[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16915 4846 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
006/12:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 212
6
008/21:45:00
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
4
015/23:42:30
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
1
Coasting Arc #1 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2017/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5125564
69 A = 6781621
58 meter
Y = 508340
57 meter E =
0015302
Z = -4427339
28 I = 51
85145
XDOT = -3495
578489 Wp = 58
06772
YDOT = 5919
064937 meter/sec RA = 143
19757 deg
ZDOT = -3367
893947 TA = 177
91690
MA = 177
91052
Ha = 223
391 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16816157
11 X = 5141005
04
Y = 1667784
01 feet Y = 565744
63 meter
Z = -14525391
34 Z = -4402403
53
XDOT = -11468
433364 XDOT = -3545
147741
YDOT = 19419
504388 feet/sec YDOT = 5879
698040 meter/sec
ZDOT = -11049
520823 ZDOT = -3384
994358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1725902
92 X = 526055
21
Y = 16904203
96 feet Y = 5152401
37 meter
Z = -14415990
59 Z = -4393993
93
XDOT = -20062
677227 XDOT = -6115
104019
YDOT = -7437
727616 feet/sec YDOT = -2267
019377 meter/sec
ZDOT = -11125
581181 ZDOT = -3391
077144
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 17002
52225687
00016717 00000-0 10270-3 0 9004
2 25544 51
6405 144
1592 0006806 42
2460 317
9216 15
53973499 35986
Satellite: ISS
Catalog Number: 25544
Epoch time: 17002
52225687 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 144
1592 deg
Eccentricity:
0006806
Arg of perigee: 42
2460 deg
Mean anomaly: 317
9216 deg
Mean motion: 15
53973499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3598
Checksum: 314
Coasting Arc #2 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2017/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4072678
03 A = 6778627
35 meter
Y = -1750810
67 meter E =
0009251
Z = 5119871
02 I = 51
86792
XDOT = 4629
126041 Wp = 78
86045
YDOT = -5890
951581 meter/sec RA = 138
21953 deg
ZDOT = 1667
014828 TA = 355
10645
MA = 355
11548
Ha = 223
509 n
mi
Hp = 212
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13361804
57 X = -4077667
00
Y = -5744129
49 feet Y = -1796382
18 meter
Z = 16797477
09 Z = 5100075
14
XDOT = 15187
421394 XDOT = 4686
558640
YDOT = -19327
268966 feet/sec YDOT = -5838
864514 meter/sec
ZDOT = 5469
208754 ZDOT = 1689
640839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2705095
46 X = 824513
10
Y = -14391606
24 feet Y = -4386561
58 meter
Z = 16710841
09 Z = 5093464
36
XDOT = 21088
100281 XDOT = 6427
652966
YDOT = 10433
937409 feet/sec YDOT = 3180
264122 meter/sec
ZDOT = 5569
539065 ZDOT = 1697
595507
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 17003
55118923
00016717 00000-0 10270-3 0 9013
2 25544 51
6411 139
0310 0006815 45
3940 314
7768 15
54013986 36144
Satellite: ISS
Catalog Number: 25544
Epoch time: 17003
55118923 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 139
0310 deg
Eccentricity:
0006815
Arg of perigee: 45
3940 deg
Mean anomaly: 314
7768 deg
Mean motion: 15
54013986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3614
Checksum: 291
Coasting Arc #3 (Orbit 3628)
---------------------------------------
Vector Time (GMT): 2017/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2894389
80 A = 6777734
23 meter
Y = 3037239
31 meter E =
0020585
Z = -5340377
90 I = 51
88790
XDOT = -5357
970355 Wp = 78
70844
YDOT = 5461
187852 meter/sec RA = 133
23949 deg
ZDOT = 206
617819 TA = 193
23082
MA = 193
28489
Ha = 223
502 n
mi
Hp = 212
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9496029
52 X = 2886152
34
Y = 9964695
90 feet Y = 3069560
41 meter
Z = -17520924
87 Z = -5326337
82
XDOT = -17578
642898 XDOT = -5419
644195
YDOT = 17917
282979 feet/sec YDOT = 5400
926577 meter/sec
ZDOT = 677
879983 ZDOT = 180
440890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7458925
41 X = -2273480
47
Y = 11660758
43 feet Y = 3554199
17 meter
Z = -17459773
58 Z = -5321738
99
XDOT = -20660
549100 XDOT = -6297
335366
YDOT = -12396
877253 feet/sec YDOT = -3778
568187 meter/sec
ZDOT = 562
013227 ZDOT = 171
301631
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 17004
51581098
00016717 00000-0 10270-3 0 9028
2 25544 51
6407 134
2250 0006951 49
8445 310
3315 15
54003752 36295
Satellite: ISS
Catalog Number: 25544
Epoch time: 17004
51581098 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 134
2250 deg
Eccentricity:
0006951
Arg of perigee: 49
8445 deg
Mean anomaly: 310
3315 deg
Mean motion: 15
54003752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3629
Checksum: 287
Coasting Arc #4 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2017/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1634614
91 A = 6779164
85 meter
Y = -4261906
52 meter E =
0012975
Z = 5005269
00 I = 51
91452
XDOT = 5739
484191 Wp = 55
19512
YDOT = -4651
567121 meter/sec RA = 128
25915 deg
ZDOT = -2075
316258 TA = 54
96212
MA = 54
84045
Ha = 223
642 n
mi
Hp = 212
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5362909
81 X = -1611148
83
Y = -13982632
95 feet Y = -4280054
80 meter
Z = 16421486
22 Z = 4997385
44
XDOT = 18830
328712 XDOT = 5801
153512
YDOT = -15261
046985 feet/sec YDOT = -4587
039482 meter/sec
ZDOT = -6808
780374 ZDOT = -2047
285950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12179433
49 X = 3712291
33
Y = -8777740
19 feet Y = -2675455
21 meter
Z = 16387578
00 Z = 4994933
78
XDOT = 18839
627354 XDOT = 5742
318417
YDOT = 13592
656293 feet/sec YDOT = 4143
041638 meter/sec
ZDOT = -6684
893402 ZDOT = -2037
555509
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 17005
54473527
00016717 00000-0 10270-3 0 9030
2 25544 51
6412 129
0961 0006979 53
6156 306
5640 15
53977643 36458
Satellite: ISS
Catalog Number: 25544
Epoch time: 17005
54473527 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 129
0961 deg
Eccentricity:
0006979
Arg of perigee: 53
6156 deg
Mean anomaly: 306
5640 deg
Mean motion: 15
53977643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 322
Coasting Arc #5 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2017/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 461522
16 A = 6782181
58 meter
Y = 5304344
09 meter E =
0013308
Z = -4211731
02 I = 51
94504
XDOT = -5742
642467 Wp = 85
18514
YDOT = 3443
052965 meter/sec RA = 123
28803 deg
ZDOT = 3718
153939 TA = 222
82678
MA = 222
93052
Ha = 223
573 n
mi
Hp = 212
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1514180
33 X = 422631
90
Y = 17402703
71 feet Y = 5309287
82 meter
Z = -13818015
15 Z = -4209583
37
XDOT = -18840
690507 XDOT = -5798
777783
YDOT = 11296
105529 feet/sec YDOT = 3378
520884 meter/sec
ZDOT = 12198
667778 ZDOT = 3690
121650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16350682
05 X = -4983687
89
Y = 6167479
25 feet Y = 1879847
68 meter
Z = -13809481
42 Z = -4209129
94
XDOT = -15466
129449 XDOT = -4714
076256
YDOT = -14047
819936 feet/sec YDOT = -4281
775517 meter/sec
ZDOT = 12074
959480 ZDOT = 3680
447650
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 17006
50934430
00016717 00000-0 10270-3 0 9043
2 25544 51
6420 124
2893 0006962 56
1835 303
9979 15
54007350 36605
Satellite: ISS
Catalog Number: 25544
Epoch time: 17006
50934430 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 124
2893 deg
Eccentricity:
0006962
Arg of perigee: 56
1835 deg
Mean anomaly: 303
9979 deg
Mean motion: 15
54007350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3660
Checksum: 302
Coasting Arc #6 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2017/006/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2828233
40 A = 6789069
50 meter
Y = 6044735
14 meter E =
0015943
Z = -1215820
48 I = 51
96829
XDOT = -4799
582343 Wp = 45
99112
YDOT = -1073
965912 meter/sec RA = 123
26659 deg
ZDOT = 5883
794507 TA = 300
85618
MA = 301
01292
Ha = 223
607 n
mi
Hp = 212
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9278980
98 X = -2889711
11
Y = 19831808
22 feet Y = 6012764
23 meter
Z = -3988912
33 Z = -1229708
33
XDOT = -15746
661231 XDOT = -4815
796929
YDOT = -3523
510211 feet/sec YDOT = -1127
728918 meter/sec
ZDOT = 19303
787751 ZDOT = 5860
440143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21715751
25 X = -6618960
98
Y = -2706952
58 feet Y = -825079
15 meter
Z = -4050935
96 Z = -1234725
28
XDOT = -1726
418937 XDOT = -526
212492
YDOT = -14602
176047 feet/sec YDOT = -4450
743259 meter/sec
ZDOT = 19201
391692 ZDOT = 5852
584188
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 17006
50934421
00016717 00000-0 10270-3 0 9054
2 25544 51
6423 124
2891 0007059 55
8420 304
3401 15
53994269 36608
Satellite: ISS
Catalog Number: 25544
Epoch time: 17006
50934421 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 124
2891 deg
Eccentricity:
0007059
Arg of perigee: 55
8420 deg
Mean anomaly: 304
3401 deg
Mean motion: 15
53994269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3660
Checksum: 296
Coasting Arc #7 (Orbit 3675)
---------------------------------------
Vector Time (GMT): 2017/007/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3545430
79 A = 6789563
65 meter
Y = -5766424
39 meter E =
0014313
Z = -493166
18 I = 51
98626
XDOT = 3807
902675 Wp = 109
80057
YDOT = 2843
086556 meter/sec RA = 118
32021 deg
ZDOT = -6013
894291 TA = 75
49116
MA = 75
33241
Ha = 223
628 n
mi
Hp = 212
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11631990
79 X = 3612044
50
Y = -18918715
20 feet Y = -5726404
52 meter
Z = -1617999
26 Z = -475781
97
XDOT = 12493
119011 XDOT = 3805
040200
YDOT = 9327
711799 feet/sec YDOT = 2885
653359 meter/sec
ZDOT = -19730
624315 ZDOT = -5995
403427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21669364
23 X = 6604822
22
Y = 4889168
95 feet Y = 1490218
70 meter
Z = -1540648
21 Z = -469589
57
XDOT = -4380
296745 XDOT = -1335
114448
YDOT = 13380
666159 feet/sec YDOT = 4078
427045 meter/sec
ZDOT = -19649
888734 ZDOT = -5989
286086
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 17007
53825600
00016717 00000-0 10270-3 0 9067
2 25544 51
6415 119
1609 0007019 60
3061 299
8789 15
54014127 36768
Satellite: ISS
Catalog Number: 25544
Epoch time: 17007
53825600 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 119
1609 deg
Eccentricity:
0007019
Arg of perigee: 60
3061 deg
Mean anomaly: 299
8789 deg
Mean motion: 15
54014127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3676
Checksum: 309
Coasting Arc #8 (Orbit 3691)
---------------------------------------
Vector Time (GMT): 2017/008/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3976858
69 A = 6787815
68 meter
Y = 5071938
42 meter E =
0020979
Z = 2096728
38 I = 51
99597
XDOT = -2787
382012 Wp = 67
51945
YDOT = -4498
377093 meter/sec RA = 113
37325 deg
ZDOT = 5558
292240 TA = 315
59726
MA = 315
76527
Ha = 223
693 n
mi
Hp = 212
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13047436
65 X = -4043463
76
Y = 16640217
90 feet Y = 5027093
96 meter
Z = 6879030
13 Z = 2077248
53
XDOT = -9144
954107 XDOT = -2763
872379
YDOT = -14758
455029 feet/sec YDOT = -4529
416383 meter/sec
ZDOT = 18235
866929 ZDOT = 5544
808768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20100875
62 X = -6126746
89
Y = -6653513
99 feet Y = -2027991
06 meter
Z = 6792573
98 Z = 2070376
55
XDOT = 10242
612103 XDOT = 3121
948169
YDOT = -12263
206311 feet/sec YDOT = -3737
825284 meter/sec
ZDOT = 18177
415145 ZDOT = 5540
476136
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 17008
56716261
00016717 00000-0 10270-3 0 9074
2 25544 51
6425 114
0334 0007076 63
7078 296
4801 15
54026140 36920
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
56716261 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 114
0334 deg
Eccentricity:
0007076
Arg of perigee: 63
7078 deg
Mean anomaly: 296
4801 deg
Mean motion: 15
54026140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3692
Checksum: 298
Coasting Arc #9 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2017/008/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3467190
17 A = 6777920
81 meter
Y = -2457897
47 meter E =
0010714
Z = 5272547
41 I = 51
96587
XDOT = 3428
718399 Wp = 60
90950
YDOT = -6805
977510 meter/sec RA = 111
36917 deg
ZDOT = -911
565724 TA = 37
80075
MA = 37
72555
Ha = 223
849 n
mi
Hp = 212
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11375295
83 X = -3465059
14
Y = -8063968
07 feet Y = -2496658
38 meter
Z = 17298383
90 Z = 5255709
84
XDOT = 11249
076111 XDOT = 3508
997712
YDOT = -22329
322538 feet/sec YDOT = -6767
186340 meter/sec
ZDOT = -2990
701193 ZDOT = -894
715535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10913060
71 X = -3326300
90
Y = 8824337
29 feet Y = 2689658
01 meter
Z = 17224842
50 Z = 5250132
00
XDOT = -17721
637618 XDOT = -5401
555146
YDOT = -16183
812785 feet/sec YDOT = -4932
826137 meter/sec
ZDOT = -2915
487121 ZDOT = -888
640474
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 17008
95300225
00016717 00000-0 10270-3 0 9087
2 25544 51
6403 112
1129 0007322 61
5192 298
6705 15
54019924 36989
Satellite: ISS
Catalog Number: 25544
Epoch time: 17008
95300225 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 112
1129 deg
Eccentricity:
0007322
Arg of perigee: 61
5192 deg
Mean anomaly: 298
6705 deg
Mean motion: 15
54019924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 300
Coasting Arc #10 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2017/009/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2721567
29 A = 6780060
18 meter
Y = 3983833
06 meter E =
0017135
Z = -4778484
81 I = 51
98462
XDOT = -3966
386938 Wp = 91
48248
YDOT = 5958
057860 meter/sec RA = 106
39604 deg
ZDOT = 2716
166923 TA = 205
24080
MA = 205
32462
Ha = 223
763 n
mi
Hp = 212
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8929026
53 X = 2700028
27
Y = 13070318
44 feet Y = 4014147
44 meter
Z = -15677443
62 Z = -4765316
27
XDOT = -13013
080504 XDOT = -4045
910473
YDOT = 19547
433924 feet/sec YDOT = 5913
258176 meter/sec
ZDOT = 8911
308803 ZDOT = 2696
706834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14960190
02 X = 4559865
92
Y = -5342493
64 feet Y = -1628392
06 meter
Z = -15620289
81 Z = -4761064
33
XDOT = 15111
947124 XDOT = 4606
121483
YDOT = 16591
850879 feet/sec YDOT = 5057
196148 meter/sec
ZDOT = 8824
755546 ZDOT = 2689
785490
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 17009
91759413
00016717 00000-0 10270-3 0 9092
2 25544 51
6410 107
3053 0007325 64
3159 295
8749 15
54020900 37137
Satellite: ISS
Catalog Number: 25544
Epoch time: 17009
91759413 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 107
3053 deg
Eccentricity:
0007325
Arg of perigee: 64
3159 deg
Mean anomaly: 295
8749 deg
Mean motion: 15
54020900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 303
Coasting Arc #11 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2017/010/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1928591
01 A = 6783587
10 meter
Y = -5295325
72 meter E =
0018840
Z = 3763559
15 I = 52
00513
XDOT = 4353
107523 Wp = 77
45452
YDOT = -4645
468743 meter/sec RA = 101
43182 deg
ZDOT = -4283
484561 TA = 57
73877
MA = 57
55635
Ha = 223
806 n
mi
Hp = 212
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6327398
32 X = -1887515
38
Y = -17373115
89 feet Y = -5316663
21 meter
Z = 12347635
02 Z = 3754289
99
XDOT = 14281
848830 XDOT = 4425
537749
YDOT = -15241
039182 feet/sec YDOT = -4596
383987 meter/sec
ZDOT = -14053
427036 ZDOT = -4262
163161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18406319
88 X = -5610246
30
Y = 2012314
06 feet Y = 613353
33 meter
Z = 12307851
01 Z = 3751432
99
XDOT = -11163
594510 XDOT = -3402
663607
YDOT = -16292
541855 feet/sec YDOT = -4965
966758 meter/sec
ZDOT = -13958
909192 ZDOT = -4254
675522
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 17010
94648758
00016717 00000-0 10270-3 0 9108
2 25544 51
6412 102
1774 0007422 67
5049 292
6889 15
54049657 37290
Satellite: ISS
Catalog Number: 25544
Epoch time: 17010
94648758 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 102
1774 deg
Eccentricity:
0007422
Arg of perigee: 67
5049 deg
Mean anomaly: 292
6889 deg
Mean motion: 15
54049657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 332
Coasting Arc #12 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2017/011/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1194375
67 A = 6787123
07 meter
Y = 6227081
43 meter E =
0012611
Z = -2420192
56 I = 52
02237
XDOT = -4571
822944 Wp = 60
88998
YDOT = 2961
589180 meter/sec RA = 96
47838 deg
ZDOT = 5390
944588 TA = 272
21233
MA = 272
35672
Ha = 223
796 n
mi
Hp = 212
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3918555
36 X = 1136410
04
Y = 20430057
18 feet Y = 6240113
85 meter
Z = -7940264
29 Z = -2414530
96
XDOT = -14999
419109 XDOT = -4630
786659
YDOT = 9716
499934 feet/sec YDOT = 2910
133818 meter/sec
ZDOT = 17686
826076 ZDOT = 5368
593404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20798529
81 X = 6339391
89
Y = 734985
56 feet Y = 224023
60 meter
Z = -7916505
75 Z = -2412950
95
XDOT = 6116
441259 XDOT = 1864
291296
YDOT = 15398
384201 feet/sec YDOT = 4693
427504 meter/sec
ZDOT = 17588
069641 ZDOT = 5360
843627
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
91107126
00016717 00000-0 10270-3 0 9116
2 25544 51
6412 97
3707 0007346 71
2162 288
9787 15
54036167 37448
Satellite: ISS
Catalog Number: 25544
Epoch time: 17011
91107126 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 97
3707 deg
Eccentricity:
0007346
Arg of perigee: 71
2162 deg
Mean anomaly: 288
9787 deg
Mean motion: 15
54036167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 308
Coasting Arc #13 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2017/012/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -421670
90 A = 6789305
51 meter
Y = -6726382
69 meter E =
0018767
Z = 770683
71 I = 52
03373
XDOT = 4695
658168 Wp = 108
68353
YDOT = -992
606137 meter/sec RA = 91
53236 deg
ZDOT = -5981
300190 TA = 63
03081
MA = 62
83926
Ha = 223
795 n
mi
Hp = 212
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1383434
72 X = -350166
96
Y = -22068184
69 feet Y = -6730698
36 meter
Z = 2528489
87 Z = 768808
58
XDOT = 15405
702651 XDOT = 4735
462501
YDOT = -3256
581813 feet/sec YDOT = -939
873128 meter/sec
ZDOT = -19623
688288 ZDOT = -5958
393907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21874752
55 X = -6667424
58
Y = -3232541
65 feet Y = -985278
69 meter
Z = 2521468
52 Z = 768543
61
XDOT = -183
540145 XDOT = -55
943036
YDOT = -14275
792132 feet/sec YDOT = -4351
261442 meter/sec
ZDOT = -19522
837425 ZDOT = -5950
560847
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
93995441
00016717 00000-0 10270-3 0 9125
2 25544 51
6425 92
2421 0007380 74
7484 285
4484 15
54051265 37602
Satellite: ISS
Catalog Number: 25544
Epoch time: 17012
93995441 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 92
2421 deg
Eccentricity:
0007380
Arg of perigee: 74
7484 deg
Mean anomaly: 285
4484 deg
Mean motion: 15
54051265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 311
Coasting Arc #14 (Orbit 3775)
---------------------------------------
Vector Time (GMT): 2017/013/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -299964
09 A = 6789206
97 meter
Y = 6714742
55 meter E =
0020510
Z = 895548
30 I = 52
03256
XDOT = -4720
716741 Wp = 62
79085
YDOT = -1018
602068 meter/sec RA = 86
58974 deg
ZDOT = 5960
968765 TA = 306
85313
MA = 307
04102
Ha = 223
831 n
mi
Hp = 212
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -984134
15 X = -379377
83
Y = 22029995
23 feet Y = 6710944
07 meter
Z = 2938150
57 Z = 893898
65
XDOT = -15487
915817 XDOT = -4737
930538
YDOT = -3341
870303 feet/sec YDOT = -1071
488852 meter/sec
ZDOT = 19556
984138 ZDOT = 5937
995554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21429545
13 X = 6531725
35
Y = 5207065
81 feet Y = 1587113
66 meter
Z = 2929675
72 Z = 892965
16
XDOT = -5891
270984 XDOT = -1795
659396
YDOT = 13122
374750 feet/sec YDOT = 3999
699824 meter/sec
ZDOT = 19456
198627 ZDOT = 5930
249341
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
96883183
00016717 00000-0 10270-3 0 9139
2 25544 51
6417 87
1144 0007449 77
9344 282
2643 15
54056392 37769
Satellite: ISS
Catalog Number: 25544
Epoch time: 17013
96883183 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 87
1144 deg
Eccentricity:
0007449
Arg of perigee: 77
9344 deg
Mean anomaly: 282
2643 deg
Mean motion: 15
54056392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 332
Coasting Arc #15 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2017/014/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1089915
66 A = 6786773
97 meter
Y = -6202575
86 meter E =
0011565
Z = -2536050
88 I = 52
02252
XDOT = 4636
211359 Wp = 101
24552
YDOT = 2980
951366 meter/sec RA = 81
64351 deg
ZDOT = -5320
882574 TA = 107
04193
MA = 106
91519
Ha = 223
789 n
mi
Hp = 212
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3575838
78 X = 1171512
12
Y = -20349658
33 feet Y = -6189931
39 meter
Z = -8320376
90 Z = -2530558
48
XDOT = 15210
667188 XDOT = 4628
378772
YDOT = 9780
024166 feet/sec YDOT = 3032
752946 meter/sec
ZDOT = -17456
963825 ZDOT = -5298
380667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19402925
55 X = -5914011
71
Y = -7130336
64 feet Y = -2173326
61 meter
Z = -8295099
04 Z = -2528346
19
XDOT = 11785
935878 XDOT = 3592
353256
YDOT = -11964
306976 feet/sec YDOT = -3646
720766 meter/sec
ZDOT = -17358
606721 ZDOT = -5290
903328
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
93339975
00016717 00000-0 10270-3 0 9143
2 25544 51
6424 82
3068 0007390 81
5404 278
6587 15
54073729 37918
Satellite: ISS
Catalog Number: 25544
Epoch time: 17014
93339975 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 82
3068 deg
Eccentricity:
0007390
Arg of perigee: 81
5404 deg
Mean anomaly: 278
6587 deg
Mean motion: 15
54073729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 335
Coasting Arc #16 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2017/015/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1860375
93 A = 6783181
57 meter
Y = 5244655
12 meter E =
0018593
Z = 3863477
06 I = 52
00476
XDOT = -4449
415975 Wp = 92
93912
YDOT = -4662
491230 meter/sec RA = 76
68833 deg
ZDOT = 4168
638841 TA = 313
41922
MA = 313
57383
Ha = 223
841 n
mi
Hp = 212
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6103595
59 X = -1937651
31
Y = 17206873
74 feet Y = 5223419
05 meter
Z = 12675449
66 Z = 3854252
42
XDOT = -14597
821441 XDOT = -4417
196963
YDOT = -15296
887236 feet/sec YDOT = -4712
067466 meter/sec
ZDOT = 13676
636619 ZDOT = 4147
103563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16016360
49 X = 4881786
68
Y = 8823675
18 feet Y = 2689456
20 meter
Z = 12633936
84 Z = 3850823
95
XDOT = -16778
009774 XDOT = -5113
937379
YDOT = 10920
962222 feet/sec YDOT = 3328
709285 meter/sec
ZDOT = 13582
839766 ZDOT = 4140
049561
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
96226720
00016717 00000-0 10270-3 0 9151
2 25544 51
6423 77
1785 0007389 85
3067 274
8929 15
54077085 38075
Satellite: ISS
Catalog Number: 25544
Epoch time: 17015
96226720 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 77
1785 deg
Eccentricity:
0007389
Arg of perigee: 85
3067 deg
Mean anomaly: 274
8929 deg
Mean motion: 15
54077085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 340
Coasting Arc #17 (Orbit 3807)
---------------------------------------
Vector Time (GMT): 2017/015/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3707400
91 A = 6785227
19 meter
Y = -4698060
92 meter E =
0020206
Z = 3179571
53 I = 52
01223
XDOT = 2592
460306 Wp = 90
81207
YDOT = -5348
645895 meter/sec RA = 76
23494 deg
ZDOT = -4853
967174 TA = 52
65415
MA = 52
47024
Ha = 223
824 n
mi
Hp = 212
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12163388
81 X = -3670034
98
Y = -15413585
69 feet Y = -4739310
66 meter
Z = 10431665
12 Z = 3161653
17
XDOT = 8505
447199 XDOT = 2675
655360
YDOT = -17548
050836 feet/sec YDOT = -5319
190072 meter/sec
ZDOT = -15925
089155 ZDOT = -4841
171971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10189495
89 X = -3105758
35
Y = 16832107
52 feet Y = 5130426
37 meter
Z = 10353773
15 Z = 3155830
06
XDOT = -18221
396177 XDOT = -5553
881555
YDOT = -1216
512337 feet/sec YDOT = -370
792960 meter/sec
ZDOT = -15867
862448 ZDOT = -4836
524474
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
02657057
00016717 00000-0 10270-3 0 9161
2 25544 51
6435 76
8589 0007373 85
0775 275
1219 15
54086899 38082
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
02657057 = yrday
fracday
Element set: 916
Inclination: 51
6435 deg
RA of node: 76
8589 deg
Eccentricity:
0007373
Arg of perigee: 85
0775 deg
Mean anomaly: 275
1219 deg
Mean motion: 15
54086899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 347
Coasting Arc #18 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2017/016/23:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3319247
28 A = 6788206
23 meter
Y = 5671699
14 meter E =
0013632
Z = -1695127
82 I = 52
01371
XDOT = -3463
198888 Wp = 62
11104
YDOT = 3727
618963 meter/sec RA = 71
28327 deg
ZDOT = 5732
110913 TA = 279
41299
MA = 279
56707
Ha = 223
734 n
mi
Hp = 212
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10889918
89 X = 3263812
17
Y = 18607936
81 feet Y = 5708507
23 meter
Z = -5561442
99 Z = -1679138
88
XDOT = -11362
201076 XDOT = -3532
468081
YDOT = 12229
721007 feet/sec YDOT = 3688
503888 meter/sec
ZDOT = 18806
138165 ZDOT = 5715
119729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13349154
12 X = 4068822
17
Y = -16953197
84 feet Y = -5167334
70 meter
Z = -5492218
28 Z = -1674028
13
XDOT = 14338
106268 XDOT = 4370
254790
YDOT = 5266
321438 feet/sec YDOT = 1605
174774 meter/sec
ZDOT = 18730
762993 ZDOT = 5709
136560
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
99112695
00016717 00000-0 10270-3 0 9172
2 25544 51
6434 72
0505 0007295 88
1641 272
0347 15
54103690 38230
Satellite: ISS
Catalog Number: 25544
Epoch time: 17016
99112695 = yrday
fracday
Element set: 917
Inclination: 51
6434 deg
RA of node: 72
0505 deg
Eccentricity:
0007295
Arg of perigee: 88
1641 deg
Mean anomaly: 272
0347 deg
Mean motion: 15
54103690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 306
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