[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 11th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
226/16:31:37
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
3
228/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
5
237/06:36:29
751 0
4 1
2 1
2
N/A 1
0 -0
0 221
6
000/00:02:59
502 0
3 0
0 215
2
Coasting Arc #1 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2017/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4791227
61 A = 6786878
99 meter
Y = -4131697
62 meter E =
0010779
Z = -2451540
90 I = 51
97046
XDOT = 1738
716654 Wp = 131
76026
YDOT = 5188
457429 meter/sec RA = 121
58552 deg
ZDOT = -5368
387510 TA = 75
54303
MA = 75
42345
Ha = 222
779 n
mi
Hp = 213
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15719250
70 X = 4848981
49
Y = -13555438
39 feet Y = -4077796
02 meter
Z = -8043113
20 Z = -2428126
49
XDOT = 5704
450965 XDOT = 1706
645385
YDOT = 17022
498127 feet/sec YDOT = 5207
721431 meter/sec
ZDOT = -17612
819916 ZDOT = -5360
019551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20796906
87 X = -6338897
21
Y = -15210
67 feet Y = -4636
21 meter
Z = -7938819
57 Z = -2419752
20
XDOT = 6692
513332 XDOT = 2039
878064
YDOT = -15180
137673 feet/sec YDOT = -4626
905963 meter/sec
ZDOT = -17576
523780 ZDOT = -5357
324448
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
52737354
00016717 00000-0 10270-3 0 9008
2 25544 51
6417 122
4528 0005257 130
2513 229
9100 15
54115799 30355
Satellite: ISS
Catalog Number: 25544
Epoch time: 17223
52737354 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 122
4528 deg
Eccentricity:
0005257
Arg of perigee: 130
2513 deg
Mean anomaly: 229
9100 deg
Mean motion: 15
54115799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 287
Coasting Arc #2 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2017/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4792295
59 A = 6783242
48 meter
Y = 2901574
65 meter E =
0016140
Z = 3815392
02 I = 51
97482
XDOT = -490
692572 Wp = 107
59103
YDOT = -6386
798026 meter/sec RA = 116
62698 deg
ZDOT = 4221
373408 TA = 298
01753
MA = 298
18072
Ha = 222
775 n
mi
Hp = 213
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15722754
55 X = -4842918
73
Y = 9519601
88 feet Y = 2847701
03 meter
Z = 12517690
35 Z = 3791989
68
XDOT = -1609
883767 XDOT = -439
742419
YDOT = -20954
061765 feet/sec YDOT = -6392
000252 meter/sec
ZDOT = 13849
650290 ZDOT = 4219
113776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18239642
98 X = 5559443
18
Y = 2781698
71 feet Y = 847861
77 meter
Z = 12413620
69 Z = 3783671
59
XDOT = -11883
646398 XDOT = -3622
135422
YDOT = 15869
713915 feet/sec YDOT = 4837
088801 meter/sec
ZDOT = 13840
588852 ZDOT = 4218
611482
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
55619827
00016717 00000-0 10270-3 0 9017
2 25544 51
6419 117
3235 0005252 131
1239 229
0368 15
54133466 30511
Satellite: ISS
Catalog Number: 25544
Epoch time: 17224
55619827 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 117
3235 deg
Eccentricity:
0005252
Arg of perigee: 131
1239 deg
Mean anomaly: 229
0368 deg
Mean motion: 15
54133466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 292
Coasting Arc #3 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2017/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4586999
22 A = 6779508
60 meter
Y = -1329911
45 meter E =
0014405
Z = -4824063
11 I = 51
97580
XDOT = -654
868326 Wp = 90
41579
YDOT = 7170
834584 meter/sec RA = 111
65984 deg
ZDOT = -2606
370813 TA = 154
02232
MA = 153
94995
Ha = 222
588 n
mi
Hp = 213
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15049210
03 X = 4624962
53
Y = -4363226
53 feet Y = -1278404
37 meter
Z = -15826978
70 Z = -4801688
77
XDOT = -2148
518130 XDOT = -722
345423
YDOT = 23526
360185 feet/sec YDOT = 7163
134041 meter/sec
ZDOT = -8551
085346 ZDOT = -2609
716034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14549065
27 X = -4434555
09
Y = -6080648
79 feet Y = -1853381
75 meter
Z = -15727686
84 Z = -4793798
95
XDOT = 15913
898669 XDOT = 4850
556314
YDOT = -15976
443740 feet/sec YDOT = -4869
620052 meter/sec
ZDOT = -8566
975855 ZDOT = -2611
214241
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
52071752
00016717 00000-0 10270-3 0 9025
2 25544 51
6413 112
5156 0005150 135
0415 225
1155 15
54162659 30663
Satellite: ISS
Catalog Number: 25544
Epoch time: 17225
52071752 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 112
5156 deg
Eccentricity:
0005150
Arg of perigee: 135
0415 deg
Mean anomaly: 225
1155 deg
Mean motion: 15
54162659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 272
Coasting Arc #4 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2017/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206463
17 A = 6777433
37 meter
Y = -385807
57 meter E =
0008202
Z = 5295366
93 I = 51
98032
XDOT = 1628
905032 Wp = 131
83691
YDOT = -7461
171816 meter/sec RA = 106
68541 deg
ZDOT = 744
277350 TA = 311
05514
MA = 311
12599
Ha = 222
659 n
mi
Hp = 213
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13800732
20 X = -4227558
54
Y = -1265772
88 feet Y = -432964
99 meter
Z = 17373251
09 Z = 5274882
08
XDOT = 5344
176614 XDOT = 1708
601446
YDOT = -24478
910156 feet/sec YDOT = -7442
510672 meter/sec
ZDOT = 2441
854823 ZDOT = 752
383698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10225325
16 X = 3116679
11
Y = 9520891
64 feet Y = 2901967
77 meter
Z = 17282580
58 Z = 5267730
56
XDOT = -18509
071082 XDOT = -5641
564866
YDOT = 15342
444206 feet/sec YDOT = 4676
376994 meter/sec
ZDOT = 2478
893044 ZDOT = 755
566600
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
54953645
00016717 00000-0 10270-3 0 9039
2 25544 51
6416 107
3869 0005191 140
0594 220
0941 15
54163003 30827
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
54953645 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 107
3869 deg
Eccentricity:
0005191
Arg of perigee: 140
0594 deg
Mean anomaly: 220
0941 deg
Mean motion: 15
54163003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 290
Coasting Arc #5 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2017/226/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389524
99 A = 6780490
11 meter
Y = 2402232
83 meter E =
0013635
Z = 4569888
52 I = 51
98767
XDOT = -561
429416 Wp = 124
16310
YDOT = -6986
370897 meter/sec RA = 105
76121 deg
ZDOT = 3119
138936 TA = 294
69852
MA = 294
84041
Ha = 222
635 n
mi
Hp = 213
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14401328
69 X = -4438259
35
Y = 7881341
31 feet Y = 2352873
73 meter
Z = 14993072
56 Z = 4548447
25
XDOT = -1841
960026 XDOT = -498
415433
YDOT = -22921
164359 feet/sec YDOT = -6992
296821 meter/sec
ZDOT = 10233
395458 ZDOT = 3116
564809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8535404
95 X = 2601591
43
Y = -14124809
33 feet Y = -4305241
88 meter
Z = 14897740
01 Z = 4540831
16
XDOT = 12190
343178 XDOT = 3715
616601
YDOT = 18197
966371 feet/sec YDOT = 5546
740150 meter/sec
ZDOT = 10223
059503 ZDOT = 3115
988537
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
74243973
00016717 00000-0 10270-3 0 9048
2 25544 51
6370 106
4205 0005325 142
6556 217
4967 15
54157972 30854
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
74243973 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 106
4205 deg
Eccentricity:
0005325
Arg of perigee: 142
6556 deg
Mean anomaly: 217
4967 deg
Mean motion: 15
54157972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 316
Coasting Arc #6 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2017/227/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4283341
70 A = 6777808
25 meter
Y = -657686
60 meter E =
0017194
Z = -5225737
41 I = 51
98828
XDOT = -409
679186 Wp = 96
96029
YDOT = 7535
749140 meter/sec RA = 100
78884 deg
ZDOT = -1289
867004 TA = 160
72556
MA = 160
66044
Ha = 222
588 n
mi
Hp = 213
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14052958
34 X = 4315761
74
Y = -2157764
44 feet Y = -609606
04 meter
Z = -17144807
78 Z = -5204851
62
XDOT = -1344
091817 XDOT = -487
649966
YDOT = 24723
586416 feet/sec YDOT = 7530
731878 meter/sec
ZDOT = -4231
847126 ZDOT = -1292
046402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10979917
87 X = -3346678
97
Y = 9205981
54 feet Y = 2805983
17 meter
Z = -17052194
19 Z = -5197508
79
XDOT = -11052
181562 XDOT = -3368
704940
YDOT = -21005
990042 feet/sec YDOT = -6402
625765 meter/sec
ZDOT = -4242
666570 ZDOT = -1293
164770
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
70695498
00016717 00000-0 10270-3 0 9059
2 25544 51
6386 101
6121 0005529 143
8036 216
3492 15
54163394 31001
Satellite: ISS
Catalog Number: 25544
Epoch time: 17227
70695498 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 101
6121 deg
Eccentricity:
0005529
Arg of perigee: 143
8036 deg
Mean anomaly: 216
3492 deg
Mean motion: 15
54163394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 304
Coasting Arc #7 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2017/228/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4141185
57 A = 6779042
49 meter
Y = -2161124
15 meter E =
0014321
Z = -4924866
88 I = 52
00010
XDOT = 971
675968 Wp = 92
61025
YDOT = 7220
953613 meter/sec RA = 96
98334 deg
ZDOT = -2358
168983 TA = 154
42297
MA = 154
35205
Ha = 222
378 n
mi
Hp = 213
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13586566
84 X = 4188966
49
Y = -7090302
32 feet Y = -2114547
34 meter
Z = -16157699
74 Z = -4904634
41
XDOT = 3187
913280 XDOT = 902
311890
YDOT = 23690
792693 feet/sec YDOT = 7231
431762 meter/sec
ZDOT = -7736
774880 ZDOT = -2353
617247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14145747
47 X = -4311623
83
Y = -6137103
52 feet Y = -1870589
15 meter
Z = -16067738
96 Z = -4897446
83
XDOT = 15874
801495 XDOT = 4838
639496
YDOT = -16441
090605 feet/sec YDOT = -5011
244417 meter/sec
ZDOT = -7717
741648 ZDOT = -2352
367654
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
47856386
00016717 00000-0 10270-3 0 9060
2 25544 51
6420 97
7701 0005019 145
8166 214
3311 15
54176618 31123
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
47856386 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 97
7701 deg
Eccentricity:
0005019
Arg of perigee: 145
8166 deg
Mean anomaly: 214
3311 deg
Mean motion: 15
54176618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 307
Coasting Arc #8 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2017/229/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174120
99 A = 6777281
91 meter
Y = 381540
44 meter E =
0007376
Z = 5321670
35 I = 51
99714
XDOT = -96
782743 Wp = 136
68895
YDOT = -7657
727071 meter/sec RA = 92
00987 deg
ZDOT = 467
504668 TA = 308
84324
MA = 308
90905
Ha = 222
448 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13694622
66 X = -4203927
04
Y = 1251773
08 feet Y = 334695
79 meter
Z = 17459548
41 Z = 5301321
60
XDOT = -317
528686 XDOT = -13
415704
YDOT = -25123
776481 feet/sec YDOT = -7658
343240 meter/sec
ZDOT = 1533
807966 ZDOT = 467
236824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9861799
45 X = 3005876
47
Y = 9746602
84 feet Y = 2970764
54 meter
Z = 17369343
71 Z = 5294175
96
XDOT = -18281
319877 XDOT = -5572
146298
YDOT = 15730
996832 feet/sec YDOT = 4794
807834 meter/sec
ZDOT = 1533
834284 ZDOT = 467
512690
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
50737516
00016717 00000-0 10270-3 0 9079
2 25544 51
6419 92
6417 0005091 150
6097 209
5343 15
54174779 31280
Satellite: ISS
Catalog Number: 25544
Epoch time: 17229
50737516 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 92
6417 deg
Eccentricity:
0005091
Arg of perigee: 150
6097 deg
Mean anomaly: 209
5343 deg
Mean motion: 15
54174779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 323
Coasting Arc #9 (Orbit 3142)
---------------------------------------
Vector Time (GMT): 2017/230/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132033
27 A = 6777929
09 meter
Y = 1463006
90 meter E =
0017137
Z = -5184716
27 I = 51
99966
XDOT = -775
847333 Wp = 114
57382
YDOT = 7469
887601 meter/sec RA = 87
03387 deg
ZDOT = 1486
431999 TA = 169
70787
MA = 169
67273
Ha = 222
168 n
mi
Hp = 213
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13556539
61 X = 4140550
88
Y = 4799891
39 feet Y = 1509261
83 meter
Z = -17010224
00 Z = -5164623
72
XDOT = -2545
430881 XDOT = -866
540182
YDOT = 24507
505254 feet/sec YDOT = 7460
704425 meter/sec
ZDOT = 4876
745405 ZDOT = 1482
443101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5377409
60 X = -1639034
45
Y = -13450452
84 feet Y = -4099698
03 meter
Z = -16921442
85 Z = -5157655
78
XDOT = 19172
722763 XDOT = 5843
845898
YDOT = -13789
386107 feet/sec YDOT = -4203
004885 meter/sec
ZDOT = 4857
878106 ZDOT = 1480
681247
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
47188341
00016717 00000-0 10270-3 0 9084
2 25544 51
6421 87
8332 0004927 154
6235 205
5161 15
54182939 31438
Satellite: ISS
Catalog Number: 25544
Epoch time: 17230
47188341 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 87
8332 deg
Eccentricity:
0004927
Arg of perigee: 154
6235 deg
Mean anomaly: 205
5161 deg
Mean motion: 15
54182939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3143
Checksum: 306
Coasting Arc #10 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2017/231/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3974112
86 A = 6780640
21 meter
Y = -3168147
73 meter E =
0010348
Z = 4478991
24 I = 52
00632
XDOT = 1655
046567 Wp = 96
26358
YDOT = -6733
359426 meter/sec RA = 82
06306 deg
ZDOT = -3288
861139 TA = 26
70587
MA = 26
65262
Ha = 222
124 n
mi
Hp = 213
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13038428
00 X = -3960146
77
Y = -10394185
45 feet Y = -3212510
89 meter
Z = 14694853
16 Z = 4459720
50
XDOT = 5429
942804 XDOT = 1746
193148
YDOT = -22091
074232 feet/sec YDOT = -6714
341922 meter/sec
ZDOT = -10790
226834 ZDOT = -3280
600240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1100772
72 X = 335515
53
Y = 16712720
85 feet Y = 5094037
32 meter
Z = 14609985
16 Z = 4453123
48
XDOT = -18856
593319 XDOT = -5747
489644
YDOT = 10657
228628 feet/sec YDOT = 3248
323286 meter/sec
ZDOT = -10752
540573 ZDOT = -3277
374367
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 17231
50068791
00016717 00000-0 10270-3 0 9096
2 25544 51
6420 82
7043 0004744 158
5763 201
5589 15
54218115 31599
Satellite: ISS
Catalog Number: 25544
Epoch time: 17231
50068791 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 82
7043 deg
Eccentricity:
0004744
Arg of perigee: 158
5763 deg
Mean anomaly: 201
5589 deg
Mean motion: 15
54218115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 309
Coasting Arc #11 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2017/232/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3718806
41 A = 6784577
42 meter
Y = 4605269
60 meter E =
0007438
Z = -3325334
03 I = 52
01193
XDOT = -2538
689009 Wp = 124
23685
YDOT = 5463
177608 meter/sec RA = 77
10107 deg
ZDOT = 4730
367162 TA = 197
34155
MA = 197
36697
Ha = 222
024 n
mi
Hp = 213
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12200808
42 X = 3683185
18
Y = 15109152
23 feet Y = 4646656
60 meter
Z = -10909888
54 Z = -3307356
18
XDOT = -8329
032183 XDOT = -2622
568360
YDOT = 17923
811051 feet/sec YDOT = 5434
319341 meter/sec
ZDOT = 15519
577303 ZDOT = 4717
831435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2643747
44 X = 805814
22
Y = -19283990
57 feet Y = -5877760
33 meter
Z = -10830982
52 Z = -3301283
47
XDOT = 17441
601916 XDOT = 5316
200264
YDOT = -6287
376504 feet/sec YDOT = -1916
392359 meter/sec
ZDOT = 15463
148806 ZDOT = 4713
167756
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 17232
46519312
00016717 00000-0 10270-3 0 9104
2 25544 51
6403 77
8956 0004863 162
1721 197
9603 15
54174853 31747
Satellite: ISS
Catalog Number: 25544
Epoch time: 17232
46519312 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 77
8956 deg
Eccentricity:
0004863
Arg of perigee: 162
1721 deg
Mean anomaly: 197
9603 deg
Mean motion: 15
54174853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 315
Coasting Arc #12 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2017/233/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3288258
30 A = 6787822
00 meter
Y = -5650053
45 meter E =
0017357
Z = 1790344
99 I = 52
01532
XDOT = 3443
806807 Wp = 126
97205
YDOT = -3818
234424 meter/sec RA = 72
14928 deg
ZDOT = -5696
897141 TA = 33
44751
MA = 33
33800
Ha = 221
951 n
mi
Hp = 213
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10788249
03 X = -3233529
96
Y = -18536920
76 feet Y = -5686518
91 meter
Z = 5873835
28 Z = 1774505
14
XDOT = 11298
578763 XDOT = 3513
919532
YDOT = -12527
015826 feet/sec YDOT = -3779
331638 meter/sec
ZDOT = -18690
607419 ZDOT = -5679
998096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5779644
67 X = -1761635
70
Y = 20673855
39 feet Y = 6301391
12 meter
Z = 5804575
79 Z = 1769234
70
XDOT = -15437
499300 XDOT = -4705
349787
YDOT = 936
662341 feet/sec YDOT = 285
494682 meter/sec
ZDOT = -18615
109401 ZDOT = -5673
885345
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 17233
49399523
00016717 00000-0 10270-3 0 9119
2 25544 51
6410 72
7667 0004777 165
9111 194
2175 15
54191965 31901
Satellite: ISS
Catalog Number: 25544
Epoch time: 17233
49399523 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 72
7667 deg
Eccentricity:
0004777
Arg of perigee: 165
9111 deg
Mean anomaly: 194
2175 deg
Mean motion: 15
54191965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 324
Coasting Arc #13 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2017/234/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2700756
58 A = 6789176
04 meter
Y = 6225390
45 meter E =
0009993
Z = -99216
25 I = 52
00771
XDOT = -4296
672873 Wp = 67
66414
YDOT = 1952
503956 meter/sec RA = 67
20171 deg
ZDOT = 6039
885238 TA = 291
27296
MA = 291
37963
Ha = 221
841 n
mi
Hp = 214
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8860749
93 X = 2631423
82
Y = 20424509
35 feet Y = 6255204
48 meter
Z = -325512
63 Z = -86265
84
XDOT = -14096
695777 XDOT = -4347
525215
YDOT = 6405
852874 feet/sec YDOT = 1904
171679 meter/sec
ZDOT = 19815
896449 ZDOT = 6018
890087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8146927
38 X = 2483183
47
Y = -20720389
94 feet Y = -6315574
85 meter
Z = -269155
73 Z = -82038
67
XDOT = 13086
909490 XDOT = 3988
890012
YDOT = 4914
525356 feet/sec YDOT = 1497
947329 meter/sec
ZDOT = 19722
553756 ZDOT = 6011
434385
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 17234
45849418
00016717 00000-0 10270-3 0 9120
2 25544 51
6399 67
9568 0004775 170
0300 190
0948 15
54178452 32053
Satellite: ISS
Catalog Number: 25544
Epoch time: 17234
45849418 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 67
9568 deg
Eccentricity:
0004775
Arg of perigee: 170
0300 deg
Mean anomaly: 190
0948 deg
Mean motion: 15
54178452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 327
Coasting Arc #14 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2017/235/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1869520
28 A = 6788044
51 meter
Y = -6309397
08 meter E =
0012190
Z = -1641054
31 I = 51
98926
XDOT = 5072
795425 Wp = 153
92269
YDOT = -13
880717 meter/sec RA = 62
25548 deg
ZDOT = -5752
456824 TA = 43
96235
MA = 43
86545
Ha = 221
784 n
mi
Hp = 214
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6133596
73 X = -1790856
67
Y = -20700121
65 feet Y = -6329863
62 meter
Z = -5384036
45 Z = -1649944
17
XDOT = 16643
029608 XDOT = 5100
515823
YDOT = -45
540409 feet/sec YDOT = 43
001276 meter/sec
ZDOT = -18872
889842 ZDOT = -5727
747797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9971649
16 X = -3039358
66
Y = 19138126
71 feet Y = 5833301
02 meter
Z = -5422380
73 Z = -1652741
65
XDOT = -10710
908875 XDOT = -3264
685025
YDOT = -10872
245558 feet/sec YDOT = -3313
860446 meter/sec
ZDOT = -18763
413996 ZDOT = -5719
088586
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 17235
48729146
00016717 00000-0 10270-3 0 9130
2 25544 51
6388 62
8278 0004830 173
9879 186
1333 15
54171313 32219
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
48729146 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 62
8278 deg
Eccentricity:
0004830
Arg of perigee: 173
9879 deg
Mean anomaly: 186
1333 deg
Mean motion: 15
54171313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 323
Coasting Arc #15 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2017/236/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 863033
49 A = 6784832
23 meter
Y = 5933441
94 meter E =
0013470
Z = 3168911
56 I = 51
96274
XDOT = -5659
716727 Wp = 106
96224
YDOT = -1782
082163 meter/sec RA = 57
30092 deg
ZDOT = 4857
306685 TA = 289
42741
MA = 289
57293
Ha = 221
610 n
mi
Hp = 214
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2831474
72 X = 781227
18
Y = 19466673
04 feet Y = 5942635
84 meter
Z = 10396691
47 Z = 3172904
66
XDOT = -18568
624434 XDOT = -5662
962531
YDOT = -5846
726255 feet/sec YDOT = -1845
390697 meter/sec
ZDOT = 15936
045555 ZDOT = 4829
806109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11241812
64 X = 3426504
49
Y = -16132038
55 feet Y = -4917045
35 meter
Z = 10413394
38 Z = 3174002
61
XDOT = 8508
249666 XDOT = 2593
314498
YDOT = 16181
562430 feet/sec YDOT = 4932
140229 meter/sec
ZDOT = 15814
506215 ZDOT = 4820
261494
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 17236
51608583
00016717 00000-0 10270-3 0 9147
2 25544 51
6387 57
6979 0004899 179
8917 180
2237 15
54207231 32375
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51608583 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 57
6979 deg
Eccentricity:
0004899
Arg of perigee: 179
8917 deg
Mean anomaly: 180
2237 deg
Mean motion: 15
54207231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 346
Coasting Arc #16 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2017/237/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816959
68 A = 6780225
50 meter
Y = 189978
99 meter E =
0012483
Z = -4779562
40 I = 51
93363
XDOT = 2412
380751 Wp = 129
45755
YDOT = 6749
449807 meter/sec RA = 53
19695 deg
ZDOT = 2696
505576 TA = 167
12539
MA = 167
09348
Ha = 221
601 n
mi
Hp = 215
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15803673
51 X = 4837693
87
Y = 623290
65 feet Y = 243961
04 meter
Z = -15680979
01 Z = -4756112
95
XDOT = 7914
635011 XDOT = 2323
629121
YDOT = 22143
864197 feet/sec YDOT = 6775
930684 meter/sec
ZDOT = 8846
803071 ZDOT = 2708
007937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5414353
06 X = 1650294
81
Y = -14969154
44 feet Y = -4562598
27 meter
Z = -15577127
03 Z = -4747908
32
XDOT = 22392
657468 XDOT = 6825
281996
YDOT = -1168
936590 feet/sec YDOT = -356
291873 meter/sec
ZDOT = 8896
628214 ZDOT = 2711
692279
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 17237
28768255
00016717 00000-0 10270-3 0 9156
2 25544 51
6423 53
8530 0004487 191
0421 169
0634 15
53980787 32498
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
28768255 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 53
8530 deg
Eccentricity:
0004487
Arg of perigee: 191
0421 deg
Mean anomaly: 169
0634 deg
Mean motion: 15
53980787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 328
Coasting Arc #17 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2017/238/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5389721
35 A = 6783736
36 meter
Y = -1567882
26 meter E =
0010927
Z = 3797881
59 I = 51
92486
XDOT = -1163
343006 Wp = 105
46748
YDOT = -6288
280838 meter/sec RA = 48
22883 deg
ZDOT = -4239
661190 TA = 29
14526
MA = 29
08431
Ha = 221
665 n
mi
Hp = 215
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17682812
84 X = -5390236
46
Y = -5143970
66 feet Y = -1628156
37 meter
Z = 12460241
44 Z = 3771699
00
XDOT = -3816
742146 XDOT = -1072
345224
YDOT = -20630
842644 feet/sec YDOT = -6300
781666 meter/sec
ZDOT = -13909
649572 ZDOT = -4245
090808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10019909
09 X = -3054068
29
Y = 15543942
38 feet Y = 4737793
64 meter
Z = 12344520
96 Z = 3762609
99
XDOT = -19700
519239 XDOT = -6004
718264
YDOT = -1615
296631 feet/sec YDOT = -492
342413 meter/sec
ZDOT = -13932
637833 ZDOT = -4246
668012
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 17238
31661419
00016717 00000-0 10270-3 0 9166
2 25544 51
6421 48
7256 0004390 193
0679 167
0360 15
53984934 32654
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
31661419 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 48
7256 deg
Eccentricity:
0004390
Arg of perigee: 193
0679 deg
Mean anomaly: 167
0360 deg
Mean motion: 15
53984934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 324
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