[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6283 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
297/11:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 212
0
304/00:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
2
304/02:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
2
307/03:37:49
079 -0
9 4
9 4
9
N/A 4
7 -0
0 222
7
000/00:01:38
158 1
2 0
0 215
4
308/04:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 2466)
---------------------------------------
Vector Time (GMT): 2016/295/17:18:30
587
Vector Time (MET): N/A
Weight (LBS) : 911080
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5880870
44 A = 6788636
63 meter
Y = 3298355
92 meter E =
0018795
Z = 731348
47 I = 51
86415
XDOT = -1754
366678 Wp = 67
83884
YDOT = -4478
331365 meter/sec RA = 145
82852 deg
ZDOT = 5974
404932 TA = 300
04102
MA = 300
22733
Ha = 223
267 n
mi
Hp = 211
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19294194
35 X = -5920869
04
Y = 10821377
71 feet Y = 3232368
47 meter
Z = 2399437
23 Z = 702682
98
XDOT = -5755
796188 XDOT = -1733
179937
YDOT = -14692
688207 feet/sec YDOT = -4497
831164 meter/sec
ZDOT = 19601
066049 ZDOT = 5965
934183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16609121
69 X = -5062460
29
Y = -14631946
69 feet Y = -4459817
35 meter
Z = 2273469
32 Z = 692953
45
XDOT = 10844
315881 XDOT = 3305
347481
YDOT = -9207
570358 feet/sec YDOT = -2806
467445 meter/sec
ZDOT = 19564
694492 ZDOT = 5963
318881
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 16295
78414808
00016717 00000-0 10270-3 0 9000
2 25544 51
6413 146
6083 0006931 97
2825 262
9115 15
54298046 24671
Satellite: ISS
Catalog Number: 25544
Epoch time: 16295
78414808 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 146
6083 deg
Eccentricity:
0006931
Arg of perigee: 97
2825 deg
Mean anomaly: 262
9115 deg
Mean motion: 15
54298046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2467
Checksum: 325
Coasting Arc #2 (Orbit 2481)
---------------------------------------
Vector Time (GMT): 2016/296/17:18:30
587
Vector Time (MET): N/A
Weight (LBS) : 911080
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5890693
01 A = 6786346
40 meter
Y = -2310401
39 meter E =
0011981
Z = -2453673
55 I = 51
88229
XDOT = -72
570862 Wp = 115
08981
YDOT = 5478
530792 meter/sec RA = 140
87137 deg
ZDOT = -5358
237442 TA = 92
26789
MA = 92
13070
Ha = 223
296 n
mi
Hp = 211
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19326420
62 X = 5928009
72
Y = -7580057
06 feet Y = -2244319
19 meter
Z = -8050110
06 Z = -2424966
95
XDOT = -238
093379 XDOT = -107
799493
YDOT = 17974
182389 feet/sec YDOT = 5477
522005 meter/sec
ZDOT = -17579
519168 ZDOT = -5358
675826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13843519
19 X = 4219504
65
Y = 15535047
63 feet Y = 4735082
52 meter
Z = -7924098
87 Z = -2415265
33
XDOT = -15762
391021 XDOT = -4804
376783
YDOT = 5120
893617 feet/sec YDOT = 1560
848374 meter/sec
ZDOT = -17582
299483 ZDOT = -5359
084882
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 16296
74857736
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 141
7997 0006940 100
3864 259
8072 15
54301857 24824
Satellite: ISS
Catalog Number: 25544
Epoch time: 16296
74857736 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 141
7997 deg
Eccentricity:
0006940
Arg of perigee: 100
3864 deg
Mean anomaly: 259
8072 deg
Mean motion: 15
54301857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2482
Checksum: 337
Coasting Arc #3 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2016/297/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5712298
28 A = 6785176
72 meter
Y = 2112038
72 meter E =
0019693
Z = 2973304
89 I = 51
89669
XDOT = 478
302703 Wp = 87
77944
YDOT = -5794
826071 meter/sec RA = 137
19857 deg
ZDOT = 5007
376348 TA = 306
10538
MA = 306
28754
Ha = 223
224 n
mi
Hp = 212
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18741136
09 X = -5749934
27
Y = 6929260
89 feet Y = 2047949
71 meter
Z = 9754937
31 Z = 2945464
15
XDOT = 1569
234591 XDOT = 518
742451
YDOT = -19011
896558 feet/sec YDOT = -5789
250951 meter/sec
ZDOT = 16428
400093 ZDOT = 5009
798425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15808566
37 X = 4818451
03
Y = -12316788
24 feet Y = -3754157
06 meter
Z = 9632735
70 Z = 2936057
84
XDOT = 3485
405829 XDOT = 1062
351697
YDOT = 17403
097550 feet/sec YDOT = 5304
464133 meter/sec
ZDOT = 16439
917518 ZDOT = 5010
886859
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 16297
52011673
00016717 00000-0 10270-3 0 9029
2 25544 51
6410 137
9577 0006631 98
3752 261
8153 15
54300199 24940
Satellite: ISS
Catalog Number: 25544
Epoch time: 16297
52011673 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 137
9577 deg
Eccentricity:
0006631
Arg of perigee: 98
3752 deg
Mean anomaly: 261
8153 deg
Mean motion: 15
54300199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 313
Coasting Arc #4 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2016/298/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5212864
68 A = 6781164
18 meter
Y = -744120
03 meter E =
0014109
Z = -4285736
64 I = 51
90612
XDOT = -2034
781075 Wp = 84
51843
YDOT = 6443
579440 meter/sec RA = 132
23062 deg
ZDOT = -3602
616975 TA = 148
81157
MA = 148
72777
Ha = 223
109 n
mi
Hp = 212
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17102574
41 X = 5241616
67
Y = -2441338
70 feet Y = -685665
84 meter
Z = -14060815
75 Z = -4260343
70
XDOT = -6675
790930 XDOT = -2089
183454
YDOT = 21140
352495 feet/sec YDOT = 6420
520703 meter/sec
ZDOT = -11819
609499 ZDOT = -3612
634149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15505626
74 X = -4726115
03
Y = 7819896
03 feet Y = 2383504
31 meter
Z = -13949533
73 Z = -4251817
88
XDOT = 52
197777 XDOT = 15
909882
YDOT = -21008
631178 feet/sec YDOT = -6403
430783 meter/sec
ZDOT = -11864
486204 ZDOT = -3616
295395
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 16298
48453844
00016717 00000-0 10270-3 0 9036
2 25544 51
6407 133
1485 0006516 102
3496 257
8386 15
54305585 25099
Satellite: ISS
Catalog Number: 25544
Epoch time: 16298
48453844 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 133
1485 deg
Eccentricity:
0006516
Arg of perigee: 102
3496 deg
Mean anomaly: 257
8386 deg
Mean motion: 15
54305585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 329
Coasting Arc #5 (Orbit 2524)
---------------------------------------
Vector Time (GMT): 2016/299/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4411121
75 A = 6778018
66 meter
Y = -775255
96 meter E =
0012042
Z = 5079376
94 I = 51
91642
XDOT = 3289
118148 Wp = 114
19215
YDOT = -6690
065130 meter/sec RA = 127
25363 deg
ZDOT = 1827
088901 TA = 318
15864
MA = 318
25062
Ha = 223
309 n
mi
Hp = 212
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14472184
24 X = -4426798
52
Y = -2543490
68 feet Y = -824671
31 meter
Z = 16664622
50 Z = 5057910
55
XDOT = 10791
070039 XDOT = 3354
808393
YDOT = -21949
032579 feet/sec YDOT = -6652
916551 meter/sec
ZDOT = 5994
386157 ZDOT = 1843
226927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14584995
23 X = 4445506
55
Y = -2512123
65 feet Y = -765695
29 meter
Z = 16570765
02 Z = 5050769
18
XDOT = -2922
872704 XDOT = -890
891600
YDOT = 23222
991209 feet/sec YDOT = 7078
367720 meter/sec
ZDOT = 6066
110907 ZDOT = 1848
950604
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 16299
51325111
00016717 00000-0 10270-3 0 9047
2 25544 51
6407 128
0185 0006677 105
3781 254
8109 15
54286501 25251
Satellite: ISS
Catalog Number: 25544
Epoch time: 16299
51325111 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 128
0185 deg
Eccentricity:
0006677
Arg of perigee: 105
3781 deg
Mean anomaly: 254
8109 deg
Mean motion: 15
54286501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2525
Checksum: 302
Coasting Arc #6 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2016/300/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3433251
88 A = 6776795
88 meter
Y = 2402828
23 meter E =
0021294
Z = -5344069
14 I = 51
92944
XDOT = -4200
299718 Wp = 97
10479
YDOT = 6395
035426 meter/sec RA = 122
27087 deg
ZDOT = 174
958640 TA = 174
57083
MA = 174
54771
Ha = 223
072 n
mi
Hp = 212
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11263949
72 X = 3432087
24
Y = 7883294
72 feet Y = 2441214
15 meter
Z = -17533035
23 Z = -5327394
07
XDOT = -13780
510886 XDOT = -4272
348347
YDOT = 20981
087356 feet/sec YDOT = 6347
662022 meter/sec
ZDOT = 574
011285 ZDOT = 154
378748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13425784
95 X = -4092179
25
Y = -3363400
76 feet Y = -1025164
55 meter
Z = -17460414
01 Z = -5321934
19
XDOT = 5254
535099 XDOT = 1601
582298
YDOT = -23514
997014 feet/sec YDOT = -7167
371090 meter/sec
ZDOT = 482
872130 ZDOT = 147
179425
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 16300
47766328
00016717 00000-0 10270-3 0 9055
2 25544 51
6387 123
2088 0006670 109
6854 250
5019 15
54325883 25405
Satellite: ISS
Catalog Number: 25544
Epoch time: 16300
47766328 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 123
2088 deg
Eccentricity:
0006670
Arg of perigee: 109
6854 deg
Mean anomaly: 250
5019 deg
Mean motion: 15
54325883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 314
Coasting Arc #7 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2016/301/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2354584
99 A = 6778281
29 meter
Y = -3937479
37 meter E =
0011194
Z = 4980323
15 I = 51
95141
XDOT = 4788
432853 Wp = 86
55637
YDOT = -5598
389583 meter/sec RA = 117
29085 deg
ZDOT = -2157
445758 TA = 24
37987
MA = 24
32696
Ha = 223
097 n
mi
Hp = 212
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7725016
39 X = -2334572
79
Y = -12918239
40 feet Y = -3963697
56 meter
Z = 16339642
88 Z = 4968933
94
XDOT = 15710
081540 XDOT = 4861
159718
YDOT = -18367
419893 feet/sec YDOT = -5544
435675 meter/sec
ZDOT = -7078
234113 ZDOT = -2134
007160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12041215
00 X = 3670162
33
Y = 9119877
53 feet Y = 2779738
67 meter
Z = 16290417
18 Z = 4965319
16
XDOT = -7208
781700 XDOT = -2197
236662
YDOT = 22004
836081 feet/sec YDOT = 6707
074037 meter/sec
ZDOT = -6974
692298 ZDOT = -2125
886212
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 16301
50636648
00016717 00000-0 10270-3 0 9062
2 25544 51
6392 118
0792 0006522 114
2139 245
9696 15
54320230 25566
Satellite: ISS
Catalog Number: 25544
Epoch time: 16301
50636648 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 118
0792 deg
Eccentricity:
0006522
Arg of perigee: 114
2139 deg
Mean anomaly: 245
9696 deg
Mean motion: 15
54320230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 302
Coasting Arc #8 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2016/302/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1299060
49 A = 6781663
11 meter
Y = 5261398
03 meter E =
0013953
Z = -4091921
69 I = 51
97609
XDOT = -5034
809975 Wp = 113
00012
YDOT = 4261
875935 meter/sec RA = 112
31751 deg
ZDOT = 3886
746266 TA = 197
09909
MA = 197
14615
Ha = 223
004 n
mi
Hp = 212
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4262009
49 X = 1260006
86
Y = 17261804
56 feet Y = 5275706
27 meter
Z = -13424939
93 Z = -4085706
38
XDOT = -16518
405431 XDOT = -5100
973702
YDOT = 13982
532596 feet/sec YDOT = 4205
203716 meter/sec
ZDOT = 12751
792211 ZDOT = 3862
126813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10653019
63 X = -3247040
38
Y = -14260241
23 feet Y = -4346521
53 meter
Z = -13398594
20 Z = -4083891
51
XDOT = 8905
505004 XDOT = 2714
397925
YDOT = -18516
016467 feet/sec YDOT = -5643
681819 meter/sec
ZDOT = 12643
284782 ZDOT = 3853
673202
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 16302
47077110
00016717 00000-0 10270-3 0 9073
2 25544 51
6384 113
2687 0006685 117
3795 242
8039 15
54338452 25718
Satellite: ISS
Catalog Number: 25544
Epoch time: 16302
47077110 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 113
2687 deg
Eccentricity:
0006685
Arg of perigee: 117
3795 deg
Mean anomaly: 242
8039 deg
Mean motion: 15
54338452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 315
Coasting Arc #9 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2016/303/11:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 925606
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -271545
02 A = 6785550
95 meter
Y = -6207484
69 meter E =
0019738
Z = 2702065
61 I = 52
00052
XDOT = 5048
605497 Wp = 107
97909
YDOT = -2500
909931 meter/sec RA = 107
35720 deg
ZDOT = -5212
812155 TA = 41
61796
MA = 41
46790
Ha = 222
880 n
mi
Hp = 212
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -890895
72 X = -215236
94
Y = -20365763
42 feet Y = -6210206
24 meter
Z = 8865044
65 Z = 2700883
75
XDOT = 16563
666330 XDOT = 5101
518294
YDOT = -8205
085077 feet/sec YDOT = -2444
157600 meter/sec
ZDOT = -17102
402083 ZDOT = -5188
157981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9023800
63 X = 2750454
43
Y = 18281201
63 feet Y = 5572110
26 meter
Z = 8860909
69 Z = 2700805
27
XDOT = -10659
590237 XDOT = -3249
043104
YDOT = 13538
786737 feet/sec YDOT = 4126
622197 meter/sec
ZDOT = -16994
023672 ZDOT = -5179
778415
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 16303
49946298
00016717 00000-0 10270-3 0 9089
2 25544 51
6383 108
1387 0006469 121
0886 239
0903 15
54364436 25876
Satellite: ISS
Catalog Number: 25544
Epoch time: 16303
49946298 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 108
1387 deg
Eccentricity:
0006469
Arg of perigee: 121
0886 deg
Mean anomaly: 239
0903 deg
Mean motion: 15
54364436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 339
Coasting Arc #10 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2016/304/00:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 910374
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4381359
50 A = 6778284
16 meter
Y = 1402314
07 meter E =
0012982
Z = 4971046
94 I = 51
98141
XDOT = 145
055037 Wp = 122
18948
YDOT = -7353
474005 meter/sec RA = 104
59990 deg
ZDOT = 2191
332219 TA = 306
50039
MA = 306
61991
Ha = 223
044 n
mi
Hp = 212
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14374539
05 X = -4420862
72
Y = 4600767
94 feet Y = 1353098
25 meter
Z = 16309209
13 Z = 4949666
80
XDOT = 475
902354 XDOT = 216
627862
YDOT = -24125
570881 feet/sec YDOT = -7351
451554 meter/sec
ZDOT = 7189
410168 ZDOT = 2192
211260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6440669
98 X = -1963116
21
Y = 13760995
87 feet Y = 4194351
54 meter
Z = 16215347
78 Z = 4942438
00
XDOT = -16431
214874 XDOT = -5008
234294
YDOT = -16210
514462 feet/sec YDOT = -4940
964808 meter/sec
ZDOT = 7194
502131 ZDOT = 2192
884249
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 16304
07810280
00016717 00000-0 10270-3 0 9096
2 25544 51
6383 105
2564 0006593 121
9534 238
2260 15
54355317 25963
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
07810280 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 105
2564 deg
Eccentricity:
0006593
Arg of perigee: 121
9534 deg
Mean anomaly: 238
2260 deg
Mean motion: 15
54355317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 303
Coasting Arc #11 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2016/304/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 910374
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4324415
44 A = 6777319
11 meter
Y = 571243
43 meter E =
0011091
Z = 5180348
50 I = 51
98027
XDOT = 745
194753 Wp = 123
44395
YDOT = -7501
367970 meter/sec RA = 104
26904 deg
ZDOT = 1441
084630 TA = 312
72048
MA = 312
81380
Ha = 222
990 n
mi
Hp = 212
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14187714
68 X = -4355646
37
Y = 1874158
25 feet Y = 522710
67 meter
Z = 16995894
04 Z = 5159265
14
XDOT = 2444
864676 XDOT = 822
021234
YDOT = -24610
787304 feet/sec YDOT = -7492
605036 meter/sec
ZDOT = 4727
967945 ZDOT = 1444
891838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2887200
69 X = -880018
77
Y = 14128015
57 feet Y = 4306219
15 meter
Z = 16903472
40 Z = 5152178
39
XDOT = -21449
060101 XDOT = -6537
673519
YDOT = -10093
815949 feet/sec YDOT = -3076
595101 meter/sec
ZDOT = 4745
908751 ZDOT = 1446
552987
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 16304
14239543
00016717 00000-0 10270-3 0 9103
2 25544 51
6396 104
9360 0006512 122
2864 237
8920 15
54376083 25970
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
14239543 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 104
9360 deg
Eccentricity:
0006512
Arg of perigee: 122
2864 deg
Mean anomaly: 237
8920 deg
Mean motion: 15
54376083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2597
Checksum: 307
Coasting Arc #12 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2016/305/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 910374
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4000243
41 A = 6776837
97 meter
Y = 1327018
73 meter E =
0020578
Z = -5324455
70 I = 51
98616
XDOT = -1682
993629 Wp = 103
89791
YDOT = 7443
193166 meter/sec RA = 99
28945 deg
ZDOT = 587
745549 TA = 171
71258
MA = 171
67854
Ha = 222
861 n
mi
Hp = 212
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13124158
17 X = 4010971
65
Y = 4353735
99 feet Y = 1371811
82 meter
Z = -17468686
68 Z = -5304997
01
XDOT = -5521
632641 XDOT = -1768
955324
YDOT = 24419
925084 feet/sec YDOT = 7423
892194 meter/sec
ZDOT = 1928
299044 ZDOT = 579
360548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8237128
17 X = 2510676
67
Y = -11238782
20 feet Y = -3425580
81 meter
Z = -17383700
80 Z = -5298552
00
XDOT = 20686
698395 XDOT = 6305
305671
YDOT = 12223
057996 feet/sec YDOT = 3725
588077 meter/sec
ZDOT = 1890
300873 ZDOT = 576
163706
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 16305
10678955
00016717 00000-0 10270-3 0 9115
2 25544 51
6404 100
1261 0006523 125
3247 234
8517 15
54346573 26127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
10678955 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 100
1261 deg
Eccentricity:
0006523
Arg of perigee: 125
3247 deg
Mean anomaly: 234
8517 deg
Mean motion: 15
54346573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 286
Coasting Arc #13 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2016/306/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 910374
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3553494
64 A = 6778803
04 meter
Y = -3135653
62 meter E =
0011444
Z = 4836895
99 I = 51
99779
XDOT = 2511
732223 Wp = 92
23304
YDOT = -6790
049282 meter/sec RA = 94
31401 deg
ZDOT = -2551
810317 TA = 22
74498
MA = 22
69432
Ha = 222
941 n
mi
Hp = 212
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11658446
98 X = -3541663
06
Y = -10287577
50 feet Y = -3175324
83 meter
Z = 15869081
33 Z = 4819662
39
XDOT = 8240
591282 XDOT = 2599
869546
YDOT = -22277
064573 feet/sec YDOT = -6761
468704 meter/sec
ZDOT = -8372
081091 ZDOT = -2539
394260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13282839
48 X = -4048609
47
Y = 8227527
26 feet Y = 2507750
31 meter
Z = 15794155
55 Z = 4814058
61
XDOT = -18266
030747 XDOT = -5567
486172
YDOT = -13494
336171 feet/sec YDOT = -4113
073665 meter/sec
ZDOT = -8316
521848 ZDOT = -2534
875859
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 16306
13546992
00016717 00000-0 10270-3 0 9125
2 25544 51
6410 94
9970 0006509 128
1165 232
0575 15
54357575 26280
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
13546992 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 94
9970 deg
Eccentricity:
0006509
Arg of perigee: 128
1165 deg
Mean anomaly: 232
0575 deg
Mean motion: 15
54357575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 319
Coasting Arc #14 (Orbit 2642)
---------------------------------------
Vector Time (GMT): 2016/307/02:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 910374
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3046661
26 A = 6782503
44 meter
Y = 4705540
63 meter E =
0012203
Z = -3832227
01 I = 52
01142
XDOT = -3228
287193 Wp = 118
06566
YDOT = 5518
325346 meter/sec RA = 89
34698 deg
ZDOT = 4213
981485 TA = 196
20374
MA = 196
24279
Ha = 222
750 n
mi
Hp = 212
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9995607
82 X = 3012432
08
Y = 15438125
42 feet Y = 4739418
96 meter
Z = -12572923
28 Z = -3817509
96
XDOT = -10591
493415 XDOT = -3310
224836
YDOT = 18104
741949 feet/sec YDOT = 5481
766436 meter/sec
ZDOT = 13825
398572 ZDOT = 4198
099695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17622885
57 X = 5371455
52
Y = -5410874
27 feet Y = -1649234
48 meter
Z = -12509301
96 Z = -3812835
24
XDOT = 14048
139623 XDOT = 4281
872957
YDOT = 13989
569383 feet/sec YDOT = 4264
020748 meter/sec
ZDOT = 13754
865756 ZDOT = 4192
483082
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 16307
09985348
00016717 00000-0 10270-3 0 9134
2 25544 51
6408 90
1883 0006464 131
5062 228
6647 15
54359934 26431
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
09985348 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 90
1883 deg
Eccentricity:
0006464
Arg of perigee: 131
5062 deg
Mean anomaly: 228
6647 deg
Mean motion: 15
54359934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2643
Checksum: 329
Coasting Arc #15 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/03:38:38
158
Vector Time (MET): N/A
Weight (LBS) : 909884
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937585
97 A = 6780872
77 meter
Y = 2392333
34 meter E =
0014592
Z = -4988599
45 I = 51
99883
XDOT = -1587
039909 Wp = 116
40688
YDOT = 7164
725102 meter/sec RA = 89
05710 deg
ZDOT = 2181
859544 TA = 174
80318
MA = 174
78802
Ha = 222
733 n
mi
Hp = 215
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12918589
13 X = 3934774
75
Y = 7848862
65 feet Y = 2436350
23 meter
Z = -16366796
09 Z = -4969478
02
XDOT = -5206
823849 XDOT = -1677
638559
YDOT = 23506
315950 feet/sec YDOT = 7146
471241 meter/sec
ZDOT = 7158
331837 ZDOT = 2173
929664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6526690
90 X = 1989335
39
Y = -13733802
08 feet Y = -4186062
87 meter
Z = -16283476
00 Z = -4963203
49
XDOT = 22908
514088 XDOT = 6982
515094
YDOT = 2436
790057 feet/sec YDOT = 742
733609 meter/sec
ZDOT = 7122
332363 ZDOT = 2170
886904
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 16307
16414561
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 89
8681 0003283 159
9166 200
2116 15
53458130 26440
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16414561 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 89
8681 deg
Eccentricity:
0003283
Arg of perigee: 159
9166 deg
Mean anomaly: 200
2116 deg
Mean motion: 15
53458130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 301
Coasting Arc #16 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/03:38:38
158
Vector Time (MET): N/A
Weight (LBS) : 909884
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720837
02 A = 6783705
62 meter
Y = -3752369
98 meter E =
0010629
Z = 4244264
90 I = 52
00704
XDOT = 2222
574757 Wp = 92
21560
YDOT = -6361
299471 meter/sec RA = 84
09627 deg
ZDOT = -3668
080084 TA = 35
16850
MA = 35
09839
Ha = 222
784 n
mi
Hp = 215
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12207470
55 X = -3699217
84
Y = -12310925
14 feet Y = -3793857
95 meter
Z = 13924753
60 Z = 4226242
11
XDOT = 7291
911934 XDOT = 2311
361643
YDOT = -20870
405090 feet/sec YDOT = -6335
948753 meter/sec
ZDOT = -12034
383479 ZDOT = -3657
067375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10805876
79 X = -3293631
25
Y = 13637729
23 feet Y = 4156779
87 meter
Z = 13846492
20 Z = 4220410
82
XDOT = -20588
911465 XDOT = -6275
500215
YDOT = -4120
082406 feet/sec YDOT = -1255
801117 meter/sec
ZDOT = -11985
006743 ZDOT = -3653
030055
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 16308
19342110
00016717 00000-0 10270-3 0 9152
2 25544 51
6426 84
7435 0003285 164
3278 195
7977 15
53462786 26602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19342110 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 84
7435 deg
Eccentricity:
0003285
Arg of perigee: 164
3278 deg
Mean anomaly: 195
7977 deg
Mean motion: 15
53462786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 328
Coasting Arc #17 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 909884
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3734516
74 A = 6783710
65 meter
Y = 3759752
55 meter E =
0010123
Z = -4246117
88 I = 52
00800
XDOT = -2211
388371 Wp = 125
25566
YDOT = 6344
685890 meter/sec RA = 83
93647 deg
ZDOT = 3673
482387 TA = 182
23755
MA = 182
24208
Ha = 222
594 n
mi
Hp = 215
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12252351
51 X = 3712822
99
Y = 12335146
17 feet Y = 3801393
08 meter
Z = -13930832
94 Z = -4228028
82
XDOT = -7255
211190 XDOT = -2300
016551
YDOT = 20815
898589 feet/sec YDOT = 6319
461151 meter/sec
ZDOT = 12052
107569 ZDOT = 3662
524408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7845683
96 X = 2391364
47
Y = -15585363
64 feet Y = -4750418
84 meter
Z = -13852282
79 Z = -4222175
79
XDOT = 20929
915436 XDOT = 6379
438225
YDOT = -130
695102 feet/sec YDOT = -39
835867 meter/sec
ZDOT = 12002
972963 ZDOT = 3658
506159
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 16308
19342006
00016717 00000-0 10270-3 0 9167
2 25544 51
6436 84
7434 0003206 166
7933 193
3304 15
53468684 26600
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19342006 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 84
7434 deg
Eccentricity:
0003206
Arg of perigee: 166
7933 deg
Mean anomaly: 193
3304 deg
Mean motion: 15
53468684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 311
Coasting Arc #18 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2016/309/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 909884
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3466328
89 A = 6787071
10 meter
Y = -4895210
11 meter E =
0014206
Z = 3159260
81 I = 52
01528
XDOT = 2867
699469 Wp = 107
01516
YDOT = -5185
116988 meter/sec RA = 78
98256 deg
ZDOT = -4873
830073 TA = 36
73866
MA = 36
64137
Ha = 222
665 n
mi
Hp = 215
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11372470
10 X = -3426678
44
Y = -16060400
62 feet Y = -4933751
22 meter
Z = 10365028
92 Z = 3142518
20
XDOT = 9408
462825 XDOT = 2949
143132
YDOT = -17011
538676 feet/sec YDOT = -5152
593080 meter/sec
ZDOT = -15990
256145 ZDOT = -4859
701365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11391436
72 X = -3472109
91
Y = 16093513
02 feet Y = 4905302
77 meter
Z = 10292588
45 Z = 3137180
96
XDOT = -18023
903282 XDOT = -5493
685720
YDOT = -2541
924287 feet/sec YDOT = -774
778523 meter/sec
ZDOT = -15927
428376 ZDOT = -4854
680169
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 16309
22269002
00016717 00000-0 10270-3 0 9177
2 25544 51
6440 79
6183 0003203 167
5680 192
5552 15
53470297 26760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
22269002 = yrday
fracday
Element set: 917
Inclination: 51
6440 deg
RA of node: 79
6183 deg
Eccentricity:
0003203
Arg of perigee: 167
5680 deg
Mean anomaly: 192
5552 deg
Mean motion: 15
53470297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 311
Coasting Arc #19 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2016/310/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 909884
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140367
01 A = 6789749
57 meter
Y = 5728312
73 meter E =
0005564
Z = -1848939
67 I = 52
01719
XDOT = -3528
361853 Wp = 62
37099
YDOT = 3759
027052 meter/sec RA = 74
03488 deg
ZDOT = 5668
781435 TA = 277
41580
MA = 277
47902
Ha = 222
445 n
mi
Hp = 215
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10303041
38 X = 3085059
68
Y = 18793676
94 feet Y = 5763121
18 meter
Z = -6066075
03 Z = -1833818
59
XDOT = -11575
990332 XDOT = -3597
671048
YDOT = 12332
765918 feet/sec YDOT = 3719
183003 meter/sec
ZDOT = 18598
364287 ZDOT = 5651
472862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14057372
38 X = 4284687
10
Y = -16202830
76 feet Y = -4938622
82 meter
Z = -6000898
09 Z = -1829073
74
XDOT = 14436
571705 XDOT = 4400
267056
YDOT = 5684
281044 feet/sec YDOT = 1732
568862 meter/sec
ZDOT = 18521
858082 ZDOT = 5645
462344
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 16310
18762507
00016717 00000-0 10270-3 0 9183
2 25544 51
6438 74
8128 0003127 172
9021 187
2176 15
53494695 26915
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
18762507 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 74
8128 deg
Eccentricity:
0003127
Arg of perigee: 172
9021 deg
Mean anomaly: 187
2176 deg
Mean motion: 15
53494695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 322
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