[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 15th 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) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
167/11:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
167/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2017/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601731
78 A = 6787713
10 meter
Y = -5888767
88 meter E =
0004209
Z = -2142187
67 I = 51
95030
XDOT = 5298
402323 Wp = 188
79850
YDOT = -329
884163 meter/sec RA = 51
06768 deg
ZDOT = -5530
801589 TA = 14
83811
MA = 14
82576
Ha = 219
432 n
mi
Hp = 216
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8535865
42 X = -2525283
00
Y = -19320104
58 feet Y = -5917434
50 meter
Z = -7028174
77 Z = -2154641
06
XDOT = 17383
209720 XDOT = 5328
563231
YDOT = -1082
297123 feet/sec YDOT = -270
464545 meter/sec
ZDOT = -18145
674503 ZDOT = -5504
990442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20302976
80 X = -6188347
33
Y = 5758136
16 feet Y = 1755079
90 meter
Z = -7082067
59 Z = -2158614
20
XDOT = 1747
880753 XDOT = 532
754054
YDOT = -16004
059936 feet/sec YDOT = -4878
037468 meter/sec
ZDOT = -18031
607790 ZDOT = -5496
034054
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 17165
52789449
00016717 00000-0 10270-3 0 9005
2 25544 51
6427 51
5915 0004883 275
8672 84
1924 15
54004308 21330
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
52789449 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 51
5915 deg
Eccentricity:
0004883
Arg of perigee: 275
8672 deg
Mean anomaly: 84
1924 deg
Mean motion: 15
54004308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 319
Coasting Arc #2 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2017/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1498076
80 A = 6784259
10 meter
Y = 5576010
58 meter E =
0007384
Z = 3555504
60 I = 51
91689
XDOT = -6085
275684 Wp = 86
34923
YDOT = -1239
272710 meter/sec RA = 46
10902 deg
ZDOT = 4499
915696 TA = 315
42328
MA = 315
48265
Ha = 219
564 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4914950
12 X = 1418342
19
Y = 18293997
98 feet Y = 5592316
90 meter
Z = 11665041
35 Z = 3562588
70
XDOT = -19964
815236 XDOT = -6092
823869
YDOT = -4065
855347 feet/sec YDOT = -1307
365059 meter/sec
ZDOT = 14763
502938 ZDOT = 4470
336919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18743915
64 X = 5713145
49
Y = -2605096
08 feet Y = -794033
28 meter
Z = 11695272
01 Z = 3564718
91
XDOT = -6635
717193 XDOT = -2022
566600
YDOT = 18060
237494 feet/sec YDOT = 5504
760388 meter/sec
ZDOT = 14633
095203 ZDOT = 4460
167418
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 17166
55679086
00016717 00000-0 10270-3 0 9015
2 25544 51
6419 46
4628 0004799 282
3693 77
6923 15
54018947 21494
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
55679086 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 46
4628 deg
Eccentricity:
0004799
Arg of perigee: 282
3693 deg
Mean anomaly: 77
6923 deg
Mean motion: 15
54018947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 353
Coasting Arc #3 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5438733
88 A = 6789461
47 meter
Y = -3987620
80 meter E =
0009054
Z = 738441
11 I = 51
91178
XDOT = 2282
843104 Wp = 139
74399
YDOT = -4226
695347 meter/sec RA = 41
17165 deg
ZDOT = -5976
817809 TA = 32
30685
MA = 32
25143
Ha = 219
594 n
mi
Hp = 216
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17843615
09 X = -5397326
02
Y = -13082745
40 feet Y = -4048208
95 meter
Z = 2422707
04 Z = 712121
64
XDOT = 7489
642730 XDOT = 2358
969881
YDOT = -13867
110718 feet/sec YDOT = -4200
740842 meter/sec
ZDOT = -19608
982314 ZDOT = -5965
543965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16065783
93 X = -4896850
94
Y = 15231206
11 feet Y = 4642471
62 meter
Z = 2307224
15 Z = 703241
92
XDOT = -11172
094428 XDOT = -3405
254382
YDOT = -8803
775664 feet/sec YDOT = -2683
390822 meter/sec
ZDOT = -19558
384061 ZDOT = -5961
395462
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 17167
52137711
00016717 00000-0 10270-3 0 9028
2 25544 51
6426 41
6557 0004816 283
3226 76
7390 15
54010920 21641
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52137711 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 41
6557 deg
Eccentricity:
0004816
Arg of perigee: 283
3226 deg
Mean anomaly: 76
7390 deg
Mean motion: 15
54010920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 293
Coasting Arc #4 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3159564
92 A = 6786486
06 meter
Y = -5389382
15 meter E =
0001844
Z = -2647943
87 I = 51
89420
XDOT = 5554
767342 Wp = 195
95271
YDOT = -683
560784 meter/sec RA = 40
20328 deg
ZDOT = -5237
634343 TA = 13
77965
MA = 13
77462
Ha = 219
536 n
mi
Hp = 216
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10366026
63 X = -3086202
20
Y = -17681699
98 feet Y = -5424304
11 meter
Z = -8687479
90 Z = -2663114
36
XDOT = 18224
302303 XDOT = 5587
440106
YDOT = -2242
653491 feet/sec YDOT = -621
260449 meter/sec
ZDOT = -17183
839707 ZDOT = -5210
571714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 718331
56 X = 218947
46
Y = 20455571
03 feet Y = 6234858
05 meter
Z = -8753453
20 Z = -2668052
54
XDOT = -15724
941928 XDOT = -4792
962300
YDOT = -6748
784264 feet/sec YDOT = -2057
029444 meter/sec
ZDOT = -17064
184809 ZDOT = -5201
163530
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 17167
71429259
00016717 00000-0 10270-3 0 9031
2 25544 51
6392 40
6887 0004684 283
4394 76
6236 15
54067991 21679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71429259 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 40
6887 deg
Eccentricity:
0004684
Arg of perigee: 283
4394 deg
Mean anomaly: 76
6236 deg
Mean motion: 15
54067991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 344
Coasting Arc #5 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1916228
40 A = 6782809
59 meter
Y = 5159973
44 meter E =
0006298
Z = 3958699
89 I = 51
85623
XDOT = -6482
290616 Wp = 97
04830
YDOT = -695
907608 meter/sec RA = 35
23742 deg
ZDOT = 4038
616234 TA = 310
88879
MA = 310
94332
Ha = 219
555 n
mi
Hp = 216
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6286838
59 X = 1839156
34
Y = 16929046
72 feet Y = 5180970
73 meter
Z = 12987860
52 Z = 3967821
60
XDOT = -21267
357663 XDOT = -6493
644684
YDOT = -2283
161443 feet/sec YDOT = -768
460807 meter/sec
ZDOT = 13250
053261 ZDOT = 4007
099551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2237030
85 X = 681847
00
Y = -17891070
05 feet Y = -5453198
15 meter
Z = 13027155
82 Z = 3970677
09
XDOT = 16634
996714 XDOT = 5070
346998
YDOT = 11641
470098 feet/sec YDOT = 3548
320086 meter/sec
ZDOT = 13110
997555 ZDOT = 3996
232055
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 17168
74317828
00016717 00000-0 10270-3 0 9044
2 25544 51
6389 35
5594 0004694 284
9031 75
1601 15
54070690 21836
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74317828 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 35
5594 deg
Eccentricity:
0004694
Arg of perigee: 284
9031 deg
Mean anomaly: 75
1601 deg
Mean motion: 15
54070690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 324
Coasting Arc #6 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -425990
99 A = 6779406
06 meter
Y = -4693229
17 meter E =
0008716
Z = -4881684
95 I = 51
81819
XDOT = 7018
175677 Wp = 54
13702
YDOT = 1887
151470 meter/sec RA = 30
26209 deg
ZDOT = -2424
777672 TA = 192
10918
MA = 192
13014
Ha = 219
726 n
mi
Hp = 216
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1397608
23 X = -349765
44
Y = -15397733
48 feet Y = -4697566
25 meter
Z = -16016026
73 Z = -4883569
57
XDOT = 23025
510752 XDOT = 7008
329897
YDOT = 6191
441830 feet/sec YDOT = 1965
578630 meter/sec
ZDOT = -7955
307324 ZDOT = -2390
709094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5653833
38 X = -1723288
42
Y = 14381933
64 feet Y = 4383613
37 meter
Z = -16023444
39 Z = -4883945
85
XDOT = -16907
512190 XDOT = -5153
409715
YDOT = -15349
895191 feet/sec YDOT = -4678
648054 meter/sec
ZDOT = -7805
220556 ZDOT = -2379
031226
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 17169
70775696
00016717 00000-0 10270-3 0 9053
2 25544 51
6395 30
7532 0004565 289
7186 70
3474 15
54068174 21988
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70775696 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 30
7532 deg
Eccentricity:
0004565
Arg of perigee: 289
7186 deg
Mean anomaly: 70
3474 deg
Mean motion: 15
54068174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 345
Coasting Arc #7 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1202072
14 A = 6777679
53 meter
Y = 4049100
57 meter E =
0001889
Z = 5302044
97 I = 51
78386
XDOT = -7094
286112 Wp = 295
20145
YDOT = -2852
504445 meter/sec RA = 25
27493 deg
ZDOT = 570
956642 TA = 149
36565
MA = 149
35461
Ha = 219
924 n
mi
Hp = 216
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3943806
22 X = -1273015
86
Y = 13284450
70 feet Y = 4035260
99 meter
Z = 17395160
65 Z = 5296033
71
XDOT = -23275
216903 XDOT = -7064
634846
YDOT = -9358
610385 feet/sec YDOT = -2931
671827 meter/sec
ZDOT = 1873
217331 ZDOT = 536
566234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9341527
23 X = 2847297
50
Y = -10281838
44 feet Y = -3133904
36 meter
Z = 17367830
02 Z = 5293714
59
XDOT = 16312
354994 XDOT = 4972
005802
YDOT = 17723
896771 feet/sec YDOT = 5402
243736 meter/sec
ZDOT = 1721
907582 ZDOT = 524
837431
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 17170
73663741
00016717 00000-0 10270-3 0 9066
2 25544 51
6398 25
6237 0004677 293
6331 66
4330 15
54046066 22148
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73663741 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 25
6237 deg
Eccentricity:
0004677
Arg of perigee: 293
6331 deg
Mean anomaly: 66
4330 deg
Mean motion: 15
54046066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 308
Coasting Arc #8 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2835084
01 A = 6778128
11 meter
Y = -3317218
83 meter E =
0009554
Z = -5194964
48 I = 51
75663
XDOT = 6639
815563 Wp = 92
06420
YDOT = 3579
832781 meter/sec RA = 20
28598 deg
ZDOT = 1339
499175 TA = 190
78812
MA = 190
80863
Ha = 219
953 n
mi
Hp = 216
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9301456
73 X = 2897202
16
Y = -10883263
87 feet Y = -3285167
07 meter
Z = -17043846
70 Z = -5181041
88
XDOT = 21784
171793 XDOT = 6592
784751
YDOT = 11744
858205 feet/sec YDOT = 3653
820577 meter/sec
ZDOT = 4394
682333 ZDOT = 1371
639860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13056786
93 X = -3979708
66
Y = 6049520
22 feet Y = 1843893
76 meter
Z = -16981721
36 Z = -5176028
67
XDOT = -14556
894841 XDOT = -4436
941548
YDOT = -18702
136697 feet/sec YDOT = -5700
411265 meter/sec
ZDOT = 4535
904829 ZDOT = 1382
543792
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 17171
70120745
00016717 00000-0 10270-3 0 9077
2 25544 51
6407 20
8169 0004621 297
3432 62
7250 15
54079356 22296
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
70120745 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 20
8169 deg
Eccentricity:
0004621
Arg of perigee: 297
3432 deg
Mean anomaly: 62
7250 deg
Mean motion: 15
54079356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 297
Coasting Arc #9 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4344089
91 A = 6780914
34 meter
Y = 2531814
10 meter E =
0007131
Z = 4549045
38 I = 51
73402
XDOT = -5672
360259 Wp = 36
31662
YDOT = -4105
856885 meter/sec RA = 15
29784 deg
ZDOT = -3123
522528 TA = 84
97932
MA = 84
89792
Ha = 220
193 n
mi
Hp = 216
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14252263
48 X = -4394175
70
Y = 8306476
72 feet Y = 2482954
87 meter
Z = 14924689
56 Z = 4527821
63
XDOT = -18610
105835 XDOT = -5610
853222
YDOT = -13470
659073 feet/sec YDOT = -4168
944721 meter/sec
ZDOT = -10247
777322 ZDOT = -3150
928541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16465474
97 X = 5018676
77
Y = -1953451
70 feet Y = -595412
08 meter
Z = 14830478
38 Z = 4520329
81
XDOT = 11558
304655 XDOT = 3522
971259
YDOT = 18507
413245 feet/sec YDOT = 5641
059557 meter/sec
ZDOT = -10367
980966 ZDOT = -3160
160599
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 17172
73008056
00016717 00000-0 10270-3 0 9082
2 25544 51
6401 15
6880 0004563 300
9612 59
1092 15
54042537 22451
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
73008056 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 15
6880 deg
Eccentricity:
0004563
Arg of perigee: 300
9612 deg
Mean anomaly: 59
1092 deg
Mean motion: 15
54042537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 287
Coasting Arc #10 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5567408
75 A = 6784566
06 meter
Y = -1757745
63 meter E =
0002861
Z = -3454165
41 I = 51
71524
XDOT = 4243
649807 Wp = 19
06732
YDOT = 4447
378216 meter/sec RA = 10
31730 deg
ZDOT = 4580
438605 TA = 300
48867
MA = 300
51692
Ha = 220
285 n
mi
Hp = 216
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18265776
73 X = 5603429
29
Y = -5766881
98 feet Y = -1695285
14 meter
Z = -11332563
67 Z = -3427033
27
XDOT = 13922
735586 XDOT = 4171
352996
YDOT = 14591
135880 feet/sec YDOT = 4494
428620 meter/sec
ZDOT = 15027
685713 ZDOT = 4600
878184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19156003
98 X = -5838750
01
Y = -1628419
29 feet Y = -496342
20 meter
Z = -11212416
74 Z = -3417544
62
XDOT = -7366
053857 XDOT = -2245
173216
YDOT = -17352
157023 feet/sec YDOT = -5288
937461 meter/sec
ZDOT = 15117
055695 ZDOT = 4607
678576
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 17173
69464420
00016717 00000-0 10270-3 0 9090
2 25544 51
6406 10
8804 0004776 304
7293 55
3410 15
54062800 22606
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
69464420 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 10
8804 deg
Eccentricity:
0004776
Arg of perigee: 304
7293 deg
Mean anomaly: 55
3410 deg
Mean motion: 15
54062800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 290
Coasting Arc #11 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6412370
31 A = 6787878
33 meter
Y = 977047
99 meter E =
0009494
Z = 1987590
38 I = 51
69474
XDOT = -2445
138927 Wp = 104
23770
YDOT = -4655
543726 meter/sec RA = 5
34383 deg
ZDOT = -5579
921563 TA = 53
83962
MA = 53
75182
Ha = 220
306 n
mi
Hp = 216
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21037960
33 X = -6432474
08
Y = 3205538
02 feet Y = 905227
77 meter
Z = 6520965
81 Z = 1956392
37
XDOT = -8022
109339 XDOT = -2365
793140
YDOT = -15274
093589 feet/sec YDOT = -4682
442326 meter/sec
ZDOT = -18306
829274 ZDOT = -5591
607379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20802185
96 X = 6340506
28
Y = 4681916
84 feet Y = 1427048
25 meter
Z = 6383021
06 Z = 1945544
82
XDOT = 2145
389306 XDOT = 653
914660
YDOT = 15586
878234 feet/sec YDOT = 4750
880486 meter/sec
ZDOT = -18357
503665 ZDOT = -5595
367117
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 17174
72350924
00016717 00000-0 10270-3 0 9100
2 25544 51
6410 5
7514 0004716 308
2900 51
7828 15
54075942 22761
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
72350924 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 5
7514 deg
Eccentricity:
0004716
Arg of perigee: 308
2900 deg
Mean anomaly: 51
7828 deg
Mean motion: 15
54075942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 295
Coasting Arc #12 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2017/175/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6769614
12 A = 6789428
52 meter
Y = -222174
75 meter E =
0012549
Z = -337105
47 I = 51
66806
XDOT = 451
071560 Wp = 20
35517
YDOT = 4751
312389 meter/sec RA =
37549 deg
ZDOT = 6005
446047 TA = 336
01163
MA = 336
07004
Ha = 220
515 n
mi
Hp = 215
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22210020
09 X = 6773232
89
Y = -728919
78 feet Y = -146452
05 meter
Z = -1105989
08 Z = -304212
19
XDOT = 1479
893570 XDOT = 368
736251
YDOT = 15588
295241 feet/sec YDOT = 4755
895194 meter/sec
ZDOT = 19702
906979 ZDOT = 6007
438030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21084086
17 X = -6426429
47
Y = -7041155
91 feet Y = -2146144
32 meter
Z = -960709
13 Z = -292824
14
XDOT = 3640
385116 XDOT = 1109
589383
YDOT = -13549
643199 feet/sec YDOT = -4129
931247 meter/sec
ZDOT = 19710
760424 ZDOT = 6007
839777
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 17175
68806647
00016717 00000-0 10270-3 0 9115
2 25544 51
6415
9436 0004754 314
3940 45
6823 15
54082173 22918
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
68806647 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node:
9436 deg
Eccentricity:
0004754
Arg of perigee: 314
3940 deg
Mean anomaly: 45
6823 deg
Mean motion: 15
54082173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2291
Checksum: 307
Coasting Arc #13 (Orbit 2306)
---------------------------------------
Vector Time (GMT): 2017/176/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6623958
07 A = 6788567
48 meter
Y = -555266
95 meter E =
0003866
Z = -1369227
51 I = 51
63253
XDOT = 1595
682370 Wp = 148
83358
YDOT = -4740
671546 meter/sec RA = 355
40648 deg
ZDOT = -5807
564128 TA = 46
07748
MA = 46
04558
Ha = 220
536 n
mi
Hp = 215
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21732145
90 X = -6610605
66
Y = -1821741
95 feet Y = -629265
66 meter
Z = -4492216
23 Z = -1401371
98
XDOT = 5235
178378 XDOT = 1676
785223
YDOT = -15553
384338 feet/sec YDOT = -4722
373163 meter/sec
ZDOT = -19053
688085 ZDOT = -5799
616631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19870962
31 X = 6056669
31
Y = 8913781
11 feet Y = 2716920
48 meter
Z = -4634034
87 Z = -1412453
83
XDOT = -9563
304303 XDOT = -2914
895152
YDOT = 11449
623542 feet/sec YDOT = 3489
845255 meter/sec
ZDOT = -19017
660228 ZDOT = -5796
582838
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 17176
71692483
00016717 00000-0 10270-3 0 9122
2 25544 51
6412 355
8152 0004735 316
8492 43
2289 15
54098327 23076
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
71692483 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 355
8152 deg
Eccentricity:
0004735
Arg of perigee: 316
8492 deg
Mean anomaly: 43
2289 deg
Mean motion: 15
54098327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2307
Checksum: 322
Coasting Arc #14 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2017/177/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5971663
30 A = 6785650
91 meter
Y = 1337496
29 meter E =
0011474
Z = 2915825
03 I = 51
59197
XDOT = -3494
028262 Wp = 61
18651
YDOT = 4627
972587 meter/sec RA = 350
42966 deg
ZDOT = 5023
407352 TA = 332
10676
MA = 332
16822
Ha = 220
542 n
mi
Hp = 215
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19592071
21 X = 5942099
78
Y = 4388111
18 feet Y = 1404109
78 meter
Z = 9566355
10 Z = 2944761
54
XDOT = -11463
347315 XDOT = -3569
920721
YDOT = 15183
637097 feet/sec YDOT = 4588
474977 meter/sec
ZDOT = 16480
995250 ZDOT = 5006
250954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17149790
47 X = -5227256
13
Y = -10321522
04 feet Y = -3145999
92 meter
Z = 9693853
38 Z = 2954686
51
XDOT = 15015
160462 XDOT = 4576
620909
YDOT = -9512
691391 feet/sec YDOT = -2899
468336 meter/sec
ZDOT = 16404
335747 ZDOT = 5000
041536
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 17177
74577855
00016717 00000-0 10270-3 0 9132
2 25544 51
6425 350
6866 0004752 321
2039 38
8772 15
54120157 23233
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
74577855 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 350
6866 deg
Eccentricity:
0004752
Arg of perigee: 321
2039 deg
Mean anomaly: 38
8772 deg
Mean motion: 15
54120157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 319
Coasting Arc #15 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2017/178/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4894716
47 A = 6781924
05 meter
Y = -2156695
76 meter E =
0008156
Z = -4178107
95 I = 51
54729
XDOT = 5089
445699 Wp = 34
57939
YDOT = -4363
164420 meter/sec RA = 345
44197 deg
ZDOT = -3707
132004 TA = 197
24004
MA = 197
26775
Ha = 220
813 n
mi
Hp = 215
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16058781
07 X = -4849941
02
Y = -7075773
49 feet Y = -2211180
98 meter
Z = -13707703
24 Z = -4201776
15
XDOT = 16697
656493 XDOT = 5155
864686
YDOT = -14314
843898 feet/sec YDOT = -4305
879003 meter/sec
ZDOT = -12162
506574 ZDOT = -3682
248541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13123861
47 X = 4000152
98
Y = 11526108
78 feet Y = 3513157
96 meter
Z = -13811778
47 Z = -4209830
08
XDOT = -19448
099443 XDOT = -5927
780710
YDOT = 7690
548144 feet/sec YDOT = 2344
079074 meter/sec
ZDOT = -12051
792073 ZDOT = -3673
386224
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 17178
71032659
00016717 00000-0 10270-3 0 9149
2 25544 51
6424 345
8794 0004861 324
9430 35
1402 15
54095351 23387
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
71032659 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 345
8794 deg
Eccentricity:
0004861
Arg of perigee: 324
9430 deg
Mean anomaly: 35
1402 deg
Mean motion: 15
54095351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 310
Coasting Arc #16 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2017/179/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3477156
85 A = 6778612
00 meter
Y = 2980561
25 meter E =
0002506
Z = 4995219
58 I = 51
50531
XDOT = -6269
334956 Wp = 67
28171
YDOT = 3930
979174 meter/sec RA = 340
44169 deg
ZDOT = 2018
656865 TA = 3
06972
MA = 3
06818
Ha = 220
795 n
mi
Hp = 215
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11407994
93 X = 3419304
96
Y = 9778744
26 feet Y = 3019121
24 meter
Z = 16388515
68 Z = 5011970
10
XDOT = -20568
684239 XDOT = -6322
631782
YDOT = 12896
913302 feet/sec YDOT = 3860
573033 meter/sec
ZDOT = 6622
889977 ZDOT = 1988
073643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8078580
85 X = -2462351
44
Y = -12573480
10 feet Y = -3832396
73 meter
Z = 16461888
20 Z = 5017583
52
XDOT = 22498
027667 XDOT = 6857
398833
YDOT = -5962
518567 feet/sec YDOT = -1817
375659 meter/sec
ZDOT = 6487
107271 ZDOT = 1977
270296
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 17179
73917321
00016717 00000-0 10270-3 0 9151
2 25544 51
6424 340
7512 0004909 329
1072 30
9791 15
54137672 23546
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
73917321 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 340
7512 deg
Eccentricity:
0004909
Arg of perigee: 329
1072 deg
Mean anomaly: 30
9791 deg
Mean motion: 15
54137672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 311
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