[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 16th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
136/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 214
1
136/11:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 214
2
137/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
3
137/12:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 214
3
137/21:35:06
575 0
4 0
7 0
7
N/A 0
4 -0
1 222
4
000/00:00:13
149 -0
3 0
0 214
3
138/01:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
5
138/04:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
3
138/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
3
140/17:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
7
150/04:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
8
Coasting Arc #1 (Orbit 1666)
---------------------------------------
Vector Time (GMT): 2017/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5168224
82 A = 6787634
06 meter
Y = -3784077
80 meter E =
0014744
Z = 2233491
46 I = 51
51880
XDOT = 4525
062706 Wp = 91
65992
YDOT = -2949
463055 meter/sec RA = 200
11948 deg
ZDOT = 5442
197608 TA = 293
21208
MA = 293
36729
Ha = 222
393 n
mi
Hp = 214
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16956118
17 X = -5136375
50
Y = -12414953
40 feet Y = -3841694
47 meter
Z = 7327727
89 Z = 2208462
59
XDOT = 14846
006253 XDOT = 4531
272204
YDOT = -9676
716059 feet/sec YDOT = -2898
826421 meter/sec
ZDOT = 17854
979030 ZDOT = 5464
194104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20195465
09 X = -6155577
76
Y = 5948089
81 feet Y = 1812977
77 meter
Z = 7218034
67 Z = 2200056
97
XDOT = 1710
931513 XDOT = 521
491925
YDOT = -16103
606370 feet/sec YDOT = -4908
379221 meter/sec
ZDOT = 17952
327854 ZDOT = 5471
869530
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 17135
55994289
00016717 00000-0 10270-3 0 9005
2 25544 51
6399 200
9413 0005083 161
7578 198
3758 15
54007216 16677
Satellite: ISS
Catalog Number: 25544
Epoch time: 17135
55994289 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 200
9413 deg
Eccentricity:
0005083
Arg of perigee: 161
7578 deg
Mean anomaly: 198
3758 deg
Mean motion: 15
54007216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1667
Checksum: 336
Coasting Arc #2 (Orbit 1679)
---------------------------------------
Vector Time (GMT): 2017/136/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3039484
82 A = 6778689
40 meter
Y = -3321097
37 meter E =
0006132
Z = 5062233
48 I = 51
51518
XDOT = 6658
450123 Wp = 110
27000
YDOT = 3367
209123 meter/sec RA = 195
83637 deg
ZDOT = -1789
143751 TA = 357
05876
MA = 357
06236
Ha = 222
290 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9972063
07 X = 3051806
20
Y = -10895988
75 feet Y = -3287039
26 meter
Z = 16608377
54 Z = 5077028
20
XDOT = 21845
308804 XDOT = 6628
993111
YDOT = 11047
274027 feet/sec YDOT = 3441
503841 meter/sec
ZDOT = -5869
894195 ZDOT = -1756
870038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9933108
75 X = 3027611
55
Y = -10831059
08 feet Y = -3301306
81 meter
Z = 16674061
51 Z = 5082253
95
XDOT = 21022
072214 XDOT = 6407
527611
YDOT = 10462
479559 feet/sec YDOT = 3188
963769 meter/sec
ZDOT = -5728
201888 ZDOT = -1745
955935
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 17136
39593152
00016717 00000-0 10270-3 0 9013
2 25544 51
6396 196
7723 0005291 164
4059 195
7258 15
54012284 16807
Satellite: ISS
Catalog Number: 25544
Epoch time: 17136
39593152 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 196
7723 deg
Eccentricity:
0005291
Arg of perigee: 164
4059 deg
Mean anomaly: 195
7258 deg
Mean motion: 15
54012284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1680
Checksum: 324
Coasting Arc #3 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2017/136/11:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5541756
01 A = 6787752
94 meter
Y = 3268092
14 meter E =
0011205
Z = -2149520
48 I = 51
54912
XDOT = -4128
699886 Wp = 150
50367
YDOT = 3401
890680 meter/sec RA = 195
14436 deg
ZDOT = -5493
920024 TA = 53
36474
MA = 53
26176
Ha = 222
348 n
mi
Hp = 214
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18181614
20 X = 5515240
89
Y = 10722087
06 feet Y = 3329915
70 meter
Z = -7052232
54 Z = -2122664
25
XDOT = -13545
603301 XDOT = -4139
746830
YDOT = 11161
058661 feet/sec YDOT = 3355
659377 meter/sec
ZDOT = -18024
671995 ZDOT = -5514
002766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19632764
49 X = 5984066
62
Y = -7857289
36 feet Y = -2394901
80 meter
Z = -6934391
99 Z = -2113602
68
XDOT = 38
088594 XDOT = 11
609403
YDOT = 16017
225304 feet/sec YDOT = 4882
050273 meter/sec
ZDOT = -18113
668414 ZDOT = -5521
046133
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 17136
52454405
00016717 00000-0 10270-3 0 9026
2 25544 51
6389 196
1340 0005100 164
6135 195
5174 15
54018016 16820
Satellite: ISS
Catalog Number: 25544
Epoch time: 17136
52454405 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 196
1340 deg
Eccentricity:
0005100
Arg of perigee: 164
6135 deg
Mean anomaly: 195
5174 deg
Mean motion: 15
54018016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 290
Coasting Arc #4 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2017/137/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6349486
41 A = 6789340
85 meter
Y = 2173179
85 meter E =
0014350
Z = -977310
44 I = 51
57230
XDOT = -2367
287538 Wp = 150
57474
YDOT = 4281
947711 meter/sec RA = 192
25948 deg
ZDOT = -5907
614662 TA = 40
02526
MA = 39
91960
Ha = 222
192 n
mi
Hp = 214
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20831648
32 X = 6329460
77
Y = 7129855
14 feet Y = 2244072
20 meter
Z = -3206399
10 Z = -946514
83
XDOT = -7766
691397 XDOT = -2386
296909
YDOT = 14048
384878 feet/sec YDOT = 4255
369195 meter/sec
ZDOT = -19381
937866 ZDOT = -5919
160207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10525964
66 X = -3208314
03
Y = 19360947
14 feet Y = 5901216
69 meter
Z = -3071025
10 Z = -936048
45
XDOT = -11154
445837 XDOT = -3399
875091
YDOT = -9120
201103 feet/sec YDOT = -2779
837296 meter/sec
ZDOT = -19433
453098 ZDOT = -5923
316504
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 17137
10330261
00016717 00000-0 10270-3 0 9035
2 25544 51
6388 193
2507 0004812 169
1042 191
0216 15
53996930 16915
Satellite: ISS
Catalog Number: 25544
Epoch time: 17137
10330261 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 193
2507 deg
Eccentricity:
0004812
Arg of perigee: 169
1042 deg
Mean anomaly: 191
0216 deg
Mean motion: 15
53996930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 294
Coasting Arc #5 (Orbit 1697)
---------------------------------------
Vector Time (GMT): 2017/137/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 915820
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4895329
15 A = 6785368
53 meter
Y = 3440063
17 meter E =
0008085
Z = -3198441
52 I = 51
57454
XDOT = -5199
353405 Wp = 136
94280
YDOT = 2948
845880 meter/sec RA = 190
00389 deg
ZDOT = -4799
130655 TA = 80
05419
MA = 79
96294
Ha = 222
267 n
mi
Hp = 214
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16060791
19 X = 4872034
22
Y = 11286296
49 feet Y = 3494676
00 meter
Z = -10493574
54 Z = -3174717
70
XDOT = -17058
246081 XDOT = -5208
629732
YDOT = 9674
691206 feet/sec YDOT = 2890
651614 meter/sec
ZDOT = -15745
179313 ZDOT = -4824
410063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17122433
79 X = 5218917
82
Y = -9712067
13 feet Y = -2960238
06 meter
Z = -10389543
88 Z = -3166732
97
XDOT = 737
942325 XDOT = 224
924821
YDOT = 18218
247467 feet/sec YDOT = 5552
921828 meter/sec
ZDOT = -15857
018714 ZDOT = -4833
219304
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 17137
55344884
00016717 00000-0 10270-3 0 9041
2 25544 51
6396 191
0055 0005046 167
2075 192
9206 15
54027323 16981
Satellite: ISS
Catalog Number: 25544
Epoch time: 17137
55344884 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 191
0055 deg
Eccentricity:
0005046
Arg of perigee: 167
2075 deg
Mean anomaly: 192
9206 deg
Mean motion: 15
54027323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1698
Checksum: 316
Coasting Arc #6 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2017/137/21:35:13
149
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5359454
24 A = 6784488
55 meter
Y = -2100834
68 meter E =
0013904
Z = 3574924
67 I = 51
58263
XDOT = 4623
048425 Wp = 108
69471
YDOT = 4217
135440 meter/sec RA = 188
10212 deg
ZDOT = -4442
757682 TA = 28
97965
MA = 28
90252
Ha = 222
411 n
mi
Hp = 214
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17583511
30 X = 5365182
63
Y = -6892502
23 feet Y = -2040869
81 meter
Z = 11728755
48 Z = 3600973
24
XDOT = 15167
481710 XDOT = 4597
128624
YDOT = 13835
746193 feet/sec YDOT = 4268
688822 meter/sec
ZDOT = -14575
976648 ZDOT = -4420
362884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14369974
91 X = -4379968
35
Y = 12144006
29 feet Y = 3701493
12 meter
Z = 11843863
14 Z = 3610009
48
XDOT = -18008
545212 XDOT = -5489
004581
YDOT = -7158
372465 feet/sec YDOT = -2181
871927 meter/sec
ZDOT = -14477
912491 ZDOT = -4412
867727
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 17137
93929215
00016717 00000-0 10270-3 0 9051
2 25544 51
6398 189
0847 0005261 166
1820 193
9477 15
53890377 17049
Satellite: ISS
Catalog Number: 25544
Epoch time: 17137
93929215 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 189
0847 deg
Eccentricity:
0005261
Arg of perigee: 166
1820 deg
Mean anomaly: 193
9477 deg
Mean motion: 15
53890377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 344
Coasting Arc #7 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2017/138/01:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5287031
12 A = 6786393
07 meter
Y = 3054689
50 meter E =
0008581
Z = -2956975
31 I = 51
59293
XDOT = -4735
835533 Wp = 144
18910
YDOT = 3375
151046 meter/sec RA = 187
44103 deg
ZDOT = -4995
068178 TA = 69
60467
MA = 69
51252
Ha = 222
450 n
mi
Hp = 214
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17345902
63 X = 5266843
49
Y = 10021947
17 feet Y = 3113699
94 meter
Z = -9701362
56 Z = -2931341
21
XDOT = -15537
518152 XDOT = -4748
961599
YDOT = 11073
330204 feet/sec YDOT = 3322
118610 meter/sec
ZDOT = -16388
018956 ZDOT = -5018
105275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15359778
87 X = -4681660
60
Y = 12944782
59 feet Y = 3945569
73 meter
Z = -9588847
44 Z = -2922680
70
XDOT = -4198
505127 XDOT = -1279
704363
YDOT = -17162
009756 feet/sec YDOT = -5230
980574 meter/sec
ZDOT = -16490
046657 ZDOT = -5026
166221
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 17138
06791239
00016717 00000-0 10270-3 0 9060
2 25544 51
6394 188
4429 0005113 169
8915 190
2341 15
53891633 17063
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
06791239 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 188
4429 deg
Eccentricity:
0005113
Arg of perigee: 169
8915 deg
Mean anomaly: 190
2341 deg
Mean motion: 15
53891633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 327
Coasting Arc #8 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2017/138/04:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1634440
02 A = 6779201
03 meter
Y = 4229151
67 meter E =
0014026
Z = -5051200
86 I = 51
57173
XDOT = -7398
330947 Wp = 99
49309
YDOT = 624
246373 meter/sec RA = 186
75373 deg
ZDOT = -1877
974586 TA = 152
30295
MA = 152
22818
Ha = 222
563 n
mi
Hp = 214
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5362336
02 X = 1611563
51
Y = 13875169
51 feet Y = 4247301
44 meter
Z = -16572181
29 Z = -5043316
53
XDOT = -24272
739328 XDOT = -7395
639224
YDOT = 2048
052404 feet/sec YDOT = 541
528378 meter/sec
ZDOT = -6161
333944 ZDOT = -1913
907094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9495614
14 X = -2894263
19
Y = 11499475
04 feet Y = 3505039
99 meter
Z = -16538063
83 Z = -5040801
86
XDOT = -12676
445433 XDOT = -3863
780568
YDOT = -19524
579266 feet/sec YDOT = -5951
091760 meter/sec
ZDOT = -6319
785173 ZDOT = -1926
270521
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 17138
19653654
00016717 00000-0 10270-3 0 9073
2 25544 51
6376 187
7982 0005561 166
4850 193
6453 15
53915284 17089
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
19653654 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 187
7982 deg
Eccentricity:
0005561
Arg of perigee: 166
4850 deg
Mean anomaly: 193
6453 deg
Mean motion: 15
53915284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 346
Coasting Arc #9 (Orbit 1710)
---------------------------------------
Vector Time (GMT): 2017/138/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5680937
73 A = 6785703
58 meter
Y = -1928460
19 meter E =
0015353
Z = 3151069
12 I = 51
60185
XDOT = 4143
510192 Wp = 115
36709
YDOT = 4279
650144 meter/sec RA = 185
84892 deg
ZDOT = -4839
043068 TA = 28
23948
MA = 28
15632
Ha = 222
499 n
mi
Hp = 214
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18638247
16 X = 5686773
60
Y = -6326969
12 feet Y = -1864899
63 meter
Z = 10338153
27 Z = 3178679
64
XDOT = 13594
193542 XDOT = 4118
851947
YDOT = 14040
846928 feet/sec YDOT = 4325
848057 meter/sec
ZDOT = -15876
125552 ZDOT = -4818
974694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18386039
09 X = 5604064
71
Y = -6843358
21 feet Y = -2085855
58 meter
Z = 10460125
40 Z = 3188246
22
XDOT = 13586
089268 XDOT = 4141
040009
YDOT = 12309
816135 feet/sec YDOT = 3752
031958 meter/sec
ZDOT = -15788
316642 ZDOT = -4812
278912
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 17138
38947042
00016717 00000-0 10270-3 0 9082
2 25544 51
6404 186
8373 0005724 168
8789 191
2491 15
53891912 17114
Satellite: ISS
Catalog Number: 25544
Epoch time: 17138
38947042 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 186
8373 deg
Eccentricity:
0005724
Arg of perigee: 168
8789 deg
Mean anomaly: 191
2491 deg
Mean motion: 15
53891912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1711
Checksum: 340
Coasting Arc #10 (Orbit 1725)
---------------------------------------
Vector Time (GMT): 2017/139/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6449330
96 A = 6788740
09 meter
Y = 1255848
61 meter E =
0005323
Z = -1711025
36 I = 51
64468
XDOT = -2389
519517 Wp = 85
00887
YDOT = -4539
839216 meter/sec RA = 180
87305 deg
ZDOT = 5690
359714 TA = 256
24566
MA = 256
30492
Ha = 222
417 n
mi
Hp = 214
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21159222
29 X = -6454583
46
Y = 4120238
24 feet Y = 1183698
53 meter
Z = -5613600
25 Z = -1742367
18
XDOT = -7839
630960 XDOT = -2366
217461
YDOT = -14894
485617 feet/sec YDOT = -4566
430382 meter/sec
ZDOT = 18669
159166 ZDOT = 5678
808484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20914433
69 X = -6374719
39
Y = 5069840
42 feet Y = 1545287
36 meter
Z = -5751933
63 Z = -1753189
37
XDOT = -8256
345830 XDOT = -2516
534209
YDOT = -12992
825804 feet/sec YDOT = -3960
213305 meter/sec
ZDOT = 18618
917100 ZDOT = 5675
045932
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 17139
35413725
00016717 00000-0 10270-3 0 9097
2 25544 51
6407 182
0306 0005424 173
1728 186
9499 15
53880932 17265
Satellite: ISS
Catalog Number: 25544
Epoch time: 17139
35413725 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 182
0306 deg
Eccentricity:
0005424
Arg of perigee: 173
1728 deg
Mean anomaly: 186
9499 deg
Mean motion: 15
53880932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1726
Checksum: 326
Coasting Arc #11 (Orbit 1741)
---------------------------------------
Vector Time (GMT): 2017/140/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6758214
31 A = 6789992
61 meter
Y = -541468
01 meter E =
0016907
Z = 72817
34 I = 51
68060
XDOT = 451
278173 Wp = 147
12095
YDOT = 4736
872590 meter/sec RA = 175
90558 deg
ZDOT = -6019
220919 TA = 32
09473
MA = 31
99190
Ha = 222
395 n
mi
Hp = 214
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22172619
12 X = 6763413
15
Y = -1776469
84 feet Y = -465864
01 meter
Z = 238902
02 Z = 105659
60
XDOT = 1480
571434 XDOT = 427
514413
YDOT = 15540
920570 feet/sec YDOT = 4741
786407 meter/sec
ZDOT = -19748
100127 ZDOT = -6017
086295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22016665
30 X = 6710679
58
Y = -3155492
92 feet Y = -961794
24 meter
Z = 383759
76 Z = 116969
97
XDOT = 2345
180431 XDOT = 714
810995
YDOT = 13803
092292 feet/sec YDOT = 4207
182531 meter/sec
ZDOT = -19739
391174 ZDOT = -6016
566430
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 17140
38311482
00016717 00000-0 10270-3 0 9101
2 25544 51
6399 176
9034 0005666 176
7496 183
3694 15
53900046 17429
Satellite: ISS
Catalog Number: 25544
Epoch time: 17140
38311482 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 176
9034 deg
Eccentricity:
0005666
Arg of perigee: 176
7496 deg
Mean anomaly: 183
3694 deg
Mean motion: 15
53900046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1742
Checksum: 324
Coasting Arc #12 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2017/140/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1674043
13 A = 6778357
44 meter
Y = -3980638
24 meter E =
0008070
Z = 5223036
32 I = 51
65232
XDOT = 7407
845054 Wp = 155
22929
YDOT = -1649
726600 meter/sec RA = 174
08464 deg
ZDOT = 1109
203811 TA = 284
09978
MA = 284
18945
Ha = 222
197 n
mi
Hp = 214
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5492267
49 X = -1654777
42
Y = -13059836
75 feet Y = -3999250
96 meter
Z = 17135945
92 Z = 5214950
92
XDOT = 24303
953589 XDOT = 7420
354131
YDOT = -5412
488846 feet/sec YDOT = -1566
817150 meter/sec
ZDOT = 3639
120114 ZDOT = 1145
219578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4938206
71 X = -1505165
40
Y = 13324361
85 feet Y = 4061265
49 meter
Z = 17100891
10 Z = 5212351
61
XDOT = -20351
849402 XDOT = -6203
243698
YDOT = -12450
203101 feet/sec YDOT = -3794
821905 meter/sec
ZDOT = 3798
137976 ZDOT = 1157
672455
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 17140
76898007
00016717 00000-0 10270-3 0 9117
2 25544 51
6383 174
9826 0005111 178
3650 181
7520 15
53935263 17489
Satellite: ISS
Catalog Number: 25544
Epoch time: 17140
76898007 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 174
9826 deg
Eccentricity:
0005111
Arg of perigee: 178
3650 deg
Mean anomaly: 181
7520 deg
Mean motion: 15
53935263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 320
Coasting Arc #13 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2017/141/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -52905
04 A = 6778151
79 meter
Y = 4262052
79 meter E =
0015830
Z = -5283414
32 I = 51
68405
XDOT = -7571
832980 Wp = 114
48818
YDOT = 850
382610 meter/sec RA = 169
08809 deg
ZDOT = 757
193613 TA = 162
77938
MA = 162
72562
Ha = 222
079 n
mi
Hp = 214
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -173572
98 X = -74895
88
Y = 13983112
83 feet Y = 4261338
36 meter
Z = -17334036
47 Z = -5283724
61
XDOT = -24841
971718 XDOT = -7584
457555
YDOT = 2789
969192 feet/sec YDOT = 765
638635 meter/sec
ZDOT = 2484
231015 ZDOT = 720
380805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9504070
90 X = 2896840
81
Y = -10254796
90 feet Y = -3125662
09 meter
Z = -17336036
73 Z = -5284023
99
XDOT = 19444
526950 XDOT = 5926
691814
YDOT = 14070
366666 feet/sec YDOT = 4288
647760 meter/sec
ZDOT = 2321
800125 ZDOT = 707
684678
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 17141
73364244
00016717 00000-0 10270-3 0 9127
2 25544 51
6386 170
1744 0005047 181
0088 179
1056 15
53913668 17630
Satellite: ISS
Catalog Number: 25544
Epoch time: 17141
73364244 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 170
1744 deg
Eccentricity:
0005047
Arg of perigee: 181
0088 deg
Mean anomaly: 179
1056 deg
Mean motion: 15
53913668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 311
Coasting Arc #14 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2017/142/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1715404
74 A = 6780027
28 meter
Y = -4443356
68 meter E =
0006020
Z = 4819590
21 I = 51
72180
XDOT = 7236
564621 Wp = 103
91286
YDOT = 28
880328 meter/sec RA = 164
09796 deg
ZDOT = -2547
785038 TA = 11
12016
MA = 11
10686
Ha = 221
962 n
mi
Hp = 214
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5627968
30 X = 1741552
38
Y = -14577941
85 feet Y = -4424027
83 meter
Z = 15812303
82 Z = 4827986
61
XDOT = 23742
009913 XDOT = 7248
079955
YDOT = 94
751732 feet/sec YDOT = 109
868974 meter/sec
ZDOT = -8358
874797 ZDOT = -2512
603424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13807910
76 X = -4208651
20
Y = 7234556
20 feet Y = 2205092
73 meter
Z = 15849989
43 Z = 4831076
78
XDOT = -17207
205606 XDOT = -5244
756269
YDOT = -14859
416990 feet/sec YDOT = -4529
150299 meter/sec
ZDOT = -8203
749708 ZDOT = -2500
502911
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
76261269
00016717 00000-0 10270-3 0 9135
2 25544 51
6382 165
0473 0004970 184
2339 175
8772 15
53917930 17797
Satellite: ISS
Catalog Number: 25544
Epoch time: 17142
76261269 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 165
0473 deg
Eccentricity:
0004970
Arg of perigee: 184
2339 deg
Mean anomaly: 175
8772 deg
Mean motion: 15
53917930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 336
Coasting Arc #15 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2017/143/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3216034
41 A = 6783407
75 meter
Y = 4524124
68 meter E =
0008786
Z = -3909489
14 I = 51
76364
XDOT = -6395
619249 Wp = 141
04190
YDOT = -1009
876893 meter/sec RA = 159
11622 deg
ZDOT = 4090
869289 TA = 171
81050
MA = 171
79614
Ha = 221
872 n
mi
Hp = 215
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10551294
01 X = -3247394
55
Y = 14842928
76 feet Y = 4487985
68 meter
Z = -12826407
93 Z = -3925187
90
XDOT = -20983
002785 XDOT = -6403
723066
YDOT = -3313
244400 feet/sec YDOT = -1081
442570 meter/sec
ZDOT = 13421
487167 ZDOT = 4059
780944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17606618
95 X = 5366497
46
Y = -4455449
67 feet Y = -1358021
06 meter
Z = -12896317
97 Z = -3930797
72
XDOT = 13516
179277 XDOT = 4119
731444
YDOT = 14944
039245 feet/sec YDOT = 4554
943162 meter/sec
ZDOT = 13284
543100 ZDOT = 4049
128737
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
72727020
00016717 00000-0 10270-3 0 9145
2 25544 51
6378 160
2399 0004988 188
7377 171
3689 15
53916464 17942
Satellite: ISS
Catalog Number: 25544
Epoch time: 17143
72727020 = yrday
fracday
Element set: 914
Inclination: 51
6378 deg
RA of node: 160
2399 deg
Eccentricity:
0004988
Arg of perigee: 188
7377 deg
Mean anomaly: 171
3689 deg
Mean motion: 15
53916464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 351
Coasting Arc #16 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2017/144/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429567
13 A = 6786966
77 meter
Y = -4421684
60 meter E =
0014449
Z = 2602464
06 I = 51
80650
XDOT = 5182
099008 Wp = 122
97802
YDOT = 2087
477541 meter/sec RA = 154
14592 deg
ZDOT = -5260
133082 TA = 27
77861
MA = 27
70152
Ha = 221
688 n
mi
Hp = 215
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14532700
56 X = 4466040
57
Y = -14506839
24 feet Y = -4371946
45 meter
Z = 8538267
92 Z = 2624070
25
XDOT = 17001
637165 XDOT = 5183
922858
YDOT = 6848
679597 feet/sec YDOT = 2145
437892 meter/sec
ZDOT = -17257
654468 ZDOT = -5234
954891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20401643
09 X = -6218420
81
Y = 1942363
05 feet Y = 592032
26 meter
Z = 8634232
69 Z = 2631714
12
XDOT = -8674
777628 XDOT = -2644
072221
YDOT = -14699
952731 feet/sec YDOT = -4480
545592 meter/sec
ZDOT = -17146
925116 ZDOT = -5226
382775
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
75623507
00016717 00000-0 10270-3 0 9155
2 25544 51
6386 155
1117 0004914 192
7523 167
3506 15
53931232 18101
Satellite: ISS
Catalog Number: 25544
Epoch time: 17144
75623507 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 155
1117 deg
Eccentricity:
0004914
Arg of perigee: 192
7523 deg
Mean anomaly: 167
3506 deg
Mean motion: 15
53931232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 300
Coasting Arc #17 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2017/145/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5283805
41 A = 6789398
03 meter
Y = 4126237
30 meter E =
0005300
Z = -1065368
86 I = 51
84270
XDOT = -3687
291907 Wp = 58
80262
YDOT = -3203
286191 meter/sec RA = 149
18570 deg
ZDOT = 5905
345696 TA = 289
68414
MA = 289
74132
Ha = 221
624 n
mi
Hp = 215
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17335319
60 X = -5324378
23
Y = 13537523
95 feet Y = 4066923
47 meter
Z = -3495304
66 Z = -1091134
59
XDOT = -12097
414393 XDOT = -3679
883729
YDOT = -10509
469131 feet/sec YDOT = -3244
479181 meter/sec
ZDOT = 19374
493754 ZDOT = 5887
451266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21975236
85 X = 6698052
19
Y = 234130
28 feet Y = 71362
91 meter
Z = -3609593
25 Z = -1100204
02
XDOT = 3005
114022 XDOT = 915
958754
YDOT = 14237
405417 feet/sec YDOT = 4339
561171 meter/sec
ZDOT = 19296
053297 ZDOT = 5881
437045
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
72088649
00016717 00000-0 10270-3 0 9166
2 25544 51
6379 150
3041 0004844 196
1353 163
9646 15
53926279 18255
Satellite: ISS
Catalog Number: 25544
Epoch time: 17145
72088649 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 150
3041 deg
Eccentricity:
0004844
Arg of perigee: 196
1353 deg
Mean anomaly: 163
9646 deg
Mean motion: 15
53926279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 335
Coasting Arc #18 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2017/146/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5743949
33 A = 6789788
86 meter
Y = -3554151
90 meter E =
0013941
Z = -603400
75 I = 51
87231
XDOT = 2051
060486 Wp = 157
30699
YDOT = 4322
836227 meter/sec RA = 144
23168 deg
ZDOT = -5996
270539 TA = 29
18769
MA = 29
10985
Ha = 221
592 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18844978
11 X = 5786196
95
Y = -11660603
34 feet Y = -3489682
87 meter
Z = -1979661
25 Z = -575395
80
XDOT = 6729
201071 XDOT = 2031
696360
YDOT = 14182
533554 feet/sec YDOT = 4345
665049 meter/sec
ZDOT = -19672
803607 ZDOT = -5986
353458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22053440
87 X = -6721888
78
Y = -2285733
59 feet Y = -696691
60 meter
Z = -1855558
31 Z = -565574
17
XDOT = 3065
567585 XDOT = 934
385000
YDOT = -13808
455306 feet/sec YDOT = -4208
817177 meter/sec
ZDOT = -19629
724774 ZDOT = -5983
140111
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
74984672
00016717 00000-0 10270-3 0 9171
2 25544 51
6389 145
1761 0004922 200
0464 160
0496 15
53924567 18419
Satellite: ISS
Catalog Number: 25544
Epoch time: 17146
74984672 = yrday
fracday
Element set: 917
Inclination: 51
6389 deg
RA of node: 145
1761 deg
Eccentricity:
0004922
Arg of perigee: 200
0464 deg
Mean anomaly: 160
0496 deg
Mean motion: 15
53924567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 324
Coasting Arc #19 (Orbit 1856)
---------------------------------------
Vector Time (GMT): 2017/147/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5809766
14 A = 6787940
18 meter
Y = 2737864
24 meter E =
0011091
Z = 2187079
52 I = 51
89231
XDOT = -428
933046 Wp = 89
02622
YDOT = -5323
265192 meter/sec RA = 139
27692 deg
ZDOT = 5500
569735 TA = 295
15815
MA = 295
27315
Ha = 221
408 n
mi
Hp = 215
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19060912
54 X = -5850573
73
Y = 8982494
24 feet Y = 2672667
05 meter
Z = 7175457
73 Z = 2158758
43
XDOT = -1407
260648 XDOT = -396
094359
YDOT = -17464
780813 feet/sec YDOT = -5327
878931 meter/sec
ZDOT = 18046
488633 ZDOT = 5498
565143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20691084
60 X = 6306642
59
Y = 4203142
75 feet Y = 1281117
91 meter
Z = 7050063
28 Z = 2148859
29
XDOT = -8897
495944 XDOT = -2711
956764
YDOT = 13410
111139 feet/sec YDOT = 4087
401875 meter/sec
ZDOT = 18038
479995 ZDOT = 5498
128702
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
77880402
00016717 00000-0 10270-3 0 9182
2 25544 51
6393 140
0480 0004852 204
5946 155
4976 15
53934000 18573
Satellite: ISS
Catalog Number: 25544
Epoch time: 17147
77880402 = yrday
fracday
Element set: 918
Inclination: 51
6393 deg
RA of node: 140
0480 deg
Eccentricity:
0004852
Arg of perigee: 204
5946 deg
Mean anomaly: 155
4976 deg
Mean motion: 15
53934000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1857
Checksum: 319
Coasting Arc #20 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2017/148/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5521706
88 A = 6784482
49 meter
Y = -1627149
44 meter E =
0004691
Z = -3589567
16 I = 51
90661
XDOT = -1092
924716 Wp = 142
01787
YDOT = 6132
391336 meter/sec RA = 134
31720 deg
ZDOT = -4467
715792 TA = 80
22921
MA = 80
17624
Ha = 221
326 n
mi
Hp = 215
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18115836
21 X = 5556928
14
Y = -5338416
80 feet Y = -1565204
58 meter
Z = -11776795
15 Z = -3562658
94
XDOT = -3585
711012 XDOT = -1139
715416
YDOT = 20119
394146 feet/sec YDOT = 6119
908463 meter/sec
ZDOT = -14657
860209 ZDOT = -4473
137769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17891995
42 X = -5453480
20
Y = -6272763
62 feet Y = -1911938
35 meter
Z = -11657789
50 Z = -3553294
24
XDOT = 14110
730578 XDOT = 4300
950680
YDOT = -13002
141804 feet/sec YDOT = -3963
052822 meter/sec
ZDOT = -14682
759251 ZDOT = -4475
305020
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
74344741
00016717 00000-0 10270-3 0 9192
2 25544 51
6409 135
2408 0004794 208
5428 151
5462 15
53953887 18729
Satellite: ISS
Catalog Number: 25544
Epoch time: 17148
74344741 = yrday
fracday
Element set: 919
Inclination: 51
6409 deg
RA of node: 135
2408 deg
Eccentricity:
0004794
Arg of perigee: 208
5428 deg
Mean anomaly: 151
5462 deg
Mean motion: 15
53953887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 335
Coasting Arc #21 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2017/149/17:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4951044
59 A = 6780938
06 meter
Y = 327051
11 meter E =
0009240
Z = 4621046
33 I = 51
91631
XDOT = 2384
996250 Wp = 145
14160
YDOT = -6634
480519 meter/sec RA = 129
34952 deg
ZDOT = 3014
506348 TA = 274
83975
MA = 274
94525
Ha = 221
254 n
mi
Hp = 215
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16243584
62 X = -4976780
60
Y = 1073002
33 feet Y = 271540
75 meter
Z = 15160913
14 Z = 4596933
17
XDOT = 7824
790848 XDOT = 2444
364478
YDOT = -21766
668369 feet/sec YDOT = -6607
478272 meter/sec
ZDOT = 9890
112691 ZDOT = 3026
235379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14048511
65 X = 4281986
35
Y = 8417957
62 feet Y = 2565793
48 meter
Z = 15054433
65 Z = 4588591
38
XDOT = -18154
856531 XDOT = -5533
600271
YDOT = 12455
301494 feet/sec YDOT = 3796
375896 meter/sec
ZDOT = 9942
938948 ZDOT = 3030
607791
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
77239980
00016717 00000-0 10270-3 0 9206
2 25544 51
6406 130
1132 0004774 211
3378 148
7491 15
53944116 18880
Satellite: ISS
Catalog Number: 25544
Epoch time: 17149
77239980 = yrday
fracday
Element set: 920
Inclination: 51
6406 deg
RA of node: 130
1132 deg
Eccentricity:
0004774
Arg of perigee: 211
3378 deg
Mean anomaly: 148
7491 deg
Mean motion: 15
53944116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1888
Checksum: 320
Coasting Arc #22 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2017/150/04:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 915754
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1770705
66 A = 6779100
52 meter
Y = -4189746
74 meter E =
0002377
Z = 5024466
53 I = 51
92049
XDOT = 5619
752254 Wp = 118
80450
YDOT = -4808
782202 meter/sec RA = 127
02974 deg
ZDOT = -2029
791389 TA = 350
83924
MA = 350
84358
Ha = 221
224 n
mi
Hp = 215
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5809401
77 X = -1748129
62
Y = -13745888
26 feet Y = -4209422
27 meter
Z = 16484470
24 Z = 5015919
37
XDOT = 18437
507395 XDOT = 5682
967382
YDOT = -15776
844495 feet/sec YDOT = -4745
584655 meter/sec
ZDOT = -6659
420567 ZDOT = -2002
339322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6488642
58 X = 1977738
26
Y = -13483932
45 feet Y = -4109902
61 meter
Z = 16447414
24 Z = 5013171
86
XDOT = 23049
157086 XDOT = 7025
383080
YDOT = 3118
842501 feet/sec YDOT = 950
623194 meter/sec
ZDOT = -6537
480330 ZDOT = -1992
624004
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
22256384
00016717 00000-0 10270-3 0 9216
2 25544 51
6410 127
8665 0005217 212
6502 147
4328 15
53976899 18951
Satellite: ISS
Catalog Number: 25544
Epoch time: 17150
22256384 = yrday
fracday
Element set: 921
Inclination: 51
6410 deg
RA of node: 127
8665 deg
Eccentricity:
0005217
Arg of perigee: 212
6502 deg
Mean anomaly: 147
4328 deg
Mean motion: 15
53976899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 321
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