778 54
7814 305
3786 15
54165081 22992
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
82932665 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 42
9689 deg
Eccentricity:
0004778
Arg of perigee: 54
7814 deg
Mean anomaly: 305
3786 deg
Mean motion: 15
54165081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 341
Coasting Arc #12 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2016/028/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4510703
29 A = 6779155
60 meter
Y = 1361950
24 meter E =
0011853
Z = 4867649
26 I = 51
85672
XDOT = -4401
341360 Wp = 58
37307
YDOT = -5788
786605 meter/sec RA = 37
42121 deg
ZDOT = -2448
468597 TA = 55
62004
MA = 55
50800
Ha = 222
607 n
mi
Hp = 213
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14798895
30 X = -4549242
27
Y = 4468340
67 feet Y = 1311293
31 meter
Z = 15969977
88 Z = 4845644
08
XDOT = -14440
096327 XDOT = -4324
389191
YDOT = -18992
082039 feet/sec YDOT = -5837
575172 meter/sec
ZDOT = -8033
033455 ZDOT = -2469
661685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3638320
81 X = -1108960
18
Y = 15125610
65 feet Y = 4610286
13 meter
Z = 15874258
66 Z = 4838474
04
XDOT = -22550
751391 XDOT = -6873
469024
YDOT = 3137
671392 feet/sec YDOT = 956
362240 meter/sec
ZDOT = -8123
784066 ZDOT = -2476
129383
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 16028
85813608
00016717 00000-0 10270-3 0 9115
2 25544 51
6428 37
8395 0004756 57
0350 303
1259 15
54206196 23158
Satellite: ISS
Catalog Number: 25544
Epoch time: 16028
85813608 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 37
8395 deg
Eccentricity:
0004756
Arg of perigee: 57
0350 deg
Mean anomaly: 303
1259 deg
Mean motion: 15
54206196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 307
Coasting Arc #13 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2016/029/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5529783
50 A = 6782717
90 meter
Y = -146816
35 meter E =
0010375
Z = -3933365
31 I = 51
84307
XDOT = 3043
507185 Wp = 86
42294
YDOT = 5728
479999 meter/sec RA = 32
44371 deg
ZDOT = 4074
831858 TA = 226
10334
MA = 226
18905
Ha = 222
571 n
mi
Hp = 213
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18142334
31 X = 5550120
59
Y = -481680
95 feet Y = -84865
12 meter
Z = -12904741
83 Z = -3906453
97
XDOT = 9985
259792 XDOT = 2959
430197
YDOT = 18794
225719 feet/sec YDOT = 5762
044602 meter/sec
ZDOT = 13368
870924 ZDOT = 4089
411775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8480007
66 X = 2584706
33
Y = -16138938
11 feet Y = -4919148
34 meter
Z = -12787995
11 Z = -3897780
91
XDOT = 20059
211683 XDOT = 6114
047721
YDOT = -76
450137 feet/sec YDOT = -23
302002 meter/sec
ZDOT = 13430
941923 ZDOT = 4093
751098
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 16029
82263631
00016717 00000-0 10270-3 0 9129
2 25544 51
6434 33
0306 0004750 60
6342 299
5285 15
54188676 23306
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
82263631 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 33
0306 deg
Eccentricity:
0004750
Arg of perigee: 60
6342 deg
Mean anomaly: 299
5285 deg
Mean motion: 15
54188676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 299
Coasting Arc #14 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2016/030/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6210429
21 A = 6786509
42 meter
Y = -981882
68 meter E =
0017732
Z = 2536644
70 I = 51
82824
XDOT = -1325
734346 Wp = 94
37311
YDOT = -5385
349900 meter/sec RA = 27
47504 deg
ZDOT = -5299
799550 TA = 57
20864
MA = 57
03796
Ha = 222
651 n
mi
Hp = 212
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20375423
93 X = -6211309
78
Y = -3221399
85 feet Y = -1051336
63 meter
Z = 8322325
13 Z = 2506474
24
XDOT = -4349
522131 XDOT = -1239
671649
YDOT = -17668
470801 feet/sec YDOT = -5399
694160 meter/sec
ZDOT = -17387
793799 ZDOT = -5306
030301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12506553
78 X = -3811997
59
Y = 16470546
20 feet Y = 5020222
48 meter
Z = 8191680
75 Z = 2496824
29
XDOT = -16370
113282 XDOT = -4989
610528
YDOT = -3718
905047 feet/sec YDOT = -1133
522258 meter/sec
ZDOT = -17413
717154 ZDOT = -5307
700988
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 16030
85142591
00016717 00000-0 10270-3 0 9136
2 25544 51
6434 27
9012 0004840 65
8183 294
3475 15
54190382 23460
Satellite: ISS
Catalog Number: 25544
Epoch time: 16030
85142591 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 27
9012 deg
Eccentricity:
0004840
Arg of perigee: 65
8183 deg
Mean anomaly: 294
3475 deg
Mean motion: 15
54190382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 300
Coasting Arc #15 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2016/031/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6448907
36 A = 6788694
68 meter
Y = 1895799
25 meter E =
0014428
Z = -912497
82 I = 51
80748
XDOT = -585
047748 Wp = 47
79903
YDOT = 4815
465628 meter/sec RA = 22
51262 deg
ZDOT = 5939
298246 TA = 302
34590
MA = 302
48550
Ha = 222
535 n
mi
Hp = 212
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21157832
55 X = 6431661
25
Y = 6219813
83 feet Y = 1967818
75 meter
Z = -2993759
26 Z = -881212
91
XDOT = -1919
447991 XDOT = -667
702258
YDOT = 15798
771747 feet/sec YDOT = 4808
461296 meter/sec
ZDOT = 19485
886635 ZDOT = 5936
255335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15229853
54 X = 4642059
36
Y = -15974455
48 feet Y = -4869014
03 meter
Z = -2858476
93 Z = -871263
77
XDOT = 11943
528563 XDOT = 3640
387506
YDOT = 7945
232763 feet/sec YDOT = 2421
706946 meter/sec
ZDOT = 19471
704302 ZDOT = 5934
975471
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 16031
81590385
00016717 00000-0 10270-3 0 9142
2 25544 51
6436 23
0921 0004725 67
7067 292
4586 15
54234973 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 16031
81590385 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 23
0921 deg
Eccentricity:
0004725
Arg of perigee: 67
7067 deg
Mean anomaly: 292
4586 deg
Mean motion: 15
54234973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 312
Coasting Arc #16 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2016/032/19:32:28
371
Vector Time (MET): N/A
Weight (LBS) : 922190
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6177853
87 A = 6788763
93 meter
Y = -2669979
21 meter E =
0012488
Z = -866664
35 I = 51
77735
XDOT = 2591
523365 Wp = 120
44892
YDOT = -4089
766375 meter/sec RA = 17
55251 deg
ZDOT = -5943
528897 TA = 68
90734
MA = 68
77387
Ha = 222
512 n
mi
Hp = 212
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20268549
45 X = -6143328
51
Y = -8759774
31 feet Y = -2738871
04 meter
Z = -2843386
98 Z = -896590
61
XDOT = 8502
373244 XDOT = 2665
934362
YDOT = -13417
868684 feet/sec YDOT = -4060
370335 meter/sec
ZDOT = -19499
766724 ZDOT = -5930
759212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16820418
17 X = -5126863
46
Y = 14278295
10 feet Y = 4352024
35 meter
Z = -2972610
57 Z = -906051
70
XDOT = -7171
605598 XDOT = -2185
905386
YDOT = -12450
744136 feet/sec YDOT = -3794
986813 meter/sec
ZDOT = -19443
551146 ZDOT = -5926
394389
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 16032
84467101
00016717 00000-0 10270-3 0 9156
2 25544 51
6434 17
9626 0004614 73
0641 287
1017 15
54201775 23774
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
84467101 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 17
9626 deg
Eccentricity:
0004614
Arg of perigee: 73
0641 deg
Mean anomaly: 287
1017 deg
Mean motion: 15
54201775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 294
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