[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 3rd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
216/02:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
3
219/05:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
3
221/12:26:03
547 -0
5 0
8 0
8
N/A 0
6 -0
1 222
8
000/00:02:03
094 0
0 -0
0 213
0
225/16:27:14
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
2
225/21:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2017/214/13:45:06
165
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1533431
05 A = 6777103
31 meter
Y = 3941286
97 meter E =
0020806
Z = -5313663
44 I = 51
70517
XDOT = -7311
284522 Wp = 88
58910
YDOT = 2212
775070 meter/sec RA = 165
94452 deg
ZDOT = -469
726569 TA = 176
93201
MA = 176
91923
Ha = 223
043 n
mi
Hp = 212
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5030941
78 X = 1515055
49
Y = 12930731
53 feet Y = 3958332
39 meter
Z = -17433278
99 Z = -5306258
99
XDOT = -23987
153945 XDOT = -7333
203291
YDOT = 7259
760727 feet/sec YDOT = 2130
892789 meter/sec
ZDOT = -1541
097666 ZDOT = -505
295297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 375281
76 X = 114385
88
Y = -13910244
93 feet Y = -4239842
66 meter
Z = -17401082
11 Z = -5303849
83
XDOT = 23881
035184 XDOT = 7278
939524
YDOT = 2764
872971 feet/sec YDOT = 842
733282 meter/sec
ZDOT = -1698
766245 ZDOT = -517
783952
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 17214
58998150
00016717 00000-0 10270-3 0 9007
2 25544 51
6394 167
0103 0006106 93
3583 266
8268 15
54248019 28964
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
58998150 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 167
0103 deg
Eccentricity:
0006106
Arg of perigee: 93
3583 deg
Mean anomaly: 266
8268 deg
Mean motion: 15
54248019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 325
Coasting Arc #2 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2017/215/13:45:06
165
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 280802
23 A = 6777650
15 meter
Y = -4391351
07 meter E =
0009957
Z = 5146961
60 I = 51
73846
XDOT = 7412
695850 Wp = 78
98181
YDOT = -1300
189079 meter/sec RA = 160
95052 deg
ZDOT = -1509
393483 TA = 25
54643
MA = 25
49726
Ha = 222
987 n
mi
Hp = 212
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 921267
14 X = 304885
49
Y = -14407319
77 feet Y = -4388076
60 meter
Z = 16886356
96 Z = 5148383
86
XDOT = 24319
868275 XDOT = 7434
015789
YDOT = -4265
712203 feet/sec YDOT = -1217
175980 meter/sec
ZDOT = -4952
078357 ZDOT = -1473
333625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6207136
60 X = -1891935
23
Y = 13025257
57 feet Y = 3970098
51 meter
Z = 16893275
82 Z = 5149070
47
XDOT = -23203
261274 XDOT = -7072
354036
YDOT = -4823
507308 feet/sec YDOT = -1470
205028 meter/sec
ZDOT = -4792
343147 ZDOT = -1460
706191
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 17215
61873652
00016717 00000-0 10270-3 0 9012
2 25544 51
6391 161
8821 0006024 96
5391 263
6447 15
54265652 29126
Satellite: ISS
Catalog Number: 25544
Epoch time: 17215
61873652 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 161
8821 deg
Eccentricity:
0006024
Arg of perigee: 96
5391 deg
Mean anomaly: 263
6447 deg
Mean motion: 15
54265652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 312
Coasting Arc #3 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -21723
93 A = 6777671
98 meter
Y = 4399384
37 meter E =
0019842
Z = -5173403
89 I = 51
75584
XDOT = -7321
669574 Wp = 101
78095
YDOT = 1682
857586 meter/sec RA = 158
22876 deg
ZDOT = 1462
622111 TA = 182
29728
MA = 182
30641
Ha = 222
984 n
mi
Hp = 212
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -71272
74 X = -45787
87
Y = 14433675
77 feet Y = 4399007
21 meter
Z = -16973109
88 Z = -5173567
60
XDOT = -24021
225636 XDOT = -7347
048179
YDOT = 5521
186306 feet/sec YDOT = 1600
839713 meter/sec
ZDOT = 4798
628974 ZDOT = 1426
994643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1217170
92 X = -370993
70
Y = 14380843
41 feet Y = 4383281
07 meter
Z = -16974462
37 Z = -5173816
13
XDOT = -23392
955486 XDOT = -7130
172832
YDOT = 3494
666213 feet/sec YDOT = 1065
174262 meter/sec
ZDOT = 4640
739505 ZDOT = 1414
497401
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 17216
13311327
00016717 00000-0 10270-3 0 9027
2 25544 51
6398 159
3152 0006011 102
6660 257
5165 15
54249550 29203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13311327 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 159
3152 deg
Eccentricity:
0006011
Arg of perigee: 102
6660 deg
Mean anomaly: 257
5165 deg
Mean motion: 15
54249550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 284
Coasting Arc #4 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1730334
77 A = 6780399
74 meter
Y = -4799163
87 meter E =
0014216
Z = 4454986
79 I = 51
79638
XDOT = 6908
014739 Wp = 83
66899
YDOT = -578
389336 meter/sec RA = 153
24155 deg
ZDOT = -3295
633070 TA = 39
50214
MA = 39
39860
Ha = 222
848 n
mi
Hp = 212
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5676951
34 X = 1762231
90
Y = -15745288
29 feet Y = -4779636
00 meter
Z = 14616098
39 Z = 4463469
29
XDOT = 22664
090351 XDOT = 6929
977336
YDOT = -1897
602808 feet/sec YDOT = -501
016234 meter/sec
ZDOT = -10812
444454 ZDOT = -3262
023304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6668594
46 X = 2032587
59
Y = -15315117
13 feet Y = -4668047
70 meter
Z = 14654325
21 Z = 4466638
32
XDOT = 21694
731104 XDOT = 6612
554040
YDOT = -790
086775 feet/sec YDOT = -240
818449 meter/sec
ZDOT = -10663
619350 ZDOT = -3250
271178
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 17217
16186581
00016717 00000-0 10270-3 0 9034
2 25544 51
6409 154
1856 0005885 106
1582 254
0219 15
54282291 29368
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16186581 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 154
1856 deg
Eccentricity:
0005885
Arg of perigee: 106
1582 deg
Mean anomaly: 254
0219 deg
Mean motion: 15
54282291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 316
Coasting Arc #5 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2017/218/02:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3190657
30 A = 6784284
81 meter
Y = 5010830
28 meter E =
0010472
Z = -3287612
49 I = 51
83758
XDOT = -5970
332379 Wp = 99
08301
YDOT = -694
337795 meter/sec RA = 148
26717 deg
ZDOT = 4747
267119 TA = 222
90314
MA = 222
98488
Ha = 222
919 n
mi
Hp = 212
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10468035
75 X = -3230483
28
Y = 16439731
90 feet Y = 4974927
65 meter
Z = -10786130
23 Z = -3303207
93
XDOT = -19587
704655 XDOT = -5985
183849
YDOT = -2278
011137 feet/sec YDOT = -761
185367 meter/sec
ZDOT = 15575
023357 ZDOT = 4718
229532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11250181
81 X = -3429055
42
Y = 15867214
74 feet Y = 4836327
05 meter
Z = -10855877
13 Z = -3308871
35
XDOT = -18384
657775 XDOT = -5603
643690
YDOT = -2492
164405 feet/sec YDOT = -759
611711 meter/sec
ZDOT = 15446
597528 ZDOT = 4708
122926
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 17218
12632082
00016717 00000-0 10270-3 0 9044
2 25544 51
6405 149
3777 0006022 109
2492 250
9312 15
54267551 29518
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
12632082 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 149
3777 deg
Eccentricity:
0006022
Arg of perigee: 109
2492 deg
Mean anomaly: 250
9312 deg
Mean motion: 15
54267551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 296
Coasting Arc #6 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2017/219/02:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4342493
53 A = 6787619
53 meter
Y = -4914194
07 meter E =
0019969
Z = 1714457
47 I = 51
87591
XDOT = 4666
039890 Wp = 114
35774
YDOT = 2114
538997 meter/sec RA = 143
30511 deg
ZDOT = -5713
336278 TA = 46
88741
MA = 46
72053
Ha = 222
896 n
mi
Hp = 212
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14247026
02 X = 4388794
78
Y = -16122683
95 feet Y = -4865374
52 meter
Z = 5624860
46 Z = 1735663
84
XDOT = 15308
529823 XDOT = 4669
799787
YDOT = 6937
463900 feet/sec YDOT = 2166
739022 meter/sec
ZDOT = -18744
541596 ZDOT = -5690
661368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14774609
20 X = 4503300
89
Y = -15606301
72 feet Y = -4756800
77 meter
Z = 5719441
66 Z = 1743285
82
XDOT = 14036
347641 XDOT = 4278
278761
YDOT = 6403
217253 feet/sec YDOT = 1951
700619 meter/sec
ZDOT = -18644
469717 ZDOT = -5682
834370
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 17219
15507070
00016717 00000-0 10270-3 0 9057
2 25544 51
6405 144
2489 0006027 111
4961 248
6835 15
54275249 29677
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
15507070 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 144
2489 deg
Eccentricity:
0006027
Arg of perigee: 111
4961 deg
Mean anomaly: 248
6835 deg
Mean motion: 15
54275249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 318
Coasting Arc #7 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -144621
20 A = 6778799
11 meter
Y = -4700910
92 meter E =
0011787
Z = 4872246
36 I = 51
84886
XDOT = 6746
566718 Wp = 83
86684
YDOT = -2735
875139 meter/sec RA = 142
70562 deg
ZDOT = -2433
141178 TA = 29
93799
MA = 29
87063
Ha = 223
001 n
mi
Hp = 212
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -474479
00 X = -115710
12
Y = -15422936
07 feet Y = -4702366
65 meter
Z = 15985060
24 Z = 4871613
94
XDOT = 22134
405242 XDOT = 6788
477345
YDOT = -8975
968305 feet/sec YDOT = -2660
196039 meter/sec
ZDOT = -7982
746646 ZDOT = -2400
267404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10619038
64 X = -3236682
98
Y = -11198035
43 feet Y = -3413161
20 meter
Z = 15982936
50 Z = 4871599
05
XDOT = 9915
697973 XDOT = 3022
304742
YDOT = -20617
856831 feet/sec YDOT = -6284
322762 meter/sec
ZDOT = -7836
827890 ZDOT = -2388
665141
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 17219
28366405
00016717 00000-0 10270-3 0 9067
2 25544 51
6397 143
6084 0006206 110
7714 249
4104 15
54277857 29695
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28366405 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 143
6084 deg
Eccentricity:
0006206
Arg of perigee: 110
7714 deg
Mean anomaly: 249
4104 deg
Mean motion: 15
54277857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 326
Coasting Arc #8 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1334728
43 A = 6782412
13 meter
Y = 5376397
03 meter E =
0012704
Z = -3927110
85 I = 51
88713
XDOT = -6319
500026 Wp = 110
45039
YDOT = 1411
699868 meter/sec RA = 137
73000 deg
ZDOT = 4086
898657 TA = 202
23826
MA = 202
29340
Ha = 222
952 n
mi
Hp = 212
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4379030
27 X = -1375673
94
Y = 17639097
87 feet Y = 5361242
29 meter
Z = -12884221
95 Z = -3933693
81
XDOT = -20733
267802 XDOT = -6354
668088
YDOT = 4631
561246 feet/sec YDOT = 1340
834246 meter/sec
ZDOT = 13408
460162 ZDOT = 4056
115722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8698281
66 X = 2651236
25
Y = 15933665
83 feet Y = 4856581
34 meter
Z = -12914141
26 Z = -3936230
26
XDOT = -11115
376003 XDOT = -3387
966606
YDOT = 16807
895186 feet/sec YDOT = 5123
046453 meter/sec
ZDOT = 13271
972011 ZDOT = 4045
297069
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 17220
24811550
00016717 00000-0 10270-3 0 9072
2 25544 51
6407 138
8006 0006110 114
0598 246
1194 15
54252391 29844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24811550 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 138
8006 deg
Eccentricity:
0006110
Arg of perigee: 114
0598 deg
Mean anomaly: 246
1194 deg
Mean motion: 15
54252391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 290
Coasting Arc #9 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2616075
66 A = 6786170
38 meter
Y = -5724978
00 meter E =
0019712
Z = 2510282
37 I = 51
92255
XDOT = 5522
534760 Wp = 108
24070
YDOT = 175
479999 meter/sec RA = 132
76573 deg
ZDOT = -5326
905821 TA = 43
68651
MA = 43
53066
Ha = 222
886 n
mi
Hp = 212
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8582925
39 X = 2667705
97
Y = -18782736
21 feet Y = -5695434
56 meter
Z = 8235834
55 Z = 2523115
65
XDOT = 18118
552362 XDOT = 5546
037037
YDOT = 575
721780 feet/sec YDOT = 237
368103 meter/sec
ZDOT = -17476
725133 ZDOT = -5300
022509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6674120
93 X = -2034272
06
Y = -19518222
07 feet Y = -5949154
09 meter
Z = 8293483
93 Z = 2527853
90
XDOT = 12239
696062 XDOT = 3730
659360
YDOT = -11599
740649 feet/sec YDOT = -3535
600950 meter/sec
ZDOT = -17357
719323 ZDOT = -5290
632850
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 17221
27686015
00016717 00000-0 10270-3 0 9083
2 25544 51
6398 133
6709 0006125 116
3502 243
8280 15
54283868 30005
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
27686015 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 133
6709 deg
Eccentricity:
0006125
Arg of perigee: 116
3502 deg
Mean anomaly: 243
8280 deg
Mean motion: 15
54283868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 302
Coasting Arc #10 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2017/221/12:27:05
094
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2723744
83 A = 6777457
53 meter
Y = 3220604
33 meter E =
0019696
Z = -5321931
27 I = 51
90022
XDOT = -5360
603308 Wp = 101
25397
YDOT = 5436
053933 meter/sec RA = 131
39624 deg
ZDOT = 544
095031 TA = 173
94077
MA = 173
91691
Ha = 222
843 n
mi
Hp = 213
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8936170
69 X = 2713379
58
Y = 10566287
16 feet Y = 3251005
07 meter
Z = -17460404
42 Z = -5308725
63
XDOT = -17587
281195 XDOT = -5423
635189
YDOT = 17834
822614 feet/sec YDOT = 5375
755595 meter/sec
ZDOT = 1785
088685 ZDOT = 517
902222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1135450
98 X = -346085
46
Y = -13864868
06 feet Y = -4226011
78 meter
Z = -17402398
64 Z = -5304251
11
XDOT = 23702
723147 XDOT = 7224
590015
YDOT = -4043
506734 feet/sec YDOT = -1232
460852 meter/sec
ZDOT = 1668
325587 ZDOT = 508
505639
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 17221
53404769
00016717 00000-0 10270-3 0 9097
2 25544 51
6421 132
3893 0005372 120
4715 239
6969 15
54124919 30049
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
53404769 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 132
3893 deg
Eccentricity:
0005372
Arg of perigee: 120
4715 deg
Mean anomaly: 239
6969 deg
Mean motion: 15
54124919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 310
Coasting Arc #11 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2017/222/12:27:05
094
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1461484
05 A = 6779165
96 meter
Y = -4461104
81 meter E =
0010247
Z = 4882167
58 I = 51
92627
XDOT = 5702
236928 Wp = 87
02141
YDOT = -4528
280487 meter/sec RA = 126
41791 deg
ZDOT = -2425
871792 TA = 26
67742
MA = 26
62474
Ha = 222
792 n
mi
Hp = 212
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4794895
18 X = -1435204
96
Y = -14636170
64 feet Y = -4477301
05 meter
Z = 16017610
18 Z = 4875132
21
XDOT = 18708
126403 XDOT = 5764
233060
YDOT = -14856
563278 feet/sec YDOT = -4464
167619 meter/sec
ZDOT = -7958
896957 ZDOT = -2398
021853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4359309
87 X = -1328717
65
Y = 14804769
96 feet Y = 4512493
88 meter
Z = 15987105
76 Z = 4872869
83
XDOT = -22807
303163 XDOT = -6951
666004
YDOT = 1762
316993 feet/sec YDOT = 537
154219 meter/sec
ZDOT = -7834
915225 ZDOT = -2388
082161
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 17222
56288951
00016717 00000-0 10270-3 0 9106
2 25544 51
6412 127
2615 0005234 124
3121 235
8527 15
54151188 30209
Satellite: ISS
Catalog Number: 25544
Epoch time: 17222
56288951 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 127
2615 deg
Eccentricity:
0005234
Arg of perigee: 124
3121 deg
Mean anomaly: 235
8527 deg
Mean motion: 15
54151188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 279
Coasting Arc #12 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2017/223/12:27:05
094
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 273407
45 A = 6782690
05 meter
Y = 5503814
33 meter E =
0011720
Z = -3967637
07 I = 51
95691
XDOT = -5663
238054 Wp = 116
63996
YDOT = 3194
165359 meter/sec RA = 121
44728 deg
ZDOT = 4044
721917 TA = 195
46395
MA = 195
49979
Ha = 222
697 n
mi
Hp = 213
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 897006
08 X = 231114
61
Y = 18057133
62 feet Y = 5506635
14 meter
Z = -13017182
00 Z = -3966411
88
XDOT = -18580
177341 XDOT = -5718
182179
YDOT = 10479
545141 feet/sec YDOT = 3130
528110 meter/sec
ZDOT = 13270
085028 ZDOT = 4017
078452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9264075
41 X = 2823690
19
Y = -15529385
89 feet Y = -4733356
82 meter
Z = -13012563
25 Z = -3966229
28
XDOT = 20205
749134 XDOT = 6158
712336
YDOT = 1048
586255 feet/sec YDOT = 319
609090 meter/sec
ZDOT = 13147
200672 ZDOT = 4007
266765
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 17223
52742811
00016717 00000-0 10270-3 0 9114
2 25544 51
6417 122
4533 0005173 128
7316 231
4300 15
54122665 30351
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
52742811 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 122
4533 deg
Eccentricity:
0005173
Arg of perigee: 128
7316 deg
Mean anomaly: 231
4300 deg
Mean motion: 15
54122665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 269
Coasting Arc #13 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2017/224/12:27:05
094
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 815301
98 A = 6786493
79 meter
Y = -6202589
99 meter E =
0018453
Z = 2605557
13 I = 51
98559
XDOT = 5364
005771 Wp = 111
04428
YDOT = -1520
376142 meter/sec RA = 116
48837 deg
ZDOT = -5274
217477 TA = 39
74609
MA = 39
61102
Ha = 222
752 n
mi
Hp = 213
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2674875
26 X = 871943
98
Y = -20349704
70 feet Y = -6193155
93 meter
Z = 8548415
79 Z = 2609655
38
XDOT = 17598
444132 XDOT = 5406
227696
YDOT = -4988
110702 feet/sec YDOT = -1460
156292 meter/sec
ZDOT = -17303
863112 ZDOT = -5248
058424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13264559
33 X = -4043037
68
Y = 15652173
50 feet Y = 4770782
48 meter
Z = 8567484
00 Z = 2611369
12
XDOT = -16435
278454 XDOT = -5009
472873
YDOT = -4478
036906 feet/sec YDOT = -1364
905649 meter/sec
ZDOT = -17187
789250 ZDOT = -5238
838163
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 17224
55626641
00016717 00000-0 10270-3 0 9121
2 25544 51
6417 117
3247 0005313 131
4791 228
6819 15
54109802 30519
Satellite: ISS
Catalog Number: 25544
Epoch time: 17224
55626641 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 117
3247 deg
Eccentricity:
0005313
Arg of perigee: 131
4791 deg
Mean anomaly: 228
6819 deg
Mean motion: 15
54109802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 294
Coasting Arc #14 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2017/225/12:27:05
094
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1710034
84 A = 6788831
65 meter
Y = 6489834
33 meter E =
0010393
Z = -1013909
75 I = 52
00702
XDOT = -4840
064738 Wp = 68
26846
YDOT = -356
817577 meter/sec RA = 111
53841 deg
ZDOT = 5931
579388 TA = 280
80523
MA = 280
92219
Ha = 222
581 n
mi
Hp = 213
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5610350
54 X = -1777553
75
Y = 21292107
39 feet Y = 6470334
01 meter
Z = -3326475
56 Z = -1022380
70
XDOT = -15879
477488 XDOT = -4864
527536
YDOT = -1170
661342 feet/sec YDOT = -411
079090 meter/sec
ZDOT = 19460
562296 ZDOT = 5908
008575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16011897
40 X = 4880426
33
Y = -15106007
40 feet Y = -4604311
06 meter
Z = -3364965
36 Z = -1025641
44
XDOT = 11859
816058 XDOT = 3614
871934
YDOT = 8297
138210 feet/sec YDOT = 2528
967726 meter/sec
ZDOT = 19356
224094 ZDOT = 5899
777104
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 17225
52079857
00016717 00000-0 10270-3 0 9131
2 25544 51
6413 112
5162 0005163 135
6030 224
5538 15
54143898 30665
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
52079857 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 112
5162 deg
Eccentricity:
0005163
Arg of perigee: 135
6030 deg
Mean anomaly: 224
5538 deg
Mean motion: 15
54143898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 300
Coasting Arc #15 (Orbit 3068)
---------------------------------------
Vector Time (GMT): 2017/225/16:27:14
000
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3737377
60 A = 6787472
64 meter
Y = -5262206
25 meter E =
0011840
Z = -2089214
16 I = 52
00020
XDOT = 3007
214294 Wp = 137
98394
YDOT = 4334
181918 meter/sec RA = 110
73477 deg
ZDOT = -5563
842910 TA = 65
02061
MA = 64
89768
Ha = 222
672 n
mi
Hp = 213
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12261737
54 X = 3806091
54
Y = -17264456
20 feet Y = -5220028
20 meter
Z = -6854377
16 Z = -2070892
20
XDOT = 9866
188629 XDOT = 2985
551109
YDOT = 14219
756948 feet/sec YDOT = 4367
689366 meter/sec
ZDOT = -18254
077789 ZDOT = -5549
287595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2672137
52 X = -814467
51
Y = 21033018
68 feet Y = 6410864
10 meter
Z = -6772440
31 Z = -2064239
81
XDOT = -13990
909990 XDOT = -4264
429365
YDOT = -7606
019157 feet/sec YDOT = -2318
314639 meter/sec
ZDOT = -18190
265270 ZDOT = -5544
392854
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 17225
71370465
00016717 00000-0 10270-3 0 9142
2 25544 51
6371 111
5505 0005299 136
2102 223
9471 15
54144147 30695
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
71370465 = yrday
fracday
Element set: 914
Inclination: 51
6371 deg
RA of node: 111
5505 deg
Eccentricity:
0005299
Arg of perigee: 136
2102 deg
Mean anomaly: 223
9471 deg
Mean motion: 15
54144147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3069
Checksum: 291
Coasting Arc #16 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2017/225/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4489510
24 A = 6782341
51 meter
Y = -3011734
44 meter E =
0010588
Z = -4103025
24 I = 51
98881
XDOT = 864
047732 Wp = 101
38139
YDOT = 6552
343903 meter/sec RA = 109
76025 deg
ZDOT = -3874
639554 TA = 128
73163
MA = 128
63693
Ha = 222
754 n
mi
Hp = 213
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14729364
29 X = 4542784
97
Y = -9881018
52 feet Y = -2961231
90 meter
Z = -13461368
89 Z = -4081087
22
XDOT = 2834
802270 XDOT = 809
534484
YDOT = 21497
191284 feet/sec YDOT = 6561
701383 meter/sec
ZDOT = -12712
072028 ZDOT = -3870
574849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12220966
16 X = 3724950
48
Y = 12955896
16 feet Y = 3948957
15 meter
Z = -13363752
94 Z = -4073271
90
XDOT = -19760
619772 XDOT = -6023
036907
YDOT = 5580
689890 feet/sec YDOT = 1700
994278 meter/sec
ZDOT = -12695
057191 ZDOT = -3869
453432
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 17225
90661205
00016717 00000-0 10270-3 0 9159
2 25544 51
6408 110
5886 0005600 141
4647 218
6906 15
54114420 30724
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
90661205 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 110
5886 deg
Eccentricity:
0005600
Arg of perigee: 141
4647 deg
Mean anomaly: 218
6906 deg
Mean motion: 15
54114420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 287
Coasting Arc #17 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2017/226/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4387610
43 A = 6778897
23 meter
Y = 1418462
56 meter E =
0011751
Z = 4964198
98 I = 51
98860
XDOT = 146
877916 Wp = 132
67001
YDOT = -7343
280283 meter/sec RA = 104
79209 deg
ZDOT = 2216
999059 TA = 295
75307
MA = 295
87430
Ha = 222
689 n
mi
Hp = 213
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14395047
34 X = -4427259
51
Y = 4653748
56 feet Y = 1369175
65 meter
Z = 16286742
07 Z = 4942789
10
XDOT = 481
882925 XDOT = 218
212448
YDOT = -24092
126912 feet/sec YDOT = -7341
238926 meter/sec
ZDOT = 7273
618961 ZDOT = 2217
885844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7246239
65 X = -2208653
85
Y = -13396032
89 feet Y = -4083110
82 meter
Z = 16191696
78 Z = 4935229
18
XDOT = 22782
520949 XDOT = 6944
112385
YDOT = -3481
756464 feet/sec YDOT = -1061
239370 meter/sec
ZDOT = 7278
669539 ZDOT = 2218
538476
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 17226
93544399
00016717 00000-0 10270-3 0 9168
2 25544 51
6416 105
4599 0005524 144
8631 215
2887 15
54158157 30885
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
93544399 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 105
4599 deg
Eccentricity:
0005524
Arg of perigee: 144
8631 deg
Mean anomaly: 215
2887 deg
Mean motion: 15
54158157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 337
Coasting Arc #18 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2017/227/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 902191
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4172249
08 A = 6777391
44 meter
Y = 377383
34 meter E =
0018139
Z = -5342634
44 I = 51
99086
XDOT = -1069
150549 Wp = 102
51470
YDOT = 7574
436219 meter/sec RA = 99
81771 deg
ZDOT = -304
596473 TA = 164
61840
MA = 164
56320
Ha = 222
529 n
mi
Hp = 213
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13688481
23 X = 4193670
76
Y = 1238134
30 feet Y = 424160
10 meter
Z = -17528328
22 Z = -5322315
01
XDOT = -3507
711774 XDOT = -1152
290865
YDOT = 24850
512530 feet/sec YDOT = 7562
015388 meter/sec
ZDOT = -999
332261 ZDOT = -309
991894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1563710
35 X = 476618
91
Y = 13769800
78 feet Y = 4197035
28 meter
Z = -17438382
42 Z = -5315218
96
XDOT = -24042
787091 XDOT = -7328
241505
YDOT = 1452
571018 feet/sec YDOT = 442
743646 meter/sec
ZDOT = -1024
406402 ZDOT = -312
239071
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 17227
89997340
00016717 00000-0 10270-3 0 9173
2 25544 51
6418 100
6523 0005378 147
4147 212
7339 15
54128276 31030
Satellite: ISS
Catalog Number: 25544
Epoch time: 17227
89997340 = yrday
fracday
Element set: 917
Inclination: 51
6418 deg
RA of node: 100
6523 deg
Eccentricity:
0005378
Arg of perigee: 147
4147 deg
Mean anomaly: 212
7339 deg
Mean motion: 15
54128276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 317
Coasting Arc #19 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2017/228/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 924696
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3848143
55 A = 6778086
73 meter
Y = -2155665
85 meter E =
0006902
Z = 5140424
30 I = 51
99832
XDOT = 1891
026268 Wp = 105
14380
YDOT = -7256
965086 meter/sec RA = 94
84248 deg
ZDOT = -1627
561545 TA =
47043
MA =
46978
Ha = 222
531 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12625142
88 X = -3848721
78
Y = -7072394
51 feet Y = -2198701
76 meter
Z = 16864909
11 Z = 5121729
90
XDOT = 6204
154422 XDOT = 1979
940860
YDOT = -23808
940570 feet/sec YDOT = -7235
321155 meter/sec
ZDOT = -5339
768848 ZDOT = -1618
159808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4126434
51 X = 1257737
24
Y = -13969986
90 feet Y = -4258052
01 meter
Z = 16782436
07 Z = 5115286
51
XDOT = 23578
023365 XDOT = 7186
581522
YDOT = 600
843583 feet/sec YDOT = 183
137124 meter/sec
ZDOT = -5296
979744 ZDOT = -1614
519426
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 17228
92880207
00016717 00000-0 10270-3 0 9182
2 25544 51
6419 95
5236 0005331 150
9365 209
2085 15
54168656 31196
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
92880207 = yrday
fracday
Element set: 918
Inclination: 51
6419 deg
RA of node: 95
5236 deg
Eccentricity:
0005331
Arg of perigee: 150
9365 deg
Mean anomaly: 209
2085 deg
Mean motion: 15
54168656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 322
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