[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 25th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
239/04:56:28
517 0
6 1
1 1
1
N/A 0
9 -0
1 221
4
000/00:02:57
035 0
5 -0
1 215
3
242/05:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
7
246/10:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
9
Coasting Arc #1 (Orbit 3252)
---------------------------------------
Vector Time (GMT): 2017/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4449327
43 A = 6778471
18 meter
Y = 734520
06 meter E =
0005115
Z = 5056150
58 I = 51
92075
XDOT = -3282
477790 Wp = 109
72569
YDOT = -6663
378535 meter/sec RA = 52
08600 deg
ZDOT = -1920
627506 TA = 358
81699
MA = 358
81820
Ha = 221
839 n
mi
Hp = 214
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14597530
95 X = -4481770
48
Y = 2409842
72 feet Y = 684583
68 meter
Z = 16588420
53 Z = 5034458
42
XDOT = -10769
284088 XDOT = -3198
392763
YDOT = -21861
478133 feet/sec YDOT = -6699
615453 meter/sec
ZDOT = -6301
271346 ZDOT = -1936
367857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14203799
88 X = 4329318
20
Y = 4508921
44 feet Y = 1374319
25 meter
Z = 16492199
48 Z = 5026822
40
XDOT = -5
241969 XDOT = -1
597752
YDOT = 23314
206438 feet/sec YDOT = 7106
170122 meter/sec
ZDOT = -6369
882599 ZDOT = -1941
540216
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 17237
54487963
00016717 00000-0 10270-3 0 9003
2 25544 51
6377 52
5653 0004969 179
7506 180
3650 15
54169769 32539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
54487963 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 52
5653 deg
Eccentricity:
0004969
Arg of perigee: 179
7506 deg
Mean anomaly: 180
3650 deg
Mean motion: 15
54169769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3253
Checksum: 346
Coasting Arc #2 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2017/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925218
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5242561
04 A = 6781600
03 meter
Y = 752787
77 meter E =
0010701
Z = -4246916
30 I = 51
91081
XDOT = 2043
416399 Wp = 136
09888
YDOT = 6411
244910 meter/sec RA = 47
11045 deg
ZDOT = 3656
907482 TA = 171
26104
MA = 171
24240
Ha = 221
617 n
mi
Hp = 214
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17200003
41 X = 5254382
88
Y = 2469776
16 feet Y = 811479
44 meter
Z = -13933452
43 Z = -4221421
02
XDOT = 6704
122044 XDOT = 1953
808900
YDOT = 21034
268076 feet/sec YDOT = 6433
595037 meter/sec
ZDOT = 11997
727959 ZDOT = 3666
615590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14469479
37 X = -4410297
31
Y = -9782897
09 feet Y = -2981827
03 meter
Z = -13820640
35 Z = -4212531
18
XDOT = 2529
320912 XDOT = 770
937014
YDOT = -20759
152783 feet/sec YDOT = -6327
389768 meter/sec
ZDOT = 12039
645796 ZDOT = 3669
684038
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 17238
50936438
00016717 00000-0 10270-3 0 9017
2 25544 51
6379 47
7562 0005047 181
3056 178
8084 15
54204485 32687
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
50936438 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 47
7562 deg
Eccentricity:
0005047
Arg of perigee: 181
3056 deg
Mean anomaly: 178
8084 deg
Mean motion: 15
54204485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 328
Coasting Arc #3 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2017/239/04:57:57
035
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5195140
67 A = 6781758
15 meter
Y = 222168
44 meter E =
0009907
Z = -4363820
01 I = 51
89685
XDOT = 2651
917809 Wp = 136
11689
YDOT = 6289
069939 meter/sec RA = 43
60405 deg
ZDOT = 3475
068560 TA = 169
10498
MA = 169
08351
Ha = 221
401 n
mi
Hp = 215
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17044424
76 X = 5213467
44
Y = 728899
07 feet Y = 280366
21 meter
Z = -14316994
77 Z = -4338539
20
XDOT = 8700
517747 XDOT = 2564
514539
YDOT = 20633
431557 feet/sec YDOT = 6318
237025 meter/sec
ZDOT = 11401
143570 ZDOT = 3487
737996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11738926
23 X = 3578024
72
Y = -12507369
71 feet Y = -3812246
29 meter
Z = -14205047
07 Z = -4329698
35
XDOT = 20349
895661 XDOT = 6202
648198
YDOT = 6080
038862 feet/sec YDOT = 1853
195845 meter/sec
ZDOT = 11456
191095 ZDOT = 3491
847046
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 17239
21665217
00016717 00000-0 10270-3 0 9021
2 25544 51
6413 44
2343 0004359 196
3684 163
7328 15
54004544 32793
Satellite: ISS
Catalog Number: 25544
Epoch time: 17239
21665217 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 44
2343 deg
Eccentricity:
0004359
Arg of perigee: 196
3684 deg
Mean anomaly: 163
7328 deg
Mean motion: 15
54004544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 308
Coasting Arc #4 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2017/240/04:57:57
035
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5807012
41 A = 6785544
50 meter
Y = -1444333
11 meter E =
0012445
Z = 3183735
68 I = 51
88515
XDOT = -1209
639436 Wp = 114
07368
YDOT = -5828
789408 meter/sec RA = 38
63792 deg
ZDOT = -4840
694978 TA = 29
27106
MA = 29
20139
Ha = 221
456 n
mi
Hp = 215
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19051877
97 X = -5805894
89
Y = -4738625
70 feet Y = -1509264
65 meter
Z = 10445327
02 Z = 3155529
88
XDOT = -3968
633321 XDOT = -1120
856797
YDOT = -19123
324828 feet/sec YDOT = -5841
820280 meter/sec
ZDOT = -15881
545203 ZDOT = -4846
355048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15872212
82 X = -4837850
47
Y = 11665793
86 feet Y = 3555733
97 meter
Z = 10320639
42 Z = 3145730
90
XDOT = -16321
387148 XDOT = -4974
758803
YDOT = -8105
764943 feet/sec YDOT = -2470
637155 meter/sec
ZDOT = -15905
611829 ZDOT = -4848
030486
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 17240
24557193
00016717 00000-0 10270-3 0 9030
2 25544 51
6415 39
1071 0004412 200
5950 159
5025 15
53986250 32957
Satellite: ISS
Catalog Number: 25544
Epoch time: 17240
24557193 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 39
1071 deg
Eccentricity:
0004412
Arg of perigee: 200
5950 deg
Mean anomaly: 159
5025 deg
Mean motion: 15
53986250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 291
Coasting Arc #5 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2017/241/04:57:57
035
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6095077
42 A = 6788459
82 meter
Y = 2450697
25 meter E =
0003687
Z = -1707721
05 I = 51
87020
XDOT = -448
721060 Wp = 52
49475
YDOT = 5089
131369 meter/sec RA = 33
67779 deg
ZDOT = 5712
336312 TA = 288
85186
MA = 288
89184
Ha = 221
143 n
mi
Hp = 215
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19996973
17 X = 6075515
33
Y = 8040345
31 feet Y = 2518747
10 meter
Z = -5602759
33 Z = -1678160
76
XDOT = -1472
181956 XDOT = -533
343381
YDOT = 16696
625226 feet/sec YDOT = 5083
640579 meter/sec
ZDOT = 18741
260865 ZDOT = 5709
950799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18815395
77 X = 5734932
63
Y = -10580751
95 feet Y = -3225013
19 meter
Z = -5472254
63 Z = -1667943
21
XDOT = 11246
222137 XDOT = 3427
848507
YDOT = 10330
376576 feet/sec YDOT = 3148
698780 meter/sec
ZDOT = 18729
810700 ZDOT = 5708
846301
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 17241
21017892
00016717 00000-0 10270-3 0 9046
2 25544 51
6425 34
2989 0004315 205
2483 154
8460 15
54020140 33104
Satellite: ISS
Catalog Number: 25544
Epoch time: 17241
21017892 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 34
2989 deg
Eccentricity:
0004315
Arg of perigee: 205
2483 deg
Mean anomaly: 154
8460 deg
Mean motion: 15
54020140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 274
Coasting Arc #6 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/04:57:57
035
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5961036
63 A = 6789771
26 meter
Y = -3232892
54 meter E =
0014003
Z = 37801
79 I = 51
84596
XDOT = 2225
445474 Wp = 151
63399
YDOT = -4184
521289 meter/sec RA = 28
72355 deg
ZDOT = -6032
302950 TA = 27
95985
MA = 27
88468
Ha = 221
137 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19557206
79 X = -5924626
16
Y = -10606602
82 feet Y = -3299349
33 meter
Z = 124021
61 Z = 8933
59
XDOT = 7301
330296 XDOT = 2301
374358
YDOT = -13728
744388 feet/sec YDOT = -4159
210534 meter/sec
ZDOT = -19791
020176 ZDOT = -6021
307886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20367295
83 X = -6207951
77
Y = 8953937
25 feet Y = 2729160
08 meter
Z = -3272
88 Z = -997
58
XDOT = -5642
655824 XDOT = -1719
881495
YDOT = -12801
413590 feet/sec YDOT = -3901
870862 meter/sec
ZDOT = -19741
590341 ZDOT = -6017
236736
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 17242
23909212
00016717 00000-0 10270-3 0 9056
2 25544 51
6420 29
1717 0004414 208
2421 151
8492 15
53977548 33267
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23909212 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 29
1717 deg
Eccentricity:
0004414
Arg of perigee: 208
2421 deg
Mean anomaly: 151
8492 deg
Mean motion: 15
53977548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 297
Coasting Arc #7 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2017/242/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5005265
67 A = 6781530
32 meter
Y = -1228188
86 meter E =
0009153
Z = -4417007
23 I = 51
81804
XDOT = 4298
422068 Wp = 137
50651
YDOT = 5366
321817 meter/sec RA = 28
58920 deg
ZDOT = 3376
236261 TA = 166
61280
MA = 166
58850
Ha = 220
992 n
mi
Hp = 215
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16421475
29 X = 5040083
17
Y = -4029491
01 feet Y = -1172022
07 meter
Z = -14491493
54 Z = -4392608
69
XDOT = 14102
434607 XDOT = 4221
694931
YDOT = 17606
042707 feet/sec YDOT = 5413
960823 meter/sec
ZDOT = 11076
890619 ZDOT = 3396
930014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4699582
48 X = 1432432
74
Y = -16338361
81 feet Y = -4979932
68 meter
Z = -14383215
62 Z = -4384004
12
XDOT = 21057
361296 XDOT = 6418
283723
YDOT = -3781
528952 feet/sec YDOT = -1152
610025 meter/sec
ZDOT = 11167
606532 ZDOT = 3403
886471
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 17242
23909077
00016717 00000-0 10270-3 0 9066
2 25544 51
6420 29
1715 0004280 210
9029 149
1872 15
54013446 33261
Satellite: ISS
Catalog Number: 25544
Epoch time: 17242
23909077 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 29
1715 deg
Eccentricity:
0004280
Arg of perigee: 210
9029 deg
Mean anomaly: 149
1872 deg
Mean motion: 15
54013446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 291
Coasting Arc #8 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2017/243/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5941102
03 A = 6785223
84 meter
Y = 200226
65 meter E =
0011213
Z = 3257871
95 I = 51
80165
XDOT = -2798
955410 Wp = 111
58468
YDOT = -5318
735754 meter/sec RA = 23
61652 deg
ZDOT = -4768
196483 TA = 30
71329
MA = 30
64772
Ha = 220
983 n
mi
Hp = 215
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19491804
55 X = -5958724
51
Y = 656911
58 feet Y = 133690
78 meter
Z = 10688556
27 Z = 3228969
28
XDOT = -9182
924574 XDOT = -2716
110446
YDOT = -17449
920454 feet/sec YDOT = -5349
572530 meter/sec
ZDOT = -15643
689250 ZDOT = -4781
591463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8840217
13 X = -2694498
18
Y = 17462340
10 feet Y = 5322521
26 meter
Z = 10560513
80 Z = 3218844
61
XDOT = -18393
859306 XDOT = -5606
448317
YDOT = 202
526405 feet/sec YDOT = 61
730048 meter/sec
ZDOT = -15702
079916 ZDOT = -4785
993959
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 17243
26800013
00016717 00000-0 10270-3 0 9071
2 25544 51
6423 24
0439 0004203 214
4739 145
6142 15
54028626 33428
Satellite: ISS
Catalog Number: 25544
Epoch time: 17243
26800013 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 24
0439 deg
Eccentricity:
0004203
Arg of perigee: 214
4739 deg
Mean anomaly: 145
6142 deg
Mean motion: 15
54028626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 273
Coasting Arc #9 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2017/244/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6508185
09 A = 6788309
30 meter
Y = 708692
13 meter E =
0003305
Z = -1790278
38 I = 51
78200
XDOT = 1007
847288 Wp = 35
72139
YDOT = 5054
431562 meter/sec RA = 18
64974 deg
ZDOT = 5672
543014 TA = 304
66100
MA = 304
69215
Ha = 220
708 n
mi
Hp = 215
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21352313
30 X = 6508472
83
Y = 2325105
42 feet Y = 781472
63 meter
Z = -5873616
74 Z = -1758663
22
XDOT = 3306
585592 XDOT = 923
698178
YDOT = 16582
780714 feet/sec YDOT = 5065
231689 meter/sec
ZDOT = 18610
705428 ZDOT = 5677
234224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12029671
18 X = 3666643
78
Y = -17839231
02 feet Y = -5437397
61 meter
Z = -5733726
54 Z = -1747639
85
XDOT = 14855
333557 XDOT = 4527
905668
YDOT = 4037
968282 feet/sec YDOT = 1230
772732 meter/sec
ZDOT = 18630
591189 ZDOT = 5678
604194
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 17244
23259725
00016717 00000-0 10270-3 0 9088
2 25544 51
6425 19
2353 0004223 219
9141 140
1702 15
54032426 33571
Satellite: ISS
Catalog Number: 25544
Epoch time: 17244
23259725 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 19
2353 deg
Eccentricity:
0004223
Arg of perigee: 219
9141 deg
Mean anomaly: 140
1702 deg
Mean motion: 15
54032426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 283
Coasting Arc #10 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2017/245/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 925097
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6610156
05 A = 6789730
69 meter
Y = -1510915
81 meter E =
0013137
Z = 122078
43 I = 51
75439
XDOT = 948
234931 Wp = 152
34342
YDOT = -4655
148045 meter/sec RA = 13
68830 deg
ZDOT = -6022
895691 TA = 26
34320
MA = 26
27646
Ha = 220
714 n
mi
Hp = 215
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21686863
68 X = -6593362
30
Y = -4957072
88 feet Y = -1584741
18 meter
Z = 400519
77 Z = 90009
53
XDOT = 3111
006991 XDOT = 1029
475529
YDOT = -15272
795423 feet/sec YDOT = -4644
090250 meter/sec
ZDOT = -19760
156466 ZDOT = -6018
091989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14205276
32 X = -4329768
22
Y = 17122973
10 feet Y = 5219082
20 meter
Z = 258767
80 Z = 78872
43
XDOT = -10923
164117 XDOT = -3329
380423
YDOT = -8744
564769 feet/sec YDOT = -2665
343342 meter/sec
ZDOT = -19738
062788 ZDOT = -6016
161538
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 17245
26149887
00016717 00000-0 10270-3 0 9090
2 25544 51
6418 14
1072 0004298 221
7539 138
3286 15
53990457 33739
Satellite: ISS
Catalog Number: 25544
Epoch time: 17245
26149887 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 14
1072 deg
Eccentricity:
0004298
Arg of perigee: 221
7539 deg
Mean anomaly: 138
3286 deg
Mean motion: 15
53990457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3373
Checksum: 333
Coasting Arc #11 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2017/246/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6237185
01 A = 6788487
99 meter
Y = 2183353
80 meter E =
0009789
Z = 1535702
13 I = 51
71859
XDOT = -2880
726064 Wp = 68
68674
YDOT = 4158
430251 meter/sec RA = 8
72447 deg
ZDOT = 5761
686094 TA = 308
07323
MA = 308
16150
Ha = 220
425 n
mi
Hp = 215
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20463205
42 X = 6204847
02
Y = 7163234
24 feet Y = 2252921
52 meter
Z = 5038392
81 Z = 1565921
40
XDOT = -9451
200997 XDOT = -2954
999743
YDOT = 13643
143867 feet/sec YDOT = 4125
801051 meter/sec
ZDOT = 18903
169600 ZDOT = 5747
511954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15346492
42 X = 4677610
89
Y = -15270149
29 feet Y = -4654341
50 meter
Z = 5171828
90 Z = 1576373
45
XDOT = 6998
768426 XDOT = 2133
224616
YDOT = 13442
785272 feet/sec YDOT = 4097
360951 meter/sec
ZDOT = 18839
670628 ZDOT = 5742
331607
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 17246
29039408
00016717 00000-0 10270-3 0 9103
2 25544 51
6413 8
9786 0004322 228
3504 131
7279 15
54056088 33890
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
29039408 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 8
9786 deg
Eccentricity:
0004322
Arg of perigee: 228
3504 deg
Mean anomaly: 131
7279 deg
Mean motion: 15
54056088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3389
Checksum: 317
Coasting Arc #12 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2017/246/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6670515
16 A = 6788969
60 meter
Y = -85370
00 meter E =
0004693
Z = -1248110
69 I = 51
71223
XDOT = 1153
402310 Wp = 33
88671
YDOT = 4817
283520 meter/sec RA = 7
75999 deg
ZDOT = 5849
249861 TA = 312
56307
MA = 312
60266
Ha = 220
664 n
mi
Hp = 215
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21884892
25 X = 6677036
66
Y = -280085
32 feet Y = -10739
37 meter
Z = -4094851
35 Z = -1215691
95
XDOT = 3784
128315 XDOT = 1071
036005
YDOT = 15804
735959 feet/sec YDOT = 4829
721468 meter/sec
ZDOT = 19190
452299 ZDOT = 5854
652317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14831948
43 X = -4520777
88
Y = -16130575
72 feet Y = -4916599
48 meter
Z = -3951277
89 Z = -1204349
50
XDOT = 8153
569712 XDOT = 2485
208048
YDOT = -12191
618984 feet/sec YDOT = -3716
005466 meter/sec
ZDOT = 19213
528733 ZDOT = 5856
283558
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 17246
41900815
00016717 00000-0 10270-3 0 9117
2 25544 51
6398 8
3326 0004491 221
6790 138
4021 15
54039015 33919
Satellite: ISS
Catalog Number: 25544
Epoch time: 17246
41900815 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 8
3326 deg
Eccentricity:
0004491
Arg of perigee: 221
6790 deg
Mean anomaly: 138
4021 deg
Mean motion: 15
54039015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 290
Coasting Arc #13 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2017/247/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6732922
16 A = 6789408
18 meter
Y = -681902
10 meter E =
0011962
Z = -446562
35 I = 51
68155
XDOT = 870
034981 Wp = 159
20125
YDOT = -4702
539876 meter/sec RA = 2
79389 deg
ZDOT = -5997
096583 TA = 25
61288
MA = 25
55367
Ha = 220
407 n
mi
Hp = 215
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22089639
63 X = -6722627
39
Y = -2237211
60 feet Y = -757136
69 meter
Z = -1465099
57 Z = -479243
32
XDOT = 2854
445477 XDOT = 951
685958
YDOT = -15428
280433 feet/sec YDOT = -4692
354493 meter/sec
ZDOT = -19675
513724 ZDOT = -5992
671585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13375836
52 X = 4076954
97
Y = 17708746
57 feet Y = 5397625
95 meter
Z = -1609690
63 Z = -490633
70
XDOT = -12049
722974 XDOT = -3672
755562
YDOT = 7331
165014 feet/sec YDOT = 2234
539096 meter/sec
ZDOT = -19655
096116 ZDOT = -5990
873296
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 17247
44789905
00016717 00000-0 10270-3 0 9127
2 25544 51
6398 3
2037 0004340 227
2908 132
7880 15
54066739 34079
Satellite: ISS
Catalog Number: 25544
Epoch time: 17247
44789905 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 3
2037 deg
Eccentricity:
0004340
Arg of perigee: 227
2908 deg
Mean anomaly: 132
7880 deg
Mean motion: 15
54066739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 320
Coasting Arc #14 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2017/248/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6304380
78 A = 6787572
69 meter
Y = 1403582
17 meter E =
0009865
Z = 2074763
73 I = 51
64384
XDOT = -2827
831013 Wp = 78
67953
YDOT = 4490
292777 meter/sec RA = 357
82481 deg
ZDOT = 5534
534557 TA = 304
27619
MA = 304
36956
Ha = 220
352 n
mi
Hp = 215
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20683663
96 X = 6278138
92
Y = 4604928
39 feet Y = 1473935
53 meter
Z = 6806967
63 Z = 2105324
24
XDOT = -9277
660804 XDOT = -2904
716243
YDOT = 14731
931684 feet/sec YDOT = 4458
240695 meter/sec
ZDOT = 18157
921774 ZDOT = 5520
610807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10972255
20 X = -3344343
39
Y = -18076833
50 feet Y = -5509818
85 meter
Z = 6942033
92 Z = 2115931
94
XDOT = 15817
374772 XDOT = 4821
135831
YDOT = -2626
379721 feet/sec YDOT = -800
520539 meter/sec
ZDOT = 18095
489444 ZDOT = 5515
505183
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 17248
47678469
00016717 00000-0 10270-3 0 9134
2 25544 51
6406 358
0760 0004469 229
2512 130
8253 15
54080594 34234
Satellite: ISS
Catalog Number: 25544
Epoch time: 17248
47678469 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 358
0760 deg
Eccentricity:
0004469
Arg of perigee: 229
2512 deg
Mean anomaly: 130
8253 deg
Mean motion: 15
54080594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 322
Coasting Arc #15 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2017/249/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5396514
98 A = 6784197
50 meter
Y = -2130847
39 meter E =
0002629
Z = -3515405
32 I = 51
59964
XDOT = 4582
802685 Wp = 141
79889
YDOT = -4175
989807 meter/sec RA = 352
84613 deg
ZDOT = -4507
648637 TA = 79
59497
MA = 79
56534
Ha = 220
181 n
mi
Hp = 215
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17705101
63 X = -5355210
23
Y = -6990969
14 feet Y = -2190964
35 meter
Z = -11533482
02 Z = -3541519
13
XDOT = 15035
441880 XDOT = 4651
054872
YDOT = -13700
753959 feet/sec YDOT = -4124
360665 meter/sec
ZDOT = -14788
873482 ZDOT = -4485
220757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7467478
39 X = 2276087
41
Y = 17432998
83 feet Y = 5313578
04 meter
Z = -11648725
21 Z = -3550531
44
XDOT = -19114
268825 XDOT = -5826
029138
YDOT = -1619
131464 feet/sec YDOT = -493
511270 meter/sec
ZDOT = -14688
854884 ZDOT = -4477
162969
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 17249
44136269
00016717 00000-0 10270-3 0 9140
2 25544 51
6405 353
2688 0004424 234
0370 126
0372 15
54054925 34380
Satellite: ISS
Catalog Number: 25544
Epoch time: 17249
44136269 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 353
2688 deg
Eccentricity:
0004424
Arg of perigee: 234
0370 deg
Mean anomaly: 126
0372 deg
Mean motion: 15
54054925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 304
Coasting Arc #16 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2017/250/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4116858
14 A = 6780428
74 meter
Y = 2834123
00 meter E =
0006972
Z = 4581388
06 I = 51
55639
XDOT = -5963
101967 Wp = 145
79790
YDOT = 3746
217149 meter/sec RA = 347
85463 deg
ZDOT = 3033
106964 TA = 273
82691
MA = 273
90663
Ha = 219
969 n
mi
Hp = 216
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13506752
43 X = 4062606
21
Y = 9298303
81 feet Y = 2879857
72 meter
Z = 15030800
74 Z = 4601254
28
XDOT = -19563
982830 XDOT = -6019
283253
YDOT = 12290
738677 feet/sec YDOT = 3679
219910 meter/sec
ZDOT = 9951
138333 ZDOT = 3004
003299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3131069
37 X = -954349
94
Y = -16014072
25 feet Y = -4881089
22 meter
Z = 15118256
53 Z = 4608044
59
XDOT = 21474
210791 XDOT = 6545
339449
YDOT = 5097
910762 feet/sec YDOT = 1553
843200 meter/sec
ZDOT = 9821
653822 ZDOT = 2993
640085
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 17250
47023809
00016717 00000-0 10270-3 0 9151
2 25544 51
6417 348
1404 0004447 238
9357 121
1359 15
54092530 34548
Satellite: ISS
Catalog Number: 25544
Epoch time: 17250
47023809 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 348
1404 deg
Eccentricity:
0004447
Arg of perigee: 238
9357 deg
Mean anomaly: 121
1359 deg
Mean motion: 15
54092530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 303
Coasting Arc #17 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2017/251/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2555776
05 A = 6777961
45 meter
Y = -3534871
18 meter E =
0010166
Z = -5196687
83 I = 51
51607
XDOT = 6872
394908 Wp = 87
80862
YDOT = -3150
719765 meter/sec RA = 342
85311 deg
ZDOT = -1238
450603 TA = 170
28297
MA = 170
26330
Ha = 219
952 n
mi
Hp = 216
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8385092
02 X = -2490815
27
Y = -11597346
38 feet Y = -3563089
01 meter
Z = -17049500
75 Z = -5208944
79
XDOT = 22547
227388 XDOT = 6913
132109
YDOT = -10337
007103 feet/sec YDOT = -3073
640333 meter/sec
ZDOT = -4063
158145 ZDOT = -1204
967326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1910722
16 X = -582388
11
Y = 14118256
15 feet Y = 4303244
48 meter
Z = -17103147
99 Z = -5213039
51
XDOT = -22501
210083 XDOT = -6858
368833
YDOT = -7780
430276 feet/sec YDOT = -2371
475148 meter/sec
ZDOT = -3914
404540 ZDOT = -1193
110504
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 17251
43480555
00016717 00000-0 10270-3 0 9164
2 25544 51
6416 343
3338 0004265 243
0298 117
0420 15
54081295 34694
Satellite: ISS
Catalog Number: 25544
Epoch time: 17251
43480555 = yrday
fracday
Element set: 916
Inclination: 51
6416 deg
RA of node: 343
3338 deg
Eccentricity:
0004265
Arg of perigee: 243
0298 deg
Mean anomaly: 117
0420 deg
Mean motion: 15
54081295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 302
Coasting Arc #18 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2017/252/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909865
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 875802
18 A = 6777625
40 meter
Y = 4172169
44 meter E =
0001209
Z = 5269984
30 I = 51
48366
XDOT = -7259
279717 Wp = 258
35482
YDOT = 2375
926742 meter/sec RA = 337
84399 deg
ZDOT = -674
959929 TA = 198
10246
MA = 198
10677
Ha = 219
783 n
mi
Hp = 216
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2873366
74 X = 803483
68
Y = 13688219
94 feet Y = 4181559
50 meter
Z = 17289974
72 Z = 5274062
56
XDOT = -23816
534503 XDOT = -7282
029798
YDOT = 7795
035242 feet/sec YDOT = 2294
621247 meter/sec
ZDOT = -2214
435462 ZDOT = -710
278923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7155474
41 X = 2180988
60
Y = -11992623
12 feet Y = -3655351
53 meter
Z = 17307310
71 Z = 5275268
31
XDOT = 21989
917075 XDOT = 6702
526724
YDOT = 9700
195226 feet/sec YDOT = 2956
619505 meter/sec
ZDOT = -2371
166651 ZDOT = -722
731595
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 17252
46367210
00016717 00000-0 10270-3 0 9171
2 25544 51
6412 338
2051 0004267 247
3505 112
7196 15
54092457 34857
Satellite: ISS
Catalog Number: 25544
Epoch time: 17252
46367210 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 338
2051 deg
Eccentricity:
0004267
Arg of perigee: 247
3505 deg
Mean anomaly: 112
7196 deg
Mean motion: 15
54092457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 302
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