[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 11th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26390 9556 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
013/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 212
3
013/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
8
000/00:00:00
000 0
0 0
0 212
1
016/00:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 212
2
021/11:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
8
000/00:00:00
000 0
0 0
0 212
0
Coasting Arc #1 (Orbit 3737)
---------------------------------------
Vector Time (GMT): 2017/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3391215
48 A = 6784826
92 meter
Y = -4816045
86 meter E =
0011715
Z = -3379265
65 I = 52
01432
XDOT = 2899
880800 Wp = 81
09716
YDOT = 5319
848930 meter/sec RA = 98
53588 deg
ZDOT = -4683
642773 TA = 138
05461
MA = 137
96482
Ha = 223
722 n
mi
Hp = 212
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11126035
05 X = 3461232
36
Y = -15800675
40 feet Y = -4777731
21 meter
Z = -11086829
55 Z = -3362622
72
XDOT = 9514
044618 XDOT = 2862
927966
YDOT = 17453
572606 feet/sec YDOT = 5352
071161 meter/sec
ZDOT = -15366
282065 ZDOT = -4669
645455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18707645
80 X = 5702090
44
Y = 5010923
34 feet Y = 1527329
43 meter
Z = -11012829
98 Z = -3356710
58
XDOT = -12659
992333 XDOT = -3858
765663
YDOT = 13713
637042 feet/sec YDOT = 4179
916570 meter/sec
ZDOT = -15305
727734 ZDOT = -4665
185813
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 17011
52522761
00016717 00000-0 10270-3 0 9007
2 25544 51
6427 99
2915 0007121 73
3624 286
8310 15
54035554 37384
Satellite: ISS
Catalog Number: 25544
Epoch time: 17011
52522761 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 99
2915 deg
Eccentricity:
0007121
Arg of perigee: 73
3624 deg
Mean anomaly: 286
8310 deg
Mean motion: 15
54035554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3738
Checksum: 295
Coasting Arc #2 (Orbit 3753)
---------------------------------------
Vector Time (GMT): 2017/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3726484
34 A = 6781015
77 meter
Y = 3443063
68 meter E =
0015446
Z = 4486650
13 I = 52
00663
XDOT = -2148
142977 Wp = 95
97010
YDOT = -6603
278721 meter/sec RA = 93
57533 deg
ZDOT = 3271
987737 TA = 321
23147
MA = 321
34220
Ha = 223
766 n
mi
Hp = 212
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12225998
50 X = -3786502
23
Y = 11296140
67 feet Y = 3401055
68 meter
Z = 14719980
73 Z = 4468402
79
XDOT = -7047
713180 XDOT = -2090
037234
YDOT = -21664
300265 feet/sec YDOT = -6626
976076 meter/sec
ZDOT = 10734
867903 ZDOT = 3261
693473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15003333
98 X = -4573016
20
Y = -7372277
23 feet Y = -2247070
10 meter
Z = 14639165
41 Z = 4462017
62
XDOT = 17057
014225 XDOT = 5198
977936
YDOT = -13410
615526 feet/sec YDOT = -4087
555612 meter/sec
ZDOT = 10690
821330 ZDOT = 3258
562341
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 17012
55411171
00016717 00000-0 10270-3 0 9014
2 25544 51
6434 94
1634 0007083 76
3811 283
8130 15
54076643 37541
Satellite: ISS
Catalog Number: 25544
Epoch time: 17012
55411171 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 94
1634 deg
Eccentricity:
0007083
Arg of perigee: 76
3811 deg
Mean anomaly: 283
8130 deg
Mean motion: 15
54076643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3754
Checksum: 289
Coasting Arc #3 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008244
40 A = 6778368
28 meter
Y = -1788134
75 meter E =
0020849
Z = -5184045
77 I = 51
99771
XDOT = 1352
792667 Wp = 78
70207
YDOT = 7380
870372 meter/sec RA = 88
60614 deg
ZDOT = -1501
058991 TA = 176
89023
MA = 176
87725
Ha = 223
736 n
mi
Hp = 212
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13150408
15 X = 4053122
98
Y = -5866583
83 feet Y = -1743060
62 meter
Z = -17008024
19 Z = -5164466
42
XDOT = 4438
296153 XDOT = 1277
448607
YDOT = 24215
453975 feet/sec YDOT = 7395
577027 meter/sec
ZDOT = -4924
734222 ZDOT = -1494
670209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10461028
16 X = 3188521
38
Y = 10042295
84 feet Y = 3060891
77 meter
Z = -16921646
23 Z = -5157717
77
XDOT = -19975
512502 XDOT = -6088
536211
YDOT = 12561
432732 feet/sec YDOT = 3828
724697 meter/sec
ZDOT = -4897
997984 ZDOT = -1492
909786
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 17013
51868835
00016717 00000-0 10270-3 0 9025
2 25544 51
6427 89
3564 0007135 78
8851 281
3104 15
54036288 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
51868835 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 89
3564 deg
Eccentricity:
0007135
Arg of perigee: 78
8851 deg
Mean anomaly: 281
3104 deg
Mean motion: 15
54036288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 330
Coasting Arc #4 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/013/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179816
73 A = 6777698
14 meter
Y = 485328
82 meter E =
0021726
Z = -5331928
25 I = 51
99553
XDOT = -219
830220 Wp = 88
86403
YDOT = 7631
095790 meter/sec RA = 88
57242 deg
ZDOT = 524
536782 TA = 186
11328
MA = 186
13984
Ha = 223
739 n
mi
Hp = 212
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13713309
49 X = 4199978
43
Y = 1592286
16 feet Y = 532183
40 meter
Z = -17493202
93 Z = -5311575
37
XDOT = -721
227756 XDOT = -307
694658
YDOT = 25036
403509 feet/sec YDOT = 7628
146189 meter/sec
ZDOT = 1720
921200 ZDOT = 523
255992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4066947
73 X = 1239605
67
Y = 13310473
69 feet Y = 4057032
38 meter
Z = -17403838
87 Z = -5304690
09
XDOT = -22272
836509 XDOT = -6788
760568
YDOT = 9036
585870 feet/sec YDOT = 2754
351373 meter/sec
ZDOT = 1713
903530 ZDOT = 522
397796
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 17013
51868815
00016717 00000-0 10270-3 0 9034
2 25544 51
6427 89
3565 0007177 78
2512 281
9445 15
54043973 37699
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
51868815 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 89
3565 deg
Eccentricity:
0007177
Arg of perigee: 78
2512 deg
Mean anomaly: 281
9445 deg
Mean motion: 15
54043973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 337
Coasting Arc #5 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2017/013/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -698277
43 A = 6789482
71 meter
Y = -6735926
52 meter E =
0018286
Z = 403836
96 I = 52
03371
XDOT = 4662
327669 Wp = 111
50753
YDOT = -857
380557 meter/sec RA = 86
74876 deg
ZDOT = -6027
446431 TA = 64
16214
MA = 63
97366
Ha = 223
835 n
mi
Hp = 212
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2290936
43 X = -624864
27
Y = -22099496
47 feet Y = -6743324
67 meter
Z = 1324924
41 Z = 400622
97
XDOT = 15296
350621 XDOT = 4700
846438
YDOT = -2812
928336 feet/sec YDOT = -805
027587 meter/sec
ZDOT = -19775
086715 ZDOT = -6004
705200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21173499
97 X = -6453682
79
Y = -6734466
88 feet Y = -2052665
51 meter
Z = 1312026
43 Z = 399905
66
XDOT = 3100
620097 XDOT = 945
069005
YDOT = -13718
370172 feet/sec YDOT = -4181
359228 meter/sec
ZDOT = -19674
978921 ZDOT = -5996
933575
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 17013
90451886
00016717 00000-0 10270-3 0 9044
2 25544 51
6417 87
4343 0007468 77
5378 282
6610 15
54052649 37755
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
90451886 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 87
4343 deg
Eccentricity:
0007468
Arg of perigee: 77
5378 deg
Mean anomaly: 282
6610 deg
Mean motion: 15
54052649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 333
Coasting Arc #6 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2017/014/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -32201
36 A = 6788853
10 meter
Y = 6662616
57 meter E =
0020793
Z = 1257496
78 I = 52
02829
XDOT = -4798
308472 Wp = 66
53096
YDOT = -1145
145864 meter/sec RA = 81
80599 deg
ZDOT = 5875
932126 TA = 307
07626
MA = 307
26619
Ha = 223
811 n
mi
Hp = 212
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -105647
52 X = -112810
26
Y = 21858978
25 feet Y = 6661805
73 meter
Z = 4125645
59 Z = 1257144
75
XDOT = -15742
481865 XDOT = -4813
688396
YDOT = -3757
040237 feet/sec YDOT = -1198
889931 meter/sec
ZDOT = 19277
992540 ZDOT = 5852
586485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20130076
54 X = 6135647
33
Y = 8522261
71 feet Y = 2597585
37 meter
Z = 4122877
27 Z = 1256652
99
XDOT = -8942
949912 XDOT = -2725
811133
YDOT = 11738
188982 feet/sec YDOT = 3577
800002 meter/sec
ZDOT = 19175
590481 ZDOT = 5844
719979
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 17014
93339447
00016717 00000-0 10270-3 0 9057
2 25544 51
6411 82
3068 0007397 81
3534 278
8457 15
54064279 37911
Satellite: ISS
Catalog Number: 25544
Epoch time: 17014
93339447 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 82
3068 deg
Eccentricity:
0007397
Arg of perigee: 81
3534 deg
Mean anomaly: 278
8457 deg
Mean motion: 15
54064279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 332
Coasting Arc #7 (Orbit 3805)
---------------------------------------
Vector Time (GMT): 2017/015/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 866037
81 A = 6786019
25 meter
Y = -6098376
42 meter E =
0011563
Z = -2855753
11 I = 52
01469
XDOT = 4813
237163 Wp = 96
91733
YDOT = 3067
224982 meter/sec RA = 76
85734 deg
ZDOT = -5109
345477 TA = 115
33637
MA = 115
21656
Ha = 223
782 n
mi
Hp = 212
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2841331
38 X = 948038
67
Y = -20007796
65 feet Y = -6088233
29 meter
Z = -9369268
73 Z = -2851347
11
XDOT = 15791
460509 XDOT = 4803
399201
YDOT = 10063
074088 feet/sec YDOT = 3120
994859 meter/sec
ZDOT = -16762
944479 ZDOT = -5085
988546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17532917
88 X = -5344033
37
Y = -10068039
36 feet Y = -3068738
40 meter
Z = -9348778
61 Z = -2849507
72
XDOT = 14476
563049 XDOT = 4412
456417
YDOT = -9797
656288 feet/sec YDOT = -2986
325636 meter/sec
ZDOT = -16660
846536 ZDOT = -5078
226024
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 17015
89796104
00016717 00000-0 10270-3 0 9061
2 25544 51
6423 77
4985 0007398 84
2101 275
9894 15
54082154 38062
Satellite: ISS
Catalog Number: 25544
Epoch time: 17015
89796104 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 77
4985 deg
Eccentricity:
0007398
Arg of perigee: 84
2101 deg
Mean anomaly: 275
9894 deg
Mean motion: 15
54082154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3806
Checksum: 337
Coasting Arc #8 (Orbit 3807)
---------------------------------------
Vector Time (GMT): 2017/016/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 740909
90 A = 6786237
75 meter
Y = -6142574
69 meter E =
0011368
Z = -2795136
10 I = 52
01558
XDOT = 4858
634507 Wp = 99
01380
YDOT = 2921
560672 meter/sec RA = 76
22135 deg
ZDOT = -5152
074351 TA = 112
47619
MA = 112
35578
Ha = 223
739 n
mi
Hp = 212
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2430806
77 X = 823119
86
Y = -20152804
11 feet Y = -6133829
67 meter
Z = -9170394
02 Z = -2791337
39
XDOT = 15940
401927 XDOT = 4850
629587
YDOT = 9585
172810 feet/sec YDOT = 2975
848451 meter/sec
ZDOT = -16903
131073 ZDOT = -5128
492446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19343539
76 X = -5895910
92
Y = 6180493
53 feet Y = 1883814
43 meter
Z = -9152564
18 Z = -2789701
56
XDOT = 2430
129427 XDOT = 740
703449
YDOT = -17177
857416 feet/sec YDOT = -5235
810940 meter/sec
ZDOT = -16800
017766 ZDOT = -5120
645415
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 17016
02656883
00016717 00000-0 10270-3 0 9077
2 25544 51
6436 76
8590 0007164 85
3222 274
8748 15
54056039 38089
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
02656883 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 76
8590 deg
Eccentricity:
0007164
Arg of perigee: 85
3222 deg
Mean anomaly: 274
8748 deg
Mean motion: 15
54056039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 330
Coasting Arc #9 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2017/017/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1596454
22 A = 6782542
01 meter
Y = 5179438
54 meter E =
0017921
Z = 4063729
70 I = 51
99413
XDOT = -4776
645268 Wp = 96
01260
YDOT = -4557
221127 meter/sec RA = 71
26308 deg
ZDOT = 3915
299856 TA = 313
56892
MA = 313
71757
Ha = 223
859 n
mi
Hp = 212
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5237710
68 X = -1673992
71
Y = 16992908
60 feet Y = 5161152
41 meter
Z = 13332446
53 Z = 4055786
36
XDOT = -15671
408358 XDOT = -4744
348573
YDOT = -14951
512884 feet/sec YDOT = -4610
456172 meter/sec
ZDOT = 12845
471969 ZDOT = 3892
175211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17619712
44 X = 5370488
35
Y = -2587204
61 feet Y = -788579
96 meter
Z = 13296570
70 Z = 4052794
75
XDOT = -6810
199895 XDOT = -2075
748928
YDOT = 19400
299377 feet/sec YDOT = 5913
211250 meter/sec
ZDOT = 12744
676125 ZDOT = 3884
577283
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 17017
05543522
00016717 00000-0 10270-3 0 9087
2 25544 51
6431 71
7298 0007378 87
4896 272
7101 15
54063192 38246
Satellite: ISS
Catalog Number: 25544
Epoch time: 17017
05543522 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 71
7298 deg
Eccentricity:
0007378
Arg of perigee: 87
4896 deg
Mean anomaly: 272
7101 deg
Mean motion: 15
54063192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 317
Coasting Arc #10 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2017/018/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2539462
47 A = 6779083
22 meter
Y = -3876252
21 meter E =
0019355
Z = -4965480
47 I = 51
97044
XDOT = 4464
066848 Wp = 80
04460
YDOT = 5796
757229 meter/sec RA = 66
29446 deg
ZDOT = -2246
337815 TA = 168
10150
MA = 168
05570
Ha = 223
707 n
mi
Hp = 212
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8331569
77 X = 2606738
58
Y = -12717362
88 feet Y = -3847478
12 meter
Z = -16290946
41 Z = -4952981
24
XDOT = 14645
888610 XDOT = 4409
825720
YDOT = 19018
232378 feet/sec YDOT = 5846
374123 meter/sec
ZDOT = -7369
874722 ZDOT = -2224
784822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15154790
38 X = -4619180
11
Y = -1813622
50 feet Y = -552792
14 meter
Z = -16235282
89 Z = -4948514
22
XDOT = 10242
264559 XDOT = 3121
842237
YDOT = -20572
907409 feet/sec YDOT = -6270
622178 meter/sec
ZDOT = -7276
226723 ZDOT = -2217
793905
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 17018
01999271
00016717 00000-0 10270-3 0 9091
2 25544 51
6420 66
9217 0007249 91
3105 268
8878 15
54095406 38391
Satellite: ISS
Catalog Number: 25544
Epoch time: 17018
01999271 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 66
9217 deg
Eccentricity:
0007249
Arg of perigee: 91
3105 deg
Mean anomaly: 268
8878 deg
Mean motion: 15
54095406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 336
Coasting Arc #11 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2017/019/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3453590
81 A = 6777490
68 meter
Y = 2365532
14 meter E =
0009771
Z = 5321969
22 I = 51
95207
XDOT = -3932
459505 Wp = 97
75550
YDOT = -6582
001654 meter/sec RA = 61
31870 deg
ZDOT = 371
834984 TA = 348
70701
MA = 348
72892
Ha = 223
837 n
mi
Hp = 212
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11330678
52 X = -3505637
41
Y = 7760932
20 feet Y = 2326620
79 meter
Z = 17460528
92 Z = 5305066
46
XDOT = -12901
770029 XDOT = -3860
371773
YDOT = -21594
493616 feet/sec YDOT = -6625
573996 meter/sec
ZDOT = 1219
931050 ZDOT = 352
907624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12194833
92 X = 3716985
38
Y = 6519717
51 feet Y = 1987209
90 meter
Z = 17385790
86 Z = 5299189
05
XDOT = -12635
607247 XDOT = -3851
333089
YDOT = 20583
322976 feet/sec YDOT = 6273
796843 meter/sec
ZDOT = 1137
982726 ZDOT = 346
857135
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 17019
04885177
00016717 00000-0 10270-3 0 9106
2 25544 51
6429 61
7935 0007226 95
4185 264
7790 15
54090052 38556
Satellite: ISS
Catalog Number: 25544
Epoch time: 17019
04885177 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 61
7935 deg
Eccentricity:
0007226
Arg of perigee: 95
4185 deg
Mean anomaly: 264
7790 deg
Mean motion: 15
54090052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 326
Coasting Arc #12 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2017/020/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335275
75 A = 6778225
11 meter
Y = -791646
91 meter E =
0020781
Z = -5168518
55 I = 51
93752
XDOT = 3090
390376 Wp = 100
43005
YDOT = 6827
588270 meter/sec RA = 56
33880 deg
ZDOT = 1548
035557 TA = 184
44843
MA = 184
46693
Ha = 223
649 n
mi
Hp = 212
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14223345
64 X = 4368911
89
Y = -2597266
77 feet Y = -742978
86 meter
Z = -16957081
86 Z = -5147377
58
XDOT = 10139
076038 XDOT = 3006
293296
YDOT = 22400
223984 feet/sec YDOT = 6861
676881 meter/sec
ZDOT = 5078
856815 ZDOT = 1562
843355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9163902
89 X = -2793157
60
Y = -11323423
12 feet Y = -3451379
37 meter
Z = -16864013
57 Z = -5140151
34
XDOT = 13967
828618 XDOT = 4257
394163
YDOT = -18954
956977 feet/sec YDOT = -5777
470887 meter/sec
ZDOT = 5142
639269 ZDOT = 1567
476449
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 17020
01340193
00016717 00000-0 10270-3 0 9110
2 25544 51
6422 56
9841 0007193 98
4871 261
7097 15
54111245 38701
Satellite: ISS
Catalog Number: 25544
Epoch time: 17020
01340193 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 56
9841 deg
Eccentricity:
0007193
Arg of perigee: 98
4871 deg
Mean anomaly: 261
7097 deg
Mean motion: 15
54111245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 295
Coasting Arc #13 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2017/021/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5052913
97 A = 6781014
29 meter
Y = -740498
99 meter E =
0015802
Z = 4448680
92 I = 51
92814
XDOT = -1966
563634 Wp = 83
30362
YDOT = -6632
912405 meter/sec RA = 51
36485 deg
ZDOT = -3325
847888 TA = 40
14664
MA = 40
03000
Ha = 223
712 n
mi
Hp = 212
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16577801
75 X = -5065867
35
Y = -2429458
63 feet Y = -797076
55 meter
Z = 14595409
84 Z = 4424104
12
XDOT = -6451
980425 XDOT = -1876
091305
YDOT = -21761
523637 feet/sec YDOT = -6654
397947 meter/sec
ZDOT = -10911
574436 ZDOT = -3335
181111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6149012
96 X = 1874219
15
Y = 15686067
44 feet Y = 4781113
36 meter
Z = 14487535
90 Z = 4415800
94
XDOT = -14600
665852 XDOT = -4450
282952
YDOT = 15874
393086 feet/sec YDOT = 4838
515013 meter/sec
ZDOT = -10951
320168 ZDOT = -3337
962387
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 17021
04225155
00016717 00000-0 10270-3 0 9125
2 25544 51
6420 51
8562 0007115 101
8244 258
3707 15
54137024 38860
Satellite: ISS
Catalog Number: 25544
Epoch time: 17021
04225155 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 51
8562 deg
Eccentricity:
0007115
Arg of perigee: 101
8244 deg
Mean anomaly: 258
3707 deg
Mean motion: 15
54137024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 279
Coasting Arc #14 (Orbit 3892)
---------------------------------------
Vector Time (GMT): 2017/021/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5384884
91 A = 6787088
35 meter
Y = 3429096
90 meter E =
0011660
Z = -2309873
33 I = 51
93923
XDOT = -1044
582684 Wp = 78
81726
YDOT = 5289
578094 meter/sec RA = 48
94651 deg
ZDOT = 5442
841059 TA = 255
58038
MA = 255
70982
Ha = 223
755 n
mi
Hp = 211
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17666945
25 X = 5357359
81
Y = 11250317
92 feet Y = 3489160
44 meter
Z = -7578324
59 Z = -2283782
21
XDOT = -3427
108544 XDOT = -1130
092953
YDOT = 17354
258839 feet/sec YDOT = 5277
418666 meter/sec
ZDOT = 17857
090088 ZDOT = 5437
559226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2418689
68 X = -737216
61
Y = 20845995
93 feet Y = 6353859
56 meter
Z = -7464315
45 Z = -2275123
35
XDOT = -15647
983740 XDOT = -4769
505444
YDOT = 4539
481373 feet/sec YDOT = 1383
633922 meter/sec
ZDOT = 17832
855890 ZDOT = 5435
454475
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 17021
49237480
00016717 00000-0 10270-3 0 9139
2 25544 51
6426 49
6126 0007616 105
7105 254
4888 15
54142212 38932
Satellite: ISS
Catalog Number: 25544
Epoch time: 17021
49237480 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 49
6126 deg
Eccentricity:
0007616
Arg of perigee: 105
7105 deg
Mean anomaly: 254
4888 deg
Mean motion: 15
54142212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3893
Checksum: 305
Coasting Arc #15 (Orbit 3908)
---------------------------------------
Vector Time (GMT): 2017/022/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5187524
13 A = 6789235
89 meter
Y = -4320781
08 meter E =
0020386
Z = 631555
28 I = 51
92390
XDOT = 2600
744832 Wp = 120
98611
YDOT = -4018
194376 meter/sec RA = 43
99430 deg
ZDOT = -5995
670291 TA = 52
21881
MA = 52
03434
Ha = 223
755 n
mi
Hp = 212
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17019436
14 X = -5141890
26
Y = -14175790
95 feet Y = -4378536
33 meter
Z = 2072031
75 Z = 606466
81
XDOT = 8532
627403 XDOT = 2674
607835
YDOT = -13183
052414 feet/sec YDOT = -3988
697951 meter/sec
ZDOT = -19670
834289 ZDOT = -5982
857474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4979726
07 X = 1517820
51
Y = -21593009
54 feet Y = -6581549
31 meter
Z = 1962610
03 Z = 598203
54
XDOT = 14098
237414 XDOT = 4297
142764
YDOT = 1426
857157 feet/sec YDOT = 434
906062 meter/sec
ZDOT = -19613
741345 ZDOT = -5978
268362
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 17022
52121953
00016717 00000-0 10270-3 0 9142
2 25544 51
6424 44
4839 0007579 108
8475 251
3500 15
54110012 39094
Satellite: ISS
Catalog Number: 25544
Epoch time: 17022
52121953 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 44
4839 deg
Eccentricity:
0007579
Arg of perigee: 108
8475 deg
Mean anomaly: 251
3500 deg
Mean motion: 15
54110012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3909
Checksum: 290
Coasting Arc #16 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2017/023/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4646572
55 A = 6788860
39 meter
Y = 4828801
51 meter E =
0019020
Z = 1050198
04 I = 51
89908
XDOT = -4103
358668 Wp = 75
10702
YDOT = 2643
730589 meter/sec RA = 39
04319 deg
ZDOT = 5914
916217 TA = 296
23976
MA = 296
43513
Ha = 223
696 n
mi
Hp = 212
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15244660
59 X = 4587129
00
Y = 15842524
65 feet Y = 4880430
21 meter
Z = 3445531
62 Z = 1072625
23
XDOT = -13462
462823 XDOT = -4161
348072
YDOT = 8673
656787 feet/sec YDOT = 2597
519631 meter/sec
ZDOT = 19405
893100 ZDOT = 5894
842800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6926360
23 X = -2111154
60
Y = 20850145
60 feet Y = 6355124
38 meter
Z = 3543150
38 Z = 1079952
24
XDOT = -12486
761777 XDOT = -3805
964990
YDOT = -7476
486550 feet/sec YDOT = -2278
833100 meter/sec
ZDOT = 19317
155387 ZDOT = 5887
868962
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 17023
55005937
00016717 00000-0 10270-3 0 9150
2 25544 51
6426 39
3560 0007517 111
2643 248
9313 15
54121054 39257
Satellite: ISS
Catalog Number: 25544
Epoch time: 17023
55005937 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 39
3560 deg
Eccentricity:
0007517
Arg of perigee: 111
2643 deg
Mean anomaly: 248
9313 deg
Mean motion: 15
54121054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 291
Coasting Arc #17 (Orbit 3939)
---------------------------------------
Vector Time (GMT): 2017/024/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3674409
89 A = 6786269
51 meter
Y = -5033568
84 meter E =
0012334
Z = -2686782
81 I = 51
86305
XDOT = 5481
491376 Wp = 118
41011
YDOT = -1231
971029 meter/sec RA = 34
08608 deg
ZDOT = -5212
239367 TA = 91
81146
MA = 91
67019
Ha = 223
647 n
mi
Hp = 212
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12055150
55 X = -3604799
22
Y = -16514333
46 feet Y = -5074269
25 meter
Z = -8814904
22 Z = -2704462
86
XDOT = 17983
895589 XDOT = 5520
178399
YDOT = -4041
899700 feet/sec YDOT = -1170
456787 meter/sec
ZDOT = -17100
522857 ZDOT = -5185
518381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8707173
39 X = 2653946
45
Y = -18462847
62 feet Y = -5627475
95 meter
Z = -8891613
48 Z = -2710163
79
XDOT = 10903
067395 XDOT = 3323
254942
YDOT = 13283
412764 feet/sec YDOT = 4048
784210 meter/sec
ZDOT = -16982
846768 ZDOT = -5176
371695
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 17024
51459404
00016717 00000-0 10270-3 0 9160
2 25544 51
6410 34
5479 0007494 115
7786 244
4141 15
54108164 39401
Satellite: ISS
Catalog Number: 25544
Epoch time: 17024
51459404 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 34
5479 deg
Eccentricity:
0007494
Arg of perigee: 115
7786 deg
Mean anomaly: 244
4141 deg
Mean motion: 15
54108164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3940
Checksum: 305
Coasting Arc #18 (Orbit 3955)
---------------------------------------
Vector Time (GMT): 2017/025/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2400840
09 A = 6782545
74 meter
Y = 4925427
51 meter E =
0018073
Z = 3986728
01 I = 51
82276
XDOT = -6551
834286 Wp = 107
76093
YDOT = -55
165526 meter/sec RA = 29
11792 deg
ZDOT = 3993
472674 TA = 300
69295
MA = 300
87091
Ha = 223
559 n
mi
Hp = 212
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7876771
96 X = 2326218
98
Y = 16159539
09 feet Y = 4951857
94 meter
Z = 13079816
31 Z = 3998209
31
XDOT = -21495
519311 XDOT = -6570
128506
YDOT = -180
989257 feet/sec YDOT = -128
534987 meter/sec
ZDOT = 13101
944469 ZDOT = 3961
601939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10167029
42 X = -3098910
57
Y = 14782043
83 feet Y = 4505566
96 meter
Z = 13129300
34 Z = 4001810
74
XDOT = -9471
141837 XDOT = -2886
804032
YDOT = -18085
653820 feet/sec YDOT = -5512
507284 meter/sec
ZDOT = 12961
891777 ZDOT = 3950
784614
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 17025
54342727
00016717 00000-0 10270-3 0 9174
2 25544 51
6404 29
4192 0007407 118
6384 241
5514 15
54123882 39562
Satellite: ISS
Catalog Number: 25544
Epoch time: 17025
54342727 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 29
4192 deg
Eccentricity:
0007407
Arg of perigee: 118
6384 deg
Mean anomaly: 241
5514 deg
Mean motion: 15
54123882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3956
Checksum: 310
Coasting Arc #19 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2017/026/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -807872
43 A = 6779061
32 meter
Y = -4608317
37 meter E =
0018079
Z = -4921245
54 I = 51
78269
XDOT = 7191
398461 Wp = 90
98600
YDOT = 1215
283879 meter/sec RA = 24
13726 deg
ZDOT = -2326
236271 TA = 156
30229
MA = 156
21892
Ha = 223
585 n
mi
Hp = 212
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2650500
10 X = -732376
43
Y = -15119151
49 feet Y = -4616929
28 meter
Z = -16145818
70 Z = -4924986
63
XDOT = 23593
826972 XDOT = 7188
573875
YDOT = 3987
151833 feet/sec YDOT = 1295
687214 meter/sec
ZDOT = -7632
008763 ZDOT = -2291
310150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11697519
70 X = 3565404
00
Y = -9913639
00 feet Y = -3021677
17 meter
Z = -16161347
36 Z = -4925978
68
XDOT = 7930
026591 XDOT = 2417
072105
YDOT = 21507
870151 feet/sec YDOT = 6555
598822 meter/sec
ZDOT = -7478
761007 ZDOT = -2279
526355
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 17026
50795378
00016717 00000-0 10270-3 0 9186
2 25544 51
6407 24
6109 0007508 121
5812 238
6074 15
54132661 39700
Satellite: ISS
Catalog Number: 25544
Epoch time: 17026
50795378 = yrday
fracday
Element set: 918
Inclination: 51
6407 deg
RA of node: 24
6109 deg
Eccentricity:
0007508
Arg of perigee: 121
5812 deg
Mean anomaly: 238
6074 deg
Mean motion: 15
54132661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3970
Checksum: 310
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