[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 5th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
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
6
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
7
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 2925)
---------------------------------------
Vector Time (GMT): 2017/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3249128
92 A = 6777860
83 meter
Y = 3006534
65 meter E =
0019242
Z = -5149497
59 I = 51
76689
XDOT = -6272
675962 Wp = 85
33510
YDOT = 4095
817239 meter/sec RA = 156
36077 deg
ZDOT = -1569
996891 TA = 169
54798
MA = 169
50792
Ha = 223
007 n
mi
Hp = 212
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10659871
80 X = 3240280
95
Y = 9863958
84 feet Y = 3042819
46 meter
Z = -16894677
14 Z = -5133735
87
XDOT = -20579
645544 XDOT = -6310
384112
YDOT = 13437
720599 feet/sec YDOT = 4025
461169 meter/sec
ZDOT = -5150
908435 ZDOT = -1600
558511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 25976
91 X = 7917
76
Y = -14603674
37 feet Y = -4451199
95 meter
Z = -16825358
43 Z = -5128369
25
XDOT = 22709
506416 XDOT = 6921
857556
YDOT = 6118
011510 feet/sec YDOT = 1864
769908 meter/sec
ZDOT = -5286
734311 ZDOT = -1611
396618
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
51889490
00016717 00000-0 10270-3 0 9008
2 25544 51
6388 157
3927 0006055 100
9477 259
2357 15
54251671 29260
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
51889490 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 157
3927 deg
Eccentricity:
0006055
Arg of perigee: 100
9477 deg
Mean anomaly: 259
2357 deg
Mean motion: 15
54251671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2926
Checksum: 332
Coasting Arc #2 (Orbit 2941)
---------------------------------------
Vector Time (GMT): 2017/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1604873
28 A = 6776950
87 meter
Y = -3884581
01 meter E =
0008222
Z = 5309050
35 I = 51
79471
XDOT = 6874
117978 Wp = 95
38734
YDOT = -3390
830634 meter/sec RA = 151
37070 deg
ZDOT = -403
278620 TA = 358
44520
MA = 358
44775
Ha = 222
959 n
mi
Hp = 212
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5265332
27 X = -1587103
91
Y = -12744688
34 feet Y = -3902428
72 meter
Z = 17418144
19 Z = 5301297
46
XDOT = 22552
880504 XDOT = 6913
483143
YDOT = -11124
772421 feet/sec YDOT = -3313
739450 meter/sec
ZDOT = -1323
092584 ZDOT = -369
791427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5570681
23 X = -1697943
64
Y = 12660691
80 feet Y = 3858978
86 meter
Z = 17384387
98 Z = 5298761
46
XDOT = -22655
814512 XDOT = -6905
492263
YDOT = -8356
935111 feet/sec YDOT = -2547
193822 meter/sec
ZDOT = -1174
399149 ZDOT = -357
956861
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
54764439
00016717 00000-0 10270-3 0 9018
2 25544 51
6398 152
2643 0005880 104
2268 255
9538 15
54276939 29426
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
54764439 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 152
2643 deg
Eccentricity:
0005880
Arg of perigee: 104
2268 deg
Mean anomaly: 255
9538 deg
Mean motion: 15
54276939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2942
Checksum: 338
Coasting Arc #3 (Orbit 2956)
---------------------------------------
Vector Time (GMT): 2017/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51681
49 A = 6778717
38 meter
Y = 4679658
44 meter E =
0018183
Z = -4920931
76 I = 51
82883
XDOT = -6891
015469 Wp = 107
14498
YDOT = 2377
237600 meter/sec RA = 146
38254 deg
ZDOT = 2334
956778 TA = 185
67605
MA = 185
69669
Ha = 222
960 n
mi
Hp = 212
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -169558
69 X = -80103
82
Y = 15353210
11 feet Y = 4678921
79 meter
Z = -16144789
25 Z = -4921251
65
XDOT = -22608
318467 XDOT = -6928
428071
YDOT = 7799
335959 feet/sec YDOT = 2299
968300 meter/sec
ZDOT = 7660
619352 ZDOT = 2301
392240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11022416
01 X = 3359632
40
Y = -10685913
05 feet Y = -3257066
30 meter
Z = -16146877
06 Z = -4921568
13
XDOT = 20637
266607 XDOT = 6290
238862
YDOT = 9946
058089 feet/sec YDOT = 3031
558505 meter/sec
ZDOT = 7511
708282 ZDOT = 2289
568684
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
51209605
00016717 00000-0 10270-3 0 9026
2 25544 51
6400 147
4553 0006036 106
9706 253
2108 15
54258585 29573
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
51209605 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 147
4553 deg
Eccentricity:
0006036
Arg of perigee: 106
9706 deg
Mean anomaly: 253
2108 deg
Mean motion: 15
54258585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2957
Checksum: 303
Coasting Arc #4 (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 = -139006
51 A = 6778791
63 meter
Y = -4703162
72 meter E =
0011785
Z = 4870215
48 I = 51
84904
XDOT = 6746
719976 Wp = 84
04158
YDOT = -2730
864611 meter/sec RA = 142
70543 deg
ZDOT = -2438
379364 TA = 29
81736
MA = 29
75026
Ha = 222
991 n
mi
Hp = 212
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -456058
09 X = -110060
80
Y = -15430323
88 feet Y = -4704555
48 meter
Z = 15978397
23 Z = 4869610
41
XDOT = 22134
908059 XDOT = 6788
600008
YDOT = -8959
529563 feet/sec YDOT = -2655
183968 meter/sec
ZDOT = -7999
932298 ZDOT = -2405
504920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10610052
50 X = -3233944
00
Y = -11215776
97 feet Y = -3418568
82 meter
Z = 15976394
93 Z = 4869605
17
XDOT = 9925
721215 XDOT = 3025
359826
YDOT = -20606
575260 feet/sec YDOT = -6280
884139 meter/sec
ZDOT = -7854
011294 ZDOT = -2393
902642
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
28365416
00016717 00000-0 10270-3 0 9035
2 25544 51
6398 143
6084 0006209 111
1372 249
0445 15
54283249 29690
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28365416 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 143
6084 deg
Eccentricity:
0006209
Arg of perigee: 111
1372 deg
Mean anomaly: 249
0445 deg
Mean motion: 15
54283249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 319
Coasting Arc #5 (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 = -1342141
57 A = 6782408
80 meter
Y = 5378038
25 meter E =
0012682
Z = -3922311
45 I = 51
88734
XDOT = -6317
495912 Wp = 110
59766
YDOT = 1403
713888 meter/sec RA = 137
72981 deg
ZDOT = 4092
767808 TA = 202
16689
MA = 202
22177
Ha = 222
940 n
mi
Hp = 212
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4403351
62 X = -1383128
20
Y = 17644482
44 feet Y = 5362800
38 meter
Z = -12868475
89 Z = -3928930
52
XDOT = -20726
692626 XDOT = -6352
603331
YDOT = 4605
360525 feet/sec YDOT = 1332
871016 meter/sec
ZDOT = 13427
715907 ZDOT = 4061
994756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8683846
94 X = 2646836
55
Y = 15954090
74 feet Y = 4862806
86 meter
Z = -12898555
30 Z = -3931479
66
XDOT = -11126
755140 XDOT = -3391
434967
YDOT = 16785
233230 feet/sec YDOT = 5116
139088 meter/sec
ZDOT = 13291
272658 ZDOT = 4051
179906
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
24810192
00016717 00000-0 10270-3 0 9040
2 25544 51
6408 138
8005 0006112 114
4462 245
7329 15
54258952 29844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24810192 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 138
8005 deg
Eccentricity:
0006112
Arg of perigee: 114
4462 deg
Mean anomaly: 245
7329 deg
Mean motion: 15
54258952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 298
Coasting Arc #6 (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 = 2624615
69 A = 6786166
25 meter
Y = -5724665
78 meter E =
0019715
Z = 2502004
92 I = 51
92276
XDOT = 5517
327853 Wp = 108
44756
YDOT = 186
862524 meter/sec RA = 132
76556 deg
ZDOT = -5331
945586 TA = 43
58036
MA = 43
42478
Ha = 222
871 n
mi
Hp = 212
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8610943
88 X = 2676282
08
Y = -18781711
87 feet Y = -5695026
63 meter
Z = 8208677
56 Z = 2514879
77
XDOT = 18101
469334 XDOT = 5540
727715
YDOT = 613
066024 feet/sec YDOT = 248
691829 meter/sec
ZDOT = -17493
259795 ZDOT = -5305
087816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6652899
96 X = -2027803
91
Y = -19536815
53 feet Y = -5954821
37 meter
Z = 8266510
96 Z = 2519632
54
XDOT = 12251
597295 XDOT = 3734
286856
YDOT = -11562
469752 feet/sec YDOT = -3524
240781 meter/sec
ZDOT = -17374
368721 ZDOT = -5295
707586
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
27684191
00016717 00000-0 10270-3 0 9053
2 25544 51
6400 133
6708 0006125 116
7522 243
4258 15
54291347 30006
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
27684191 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 133
6708 deg
Eccentricity:
0006125
Arg of perigee: 116
7522 deg
Mean anomaly: 243
4258 deg
Mean motion: 15
54291347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 283
Coasting Arc #7 (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 = 2714693
14 A = 6777438
54 meter
Y = 3229724
20 meter E =
0019680
Z = -5320989
12 I = 51
90038
XDOT = -5366
408602 Wp = 101
43860
YDOT = 5429
204817 meter/sec RA = 131
39590 deg
ZDOT = 555
484813 TA = 173
86505
MA = 173
84091
Ha = 222
827 n
mi
Hp = 212
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8906473
57 X = 2704222
01
Y = 10596208
02 feet Y = 3260023
13 meter
Z = -17457313
38 Z = -5307827
71
XDOT = -17606
327435 XDOT = -5429
418788
YDOT = 17812
351763 feet/sec YDOT = 5368
841682 meter/sec
ZDOT = 1822
456734 ZDOT = 529
263856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1093833
89 X = -333400
57
Y = -13871677
92 feet Y = -4228087
43 meter
Z = -17399504
75 Z = -5303369
05
XDOT = 23704
676628 XDOT = 7225
185436
YDOT = -4017
030136 feet/sec YDOT = -1224
390786 meter/sec
ZDOT = 1705
569997 ZDOT = 519
857735
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
53402815
00016717 00000-0 10270-3 0 9064
2 25544 51
6422 132
3892 0005374 120
9216 239
2465 15
54132756 30047
Satellite: ISS
Catalog Number: 25544
Epoch time: 17221
53402815 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 132
3892 deg
Eccentricity:
0005374
Arg of perigee: 120
9216 deg
Mean anomaly: 239
2465 deg
Mean motion: 15
54132756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 285
Coasting Arc #8 (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 = -1449279
62 A = 6779161
56 meter
Y = -4470752
65 meter E =
0010259
Z = 4876958
55 I = 51
92649
XDOT = 5706
218301 Wp = 87
20037
YDOT = -4516
056059 meter/sec RA = 126
41755 deg
ZDOT = -2439
302317 TA = 26
63747
MA = 26
58480
Ha = 222
774 n
mi
Hp = 212
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4754854
40 X = -1422868
25
Y = -14667823
67 feet Y = -4486811
68 meter
Z = 16000520
18 Z = 4869982
78
XDOT = 18721
188653 XDOT = 5768
142679
YDOT = -14816
456887 feet/sec YDOT = -4451
899070 meter/sec
ZDOT = -8002
960356 ZDOT = -2411
433212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4410352
40 X = -1344275
41
Y = 14807742
93 feet Y = 4513400
05 meter
Z = 15970281
10 Z = 4867741
68
XDOT = -22795
078809 XDOT = -6947
940021
YDOT = 1725
514031 feet/sec YDOT = 525
936677 meter/sec
ZDOT = -7878
895535 ZDOT = -2401
487359
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
56286437
00016717 00000-0 10270-3 0 9079
2 25544 51
6413 127
2614 0005236 124
7823 235
3824 15
54159986 30203
Satellite: ISS
Catalog Number: 25544
Epoch time: 17222
56286437 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 127
2614 deg
Eccentricity:
0005236
Arg of perigee: 124
7823 deg
Mean anomaly: 235
3824 deg
Mean motion: 15
54159986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 306
Coasting Arc #9 (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 = 258208
49 A = 6782696
51 meter
Y = 5512337
39 meter E =
0011661
Z = -3956751
34 I = 51
95718
XDOT = -5664
134733 Wp = 116
79131
YDOT = 3175
413636 meter/sec RA = 121
44693 deg
ZDOT = 4058
286539 TA = 195
48619
MA = 195
52190
Ha = 222
677 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 847140
72 X = 215768
60
Y = 18085096
41 feet Y = 5514987
41 meter
Z = -12981467
66 Z = -3955600
34
XDOT = -18583
119204 XDOT = -5718
934995
YDOT = 10418
023740 feet/sec YDOT = 3111
767164 meter/sec
ZDOT = 13314
588382 ZDOT = 4030
639069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9321252
69 X = 2841117
82
Y = -15524623
78 feet Y = -4731905
33 meter
Z = -12977178
70 Z = -3955444
07
XDOT = 20174
439334 XDOT = 6149
169109
YDOT = 1097
262844 feet/sec YDOT = 334
445715 meter/sec
ZDOT = 13191
689035 ZDOT = 4020
826818
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
52739701
00016717 00000-0 10270-3 0 9084
2 25544 51
6419 122
4532 0005175 129
2285 230
9327 15
54132818 30359
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
52739701 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 122
4532 deg
Eccentricity:
0005175
Arg of perigee: 129
2285 deg
Mean anomaly: 230
9327 deg
Mean motion: 15
54132818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 297
Coasting Arc #10 (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 = 832762
19 A = 6786500
00 meter
Y = -6207465
55 meter E =
0018462
Z = 2588332
81 I = 51
98587
XDOT = 5360
562813 Wp = 111
36438
YDOT = -1494
458132 meter/sec RA = 116
48807 deg
ZDOT = -5285
141122 TA = 39
63759
MA = 39
50277
Ha = 222
730 n
mi
Hp = 213
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2732159
40 X = 889541
07
Y = -20365700
62 feet Y = -6197835
47 meter
Z = 8491905
55 Z = 2592516
21
XDOT = 17587
148337 XDOT = 5402
548233
YDOT = -4903
077862 feet/sec YDOT = -1434
278107 meter/sec
ZDOT = -17339
701845 ZDOT = -5258
999370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13321642
64 X = -4060436
68
Y = 15634246
01 feet Y = 4765318
18 meter
Z = 8511351
58 Z = 2594259
96
XDOT = -16381
059860 XDOT = -4992
947045
YDOT = -4539
214065 feet/sec YDOT = -1383
552447 meter/sec
ZDOT = -17223
708436 ZDOT = -5249
786331
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
55622825
00016717 00000-0 10270-3 0 9097
2 25544 51
6418 117
3246 0005314 131
9913 228
1693 15
54120679 30511
Satellite: ISS
Catalog Number: 25544
Epoch time: 17224
55622825 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 117
3246 deg
Eccentricity:
0005314
Arg of perigee: 131
9913 deg
Mean anomaly: 228
1693 deg
Mean motion: 15
54120679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 302
Coasting Arc #11 (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 = -1728992
50 A = 6788816
00 meter
Y = 6488358
84 meter E =
0010412
Z = -990608
75 I = 52
00723
XDOT = -4831
442772 Wp = 68
26982
YDOT = -389
281916 meter/sec RA = 111
53814 deg
ZDOT = 5936
624165 TA = 281
05790
MA = 281
17498
Ha = 222
555 n
mi
Hp = 213
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5672547
58 X = -1796606
68
Y = 21287266
55 feet Y = 6468645
99 meter
Z = -3250028
71 Z = -999172
02
XDOT = -15851
190197 XDOT = -4855
567690
YDOT = -1277
171639 feet/sec YDOT = -443
445122 meter/sec
ZDOT = 19477
113402 ZDOT = 5913
096057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16062530
68 X = 4895859
35
Y = -15068718
13 feet Y = -4592945
29 meter
Z = -3288927
16 Z = -1002465
00
XDOT = 11782
249124 XDOT = 3591
229533
YDOT = 8368
893273 feet/sec YDOT = 2550
838670 meter/sec
ZDOT = 19372
969198 ZDOT = 5904
881012
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
52075311
00016717 00000-0 10270-3 0 9109
2 25544 51
6414 112
5160 0005163 136
1416 224
0148 15
54156142 30666
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
52075311 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 112
5160 deg
Eccentricity:
0005163
Arg of perigee: 136
1416 deg
Mean anomaly: 224
0148 deg
Mean motion: 15
54156142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 259
Coasting Arc #12 (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 = 3749394
85 A = 6787397
50 meter
Y = -5244650
01 meter E =
0011775
Z = -2111601
15 I = 52
00021
XDOT = 2987
957427 Wp = 138
06003
YDOT = 4361
257933 meter/sec RA = 110
73444 deg
ZDOT = -5553
042293 TA = 65
20555
MA = 65
08311
Ha = 222
647 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12301164
20 X = 3818020
32
Y = -17206856
97 feet Y = -5202338
07 meter
Z = -6927825
30 Z = -2093221
03
XDOT = 9803
009932 XDOT = 2965
940438
YDOT = 14308
589020 feet/sec YDOT = 4394
548060 meter/sec
ZDOT = -18218
642692 ZDOT = -5538
581381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2734545
87 X = -833489
58
Y = 21001164
06 feet Y = 6401154
81 meter
Z = -6845633
51 Z = -2086549
09
XDOT = -13979
405699 XDOT = -4260
922857
YDOT = -7709
732923 feet/sec YDOT = -2349
926595 meter/sec
ZDOT = -18155
252345 ZDOT = -5533
720915
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
71365766
00016717 00000-0 10270-3 0 9117
2 25544 51
6372 111
5503 0005300 136
7328 223
4241 15
54156474 30698
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
71365766 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 111
5503 deg
Eccentricity:
0005300
Arg of perigee: 136
7328 deg
Mean anomaly: 223
4241 deg
Mean motion: 15
54156474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3069
Checksum: 289
Coasting Arc #13 (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 = 4492995
73 A = 6782249
68 meter
Y = -2984356
27 meter E =
0010614
Z = -4119111
62 I = 51
98878
XDOT = 840
209454 Wp = 101
26693
YDOT = 6568
317244 meter/sec RA = 109
75971 deg
ZDOT = -3852
769511 TA = 129
11611
MA = 129
02169
Ha = 222
728 n
mi
Hp = 213
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14740799
65 X = 4546042
20
Y = -9791195
10 feet Y = -2933816
02 meter
Z = -13514145
73 Z = -4097157
23
XDOT = 2756
592698 XDOT = 785
413126
YDOT = 21549
597257 feet/sec YDOT = 6577
406566 meter/sec
ZDOT = -12640
319917 ZDOT = -3848
821292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12134382
34 X = 3698559
74
Y = 12982532
10 feet Y = 3957075
78 meter
Z = -13416461
38 Z = -4089337
43
XDOT = -19823
509181 XDOT = -6042
205598
YDOT = 5518
199015 feet/sec YDOT = 1681
947060 meter/sec
ZDOT = -12623
823399 ZDOT = -3847
741372
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
90656350
00016717 00000-0 10270-3 0 9121
2 25544 51
6410 110
5884 0005602 141
9695 218
1854 15
54126904 30722
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
90656350 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 110
5884 deg
Eccentricity:
0005602
Arg of perigee: 141
9695 deg
Mean anomaly: 218
1854 deg
Mean motion: 15
54126904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 297
Coasting Arc #14 (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 = -4386799
33 A = 6778812
71 meter
Y = 1382500
31 meter E =
0011671
Z = 4974985
74 I = 51
98860
XDOT = 174
322115 Wp = 133
10059
YDOT = -7352
037853 meter/sec RA = 104
79130 deg
ZDOT = 2185
784569 TA = 295
64055
MA = 295
76107
Ha = 222
661 n
mi
Hp = 213
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14392386
26 X = -4426098
73
Y = 4535762
18 feet Y = 1333224
43 meter
Z = 16322131
68 Z = 4953580
64
XDOT = 571
922950 XDOT = 245
904161
YDOT = -24120
859099 feet/sec YDOT = -7349
688213 meter/sec
ZDOT = 7171
209216 ZDOT = 2186
805270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7129827
10 X = -2173171
30
Y = -13415374
36 feet Y = -4089006
10 meter
Z = 16227113
10 Z = 4946024
07
XDOT = 22826
065722 XDOT = 6957
384832
YDOT = -3406
381317 feet/sec YDOT = -1038
265025 meter/sec
ZDOT = 7176
854276 ZDOT = 2187
505183
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
93538674
00016717 00000-0 10270-3 0 9134
2 25544 51
6417 105
4596 0005526 145
3696 214
7817 15
54171566 30888
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
93538674 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 105
4596 deg
Eccentricity:
0005526
Arg of perigee: 145
3696 deg
Mean anomaly: 214
7817 deg
Mean motion: 15
54171566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 336
Coasting Arc #15 (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 = 4166034
50 A = 6777340
66 meter
Y = 420377
73 meter E =
0018137
Z = -5344209
79 I = 51
99098
XDOT = -1099
183039 Wp = 102
85035
YDOT = 7571
620958 meter/sec RA = 99
81672 deg
ZDOT = -265
949780 TA = 164
65021
MA = 164
59512
Ha = 222
497 n
mi
Hp = 213
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13668092
20 X = 4186983
52
Y = 1379192
03 feet Y = 467082
36 meter
Z = -17533496
70 Z = -5323921
70
XDOT = -3606
243565 XDOT = -1182
477368
YDOT = 24841
276108 feet/sec YDOT = 7558
863422 meter/sec
ZDOT = -872
538649 ZDOT = -271
491463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1421441
01 X = 433255
22
Y = 13778221
35 feet Y = 4199601
87 meter
Z = -17443696
38 Z = -5316838
66
XDOT = -24053
112229 XDOT = -7331
388608
YDOT = 1363
759171 feet/sec YDOT = 415
673795 meter/sec
ZDOT = -898
260219 ZDOT = -273
789715
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
89990745
00016717 00000-0 10270-3 0 9142
2 25544 51
6420 100
6520 0005379 147
9261 212
2220 15
54143170 31037
Satellite: ISS
Catalog Number: 25544
Epoch time: 17227
89990745 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 100
6520 deg
Eccentricity:
0005379
Arg of perigee: 147
9261 deg
Mean anomaly: 212
2220 deg
Mean motion: 15
54143170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 283
Coasting Arc #16 (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 = -3835748
41 A = 6778089
79 meter
Y = -2202707
75 meter E =
0006936
Z = 5129709
50 I = 51
99862
XDOT = 1922
909224 Wp = 104
81658
YDOT = -7238
861067 meter/sec RA = 94
84140 deg
ZDOT = -1670
373825 TA = 1
21968
MA = 1
21799
Ha = 222
499 n
mi
Hp = 213
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12584476
40 X = -3835749
48
Y = -7226731
45 feet Y = -2245601
82 meter
Z = 16829755
58 Z = 5111076
72
XDOT = 6308
757298 XDOT = 2011
826962
YDOT = -23749
544182 feet/sec YDOT = -7216
860580 meter/sec
ZDOT = -5480
229085 ZDOT = -1660
817204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4285976
83 X = 1306365
74
Y = -13963699
63 feet Y = -4256135
65 meter
Z = 16747562
86 Z = 5104657
16
XDOT = 23543
513874 XDOT = 7176
063029
YDOT = 705
133724 feet/sec YDOT = 214
924759 meter/sec
ZDOT = -5436
756721 ZDOT = -1657
123449
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
92872631
00016717 00000-0 10270-3 0 9151
2 25544 51
6420 95
5233 0005331 151
4632 208
6813 15
54183450 31199
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
92872631 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 95
5233 deg
Eccentricity:
0005331
Arg of perigee: 151
4632 deg
Mean anomaly: 208
6813 deg
Mean motion: 15
54183450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 294
Coasting Arc #17 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2017/229/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 924696
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446973
76 A = 6781071
12 meter
Y = 3852515
07 meter E =
0013326
Z = -4402493
95 I = 52
00971
XDOT = -2665
067479 Wp = 127
01756
YDOT = 6305
221763 meter/sec RA = 89
87268 deg
ZDOT = 3430
254147 TA = 177
62807
MA = 177
62174
Ha = 222
336 n
mi
Hp = 213
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11308969
04 X = 3425022
63
Y = 12639485
14 feet Y = 3890938
85 meter
Z = -14443877
78 Z = -4385803
04
XDOT = -8743
659707 XDOT = -2752
038353
YDOT = 20686
423106 feet/sec YDOT = 6274
932799 meter/sec
ZDOT = 11254
114655 ZDOT = 3417
097149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9609933
40 X = -2929107
70
Y = 14050319
75 feet Y = 4282537
46 meter
Z = -14370548
55 Z = -4380143
20
XDOT = -21154
087692 XDOT = -6447
765928
YDOT = -3016
493703 feet/sec YDOT = -919
427281 meter/sec
ZDOT = 11194
824488 ZDOT = 3412
182504
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 17229
89324397
00016717 00000-0 10270-3 0 9160
2 25544 51
6415 90
7163 0005442 154
5656 205
5765 15
54178440 31347
Satellite: ISS
Catalog Number: 25544
Epoch time: 17229
89324397 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 90
7163 deg
Eccentricity:
0005442
Arg of perigee: 154
5656 deg
Mean anomaly: 205
5765 deg
Mean motion: 15
54178440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 321
Coasting Arc #18 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2017/230/21:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 924696
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960458
73 A = 6784954
60 meter
Y = -5195085
33 meter E =
0015939
Z = 3187180
17 I = 52
02205
XDOT = 3365
934664 Wp = 111
23590
YDOT = -4903
005565 meter/sec RA = 84
91262 deg
ZDOT = -4851
560970 TA = 32
12745
MA = 32
03041
Ha = 222
324 n
mi
Hp = 213
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9712791
11 X = -2917627
39
Y = -17044243
20 feet Y = -5227951
75 meter
Z = 10456627
86 Z = 3172903
37
XDOT = 11043
092731 XDOT = 3444
077324
YDOT = -16085
976262 feet/sec YDOT = -4864
928402 meter/sec
ZDOT = -15917
194782 ZDOT = -4835
020849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14038243
79 X = 4278856
71
Y = -13750407
18 feet Y = -4191124
11 meter
Z = 10394210
75 Z = 3168155
44
XDOT = 17369
745948 XDOT = 5294
298565
YDOT = 5722
743848 feet/sec YDOT = 1744
292325 meter/sec
ZDOT = -15843
128244 ZDOT = -4828
985489
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 17230
92205911
00016717 00000-0 10270-3 0 9177
2 25544 51
6420 85
5875 0005258 157
6275 202
5107 15
54167870 31501
Satellite: ISS
Catalog Number: 25544
Epoch time: 17230
92205911 = yrday
fracday
Element set: 917
Inclination: 51
6420 deg
RA of node: 85
5875 deg
Eccentricity:
0005258
Arg of perigee: 157
6275 deg
Mean anomaly: 202
5107 deg
Mean motion: 15
54167870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 302
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