[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 23rd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
152/21:55:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
1
153/10:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
2
153/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
155/13:34:21
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
4
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2017/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5169151
83 A = 6786819
88 meter
Y = 3521752
39 meter E =
0004605
Z = -2641053
11 I = 51
73993
XDOT = -4721
263500 Wp = 121
30624
YDOT = -3014
085026 meter/sec RA = 165
18364 deg
ZDOT = 5225
825584 TA = 208
99799
MA = 209
02358
Ha = 222
067 n
mi
Hp = 214
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16959159
54 X = -5195319
63
Y = 11554305
73 feet Y = 3463801
21 meter
Z = -8664872
41 Z = -2666227
14
XDOT = -15489
709645 XDOT = -4712
593265
YDOT = -9888
730401 feet/sec YDOT = -3066
833091 meter/sec
ZDOT = 17145
097060 ZDOT = 5202
911696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1356193
94 X = 413367
91
Y = 20428673
34 feet Y = 6226659
63 meter
Z = -8776396
23 Z = -2675045
57
XDOT = -14955
975335 XDOT = -4558
581282
YDOT = 8309
279543 feet/sec YDOT = 2532
668405 meter/sec
ZDOT = 17044
511913 ZDOT = 5195
167231
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 17142
50539987
00016717 00000-0 10270-3 0 9008
2 25544 51
6402 166
3292 0005192 180
9924 179
1219 15
53947814 17756
Satellite: ISS
Catalog Number: 25544
Epoch time: 17142
50539987 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 166
3292 deg
Eccentricity:
0005192
Arg of perigee: 180
9924 deg
Mean anomaly: 179
1219 deg
Mean motion: 15
53947814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 328
Coasting Arc #2 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2017/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5955600
10 A = 6789416
79 meter
Y = -3051470
89 meter E =
0016710
Z = 1086804
53 I = 51
77727
XDOT = 3051
784984 Wp = 138
98777
YDOT = 3840
829791 meter/sec RA = 160
21939 deg
ZDOT = -5900
447822 TA = 29
23810
MA = 29
14467
Ha = 222
004 n
mi
Hp = 214
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19539370
39 X = 5984000
53
Y = -10011387
44 feet Y = -2984712
60 meter
Z = 3565631
65 Z = 1115804
43
XDOT = 10012
417928 XDOT = 3037
271086
YDOT = 12601
147607 feet/sec YDOT = 3874
876056 meter/sec
ZDOT = -19358
424613 ZDOT = -5885
657947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 923891
59 X = 281602
16
Y = -21914141
44 feet Y = -6679430
31 meter
Z = 3693972
42 Z = 1125922
79
XDOT = 14363
675948 XDOT = 4378
048429
YDOT = -2667
527520 feet/sec YDOT = -813
062388 meter/sec
ZDOT = -19293
780972 ZDOT = -5880
744440
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 17143
53437414
00016717 00000-0 10270-3 0 9015
2 25544 51
6381 161
2014 0005157 184
8795 175
2308 15
53915403 17911
Satellite: ISS
Catalog Number: 25544
Epoch time: 17143
53437414 = yrday
fracday
Element set: 901
Inclination: 51
6381 deg
RA of node: 161
2014 deg
Eccentricity:
0005157
Arg of perigee: 184
8795 deg
Mean anomaly: 175
2308 deg
Mean motion: 15
53915403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 300
Coasting Arc #3 (Orbit 1806)
---------------------------------------
Vector Time (GMT): 2017/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6311089
55 A = 6789754
16 meter
Y = 2436694
56 meter E =
0009627
Z = 544140
16 I = 51
80919
XDOT = -1256
584888 Wp = 71
02181
YDOT = -4611
409495 meter/sec RA = 155
26084 deg
ZDOT = 5992
468082 TA = 294
83300
MA = 294
93309
Ha = 221
826 n
mi
Hp = 215
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20705674
38 X = -6340511
48
Y = 7994404
72 feet Y = 2365955
13 meter
Z = 1785236
76 Z = 513410
87
XDOT = -4122
653831 XDOT = -1234
034628
YDOT = -15129
296242 feet/sec YDOT = -4625
335828 meter/sec
ZDOT = 19660
328354 ZDOT = 5986
418281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2892245
80 X = -881556
52
Y = 22016746
23 feet Y = 6710704
25 meter
Z = 1649341
78 Z = 502719
38
XDOT = -13712
016010 XDOT = -4179
422480
YDOT = -3294
370380 feet/sec YDOT = -1004
124092 meter/sec
ZDOT = 19634
346078 ZDOT = 5984
548685
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 17144
56334323
00016717 00000-0 10270-3 0 9025
2 25544 51
6384 156
0736 0005136 190
4110 169
6937 15
53945032 18072
Satellite: ISS
Catalog Number: 25544
Epoch time: 17144
56334323 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 156
0736 deg
Eccentricity:
0005136
Arg of perigee: 190
4110 deg
Mean anomaly: 169
6937 deg
Mean motion: 15
53945032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1807
Checksum: 301
Coasting Arc #4 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2017/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6228332
66 A = 6788048
24 meter
Y = -1599709
49 meter E =
0010162
Z = -2157809
09 I = 51
83113
XDOT = -543
651847 Wp = 162
46965
YDOT = 5300
763045 meter/sec RA = 150
30178 deg
ZDOT = -5515
156018 TA = 41
39901
MA = 41
32205
Ha = 221
863 n
mi
Hp = 215
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20434162
26 X = 6256239
92
Y = -5248390
71 feet Y = -1529903
80 meter
Z = -7079426
16 Z = -2127485
52
XDOT = -1783
634670 XDOT = -576
095477
YDOT = 17390
954873 feet/sec YDOT = 5294
502705 meter/sec
ZDOT = -18094
343892 ZDOT = -5517
875244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4836441
86 X = 1474147
48
Y = -20581271
84 feet Y = -6273171
66 meter
Z = -6945426
32 Z = -2116965
94
XDOT = 13138
136487 XDOT = 4004
504001
YDOT = 9179
595661 feet/sec YDOT = 2797
940757 meter/sec
ZDOT = -18107
151377 ZDOT = -5519
059740
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 17145
52800110
00016717 00000-0 10270-3 0 9035
2 25544 51
6373 151
2655 0005007 192
7637 167
3390 15
53914736 18225
Satellite: ISS
Catalog Number: 25544
Epoch time: 17145
52800110 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 151
2655 deg
Eccentricity:
0005007
Arg of perigee: 192
7637 deg
Mean anomaly: 167
3390 deg
Mean motion: 15
53914736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 294
Coasting Arc #5 (Orbit 1837)
---------------------------------------
Vector Time (GMT): 2017/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5757288
20 A = 6784692
17 meter
Y = 605355
03 meter E =
0011734
Z = 3534122
94 I = 51
84673
XDOT = 2168
657824 Wp = 115
88025
YDOT = -5808
108320 meter/sec RA = 145
33837 deg
ZDOT = 4511
106691 TA = 285
62007
MA = 285
74954
Ha = 221
613 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18888740
80 X = -5780796
87
Y = 1986072
93 feet Y = 540841
26 meter
Z = 11594891
53 Z = 3506098
31
XDOT = 7115
019108 XDOT = 2211
531318
YDOT = -19055
473490 feet/sec YDOT = -5783
617746 meter/sec
ZDOT = 14800
218802 ZDOT = 4521
744972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6718903
11 X = -2047921
67
Y = 17844865
87 feet Y = 5439115
12 meter
Z = 11471165
06 Z = 3496411
11
XDOT = -12589
972668 XDOT = -3837
423669
YDOT = -14320
513345 feet/sec YDOT = -4364
892467 meter/sec
ZDOT = 14848
051810 ZDOT = 4525
686192
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 17146
55696500
00016717 00000-0 10270-3 0 9046
2 25544 51
6361 146
1377 0005003 199
3405 160
7558 15
53942169 18389
Satellite: ISS
Catalog Number: 25544
Epoch time: 17146
55696500 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 146
1377 deg
Eccentricity:
0005003
Arg of perigee: 199
3405 deg
Mean anomaly: 160
7558 deg
Mean motion: 15
53942169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1838
Checksum: 319
Coasting Arc #6 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2017/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4953691
11 A = 6781083
98 meter
Y = 586379
38 meter E =
0007650
Z = -4599421
69 I = 51
86120
XDOT = -3552
437076 Wp = 98
78042
YDOT = 6060
978577 meter/sec RA = 140
36629 deg
ZDOT = -3058
824910 TA = 140
74614
MA = 140
69064
Ha = 221
568 n
mi
Hp = 215
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16252267
44 X = 4969107
88
Y = 1923816
87 feet Y = 641861
72 meter
Z = -15089966
19 Z = -4575320
39
XDOT = -11654
977283 XDOT = -3605
090061
YDOT = 19885
100319 feet/sec YDOT = 6020
958826 meter/sec
ZDOT = -10035
514798 ZDOT = -3076
208835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8805432
82 X = 2683895
92
Y = -13910317
20 feet Y = -4239864
68 meter
Z = -14983717
03 Z = -4567036
95
XDOT = 11900
887736 XDOT = 3627
390582
YDOT = 18407
506021 feet/sec YDOT = 5610
607835 meter/sec
ZDOT = -10113
167679 ZDOT = -3082
493509
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 17147
52161812
00016717 00000-0 10270-3 0 9058
2 25544 51
6366 141
3295 0004894 201
4157 158
6792 15
53925717 18539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17147
52161812 = yrday
fracday
Element set: 905
Inclination: 51
6366 deg
RA of node: 141
3295 deg
Eccentricity:
0004894
Arg of perigee: 201
4157 deg
Mean anomaly: 158
6792 deg
Mean motion: 15
53925717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 321
Coasting Arc #7 (Orbit 1868)
---------------------------------------
Vector Time (GMT): 2017/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3932040
24 A = 6778552
28 meter
Y = -1854173
12 meter E =
0006983
Z = 5201052
07 I = 51
87771
XDOT = 4593
026089 Wp = 168
23712
YDOT = -5995
170360 meter/sec RA = 135
38850 deg
ZDOT = 1328
113449 TA = 269
00459
MA = 269
08460
Ha = 221
453 n
mi
Hp = 215
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12900394
49 X = -3936278
46
Y = -6083245
14 feet Y = -1898168
23 meter
Z = 17063819
14 Z = 5181940
79
XDOT = 15068
983233 XDOT = 4653
272930
YDOT = -19669
194095 feet/sec YDOT = -5943
471346 meter/sec
ZDOT = 4357
327589 ZDOT = 1350
570633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10953111
36 X = -3338508
34
Y = 9290669
66 feet Y = 2831796
11 meter
Z = 16979775
67 Z = 5175435
62
XDOT = -10928
815939 XDOT = -3331
103098
YDOT = -21072
804200 feet/sec YDOT = -6422
990720 meter/sec
ZDOT = 4457
377838 ZDOT = 1358
608765
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 17148
55057713
00016717 00000-0 10270-3 0 9067
2 25544 51
6371 136
2016 0004822 206
4832 153
6075 15
53926638 18694
Satellite: ISS
Catalog Number: 25544
Epoch time: 17148
55057713 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 136
2016 deg
Eccentricity:
0004822
Arg of perigee: 206
4832 deg
Mean anomaly: 153
6075 deg
Mean motion: 15
53926638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1869
Checksum: 315
Coasting Arc #8 (Orbit 1883)
---------------------------------------
Vector Time (GMT): 2017/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2774672
77 A = 6778043
08 meter
Y = 3174136
03 meter E =
0013330
Z = -5318323
43 I = 51
89847
XDOT = -5270
632149 Wp = 113
07092
YDOT = 5529
938248 meter/sec RA = 130
40809 deg
ZDOT = 546
645869 TA = 162
15643
MA = 162
10958
Ha = 221
232 n
mi
Hp = 215
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9103257
12 X = 2764806
39
Y = 10413832
13 feet Y = 3205109
76 meter
Z = -17448567
69 Z = -5304868
49
XDOT = -17292
100228 XDOT = -5334
732987
YDOT = 18142
842020 feet/sec YDOT = 5470
639997 meter/sec
ZDOT = 1793
457574 ZDOT = 520
887673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13235696
21 X = 4034240
20
Y = -4264358
44 feet Y = -1299776
45 meter
Z = -17389689
40 Z = -5300377
33
XDOT = 9364
113908 XDOT = 2854
181919
YDOT = 22164
259893 feet/sec YDOT = 6755
666415 meter/sec
ZDOT = 1678
891831 ZDOT = 511
726230
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17149
51522333
00016717 00000-0 10270-3 0 9070
2 25544 51
6371 131
3945 0004784 210
2753 149
8123 15
53923086 18845
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
51522333 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 131
3945 deg
Eccentricity:
0004784
Arg of perigee: 210
2753 deg
Mean anomaly: 149
8123 deg
Mean motion: 15
53923086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1884
Checksum: 309
Coasting Arc #9 (Orbit 1899)
---------------------------------------
Vector Time (GMT): 2017/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1594874
93 A = 6779667
78 meter
Y = -4392420
47 meter E =
0002978
Z = 4909211
86 I = 51
92463
XDOT = 5600
508004 Wp = 98
95480
YDOT = -4676
777789 meter/sec RA = 125
43093 deg
ZDOT = -2364
227469 TA = 14
10182
MA = 14
09351
Ha = 221
118 n
mi
Hp = 215
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5232529
29 X = -1569485
74
Y = -14410828
32 feet Y = -4410113
97 meter
Z = 16106338
11 Z = 4901525
67
XDOT = 18374
370093 XDOT = 5663
872977
YDOT = -15343
759151 feet/sec YDOT = -4613
794586 meter/sec
ZDOT = -7756
651802 ZDOT = -2336
868490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15353334
94 X = -4679696
49
Y = -628920
74 feet Y = -191695
04 meter
Z = 16073115
06 Z = 4899085
47
XDOT = -7102
898428 XDOT = -2164
963441
YDOT = -21795
848013 feet/sec YDOT = -6643
374474 meter/sec
ZDOT = -7635
137700 ZDOT = -2327
189971
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17150
54417731
00016717 00000-0 10270-3 0 9081
2 25544 51
6371 126
2667 0004833 215
4629 144
6202 15
53947119 19006
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
54417731 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 126
2667 deg
Eccentricity:
0004833
Arg of perigee: 215
4629 deg
Mean anomaly: 144
6202 deg
Mean motion: 15
53947119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1900
Checksum: 301
Coasting Arc #10 (Orbit 1914)
---------------------------------------
Vector Time (GMT): 2017/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 466635
07 A = 6783009
58 meter
Y = 5437052
50 meter E =
0006954
Z = -4036242
71 I = 51
95471
XDOT = -5600
466412 Wp = 147
62676
YDOT = 3418
154600 meter/sec RA = 120
46162 deg
ZDOT = 3954
404815 TA = 163
33953
MA = 163
31667
Ha = 220
921 n
mi
Hp = 216
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1530954
96 X = 425407
94
Y = 17838098
76 feet Y = 5442040
55 meter
Z = -13242266
12 Z = -4034075
63
XDOT = -18374
233634 XDOT = -5657
481438
YDOT = 11214
417980 feet/sec YDOT = 3355
207278 meter/sec
ZDOT = 12973
769077 ZDOT = 3927
061273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17172137
78 X = 5234067
60
Y = 5088154
66 feet Y = 1550869
54 meter
Z = -13233577
31 Z = -4033594
36
XDOT = 3972
014968 XDOT = 1210
670162
YDOT = 20044
272467 feet/sec YDOT = 6109
494248 meter/sec
ZDOT = 12852
509477 ZDOT = 3917
444889
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17151
50881824
00016717 00000-0 10270-3 0 9097
2 25544 51
6381 121
4594 0004725 219
1178 140
9634 15
53933253 19151
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
50881824 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 121
4594 deg
Eccentricity:
0004725
Arg of perigee: 219
1178 deg
Mean anomaly: 140
9634 deg
Mean motion: 15
53933253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1915
Checksum: 312
Coasting Arc #11 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2017/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 554759
75 A = 6786593
75 meter
Y = -6168894
97 meter E =
0011580
Z = 2756978
81 I = 51
98245
XDOT = 5357
836670 Wp = 120
62454
YDOT = -1835
481382 meter/sec RA = 115
50285 deg
ZDOT = -5174
751557 TA = 28
29947
MA = 28
23661
Ha = 220
762 n
mi
Hp = 216
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1820077
92 X = 610308
64
Y = -20239156
71 feet Y = -6162380
86 meter
Z = 9045206
08 Z = 2759808
17
XDOT = 17578
204299 XDOT = 5403
099752
YDOT = -6021
920543 feet/sec YDOT = -1775
312987 meter/sec
ZDOT = -16977
531355 ZDOT = -5148
614982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18309334
58 X = -5580685
18
Y = -8801142
04 feet Y = -2682588
09 meter
Z = 9058701
18 Z = 2761092
12
XDOT = -23
749443 XDOT = -7
238830
YDOT = -17340
771897 feet/sec YDOT = -5285
467274 meter/sec
ZDOT = -16861
844186 ZDOT = -5139
490108
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17152
53776533
00016717 00000-0 10270-3 0 9103
2 25544 51
6380 116
3312 0004665 223
9457 136
1325 15
53957562 19318
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
53776533 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 116
3312 deg
Eccentricity:
0004665
Arg of perigee: 223
9457 deg
Mean anomaly: 136
1325 deg
Mean motion: 15
53957562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1931
Checksum: 305
Coasting Arc #12 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2017/152/21:55:46
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1600801
28 A = 6781721
73 meter
Y = 4927366
62 meter E =
0008441
Z = -4384493
60 I = 51
97084
XDOT = -4976
589383 Wp = 143
66654
YDOT = 4690
780354 meter/sec RA = 113
44573 deg
ZDOT = 3451
376080 TA = 161
23746
MA = 161
20632
Ha = 220
824 n
mi
Hp = 216
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5251972
71 X = 1566880
98
Y = 16165900
98 feet Y = 4945078
49 meter
Z = -14384821
53 Z = -4376799
45
XDOT = -16327
392990 XDOT = -5045
438191
YDOT = 15389
699325 feet/sec YDOT = 4634
743580 meter/sec
ZDOT = 11323
412337 ZDOT = 3427
034357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14270594
05 X = -4349677
07
Y = -9285620
00 feet Y = -2830256
98 meter
Z = -14351657
36 Z = -4374385
16
XDOT = 2519
564498 XDOT = 767
963259
YDOT = -21222
508684 feet/sec YDOT = -6468
620647 meter/sec
ZDOT = 11215
178678 ZDOT = 3418
386461
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17152
92361977
00016717 00000-0 10270-3 0 9119
2 25544 51
6369 114
4048 0004917 221
5064 138
5716 15
53959562 19376
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
92361977 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 114
4048 deg
Eccentricity:
0004917
Arg of perigee: 221
5064 deg
Mean anomaly: 138
5716 deg
Mean motion: 15
53959562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 329
Coasting Arc #13 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/10:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4573510
33 A = 6780292
53 meter
Y = 1557852
07 meter E =
0007616
Z = 4757069
45 I = 51
97326
XDOT = 426
057632 Wp = 154
01665
YDOT = -7147
490753 meter/sec RA = 110
83763 deg
ZDOT = 2741
966472 TA = 268
93953
MA = 269
02679
Ha = 220
680 n
mi
Hp = 216
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15004955
14 X = -4613698
34
Y = 5111063
21 feet Y = 1506482
98 meter
Z = 15607183
23 Z = 4734755
13
XDOT = 1397
826875 XDOT = 492
631894
YDOT = -23449
772811 feet/sec YDOT = -7142
354218 meter/sec
ZDOT = 8995
952991 ZDOT = 2744
197395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5275718
90 X = -1608039
12
Y = 15050311
80 feet Y = 4587335
04 meter
Z = 15508408
01 Z = 4726962
76
XDOT = -16552
184827 XDOT = -5045
105935
YDOT = -15111
624308 feet/sec YDOT = -4606
023089 meter/sec
ZDOT = 9006
976688 ZDOT = 2745
326495
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17153
50240004
00016717 00000-0 10270-3 0 9122
2 25544 51
6372 111
5243 0004839 227
7565 132
3177 15
53978012 19466
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50240004 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 111
5243 deg
Eccentricity:
0004839
Arg of perigee: 227
7565 deg
Mean anomaly: 132
3177 deg
Mean motion: 15
53978012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 292
Coasting Arc #14 (Orbit 1946)
---------------------------------------
Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298369
86 A = 6778286
82 meter
Y = 208631
99 meter E =
0010532
Z = -5245812
58 I = 51
96923
XDOT = -1764
778625 Wp = 95
35978
YDOT = 7364
496167 meter/sec RA = 110
33354 deg
ZDOT = -1156
096147 TA = 163
61165
MA = 163
57757
Ha = 220
640 n
mi
Hp = 216
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14102263
32 X = 4321199
12
Y = 684488
16 feet Y = 256827
25 meter
Z = -17210671
21 Z = -5224876
87
XDOT = -5789
956118 XDOT = -1841
383415
YDOT = 24161
732830 feet/sec YDOT = 7344
332964 meter/sec
ZDOT = -3792
966360 ZDOT = -1164
854546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1219903
48 X = 371826
58
Y = -14178368
96 feet Y = -4321566
86 meter
Z = -17118272
32 Z = -5217649
40
XDOT = 22892
243241 XDOT = 6977
555740
YDOT = 6585
497002 feet/sec YDOT = 2007
259486 meter/sec
ZDOT = -3832
846516 ZDOT = -1168
251618
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17153
56671016
00016717 00000-0 10270-3 0 9130
2 25544 51
6389 111
2033 0004718 228
0697 132
0054 15
53962983 19476
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
56671016 = yrday
fracday
Element set: 913
Inclination: 51
6389 deg
RA of node: 111
2033 deg
Eccentricity:
0004718
Arg of perigee: 228
0697 deg
Mean anomaly: 132
0054 deg
Mean motion: 15
53962983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1947
Checksum: 310
Coasting Arc #15 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3783177
76 A = 6777938
48 meter
Y = -1877728
66 meter E =
0001836
Z = 5301956
29 I = 51
97940
XDOT = 2560
471539 Wp = 217
47171
YDOT = -7191
724467 meter/sec RA = 105
35922 deg
ZDOT = -721
545015 TA = 239
37940
MA = 239
39750
Ha = 220
517 n
mi
Hp = 216
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12412000
52 X = -3787653
84
Y = -6160527
10 feet Y = -1920060
08 meter
Z = 17394869
70 Z = 5283567
64
XDOT = 8400
497175 XDOT = 2644
205928
YDOT = -23594
896546 feet/sec YDOT = -7162
623307 meter/sec
ZDOT = -2367
273672 ZDOT = -708
904007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6415876
11 X = -1955559
04
Y = 12395709
26 feet Y = 3778212
18 meter
Z = 17313990
55 Z = 5277304
32
XDOT = -22512
695015 XDOT = -6861
869441
YDOT = -8432
529060 feet/sec YDOT = -2570
234858 meter/sec
ZDOT = -2310
263267 ZDOT = -704
168244
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17154
59565066
00016717 00000-0 10270-3 0 9142
2 25544 51
6396 106
0761 0004781 233
6739 126
3972 15
53981921 19639
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
59565066 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 106
0761 deg
Eccentricity:
0004781
Arg of perigee: 233
6739 deg
Mean anomaly: 126
3972 deg
Mean motion: 15
53981921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 335
Coasting Arc #16 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3215087
19 A = 6779894
13 meter
Y = 3489185
54 meter E =
0009418
Z = -4851712
98 I = 51
99373
XDOT = -3202
414879 Wp = 130
62224
YDOT = 6480
691349 meter/sec RA = 100
38585 deg
ZDOT = 2535
800559 TA = 164
23355
MA = 164
20421
Ha = 220
291 n
mi
Hp = 216
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10548186
32 X = 3199398
75
Y = 11447459
11 feet Y = 3525051
44 meter
Z = -15917693
51 Z = -4836132
78
XDOT = -10506
610497 XDOT = -3286
963466
YDOT = 21262
110724 feet/sec YDOT = 6444
406858 meter/sec
ZDOT = 8319
555640 ZDOT = 2520
039149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11482339
78 X = 3499817
16
Y = -10612782
11 feet Y = -3234775
99 meter
Z = -15849487
39 Z = -4830923
76
XDOT = 20452
777426 XDOT = 6234
006559
YDOT = 9795
930680 feet/sec YDOT = 2985
799671 meter/sec
ZDOT = 8248
868720 ZDOT = 2514
255186
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17155
56027953
00016717 00000-0 10270-3 0 9159
2 25544 51
6397 101
2676 0004636 236
5547 123
5162 15
53976270 19787
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
56027953 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 101
2676 deg
Eccentricity:
0004636
Arg of perigee: 236
5547 deg
Mean anomaly: 123
5162 deg
Mean motion: 15
53976270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 330
Coasting Arc #17 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2017/155/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3078828
11 A = 6786918
82 meter
Y = 5443690
78 meter E =
0009409
Z = 2627295
53 I = 52
01733
XDOT = -3363
726798 Wp = 86
91885
YDOT = -4449
230101 meter/sec RA = 100
34345 deg
ZDOT = 5261
170906 TA = 302
51277
MA = 302
60366
Ha = 220
320 n
mi
Hp = 216
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10101142
09 X = -3152234
31
Y = 17859877
89 feet Y = 5408850
61 meter
Z = 8619735
99 Z = 2612161
46
XDOT = -11035
849074 XDOT = -3339
280803
YDOT = -14597
211617 feet/sec YDOT = -4486
709258 meter/sec
ZDOT = 17261
059404 ZDOT = 5244
889849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18811354
69 X = 5733700
91
Y = 8264653
45 feet Y = 2519066
37 meter
Z = 8551993
72 Z = 2606647
69
XDOT = -12767
841939 XDOT = -3891
638223
YDOT = 11219
871379 feet/sec YDOT = 3419
816796 meter/sec
ZDOT = 17189
920507 ZDOT = 5239
487770
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17155
62458830
00016717 00000-0 10270-3 0 9169
2 25544 51
6399 100
9474 0004633 236
7532 123
3177 15
53967717 19795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
62458830 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 100
9474 deg
Eccentricity:
0004633
Arg of perigee: 236
7532 deg
Mean anomaly: 123
3177 deg
Mean motion: 15
53967717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 338
Coasting Arc #18 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/13:34:21
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3496580
07 A = 6783215
68 meter
Y = -4271489
38 meter E =
0002308
Z = -3943743
37 I = 52
01097
XDOT = 2641
307945 Wp = 100
48640
YDOT = 5926
652480 meter/sec RA = 95
38880 deg
ZDOT = -4079
795994 TA = 127
04020
MA = 127
01909
Ha = 220
205 n
mi
Hp = 216
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11471719
38 X = 3563242
12
Y = -14014072
78 feet Y = -4232015
19 meter
Z = -12938790
60 Z = -3926596
30
XDOT = 8665
708482 XDOT = 2594
656153
YDOT = 19444
397900 feet/sec YDOT = 5955
928871 meter/sec
ZDOT = -13385
157460 ZDOT = -4067
077988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15301021
16 X = -4663751
25
Y = -9790083
66 feet Y = -2984017
50 meter
Z = -12862344
15 Z = -3920442
50
XDOT = 17538
048617 XDOT = 5345
597219
YDOT = -9907
776644 feet/sec YDOT = -3019
890321 meter/sec
ZDOT = -13330
012544 ZDOT = -4062
987824
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17156
58921411
00016717 00000-0 10270-3 0 9176
2 25544 51
6408 96
1403 0004624 240
9201 119
1489 15
53990461 19942
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58921411 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 96
1403 deg
Eccentricity:
0004624
Arg of perigee: 240
9201 deg
Mean anomaly: 119
1489 deg
Mean motion: 15
53990461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 312
Coasting Arc #19 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1534562
80 A = 6789005
78 meter
Y = 6471437
30 meter E =
0008880
Z = 1340814
80 I = 52
02813
XDOT = -4409
294257 Wp = 58
98773
YDOT = -2262
680745 meter/sec RA = 94
28712 deg
ZDOT = 5850
262512 TA = 315
53070
MA = 315
60194
Ha = 220
118 n
mi
Hp = 216
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5034654
86 X = -1613327
16
Y = 21231749
69 feet Y = 6453836
27 meter
Z = 4398998
70 Z = 1333169
53
XDOT = -14466
188506 XDOT = -4412
082731
YDOT = -7423
493258 feet/sec YDOT = -2312
004562 meter/sec
ZDOT = 19193
774646 ZDOT = 5828
836276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6523751
48 X = 1988439
45
Y = -20829814
67 feet Y = -6348927
51 meter
Z = 4364128
92 Z = 1330186
50
XDOT = 12522
380028 XDOT = 3816
821432
YDOT = 7940
247875 feet/sec YDOT = 2420
187552 meter/sec
ZDOT = 19099
550760 ZDOT = 5821
543072
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 17156
84644536
00016717 00000-0 10270-3 0 9186
2 25544 51
6380 94
8564 0004922 241
3129 118
7529 15
53982192 19985
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84644536 = yrday
fracday
Element set: 918
Inclination: 51
6380 deg
RA of node: 94
8564 deg
Eccentricity:
0004922
Arg of perigee: 241
3129 deg
Mean anomaly: 118
7529 deg
Mean motion: 15
53982192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 345
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