[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 8th 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) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
315/12:37:22
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
4
317/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
317/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2017/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 307202
34 A = 6779317
71 meter
Y = -4673839
97 meter E =
0015693
Z = -4915343
03 I = 51
86403
XDOT = 6676
776720 Wp = 80
06065
YDOT = 2912
982277 meter/sec RA = 38
28295 deg
ZDOT = -2356
330880 TA = 166
92491
MA = 166
88418
Ha = 222
544 n
mi
Hp = 213
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1007881
70 X = 383320
39
Y = -15334120
63 feet Y = -4669978
85 meter
Z = -16126453
50 Z = -4913665
99
XDOT = 21905
435434 XDOT = 6655
152843
YDOT = 9557
028469 feet/sec YDOT = 2987
525729 meter/sec
ZDOT = -7730
744358 ZDOT = -2323
949008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10455608
95 X = 3186869
61
Y = 11273759
34 feet Y = 3436241
85 meter
Z = -16118193
92 Z = -4912825
51
XDOT = -21141
171131 XDOT = -6443
828961
YDOT = 8776
626138 feet/sec YDOT = 2675
115647 meter/sec
ZDOT = -7587
524839 ZDOT = -2312
677571
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 17312
52015916
00016717 00000-0 10270-3 0 9000
2 25544 51
6417 38
8027 0003993 102
8832 257
2767 15
54062835 4191
Satellite: ISS
Catalog Number: 25544
Epoch time: 17312
52015916 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 38
8027 deg
Eccentricity:
0003993
Arg of perigee: 102
8832 deg
Mean anomaly: 257
2767 deg
Mean motion: 15
54062835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 305
Coasting Arc #2 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2017/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1827168
36 A = 6777431
04 meter
Y = 3790783
60 meter E =
0006692
Z = 5307302
42 I = 51
83273
XDOT = -6604
807256 Wp = 105
92146
YDOT = -3875
699590 meter/sec RA = 33
29940 deg
ZDOT = 492
077859 TA = 339
38670
MA = 339
41369
Ha = 222
527 n
mi
Hp = 213
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5994646
85 X = -1895202
75
Y = 12436954
06 feet Y = 3769970
42 meter
Z = 17412409
53 Z = 5298261
33
XDOT = -21669
315144 XDOT = -6563
367568
YDOT = -12715
549837 feet/sec YDOT = -3949
327363 meter/sec
ZDOT = 1614
428672 ZDOT = 460
093863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5152150
15 X = -1570375
37
Y = -12864212
39 feet Y = -3921011
94 meter
Z = 17371615
10 Z = 5294868
28
XDOT = 23019
934699 XDOT = 7016
476096
YDOT = -7219
988755 feet/sec YDOT = -2200
652573 meter/sec
ZDOT = 1473
148405 ZDOT = 449
015634
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 17313
54901810
00016717 00000-0 10270-3 0 9011
2 25544 51
6425 33
6740 0004009 104
3632 255
7966 15
54120801 4359
Satellite: ISS
Catalog Number: 25544
Epoch time: 17313
54901810 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 33
6740 deg
Eccentricity:
0004009
Arg of perigee: 104
3632 deg
Mean anomaly: 255
7966 deg
Mean motion: 15
54120801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 274
Coasting Arc #3 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2017/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3354753
15 A = 6778164
36 meter
Y = -2825217
71 meter E =
0017821
Z = -5183732
87 I = 51
80575
XDOT = 6012
471769 Wp = 101
75375
YDOT = 4516
978222 meter/sec RA = 28
31294 deg
ZDOT = 1429
884139 TA = 181
99206
MA = 181
99917
Ha = 222
510 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11006407
96 X = 3411276
49
Y = -9269086
97 feet Y = -2787386
49 meter
Z = -17006997
60 Z = -5167299
05
XDOT = 19725
957247 XDOT = 5954
569091
YDOT = 14819
482357 feet/sec YDOT = 4583
890024 meter/sec
ZDOT = 4691
220929 ZDOT = 1458
950607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -305300
51 X = -93055
60
Y = 14472604
55 feet Y = 4411249
87 meter
Z = -16933560
34 Z = -5161349
19
XDOT = -23053
041181 XDOT = -7026
566952
YDOT = 5150
236062 feet/sec YDOT = 1569
791952 meter/sec
ZDOT = 4819
432809 ZDOT = 1468
963120
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 17314
51357107
00016717 00000-0 10270-3 0 9024
2 25544 51
6414 28
8667 0004079 105
6093 254
5510 15
54097589 4508
Satellite: ISS
Catalog Number: 25544
Epoch time: 17314
51357107 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 28
8667 deg
Eccentricity:
0004079
Arg of perigee: 105
6093 deg
Mean anomaly: 254
5510 deg
Mean motion: 15
54097589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 450
Checksum: 306
Coasting Arc #4 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4726284
84 A = 6780819
36 meter
Y = 1819680
95 meter E =
0012368
Z = 4499529
70 I = 51
78610
XDOT = -4956
880201 Wp = 80
43558
YDOT = -4896
081793 meter/sec RA = 23
32862 deg
ZDOT = -3217
103651 TA = 41
85738
MA = 41
76288
Ha = 222
526 n
mi
Hp = 213
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15506183
86 X = -4768138
50
Y = 5970081
86 feet Y = 1766594
43 meter
Z = 14762236
56 Z = 4476468
93
XDOT = -16262
730319 XDOT = -4886
135198
YDOT = -16063
260476 feet/sec YDOT = -4951
117486 meter/sec
ZDOT = -10554
802006 ZDOT = -3241
011050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5467545
95 X = 1666508
01
Y = -15786395
02 feet Y = -4811693
20 meter
Z = 14659567
43 Z = 4468236
15
XDOT = 21565
033756 XDOT = 6573
022289
YDOT = -2459
409915 feet/sec YDOT = -749
628142 meter/sec
ZDOT = -10660
042179 ZDOT = -3249
180856
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 17315
54242153
00016717 00000-0 10270-3 0 9033
2 25544 51
6418 23
7380 0003984 109
7372 250
4211 15
54137470 4661
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242153 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 23
7380 deg
Eccentricity:
0003984
Arg of perigee: 109
7372 deg
Mean anomaly: 250
4211 deg
Mean motion: 15
54137470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 288
Coasting Arc #5 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2017/315/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1384547
72 A = 6777519
94 meter
Y = -3973685
90 meter E =
0018687
Z = -5329055
11 I = 51
77275
XDOT = 7109
009391 Wp = 92
41501
YDOT = 2826
123359 meter/sec RA = 23
22510 deg
ZDOT = -261
899915 TA = 175
09790
MA = 175
07957
Ha = 222
514 n
mi
Hp = 213
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4542479
41 X = 1454765
89
Y = -13037027
23 feet Y = -3957810
38 meter
Z = -17483776
61 Z = -5322158
74
XDOT = 23323
521624 XDOT = 7078
150762
YDOT = 9272
058264 feet/sec YDOT = 2905
448614 meter/sec
ZDOT = -859
251688 ZDOT = -227
441115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8837509
44 X = 2693672
88
Y = 10657882
16 feet Y = 3248522
48 meter
Z = -17452467
38 Z = -5319512
06
XDOT = -19099
836089 XDOT = -5821
630040
YDOT = 14688
545283 feet/sec YDOT = 4477
068602 meter/sec
ZDOT = -706
817083 ZDOT = -215
437847
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 17315
54242294
00016717 00000-0 10270-3 0 9040
2 25544 51
6407 23
7385 0004056 109
7111 250
4479 15
54078966 4666
Satellite: ISS
Catalog Number: 25544
Epoch time: 17315
54242294 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 23
7385 deg
Eccentricity:
0004056
Arg of perigee: 109
7111 deg
Mean anomaly: 250
4479 deg
Mean motion: 15
54078966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 310
Coasting Arc #6 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2017/316/12:37:22
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3036120
35 A = 6778277
05 meter
Y = 3243836
60 meter E =
0008098
Z = 5112549
28 I = 51
74619
XDOT = -6596
909175 Wp = 79
16768
YDOT = -3551
686601 meter/sec RA = 18
23431 deg
ZDOT = -1660
409335 TA = 26
84689
MA = 26
80501
Ha = 222
495 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9961024
78 X = -3097002
75
Y = 10642508
53 feet Y = 3209544
33 meter
Z = 16773455
64 Z = 5097652
59
XDOT = -21643
402806 XDOT = -6548
637401
YDOT = -11652
515095 feet/sec YDOT = -3625
187881 meter/sec
ZDOT = -5447
537189 ZDOT = -1692
338195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4257674
44 X = -1297739
17
Y = -14021048
81 feet Y = -4273615
68 meter
Z = 16706771
54 Z = 5092223
96
XDOT = 19803
506653 XDOT = 6036
108828
YDOT = -12687
274053 feet/sec YDOT = -3867
081131 meter/sec
ZDOT = -5588
605043 ZDOT = -1703
406817
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 17316
57126734
00016717 00000-0 10270-3 0 9055
2 25544 51
6415 18
6100 0004013 112
2135 247
9444 15
54137822 4829
Satellite: ISS
Catalog Number: 25544
Epoch time: 17316
57126734 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 18
6100 deg
Eccentricity:
0004013
Arg of perigee: 112
2135 deg
Mean anomaly: 247
9444 deg
Mean motion: 15
54137822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 482
Checksum: 278
Coasting Arc #7 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2017/317/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5331856
55 A = 6786586
53 meter
Y = -3351221
35 meter E =
0009262
Z = -2528178
92 I = 51
74539
XDOT = 4516
368790 Wp = 122
76642
YDOT = -3201
056877 meter/sec RA = 13
69716 deg
ZDOT = -5300
733562 TA = 85
55571
MA = 85
44990
Ha = 222
416 n
mi
Hp = 213
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17492967
68 X = -5281705
16
Y = -10994820
71 feet Y = -3410565
48 meter
Z = -8294550
25 Z = -2553957
95
XDOT = 14817
482906 XDOT = 4577
576994
YDOT = -10502
155107 feet/sec YDOT = -3150
209672 meter/sec
ZDOT = -17390
858142 ZDOT = -5278
645313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20614853
31 X = 6283407
29
Y = 130379
56 feet Y = 39739
69 meter
Z = -8408352
31 Z = -2562865
78
XDOT = -7124
838561 XDOT = -2171
650793
YDOT = 15300
712731 feet/sec YDOT = 4663
657240 meter/sec
ZDOT = -17292
271546 ZDOT = -5270
684367
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 17317
47150436
00016717 00000-0 10270-3 0 9062
2 25544 51
6418 14
1219 0004145 116
4041 243
7537 15
54112601 4962
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
47150436 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 14
1219 deg
Eccentricity:
0004145
Arg of perigee: 116
4041 deg
Mean anomaly: 243
7537 deg
Mean motion: 15
54112601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 278
Coasting Arc #8 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4950971
79 A = 6782476
63 meter
Y = -2271196
23 meter E =
0011115
Z = -4052966
60 I = 51
71711
XDOT = 5103
517088 Wp = 108
73038
YDOT = 4165
289641 meter/sec RA = 11
32057 deg
ZDOT = 3905
442472 TA = 201
76299
MA = 201
81025
Ha = 222
453 n
mi
Hp = 213
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16243345
77 X = 4995688
63
Y = -7451431
20 feet Y = -2215581
17 meter
Z = -13297134
50 Z = -4028807
19
XDOT = 16743
822466 XDOT = 5037
589324
YDOT = 13665
648428 feet/sec YDOT = 4221
992148 meter/sec
ZDOT = 12813
131471 ZDOT = 3930
073977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12584407
78 X = 3835727
49
Y = -12800507
50 feet Y = -3901594
69 meter
Z = -13189525
51 Z = -4020167
37
XDOT = 19512
056425 XDOT = 5947
274798
YDOT = 5886
295174 feet/sec YDOT = 1794
142769 meter/sec
ZDOT = 12921
691742 ZDOT = 3938
531643
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 17317
92162213
00016717 00000-0 10270-3 0 9079
2 25544 51
6423 11
8803 0004112 111
5496 248
6096 15
54132740 5034
Satellite: ISS
Catalog Number: 25544
Epoch time: 17317
92162213 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 11
8803 deg
Eccentricity:
0004112
Arg of perigee: 111
5496 deg
Mean anomaly: 248
6096 deg
Mean motion: 15
54132740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 277
Coasting Arc #9 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2017/318/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6025739
29 A = 6786339
58 meter
Y = 1492249
10 meter E =
0017542
Z = 2720758
74 I = 51
69714
XDOT = -3457
981121 Wp = 104
84828
YDOT = -4493
476978 meter/sec RA = 6
34405 deg
ZDOT = -5170
531142 TA = 44
38592
MA = 44
24545
Ha = 222
517 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19769485
86 X = -6055194
57
Y = 4895830
39 feet Y = 1424700
54 meter
Z = 8926373
80 Z = 2691415
34
XDOT = -11345
082418 XDOT = -3382
360402
YDOT = -14742
378537 feet/sec YDOT = -4531
723798 meter/sec
ZDOT = -16963
684848 ZDOT = -5187
145516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16561481
89 X = -5047939
68
Y = 11951199
66 feet Y = 3642725
66 meter
Z = 8795909
27 Z = 2680993
15
XDOT = -15057
683263 XDOT = -4589
581859
YDOT = -8270
221255 feet/sec YDOT = -2520
763439 meter/sec
ZDOT = -17036
602932 ZDOT = -5192
756574
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 17318
95045872
00016717 00000-0 10270-3 0 9085
2 25544 51
6419 6
7527 0004108 116
7861 243
3712 15
54109104 5195
Satellite: ISS
Catalog Number: 25544
Epoch time: 17318
95045872 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 6
7527 deg
Eccentricity:
0004108
Arg of perigee: 116
7861 deg
Mean anomaly: 243
3712 deg
Mean motion: 15
54109104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 304
Coasting Arc #10 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2017/319/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6647100
54 A = 6788754
36 meter
Y = -746931
74 meter E =
0010797
Z = -1146064
19 I = 51
67409
XDOT = 1530
717617 Wp = 58
94624
YDOT = 4681
068388 meter/sec RA = 1
37265 deg
ZDOT = 5873
667316 TA = 288
62254
MA = 288
73975
Ha = 222
338 n
mi
Hp = 213
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21808072
63 X = 6660526
05
Y = -2450563
45 feet Y = -672524
27 meter
Z = -3760053
11 Z = -1113741
22
XDOT = 5022
039427 XDOT = 1449
726798
YDOT = 15357
835918 feet/sec YDOT = 4697
733160 meter/sec
ZDOT = 19270
562061 ZDOT = 5880
906460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19152491
77 X = 5837679
49
Y = -10762815
44 feet Y = -3280506
15 meter
Z = -3616511
46 Z = -1102312
69
XDOT = 9707
578606 XDOT = 2958
869959
YDOT = 10842
113981 feet/sec YDOT = 3304
676342 meter/sec
ZDOT = 19301
842679 ZDOT = 5883
201648
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 17319
91498705
00016717 00000-0 10270-3 0 9090
2 25544 51
6429 1
9442 0003946 119
3978 240
7569 15
54147005 5346
Satellite: ISS
Catalog Number: 25544
Epoch time: 17319
91498705 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 1
9442 deg
Eccentricity:
0003946
Arg of perigee: 119
3978 deg
Mean anomaly: 240
7569 deg
Mean motion: 15
54147005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 330
Coasting Arc #11 (Orbit 549)
---------------------------------------
Vector Time (GMT): 2017/320/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6756630
18 A = 6789224
33 meter
Y = -48292
46 meter E =
0014626
Z = -596291
88 I = 51
64210
XDOT = 552
751395 Wp = 134
72093
YDOT = -4773
987337 meter/sec RA = 356
40465 deg
ZDOT = -5976
699945 TA = 51
71588
MA = 51
58441
Ha = 222
338 n
mi
Hp = 213
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22167421
84 X = -6752691
42
Y = -158439
83 feet Y = -123827
69 meter
Z = -1956338
20 Z = -629104
79
XDOT = 1813
488828 XDOT = 635
126953
YDOT = -15662
688114 feet/sec YDOT = -4767
345498 meter/sec
ZDOT = -19608
595619 ZDOT = -5973
814701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20316501
51 X = -6192469
66
Y = 8835651
14 feet Y = 2693106
47 meter
Z = -2101901
17 Z = -640659
48
XDOT = -3930
061585 XDOT = -1197
882771
YDOT = -13625
420183 feet/sec YDOT = -4153
028072 meter/sec
ZDOT = -19594
938297 ZDOT = -5972
537193
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 17320
94381529
00016717 00000-0 10270-3 0 9102
2 25544 51
6424 356
8161 0004041 124
1032 236
0505 15
54104525 5509
Satellite: ISS
Catalog Number: 25544
Epoch time: 17320
94381529 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 356
8161 deg
Eccentricity:
0004041
Arg of perigee: 124
1032 deg
Mean anomaly: 236
0505 deg
Mean motion: 15
54104525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 550
Checksum: 265
Coasting Arc #12 (Orbit 565)
---------------------------------------
Vector Time (GMT): 2017/321/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6350989
48 A = 6787134
72 meter
Y = 828396
56 meter E =
0016471
Z = 2227627
79 I = 51
60224
XDOT = -2544
671852 Wp = 82
33251
YDOT = 4754
872919 meter/sec RA = 351
43095 deg
ZDOT = 5454
246675 TA = 302
44915
MA = 302
60832
Ha = 222
220 n
mi
Hp = 213
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20836579
67 X = 6330433
10
Y = 2717836
49 feet Y = 899302
68 meter
Z = 7308490
11 Z = 2258429
84
XDOT = -8348
660931 XDOT = -2624
147748
YDOT = 15599
976769 feet/sec YDOT = 4725
972176 meter/sec
ZDOT = 17894
510089 ZDOT = 5441
692172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20000303
61 X = 6096092
54
Y = -6286795
02 feet Y = -1916215
12 meter
Z = 7444983
47 Z = 2269230
96
XDOT = -1568
703496 XDOT = -478
140826
YDOT = 16257
293744 feet/sec YDOT = 4955
223133 meter/sec
ZDOT = 17837
959983 ZDOT = 5437
010203
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 17321
97263944
00016717 00000-0 10270-3 0 9117
2 25544 51
6418 351
6873 0003861 125
1590 234
9925 15
54133886 5666
Satellite: ISS
Catalog Number: 25544
Epoch time: 17321
97263944 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 351
6873 deg
Eccentricity:
0003861
Arg of perigee: 125
1590 deg
Mean anomaly: 234
9925 deg
Mean motion: 15
54133886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 566
Checksum: 327
Coasting Arc #13 (Orbit 580)
---------------------------------------
Vector Time (GMT): 2017/322/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5454818
29 A = 6783477
02 meter
Y = -1682382
81 meter E =
0008533
Z = -3670831
63 I = 51
55824
XDOT = 4331
965706 Wp = 98
77419
YDOT = -4590
571222 meter/sec RA = 346
44722 deg
ZDOT = -4343
265687 TA = 124
90074
MA = 124
82051
Ha = 222
111 n
mi
Hp = 213
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17896385
47 X = -5417768
46
Y = -5519628
63 feet Y = -1743175
01 meter
Z = -12043410
85 Z = -3697240
21
XDOT = 14212
485913 XDOT = 4404
074740
YDOT = -15060
929207 feet/sec YDOT = -4541
724872 meter/sec
ZDOT = -14249
559339 ZDOT = -4322
046821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18439450
24 X = -5620344
43
Y = 2811681
54 feet Y = 857000
53 meter
Z = -12160254
10 Z = -3706445
45
XDOT = 6499
703358 XDOT = 1981
109583
YDOT = -18451
852008 feet/sec YDOT = -5624
124492 meter/sec
ZDOT = -14154
605155 ZDOT = -4314
323651
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 17322
93715806
00016717 00000-0 10270-3 0 9124
2 25544 51
6421 346
8791 0003743 131
2252 228
9224 15
54138929 5812
Satellite: ISS
Catalog Number: 25544
Epoch time: 17322
93715806 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 346
8791 deg
Eccentricity:
0003743
Arg of perigee: 131
2252 deg
Mean anomaly: 228
9224 deg
Mean motion: 15
54138929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 581
Checksum: 310
Coasting Arc #14 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2017/323/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4186800
80 A = 6779853
31 meter
Y = 2527786
00 meter E =
0011584
Z = 4689627
99 I = 51
51414
XDOT = -5726
428337 Wp = 121
23083
YDOT = 4269
668951 meter/sec RA = 341
45010 deg
ZDOT = 2800
003901 TA = 300
92165
MA = 301
03547
Ha = 222
080 n
mi
Hp = 213
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13736223
11 X = 4135442
79
Y = 8293261
17 feet Y = 2574318
26 meter
Z = 15385918
60 Z = 4709842
05
XDOT = -18787
494543 XDOT = -5787
348687
YDOT = 14008
100232 feet/sec YDOT = 4205
291343 meter/sec
ZDOT = 9186
364503 ZDOT = 2772
038272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15911655
80 X = 4849872
69
Y = 1236181
07 feet Y = 376787
99 meter
Z = 15475127
24 Z = 4716818
78
XDOT = -10390
393263 XDOT = -3166
991867
YDOT = 19854
766877 feet/sec YDOT = 6051
732944 meter/sec
ZDOT = 9061
544090 ZDOT = 2761
958639
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 17323
96597525
00016717 00000-0 10270-3 0 9135
2 25544 51
6417 341
7496 0003827 131
2947 228
8535 15
54137760 5970
Satellite: ISS
Catalog Number: 25544
Epoch time: 17323
96597525 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 341
7496 deg
Eccentricity:
0003827
Arg of perigee: 131
2947 deg
Mean anomaly: 228
8535 deg
Mean motion: 15
54137760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 339
Coasting Arc #15 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2017/324/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2643994
16 A = 6777491
09 meter
Y = -3403155
02 meter E =
0016988
Z = -5245483
69 I = 51
47446
XDOT = 6631
834182 Wp = 92
78768
YDOT = -3708
324292 meter/sec RA = 336
44209 deg
ZDOT = -940
354691 TA = 168
19967
MA = 168
15982
Ha = 222
049 n
mi
Hp = 213
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674521
54 X = -2580262
14
Y = -11165206
77 feet Y = -3432365
29 meter
Z = -17209592
17 Z = -5258173
09
XDOT = 21757
986160 XDOT = 6677
376641
YDOT = -12166
418282 feet/sec YDOT = -3633
907891 meter/sec
ZDOT = -3085
153187 ZDOT = -908
028221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12786956
45 X = -3897464
33
Y = -5872275
85 feet Y = -1789869
68 meter
Z = -17265264
26 Z = -5262452
55
XDOT = 13140
850646 XDOT = 4005
331277
YDOT = -20000
317835 feet/sec YDOT = -6096
096876 meter/sec
ZDOT = -2941
095206 ZDOT = -896
445819
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 17324
93048719
00016717 00000-0 10270-3 0 9140
2 25544 51
6404 336
9407 0003751 136
0453 224
0998 15
54174065 6123
Satellite: ISS
Catalog Number: 25544
Epoch time: 17324
93048719 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 336
9407 deg
Eccentricity:
0003751
Arg of perigee: 136
0453 deg
Mean anomaly: 224
0998 deg
Mean motion: 15
54174065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 307
Coasting Arc #16 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2017/325/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 993880
66 A = 6777564
34 meter
Y = 4198029
92 meter E =
0005485
Z = 5222428
04 I = 51
44598
XDOT = -7026
648293 Wp = 98
72883
YDOT = 2914
128708 meter/sec RA = 331
42982 deg
ZDOT = -1005
182756 TA =
91509
MA =
91409
Ha = 221
920 n
mi
Hp = 213
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3260763
33 X = 921494
84
Y = 13773064
06 feet Y = 4208739
09 meter
Z = 17133950
27 Z = 5227080
56
XDOT = -23053
308047 XDOT = -7053
829848
YDOT = 9560
789723 feet/sec YDOT = 2835
400015 meter/sec
ZDOT = -3297
843687 ZDOT = -1039
382487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9402467
21 X = 2865872
01
Y = 10547121
47 feet Y = 3214762
62 meter
Z = 17153832
28 Z = 5228488
08
XDOT = -14792
978730 XDOT = -4508
899917
YDOT = 18799
175909 feet/sec YDOT = 5729
988817 meter/sec
ZDOT = -3450
062659 ZDOT = -1051
579098
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 17325
95929801
00016717 00000-0 10270-3 0 9154
2 25544 51
6413 331
8122 0003684 141
6220 218
5195 15
54177938 6286
Satellite: ISS
Catalog Number: 25544
Epoch time: 17325
95929801 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 331
8122 deg
Eccentricity:
0003684
Arg of perigee: 141
6220 deg
Mean anomaly: 218
5195 deg
Mean motion: 15
54177938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 314
Coasting Arc #17 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2017/326/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 934755
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626702
37 A = 6779974
55 meter
Y = -4887537
52 meter E =
0013718
Z = -4670490
25 I = 51
42491
XDOT = 6867
745721 Wp = 117
95711
YDOT = -1837
090645 meter/sec RA = 326
41701 deg
ZDOT = 2844
110798 TA = 180
40899
MA = 180
41012
Ha = 221
927 n
mi
Hp = 213
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2056110
15 X = 703996
85
Y = -16035228
08 feet Y = -4880096
81 meter
Z = -15323130
74 Z = -4667258
47
XDOT = 22531
974151 XDOT = 6873
962627
YDOT = -6027
200279 feet/sec YDOT = -1760
256256 meter/sec
ZDOT = 9331
072173 ZDOT = 2877
487668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6105537
20 X = -1860967
74
Y = -14984805
24 feet Y = -4567368
64 meter
Z = -15307922
51 Z = -4665854
78
XDOT = 15403
120461 XDOT = 4694
871117
YDOT = -15959
461474 feet/sec YDOT = -4864
443857 meter/sec
ZDOT = 9479
443341 ZDOT = 2889
334330
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 17326
92380512
00016717 00000-0 10270-3 0 9163
2 25544 51
6405 327
0023 0003669 144
2986 215
8413 15
54179684 6435
Satellite: ISS
Catalog Number: 25544
Epoch time: 17326
92380512 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 327
0023 deg
Eccentricity:
0003669
Arg of perigee: 144
2986 deg
Mean anomaly: 215
8413 deg
Mean motion: 15
54179684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 312
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