[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 10th 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) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
164/08:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 214
2
166/13:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
2
170/05:52:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
171/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2016/162/14:03:15
360
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1042492
70 A = 6787531
32 meter
Y = 6569210
73 meter E =
0013744
Z = 1318067
81 I = 52
03101
XDOT = -4568
580510 Wp = 57
73515
YDOT = -1908
089765 meter/sec RA = 90
12081 deg
ZDOT = 5859
187706 TA = 316
53961
MA = 316
64786
Ha = 220
344 n
mi
Hp = 214
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3420251
63 X = -1122276
36
Y = 21552528
64 feet Y = 6557106
67 meter
Z = 4324369
47 Z = 1312810
46
XDOT = -14988
781201 XDOT = -4575
365519
YDOT = -6260
137023 feet/sec YDOT = -1959
217128 meter/sec
ZDOT = 19223
056778 ZDOT = 5836
978124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21479954
97 X = 6547090
27
Y = -3876797
90 feet Y = -1181648
00 meter
Z = 4300204
19 Z = 1310702
24
XDOT = -1188
744629 XDOT = -362
329363
YDOT = 14765
532222 feet/sec YDOT = 4500
534221 meter/sec
ZDOT = 19126
623424 ZDOT = 5829
794820
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 16162
64733618
00016717 00000-0 10270-3 0 9001
2 25544 51
6440 90
6567 0000425 322
0926 38
0197 15
54497751 3964
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
64733618 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 90
6567 deg
Eccentricity:
0000425
Arg of perigee: 322
0926 deg
Mean anomaly: 38
0197 deg
Mean motion: 15
54497751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 396
Checksum: 309
Coasting Arc #2 (Orbit 410)
---------------------------------------
Vector Time (GMT): 2016/163/14:03:15
360
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1876769
45 A = 6784416
01 meter
Y = -5779637
43 meter E =
0004056
Z = -3018519
60 I = 52
01955
XDOT = 4244
639306 Wp = 109
38858
YDOT = 3980
004105 meter/sec RA = 85
17082 deg
ZDOT = -4988
256118 TA = 104
97216
MA = 104
92726
Ha = 220
275 n
mi
Hp = 214
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6157380
09 X = 1955921
95
Y = -18962065
05 feet Y = -5758207
34 meter
Z = -9903279
51 Z = -3009210
93
XDOT = 13925
981975 XDOT = 4224
049174
YDOT = 13057
756249 feet/sec YDOT = 4027
355747 meter/sec
ZDOT = -16365
669678 ZDOT = -4967
686471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19943425
72 X = -6078756
16
Y = 746218
89 feet Y = 227447
52 meter
Z = -9861597
93 Z = -3005815
05
XDOT = 7430
031133 XDOT = 2264
673489
YDOT = -16235
806110 feet/sec YDOT = -4948
673702 meter/sec
ZDOT = -16276
782140 ZDOT = -4961
163196
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 16163
61162744
00016717 00000-0 10270-3 0 9016
2 25544 51
6437 85
8481 0000474 297
4479 62
6625 15
54500064 4112
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
61162744 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 85
8481 deg
Eccentricity:
0000474
Arg of perigee: 297
4479 deg
Mean anomaly: 62
6625 deg
Mean motion: 15
54500064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 411
Checksum: 302
Coasting Arc #3 (Orbit 422)
---------------------------------------
Vector Time (GMT): 2016/164/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4243016
39 A = 6776647
77 meter
Y = -674382
30 meter E =
0003850
Z = 5238533
15 I = 51
98742
XDOT = -229
361497 Wp = 51
09794
YDOT = -7579
830422 meter/sec RA = 81
40785 deg
ZDOT = -1158
639578 TA = 49
97094
MA = 49
93717
Ha = 220
431 n
mi
Hp = 214
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13920657
44 X = -4260606
45
Y = -2212540
37 feet Y = -721929
28 meter
Z = 17186788
57 Z = 5217878
88
XDOT = -752
498350 XDOT = -138
956716
YDOT = -24868
210046 feet/sec YDOT = -7581
889727 meter/sec
ZDOT = -3801
310950 ZDOT = -1159
534733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13866117
65 X = -4226392
66
Y = 3081010
76 feet Y = 939092
08 meter
Z = 17096897
19 Z = 5211134
26
XDOT = -9559
858505 XDOT = -2913
844872
YDOT = -21863
275649 feet/sec YDOT = -6663
926418 meter/sec
ZDOT = -3803
747057 ZDOT = -1159
382103
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 16164
38305654
00016717 00000-0 10270-3 0 9021
2 25544 51
6399 81
9987 0000356 308
9387 51
1734 15
54521494 4239
Satellite: ISS
Catalog Number: 25544
Epoch time: 16164
38305654 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 81
9987 deg
Eccentricity:
0000356
Arg of perigee: 308
9387 deg
Mean anomaly: 51
1734 deg
Mean motion: 15
54521494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 423
Checksum: 324
Coasting Arc #4 (Orbit 437)
---------------------------------------
Vector Time (GMT): 2016/165/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301657
79 A = 6779400
95 meter
Y = 2556665
65 meter E =
0009575
Z = -4583176
13 I = 51
99186
XDOT = -821
894418 Wp = 108
69134
YDOT = 6952
824373 meter/sec RA = 76
43204 deg
ZDOT = 3109
449621 TA = 192
30435
MA = 192
32774
Ha = 220
321 n
mi
Hp = 214
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14113050
50 X = 4295011
95
Y = 8388010
65 feet Y = 2604732
83 meter
Z = -15036667
10 Z = -4562295
66
XDOT = -2696
503996 XDOT = -914
685960
YDOT = 22811
103586 feet/sec YDOT = 6943
114343 meter/sec
ZDOT = 10201
606367 ZDOT = 3105
232189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16336157
55 X = 4979260
82
Y = 2319610
84 feet Y = 707017
38 meter
Z = -14946157
92 Z = -4555588
93
XDOT = 6334
510394 XDOT = 1930
758768
YDOT = 20944
878287 feet/sec YDOT = 6383
998902 meter/sec
ZDOT = 10181
867699 ZDOT = 3103
433275
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 16165
34733599
00016717 00000-0 10270-3 0 9032
2 25544 51
6409 77
1891 0000404 327
4384 32
6743 15
54520372 4383
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
34733599 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 77
1891 deg
Eccentricity:
0000404
Arg of perigee: 327
4384 deg
Mean anomaly: 32
6743 deg
Mean motion: 15
54520372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 438
Checksum: 309
Coasting Arc #5 (Orbit 453)
---------------------------------------
Vector Time (GMT): 2016/166/08:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4159525
43 A = 6783405
90 meter
Y = -4174508
50 meter E =
0012349
Z = 3349060
59 I = 51
99694
XDOT = 1955
004271 Wp = 89
28784
YDOT = -5734
935611 meter/sec RA = 71
46609 deg
ZDOT = -4705
249973 TA = 51
88035
MA = 51
76908
Ha = 220
320 n
mi
Hp = 214
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13646736
99 X = -4128804
26
Y = -13695894
03 feet Y = -4220851
58 meter
Z = 10987731
61 Z = 3328928
85
XDOT = 6414
056006 XDOT = 2041
844645
YDOT = -18815
405549 feet/sec YDOT = -5712
587522 meter/sec
ZDOT = -15437
171828 ZDOT = -4695
542538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18034613
07 X = -5496950
06
Y = -7103961
21 feet Y = -2165287
38 meter
Z = 10900809
88 Z = 3322566
85
XDOT = -2031
829312 XDOT = -619
301574
YDOT = -18539
550223 feet/sec YDOT = -5650
854908 meter/sec
ZDOT = -15393
731160 ZDOT = -4692
009258
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 16166
37589243
00016717 00000-0 10270-3 0 9042
2 25544 51
6407 72
0587 0000517 331
8838 28
2287 15
54554867 4543
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
37589243 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 72
0587 deg
Eccentricity:
0000517
Arg of perigee: 331
8838 deg
Mean anomaly: 28
2287 deg
Mean motion: 15
54554867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 454
Checksum: 329
Coasting Arc #6 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2016/166/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4128185
57 A = 6784146
13 meter
Y = 4420942
39 meter E =
0004364
Z = -3073155
54 I = 52
00059
XDOT = -2156
755337 Wp = 63
95144
YDOT = 5445
505208 meter/sec RA = 70
34824 deg
ZDOT = 4943
841662 TA = 260
96226
MA = 261
01165
Ha = 220
234 n
mi
Hp = 214
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13543915
92 X = 4093370
81
Y = 14504404
17 feet Y = 4466912
10 meter
Z = -10082531
28 Z = -3053185
93
XDOT = -7075
968952 XDOT = -2241
503226
YDOT = 17865
830735 feet/sec YDOT = 5420
912675 meter/sec
ZDOT = 16219
952960 ZDOT = 4933
159230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10508986
23 X = 3203139
00
Y = -16885102
65 feet Y = -5146579
29 meter
Z = -9996366
98 Z = -3046892
66
XDOT = 17882
665858 XDOT = 5450
636553
YDOT = 1569
759632 feet/sec YDOT = 478
462736 meter/sec
ZDOT = 16172
317292 ZDOT = 4929
322311
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 16166
56874547
00016717 00000-0 10270-3 0 9058
2 25544 51
6441 71
0984 0000618 323
7901 36
3210 15
54556187 4570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
56874547 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 71
0984 deg
Eccentricity:
0000618
Arg of perigee: 323
7901 deg
Mean anomaly: 36
3210 deg
Mean motion: 15
54556187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 312
Coasting Arc #7 (Orbit 472)
---------------------------------------
Vector Time (GMT): 2016/167/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3700460
44 A = 6787370
48 meter
Y = -5515426
07 meter E =
0013399
Z = 1367170
70 I = 51
99978
XDOT = 3329
644325 Wp = 119
24460
YDOT = -3691
082629 meter/sec RA = 65
39592 deg
ZDOT = -5841
734376 TA = 45
93108
MA = 45
82084
Ha = 220
274 n
mi
Hp = 214
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12140618
25 X = -3645151
71
Y = -18095229
90 feet Y = -5556497
96 meter
Z = 4485468
17 Z = 1349328
49
XDOT = 10924
029937 XDOT = 3399
048297
YDOT = -12109
851144 feet/sec YDOT = -3653
459727 meter/sec
ZDOT = -19165
795197 ZDOT = -5825
391447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14065338
42 X = -4287115
15
Y = 16663735
48 feet Y = 5079106
57 meter
Z = 4408804
44 Z = 1343803
59
XDOT = -13461
111217 XDOT = -4102
946699
YDOT = -6278
042249 feet/sec YDOT = -1913
547277 meter/sec
ZDOT = -19093
827276 ZDOT = -5819
798554
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 16167
59729360
00016717 00000-0 10270-3 0 9065
2 25544 51
6443 65
9687 0000445 321
2893 38
8228 15
54539776 4734
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
59729360 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 65
9687 deg
Eccentricity:
0000445
Arg of perigee: 321
2893 deg
Mean anomaly: 38
8228 deg
Mean motion: 15
54539776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 473
Checksum: 343
Coasting Arc #8 (Orbit 488)
---------------------------------------
Vector Time (GMT): 2016/168/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3006566
73 A = 6787849
28 meter
Y = 6059571
35 meter E =
0012960
Z = 477635
24 I = 51
98828
XDOT = -4433
806697 Wp = 47
02931
YDOT = 1718
071487 meter/sec RA = 60
44712 deg
ZDOT = 6018
782686 TA = 318
09958
MA = 318
19869
Ha = 220
111 n
mi
Hp = 214
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9864064
08 X = 2936263
47
Y = 19880483
43 feet Y = 6092799
64 meter
Z = 1567044
74 Z = 492070
39
XDOT = -14546
609898 XDOT = -4481
925954
YDOT = 5636
717476 feet/sec YDOT = 1668
220018 meter/sec
ZDOT = 19746
662356 ZDOT = 5997
127496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16158357
60 X = 4925067
40
Y = -15206699
41 feet Y = -4635001
98 meter
Z = 1628736
82 Z = 496438
98
XDOT = 8551
170304 XDOT = 2606
396709
YDOT = 11223
001651 feet/sec YDOT = 3420
770903 meter/sec
ZDOT = 19651
931598 ZDOT = 5989
908751
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 16168
62582894
00016717 00000-0 10270-3 0 9070
2 25544 51
6448 60
8378 0000701 319
4561 40
6539 15
54602795 4891
Satellite: ISS
Catalog Number: 25544
Epoch time: 16168
62582894 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 60
8378 deg
Eccentricity:
0000701
Arg of perigee: 319
4561 deg
Mean anomaly: 40
6539 deg
Mean motion: 15
54602795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 489
Checksum: 335
Coasting Arc #9 (Orbit 503)
---------------------------------------
Vector Time (GMT): 2016/169/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1986585
90 A = 6785785
91 meter
Y = -6066012
14 meter E =
0005113
Z = -2299668
92 I = 51
96343
XDOT = 5381
066781 Wp = 134
53466
YDOT = 300
127867 meter/sec RA = 55
49595 deg
ZDOT = -5451
073608 TA = 70
95514
MA = 70
89976
Ha = 220
142 n
mi
Hp = 214
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6517670
27 X = -1907435
70
Y = -19901614
62 feet Y = -6087784
63 meter
Z = -7544845
53 Z = -2309127
82
XDOT = 17654
418573 XDOT = 5403
789907
YDOT = 984
671481 feet/sec YDOT = 360
430254 meter/sec
ZDOT = -17884
099765 ZDOT = -5424
878303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16954419
81 X = -5167707
16
Y = 12267718
51 feet Y = 3739200
60 meter
Z = -7584834
57 Z = -2311857
58
XDOT = -3626
313479 XDOT = -1105
300349
YDOT = -15976
396113 feet/sec YDOT = -4869
605535 meter/sec
ZDOT = -17769
989137 ZDOT = -5416
292689
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 16169
59007635
00016717 00000-0 10270-3 0 9083
2 25544 51
6437 56
0282 0000705 318
5733 41
5366 15
54566515 5040
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
59007635 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 56
0282 deg
Eccentricity:
0000705
Arg of perigee: 318
5733 deg
Mean anomaly: 41
5366 deg
Mean motion: 15
54566515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 504
Checksum: 307
Coasting Arc #10 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1352027
12 A = 6777819
75 meter
Y = 4495029
74 meter E =
0006323
Z = 4885643
67 I = 51
92159
XDOT = -5813
138884 Wp = 118
01356
YDOT = -4383
215041 meter/sec RA = 52
10488 deg
ZDOT = 2418
800257 TA = 308
34653
MA = 308
40334
Ha = 220
192 n
mi
Hp = 214
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4435784
53 X = -1425923
69
Y = 14747472
89 feet Y = 4479496
65 meter
Z = 16029014
65 Z = 4878896
92
XDOT = -19071
977967 XDOT = -5775
442194
YDOT = -14380
626774 feet/sec YDOT = -4448
010974 meter/sec
ZDOT = 7935
696380 ZDOT = 2390
652277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6011234
24 X = -1832224
20
Y = 14212690
15 feet Y = 4332027
96 meter
Z = 15998685
98 Z = 4876399
49
XDOT = -16529
620696 XDOT = -5038
228388
YDOT = -15806
515019 feet/sec YDOT = -4817
825778 meter/sec
ZDOT = 7813
913813 ZDOT = 2381
680930
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 16170
29718635
00016717 00000-0 10270-3 0 9092
2 25544 51
6408 52
5004 0000615 328
7691 31
3425 15
54612096 5158
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29718635 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 52
5004 deg
Eccentricity:
0000615
Arg of perigee: 328
7691 deg
Mean anomaly: 31
3425 deg
Mean motion: 15
54612096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 294
Coasting Arc #11 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2794734
44 A = 6776010
33 meter
Y = -3133993
61 meter E =
0014662
Z = -5330716
39 I = 51
89544
XDOT = 5403
896295 Wp = 85
00959
YDOT = 5415
556678 meter/sec RA = 47
11992 deg
ZDOT = -350
358343 TA = 181
65507
MA = 181
65993
Ha = 220
188 n
mi
Hp = 214
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9169076
25 X = 2855466
26
Y = -10282131
28 feet Y = -3102400
70 meter
Z = -17489227
01 Z = -5316993
15
XDOT = 17729
318552 XDOT = 5344
638448
YDOT = 17767
574404 feet/sec YDOT = 5475
655365 meter/sec
ZDOT = -1149
469630 ZDOT = -324
250607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10115307
38 X = 3083145
69
Y = -9464985
72 feet Y = -2884927
65 meter
Z = -17428764
92 Z = -5312287
55
XDOT = 15485
718046 XDOT = 4720
046860
YDOT = 18461
377830 feet/sec YDOT = 5627
027963 meter/sec
ZDOT = -1036
800721 ZDOT = -316
016860
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 16171
26142121
00016717 00000-0 10270-3 0 9103
2 25544 51
6414 47
6901 0000595 340
0872 20
0257 15
54602519 5305
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
26142121 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 47
6901 deg
Eccentricity:
0000595
Arg of perigee: 340
0872 deg
Mean anomaly: 20
0257 deg
Mean motion: 15
54602519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 262
Coasting Arc #12 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5685252
89 A = 6784422
07 meter
Y = -2302054
78 meter E =
0012976
Z = 2886051
50 I = 51
91141
XDOT = -258
195014 Wp = 97
68580
YDOT = -5747
096892 meter/sec RA = 43
68487 deg
ZDOT = -5075
001376 TA = 49
56642
MA = 49
45330
Ha = 220
165 n
mi
Hp = 214
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18652404
50 X = -5673107
42
Y = -7552673
17 feet Y = -2365563
58 meter
Z = 9468672
90 Z = 2858463
06
XDOT = -847
096503 XDOT = -169
258126
YDOT = -18855
304765 feet/sec YDOT = -5749
486173 meter/sec
ZDOT = -16650
266983 ZDOT = -5076
040460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15289584
98 X = 4660265
50
Y = -13169561
70 feet Y = -4014082
41 meter
Z = 9348907
30 Z = 2849546
95
XDOT = 16137
786712 XDOT = 4918
797390
YDOT = 6871
504221 feet/sec YDOT = 2094
434487 meter/sec
ZDOT = -16653
598999 ZDOT = -5076
016975
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 16171
96852018
00016717 00000-0 10270-3 0 9114
2 25544 51
6443 44
1620 0000476 316
9543 43
1573 15
54631968 5411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
96852018 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 44
1620 deg
Eccentricity:
0000476
Arg of perigee: 316
9543 deg
Mean anomaly: 43
1573 deg
Mean motion: 15
54631968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 299
Coasting Arc #13 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5735084
41 A = 6787447
30 meter
Y = 3429991
26 meter E =
0009627
Z = -1162933
59 I = 51
89648
XDOT = -1590
306156 Wp = 33
99610
YDOT = 4645
513297 meter/sec RA = 38
72615 deg
ZDOT = 5890
170491 TA = 313
41933
MA = 313
49942
Ha = 220
188 n
mi
Hp = 214
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18815893
72 X = 5701952
16
Y = 11253252
16 feet Y = 3493939
71 meter
Z = -3815398
91 Z = -1135153
98
XDOT = -5217
539881 XDOT = -1670
747124
YDOT = 15241
185359 feet/sec YDOT = 4627
278780 meter/sec
ZDOT = 19324
706336 ZDOT = 5882
250506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18435129
44 X = -5619027
45
Y = 11904768
00 feet Y = 3628573
29 meter
Z = -3695038
69 Z = -1126247
79
XDOT = -10430
571288 XDOT = -3179
238128
YDOT = -10198
080281 feet/sec YDOT = -3108
374870 meter/sec
ZDOT = 19289
213309 ZDOT = 5879
352216
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 16172
93274175
00016717 00000-0 10270-3 0 9125
2 25544 51
6435 39
3524 0000673 326
6566 33
4544 15
54589745 5564
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
93274175 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 39
3524 deg
Eccentricity:
0000673
Arg of perigee: 326
6566 deg
Mean anomaly: 33
4544 deg
Mean motion: 15
54589745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 323
Coasting Arc #14 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5261218
36 A = 6787578
62 meter
Y = -4216987
44 meter E =
0009877
Z = -739998
87 I = 51
87106
XDOT = 3486
066107 Wp = 139
37917
YDOT = -3310
054130 meter/sec RA = 33
77118 deg
ZDOT = -5974
339886 TA = 48
59267
MA = 48
50782
Ha = 220
089 n
mi
Hp = 213
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17261215
08 X = -5210077
34
Y = -13835260
62 feet Y = -4275535
83 meter
Z = -2427817
83 Z = -765432
84
XDOT = 11437
224760 XDOT = 3551
841498
YDOT = -10859
757644 feet/sec YDOT = -3270
701979 meter/sec
ZDOT = -19600
852643 ZDOT = -5957
246247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19880366
28 X = 6059535
64
Y = -9674138
80 feet Y = -2948677
51 meter
Z = -2537785
83 Z = -773517
12
XDOT = 4169
411425 XDOT = 1270
836602
YDOT = 13647
402952 feet/sec YDOT = 4159
728420 meter/sec
ZDOT = -19525
652607 ZDOT = -5951
418915
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 16173
96123968
00016717 00000-0 10270-3 0 9133
2 25544 51
6427 34
2220 0000485 329
8418 30
2707 15
54642818 5729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16173
96123968 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 34
2220 deg
Eccentricity:
0000485
Arg of perigee: 329
8418 deg
Mean anomaly: 30
2707 deg
Mean motion: 15
54642818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 306
Coasting Arc #15 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4279772
90 A = 6785079
34 meter
Y = 4613519
86 meter E =
0013631
Z = 2519437
66 I = 51
83592
XDOT = -5195
689583 Wp = 73
25899
YDOT = 1907
660720 meter/sec RA = 28
80975 deg
ZDOT = 5312
782037 TA = 314
95243
MA = 315
06289
Ha = 220
099 n
mi
Hp = 213
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14041249
67 X = 4215627
03
Y = 15136220
02 feet Y = 4661020
13 meter
Z = 8265871
58 Z = 2540072
39
XDOT = -17046
225667 XDOT = -5242
442376
YDOT = 6258
729395 feet/sec YDOT = 1849
296933 meter/sec
ZDOT = 17430
387260 ZDOT = 5287
429567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19555059
20 X = -5960382
04
Y = 6510212
68 feet Y = 1984312
82 meter
Z = 8354835
26 Z = 2546553
79
XDOT = 1838
352472 XDOT = 560
329834
YDOT = -16787
749737 feet/sec YDOT = -5116
906120 meter/sec
ZDOT = 17319
485716 ZDOT = 5278
979246
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 16174
98972962
00016717 00000-0 10270-3 0 9143
2 25544 51
6430 29
0907 0000573 341
3122 18
8010 15
54645032 5883
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
98972962 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 29
0907 deg
Eccentricity:
0000573
Arg of perigee: 341
3122 deg
Mean anomaly: 18
8010 deg
Mean motion: 15
54645032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 300
Coasting Arc #16 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2811506
67 A = 6780921
17 meter
Y = -4694779
22 meter E =
0007196
Z = -4012273
47 I = 51
79334
XDOT = 6534
183317 Wp = 66
76997
YDOT = -525
970390 meter/sec RA = 23
83667 deg
ZDOT = -3966
113338 TA = 162
03660
MA = 162
01115
Ha = 220
145 n
mi
Hp = 213
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9224103
25 X = -2739309
81
Y = -15402818
95 feet Y = -4725815
20 meter
Z = -13163626
85 Z = -4025756
14
XDOT = 21437
609307 XDOT = 6558
844702
YDOT = -1725
624640 feet/sec YDOT = -452
762434 meter/sec
ZDOT = -13012
182868 ZDOT = -3934
312371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17764340
47 X = 5414570
97
Y = -2287969
79 feet Y = -697373
19 meter
Z = -13221398
81 Z = -4029882
36
XDOT = -7108
028469 XDOT = -2166
527077
YDOT = 19148
661032 feet/sec YDOT = 5836
511883 meter/sec
ZDOT = -12873
469758 ZDOT = -3923
833582
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 16175
95393341
00016717 00000-0 10270-3 0 9150
2 25544 51
6428 24
2807 0000609 351
9110 8
2033 15
54653718 6036
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
95393341 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 24
2807 deg
Eccentricity:
0000609
Arg of perigee: 351
9110 deg
Mean anomaly: 8
2033 deg
Mean motion: 15
54653718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 290
Coasting Arc #17 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1008035
47 A = 6777195
99 meter
Y = 4487515
53 meter E =
0005702
Z = 4974116
45 I = 51
75070
XDOT = -7333
091504 Wp = 117
86444
YDOT = -724
672119 meter/sec RA = 18
84937 deg
ZDOT = 2135
405106 TA = 311
35288
MA = 311
40192
Ha = 220
098 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3307202
97 X = 933618
14
Y = 14722819
98 feet Y = 4498371
45 meter
Z = 16319279
70 Z = 4978832
90
XDOT = -24058
699161 XDOT = -7334
815806
YDOT = -2377
533200 feet/sec YDOT = -806
685495 meter/sec
ZDOT = 7005
922264 ZDOT = 2099
778860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14835543
11 X = -4521873
54
Y = -2639188
85 feet Y = -804424
76 meter
Z = 16338887
74 Z = 4980092
98
XDOT = 11173
520028 XDOT = 3405
688905
YDOT = -20305
969019 feet/sec YDOT = -6189
259357 meter/sec
ZDOT = 6850
806686 ZDOT = 2088
125878
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 16176
98241091
00016717 00000-0 10270-3 0 9169
2 25544 51
6422 19
1501 0000653 350
8776 9
2365 15
54676574 6190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
98241091 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 19
1501 deg
Eccentricity:
0000653
Arg of perigee: 350
8776 deg
Mean anomaly: 9
2365 deg
Mean motion: 15
54676574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 619
Checksum: 313
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