[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 30th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
152/21:55:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
1
153/10:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
2
155/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 216
3
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1883)
---------------------------------------
Vector Time (GMT): 2017/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2775666
22 A = 6778025
22 meter
Y = 3173071
36 meter E =
0013360
Z = -5318434
74 I = 51
89864
XDOT = -5269
916020 Wp = 113
18074
YDOT = 5530
740551 meter/sec RA = 130
40768 deg
ZDOT = 545
359809 TA = 162
03453
MA = 161
98726
Ha = 221
239 n
mi
Hp = 215
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9106516
48 X = 2765812
21
Y = 10410339
11 feet Y = 3204056
27 meter
Z = -17448932
87 Z = -5304974
94
XDOT = -17289
750721 XDOT = -5334
019635
YDOT = 18145
474248 feet/sec YDOT = 5471
450293 meter/sec
ZDOT = 1789
238219 ZDOT = 519
605086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13233805
49 X = 4033663
91
Y = -4268747
64 feet Y = -1301114
28 meter
Z = -17390032
97 Z = -5300482
05
XDOT = 9367
158326 XDOT = 2855
109858
YDOT = 22163
276582 feet/sec YDOT = 6755
366702 meter/sec
ZDOT = 1674
687671 ZDOT = 510
444802
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 17149
51522555
00016717 00000-0 10270-3 0 9009
2 25544 51
6372 131
3943 0004808 209
8754 150
2125 15
53929067 18849
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
51522555 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 131
3943 deg
Eccentricity:
0004808
Arg of perigee: 209
8754 deg
Mean anomaly: 150
2125 deg
Mean motion: 15
53929067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1884
Checksum: 312
Coasting Arc #2 (Orbit 1899)
---------------------------------------
Vector Time (GMT): 2017/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1594142
15 A = 6779651
60 meter
Y = -4392998
86 meter E =
0003001
Z = 4908881
99 I = 51
92481
XDOT = 5600
766228 Wp = 99
62832
YDOT = -4676
081667 meter/sec RA = 125
43048 deg
ZDOT = -2365
096626 TA = 13
43695
MA = 13
42896
Ha = 221
125 n
mi
Hp = 215
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5230125
18 X = -1568744
95
Y = -14412725
91 feet Y = -4410684
12 meter
Z = 16105255
88 Z = 4901199
39
XDOT = 18375
217285 XDOT = 5664
127620
YDOT = -15341
475286 feet/sec YDOT = -4613
095596 meter/sec
ZDOT = -7759
503367 ZDOT = -2337
736401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15354156
63 X = -4679946
94
Y = -631877
01 feet Y = -192596
11 meter
Z = 16072048
72 Z = 4898760
45
XDOT = -7100
673130 XDOT = -2164
285170
YDOT = -21795
706775 feet/sec YDOT = -6643
331425 meter/sec
ZDOT = -7637
983877 ZDOT = -2328
057486
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 17150
54417558
00016717 00000-0 10270-3 0 9011
2 25544 51
6372 126
2666 0004856 215
0615 145
0218 15
53953100 19001
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
54417558 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 126
2666 deg
Eccentricity:
0004856
Arg of perigee: 215
0615 deg
Mean anomaly: 145
0218 deg
Mean motion: 15
53953100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1900
Checksum: 286
Coasting Arc #3 (Orbit 1914)
---------------------------------------
Vector Time (GMT): 2017/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 464012
98 A = 6782998
52 meter
Y = 5438666
97 meter E =
0006985
Z = -4034381
14 I = 51
95490
XDOT = -5600
697121 Wp = 147
74469
YDOT = 3414
928576 meter/sec RA = 120
46115 deg
ZDOT = 3956
837236 TA = 163
25226
MA = 163
22918
Ha = 220
927 n
mi
Hp = 216
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1522352
31 X = 422758
95
Y = 17843395
58 feet Y = 5443625
54 meter
Z = -13236158
60 Z = -4032226
87
XDOT = -18374
990553 XDOT = -5657
687871
YDOT = 11203
833910 feet/sec YDOT = 3351
978809 meter/sec
ZDOT = 12981
749462 ZDOT = 3929
492632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17173866
70 X = 5234594
57
Y = 5098142
80 feet Y = 1553913
92 meter
Z = -13227526
58 Z = -4031750
10
XDOT = 3962
610066 XDOT = 1207
803548
YDOT = 20040
987399 feet/sec YDOT = 6108
492959 meter/sec
ZDOT = 12860
485693 ZDOT = 3919
876039
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 17151
50881279
00016717 00000-0 10270-3 0 9024
2 25544 51
6382 121
4592 0004748 218
7060 141
3752 15
53939225 19151
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
50881279 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 121
4592 deg
Eccentricity:
0004748
Arg of perigee: 218
7060 deg
Mean anomaly: 141
3752 deg
Mean motion: 15
53939225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1915
Checksum: 309
Coasting Arc #4 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2017/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 558997
00 A = 6786586
04 meter
Y = -6170320
33 meter E =
0011618
Z = 2752830
34 I = 51
98265
XDOT = 5357
265891 Wp = 120
83396
YDOT = -1829
221675 meter/sec RA = 115
50237 deg
ZDOT = -5177
619786 TA = 28
14188
MA = 28
07914
Ha = 220
768 n
mi
Hp = 216
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1833979
67 X = 614581
67
Y = -20243833
09 feet Y = -6163758
64 meter
Z = 9031595
61 Z = 2755680
37
XDOT = 17576
331665 XDOT = 5402
472950
YDOT = -6001
383449 feet/sec YDOT = -1769
059977 meter/sec
ZDOT = -16986
941554 ZDOT = -5151
486119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18308764
89 X = -5580511
54
Y = -8815882
62 feet Y = -2687081
02 meter
Z = 9045182
20 Z = 2756971
53
XDOT = -6
254070 XDOT = -1
906241
YDOT = -17331
860062 feet/sec YDOT = -5282
750947 meter/sec
ZDOT = -16871
268242 ZDOT = -5142
362560
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 17152
53775594
00016717 00000-0 10270-3 0 9031
2 25544 51
6381 116
3310 0004688 223
5232 136
5551 15
53963522 19317
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
53775594 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 116
3310 deg
Eccentricity:
0004688
Arg of perigee: 223
5232 deg
Mean anomaly: 136
5551 deg
Mean motion: 15
53963522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 302
Coasting Arc #5 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2017/152/21:55:41
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1620998
05 A = 6781653
27 meter
Y = 4908272
23 meter E =
0008544
Z = -4398458
95 I = 51
97084
XDOT = -4968
212467 Wp = 143
51368
YDOT = 4716
223456 meter/sec RA = 113
44559 deg
ZDOT = 3428
624684 TA = 161
12782
MA = 161
09613
Ha = 220
830 n
mi
Hp = 216
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5318235
08 X = 1587357
61
Y = 16103255
33 feet Y = 4926211
51 meter
Z = -14430639
58 Z = -4390666
00
XDOT = -16299
909667 XDOT = -5037
235892
YDOT = 15473
174067 feet/sec YDOT = 4660
279383 meter/sec
ZDOT = 11248
768649 ZDOT = 3404
323231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14280095
19 X = -4352573
01
Y = -9200328
64 feet Y = -2804260
17 meter
Z = -14397036
15 Z = -4388216
62
XDOT = 2459
944268 XDOT = 749
791013
YDOT = -21268
394423 feet/sec YDOT = -6482
606620 meter/sec
ZDOT = 11140
708623 ZDOT = 3395
687988
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 17152
92360889
00016717 00000-0 10270-3 0 9042
2 25544 51
6370 114
4046 0004942 221
1279 138
9501 15
53965499 19370
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
92360889 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 114
4046 deg
Eccentricity:
0004942
Arg of perigee: 221
1279 deg
Mean anomaly: 138
9501 deg
Mean motion: 15
53965499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 326
Coasting Arc #6 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4401487
68 A = 6778684
14 meter
Y = 239931
95 meter E =
0006120
Z = 5150715
82 I = 51
96789
XDOT = 1466
621478 Wp = 174
95354
YDOT = -7355
994195 meter/sec RA = 110
81894 deg
ZDOT = 1589
866053 TA = 259
74892
MA = 259
81793
Ha = 220
743 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14440576
37 X = -4428863
30
Y = 787178
31 feet Y = 190558
15 meter
Z = 16898673
95 Z = 5129268
18
XDOT = 4811
750257 XDOT = 1541
046308
YDOT = -24133
839224 feet/sec YDOT = -7339
177404 meter/sec
ZDOT = 5216
095976 ZDOT = 1597
170792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8182274
91 X = -2493957
39
Y = 12057901
96 feet Y = 3675248
52 meter
Z = 16803941
64 Z = 5121841
41
XDOT = -15435
036543 XDOT = -4704
599138
YDOT = -17817
685844 feet/sec YDOT = -5430
830645 meter/sec
ZDOT = 5249
555249 ZDOT = 1600
064440
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 17153
50238781
00016717 00000-0 10270-3 0 9053
2 25544 51
6373 111
5239 0004772 227
1825 132
8927 15
53962858 19460
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50238781 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 111
5239 deg
Eccentricity:
0004772
Arg of perigee: 227
1825 deg
Mean anomaly: 132
8927 deg
Mean motion: 15
53962858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 327
Coasting Arc #7 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2017/154/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927136
16 A = 6777867
61 meter
Y = 1454102
17 meter E =
0011727
Z = -5339170
34 I = 51
97658
XDOT = -2306
026788 Wp = 107
89529
YDOT = 7298
976138 meter/sec RA = 105
84330 deg
ZDOT = 288
704446 TA = 164
86459
MA = 164
82948
Ha = 220
542 n
mi
Hp = 216
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12884304
99 X = 3936519
41
Y = 4770676
41 feet Y = 1498070
86 meter
Z = -17516963
05 Z = -5320070
50
XDOT = -7565
704685 XDOT = -2388
876860
YDOT = 23946
772107 feet/sec YDOT = 7272
725324 meter/sec
ZDOT = 947
193063 ZDOT = 277
301616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11535739
64 X = 3516093
44
Y = -7657042
56 feet Y = -2333866
57 meter
Z = -17432873
36 Z = -5313539
80
XDOT = 14266
657136 XDOT = 4348
477095
YDOT = 19431
976293 feet/sec YDOT = 5922
866374 meter/sec
ZDOT = 895
633442 ZDOT = 272
989073
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 17154
46701668
00016717 00000-0 10270-3 0 9069
2 25544 51
6380 106
7158 0004746 230
4452 129
6290 15
53961308 19611
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
46701668 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 106
7158 deg
Eccentricity:
0004746
Arg of perigee: 230
4452 deg
Mean anomaly: 129
6290 deg
Mean motion: 15
53961308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 314
Coasting Arc #8 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2017/155/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3382372
27 A = 6779267
90 meter
Y = -3090618
14 meter E =
0001474
Z = 4995716
42 I = 51
98982
XDOT = 2992
415787 Wp = 61
93933
YDOT = -6729
810782 meter/sec RA = 100
86987 deg
ZDOT = -2136
240180 TA = 48
77201
MA = 48
75931
Ha = 220
450 n
mi
Hp = 216
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11097021
89 X = -3371827
78
Y = -10139823
28 feet Y = -3128383
50 meter
Z = 16390145
73 Z = 4979311
12
XDOT = 9817
637096 XDOT = 3077
824809
YDOT = -22079
431698 feet/sec YDOT = -6695
869862 meter/sec
ZDOT = -7008
662009 ZDOT = -2121
496816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14748025
87 X = -4495198
28
Y = 3287541
37 feet Y = 1002042
61 meter
Z = 16318228
85 Z = 4973796
15
XDOT = -12084
226938 XDOT = -3683
272371
YDOT = -19731
559728 feet/sec YDOT = -6014
179405 meter/sec
ZDOT = -6942
430052 ZDOT = -2116
052680
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 17155
49594986
00016717 00000-0 10270-3 0 9077
2 25544 51
6384 101
5877 0004723 235
7229 124
3477 15
53978316 19774
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
49594986 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 101
5877 deg
Eccentricity:
0004723
Arg of perigee: 235
7229 deg
Mean anomaly: 124
3477 deg
Mean motion: 15
53978316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 355
Coasting Arc #9 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2017/155/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2413825
02 A = 6782606
70 meter
Y = -4802922
52 meter E =
0006359
Z = 4130715
24 I = 52
00356
XDOT = 3996
895946 Wp = 91
70707
YDOT = -5307
926222 meter/sec RA = 100
20872 deg
ZDOT = -3831
191861 TA = 37
65043
MA = 37
60593
Ha = 220
432 n
mi
Hp = 216
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7919373
44 X = -2380003
29
Y = -15757619
81 feet Y = -4829726
73 meter
Z = 13552215
35 Z = 4119071
30
XDOT = 13113
175675 XDOT = 4074
563762
YDOT = -17414
456108 feet/sec YDOT = -5262
795686 meter/sec
ZDOT = -12569
527102 ZDOT = -3811
587697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13681307
21 X = -4170062
44
Y = 11189723
68 feet Y = 3410627
78 meter
Z = 13501611
59 Z = 4115291
21
XDOT = -19016
957918 XDOT = -5796
368773
YDOT = -8171
022343 feet/sec YDOT = -2490
527610 meter/sec
ZDOT = -12482
069637 ZDOT = -3804
534825
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 17155
62456727
00016717 00000-0 10270-3 0 9083
2 25544 51
6402 100
9480 0004656 235
7712 124
2999 15
53969005 19795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
62456727 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 100
9480 deg
Eccentricity:
0004656
Arg of perigee: 235
7712 deg
Mean anomaly: 124
2999 deg
Mean motion: 15
53969005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 332
Coasting Arc #10 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1722758
88 A = 6786214
64 meter
Y = 5894410
62 meter E =
0000315
Z = -2888498
04 I = 52
02121
XDOT = -4331
484461 Wp = 169
47053
YDOT = 3757
653939 meter/sec RA = 95
25141 deg
ZDOT = 5084
453642 TA = 157
84749
MA = 157
84613
Ha = 220
149 n
mi
Hp = 216
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5652096
05 X = 1670749
08
Y = 19338617
53 feet Y = 5913385
12 meter
Z = -9476699
60 Z = -2880255
13
XDOT = -14210
907024 XDOT = -4397
879702
YDOT = 12328
260956 feet/sec YDOT = 3708
844680 meter/sec
ZDOT = 16681
278354 ZDOT = 5063
251413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17500401
10 X = 5334122
26
Y = -10016675
02 feet Y = -3053082
55 meter
Z = -9441310
08 Z = -2877711
31
XDOT = 14567
522181 XDOT = 4440
180761
YDOT = 9816
400951 feet/sec YDOT = 2992
039010 meter/sec
ZDOT = 16587
013208 ZDOT = 5055
721626
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 17156
58918925
00016717 00000-0 10270-3 0 9093
2 25544 51
6408 96
1401 0004718 239
8523 120
2162 15
53992034 19947
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58918925 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 96
1401 deg
Eccentricity:
0004718
Arg of perigee: 239
8523 deg
Mean anomaly: 120
2162 deg
Mean motion: 15
53992034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 324
Coasting Arc #11 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1544297
62 A = 6788972
70 meter
Y = 6466412
93 meter E =
0008863
Z = 1353812
38 I = 52
02825
XDOT = -4404
912317 Wp = 59
45895
YDOT = -2281
004910 meter/sec RA = 94
28662 deg
ZDOT = 5846
422909 TA = 315
20333
MA = 315
27486
Ha = 220
122 n
mi
Hp = 216
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5066593
24 X = -1623068
21
Y = 21215265
51 feet Y = 6448702
99 meter
Z = 4441641
67 Z = 1346119
80
XDOT = -14451
812065 XDOT = -4407
477561
YDOT = -7483
611909 feet/sec YDOT = -2330
278477 meter/sec
ZDOT = 19181
177524 ZDOT = 5825
018500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6554746
99 X = 1997886
88
Y = -20811139
45 feet Y = -6343235
30 meter
Z = 4406563
86 Z = 1343120
67
XDOT = 12505
148334 XDOT = 3811
569212
YDOT = 7996
959785 feet/sec YDOT = 2437
473342 meter/sec
ZDOT = 19087
053164 ZDOT = 5817
733804
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 17156
84641938
00016717 00000-0 10270-3 0 9101
2 25544 51
6380 94
8562 0004945 240
8969 119
1689 15
53988523 19980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84641938 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 94
8562 deg
Eccentricity:
0004945
Arg of perigee: 240
8969 deg
Mean anomaly: 119
1689 deg
Mean motion: 15
53988523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 365
Coasting Arc #12 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2194709
46 A = 6786187
38 meter
Y = -5728649
75 meter E =
0004076
Z = -2895744
94 I = 52
02079
XDOT = 4014
395757 Wp = 183
76875
YDOT = 4104
526518 meter/sec RA = 89
33839 deg
ZDOT = -5080
986772 TA = 29
02008
MA = 28
99743
Ha = 220
012 n
mi
Hp = 216
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7200490
35 X = 2272671
90
Y = -18794782
65 feet Y = -5703670
81 meter
Z = -9500475
53 Z = -2884894
81
XDOT = 13170
589754 XDOT = 3992
880780
YDOT = 13466
294352 feet/sec YDOT = 4149
298441 meter/sec
ZDOT = -16669
904108 ZDOT = -5061
537645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8233435
52 X = -2509551
15
Y = 18390987
30 feet Y = 5605572
93 meter
Z = -9451564
79 Z = -2880836
95
XDOT = -11217
261958 XDOT = -3419
021445
YDOT = -13539
112389 feet/sec YDOT = -4126
721456 meter/sec
ZDOT = -16584
733781 ZDOT = -5055
026857
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 17157
81103821
00016717 00000-0 10270-3 0 9114
2 25544 51
6383 90
0482 0004848 245
4545 114
6103 15
53998298 20135
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81103821 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 90
0482 deg
Eccentricity:
0004848
Arg of perigee: 245
4545 deg
Mean anomaly: 114
6103 deg
Mean motion: 15
53998298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 303
Coasting Arc #13 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2796251
58 A = 6782496
62 meter
Y = 4587642
13 meter E =
0007027
Z = 4137846
32 I = 52
00718
XDOT = -3551
765859 Wp = 127
35457
YDOT = -5618
989596 meter/sec RA = 84
38100 deg
ZDOT = 3821
008146 TA = 283
38248
MA = 283
46080
Ha = 219
864 n
mi
Hp = 216
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9174053
74 X = -2867443
86
Y = 15051319
34 feet Y = 4555974
00 meter
Z = 13575611
29 Z = 4124090
45
XDOT = -11652
775129 XDOT = -3507
229692
YDOT = -18435
005236 feet/sec YDOT = -5658
459289 meter/sec
ZDOT = 12536
115963 ZDOT = 3803
862039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9783757
19 X = 2982089
19
Y = -14719074
39 feet Y = -4486373
87 meter
Z = 13514053
50 Z = 4119083
51
XDOT = 10008
611733 XDOT = 3050
624856
YDOT = 18119
906778 feet/sec YDOT = 5522
947586 meter/sec
ZDOT = 12461
390701 ZDOT = 3798
231886
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 17158
83996006
00016717 00000-0 10270-3 0 9123
2 25544 51
6383 84
9193 0004951 248
7587 111
3037 15
54004647 20297
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
83996006 = yrday
fracday
Element set: 912
Inclination: 51
6383 deg
RA of node: 84
9193 deg
Eccentricity:
0004951
Arg of perigee: 248
7587 deg
Mean anomaly: 111
3037 deg
Mean motion: 15
54004647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 324
Coasting Arc #14 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3381871
90 A = 6779252
89 meter
Y = -3118467
04 meter E =
0007766
Z = -4986695
11 I = 51
99183
XDOT = 2984
191976 Wp = 76
66867
YDOT = 6713
309303 meter/sec RA = 79
41475 deg
ZDOT = -2175
499214 TA = 172
21533
MA = 172
20327
Ha = 219
860 n
mi
Hp = 216
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11095380
23 X = 3440715
25
Y = -10231191
08 feet Y = -3080318
98 meter
Z = -16360548
25 Z = -4970124
32
XDOT = 9790
656090 XDOT = 2919
467826
YDOT = 22025
292988 feet/sec YDOT = 6746
318954 meter/sec
ZDOT = -7137
464613 ZDOT = -2161
159078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11382459
99 X = -3469373
80
Y = 10031537
68 feet Y = 3057612
69 meter
Z = -16286808
43 Z = -4964219
21
XDOT = -8711
767892 XDOT = -2655
346853
YDOT = -21366
327766 feet/sec YDOT = -6512
456703 meter/sec
ZDOT = -7075
338198 ZDOT = -2156
563083
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 17159
80457280
00016717 00000-0 10270-3 0 9138
2 25544 51
6380 80
1121 0004713 249
9948 110
0697 15
54004752 20445
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
80457280 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 80
1121 deg
Eccentricity:
0004713
Arg of perigee: 249
9948 deg
Mean anomaly: 110
0697 deg
Mean motion: 15
54004752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 297
Coasting Arc #15 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3527779
44 A = 6778578
06 meter
Y = 2683307
97 meter E =
0004619
Z = 5130352
82 I = 51
99180
XDOT = -2819
292913 Wp = 187
10980
YDOT = -6928
738381 meter/sec RA = 77
97352 deg
ZDOT = 1680
983382 TA = 246
70918
MA = 246
75780
Ha = 219
804 n
mi
Hp = 216
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11574079
54 X = -3582443
71
Y = 8803503
84 feet Y = 2643551
60 meter
Z = 16831866
21 Z = 5113083
37
XDOT = -9249
648664 XDOT = -2749
769886
YDOT = -22732
081302 feet/sec YDOT = -6959
877126 meter/sec
ZDOT = 5515
037343 ZDOT = 1667
455898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11332277
74 X = -3454078
25
Y = -9253014
83 feet Y = -2820318
92 meter
Z = 16755116
09 Z = 5106959
38
XDOT = 19194
434212 XDOT = 5850
463548
YDOT = -13601
429820 feet/sec YDOT = -4145
715809 meter/sec
ZDOT = 5456
542483 ZDOT = 1663
154149
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 17160
12610794
00016717 00000-0 10270-3 0 9147
2 25544 51
6417 78
5112 0005032 250
8855 109
1753 15
54021934 20498
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12610794 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 78
5112 deg
Eccentricity:
0005032
Arg of perigee: 250
8855 deg
Mean anomaly: 109
1753 deg
Mean motion: 15
54021934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 289
Coasting Arc #16 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4061803
68 A = 6777768
36 meter
Y = -998870
27 meter E =
0010139
Z = -5341774
80 I = 51
98063
XDOT = 2084
696285 Wp = 99
44322
YDOT = 7369
092944 meter/sec RA = 72
99935 deg
ZDOT = 205
922483 TA = 172
51961
MA = 172
50447
Ha = 219
628 n
mi
Hp = 216
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13326127
57 X = 4098619
36
Y = -3277133
43 feet Y = -953241
81 meter
Z = -17525507
86 Z = -5321954
38
XDOT = 6839
554742 XDOT = 2001
137938
YDOT = 24176
814122 feet/sec YDOT = 7391
938197 meter/sec
ZDOT = 675
598699 ZDOT = 215
847488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6592863
17 X = 2009504
69
Y = 12162498
56 feet Y = 3707129
56 meter
Z = -17437789
12 Z = -5315038
12
XDOT = -20752
755750 XDOT = -6325
439953
YDOT = 12284
967698 feet/sec YDOT = 3744
458154 meter/sec
ZDOT = 718
089882 ZDOT = 218
873796
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 17161
09071558
00016717 00000-0 10270-3 0 9154
2 25544 51
6413 73
7040 0005006 255
6494 104
4103 15
53991526 20640
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09071558 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 73
7040 deg
Eccentricity:
0005006
Arg of perigee: 255
6494 deg
Mean anomaly: 104
4103 deg
Mean motion: 15
53991526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 288
Coasting Arc #17 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4508471
55 A = 6779022
46 meter
Y = -691673
24 meter E =
0002511
Z = 5015647
18 I = 51
97553
XDOT = -1191
496886 Wp = 4
23882
YDOT = -7285
151810 meter/sec RA = 68
02527 deg
ZDOT = -2073
155213 TA = 105
84898
MA = 105
82130
Ha = 219
567 n
mi
Hp = 216
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14791573
31 X = -4524765
66
Y = -2269269
15 feet Y = -742181
87 meter
Z = 16455535
38 Z = 4993706
64
XDOT = -3909
110517 XDOT = -1099
873433
YDOT = -23901
416700 feet/sec YDOT = -7297
963332 meter/sec
ZDOT = -6801
690330 ZDOT = -2078
721698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1858054
97 X = -566335
15
Y = -14955383
87 feet Y = -4558401
00 meter
Z = 16358758
91 Z = 4986149
71
XDOT = 20867
394097 XDOT = 6360
381721
YDOT = -10066
969909 feet/sec YDOT = -3068
412428 meter/sec
ZDOT = -6824
933856 ZDOT = -2080
239839
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 17162
11962302
00016717 00000-0 10270-3 0 9165
2 25544 51
6420 68
5763 0004985 260
5024 99
5565 15
54046060 20800
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
11962302 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 68
5763 deg
Eccentricity:
0004985
Arg of perigee: 260
5024 deg
Mean anomaly: 99
5565 deg
Mean motion: 15
54046060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 299
Coasting Arc #18 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829400
28 A = 6782218
94 meter
Y = 2252760
13 meter E =
0004085
Z = -4199681
99 I = 51
97198
XDOT = 125
946247 Wp = 139
39498
YDOT = 6691
220662 meter/sec RA = 63
05684 deg
ZDOT = 3733
101073 TA = 168
81155
MA = 168
80247
Ha = 219
464 n
mi
Hp = 216
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15844489
12 X = 4824250
43
Y = 7390945
29 feet Y = 2306737
56 meter
Z = -13778484
23 Z = -4176234
40
XDOT = 413
209472 XDOT = 32
980296
YDOT = 21952
823694 feet/sec YDOT = 6692
108734 meter/sec
ZDOT = 12247
706932 ZDOT = 3733
488049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2492350
41 X = -759668
41
Y = 17386598
34 feet Y = 5299435
17 meter
Z = -13675339
96 Z = -4168243
62
XDOT = -19661
760314 XDOT = -5992
904544
YDOT = 6817
797149 feet/sec YDOT = 2078
064571 meter/sec
ZDOT = 12248
172428 ZDOT = 3733
242956
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 17163
08422296
00016717 00000-0 10270-3 0 9176
2 25544 51
6409 63
7692 0004684 263
6710 96
3909 15
54042268 20956
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
08422296 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 63
7692 deg
Eccentricity:
0004684
Arg of perigee: 263
6710 deg
Mean anomaly: 96
3909 deg
Mean motion: 15
54042268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 326
Coasting Arc #19 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4947503
75 A = 6785901
43 meter
Y = -3576550
53 meter E =
0008462
Z = 2953325
88 I = 51
96902
XDOT = 1098
247759 Wp = 103
23184
YDOT = -5682
405595 meter/sec RA = 58
09655 deg
ZDOT = -5031
519560 TA = 43
20400
MA = 43
13765
Ha = 219
388 n
mi
Hp = 216
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16231967
68 X = -4921487
91
Y = -11734089
66 feet Y = -3631731
80 meter
Z = 9689389
38 Z = 2929355
16
XDOT = 3603
175063 XDOT = 1186
148919
YDOT = -18643
062976 feet/sec YDOT = -5669
632073 meter/sec
ZDOT = -16507
610105 ZDOT = -5025
971893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6220887
15 X = 1896126
40
Y = -19091722
98 feet Y = -5819157
16 meter
Z = 9584183
74 Z = 2921259
20
XDOT = 17497
695854 XDOT = 5333
297696
YDOT = -2589
594605 feet/sec YDOT = -789
308436 meter/sec
ZDOT = -16482
042618 ZDOT = -5023
726590
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 17164
11312255
00016717 00000-0 10270-3 0 9185
2 25544 51
6410 58
6410 0004890 269
1541 90
9051 15
54063102 21118
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
11312255 = yrday
fracday
Element set: 918
Inclination: 51
6410 deg
RA of node: 58
6410 deg
Eccentricity:
0004890
Arg of perigee: 269
1541 deg
Mean anomaly: 90
9051 deg
Mean motion: 15
54063102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 267
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