[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
160/13:47:39
077 -0
2 1
9 2
0
N/A 1
9 -0
2 220
2
000/00:05:18
153 0
2 -0
0 214
9
161/01:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 214
8
Coasting Arc #1 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4534160
59 A = 6783916
95 meter
Y = 4104747
54 meter E =
0005594
Z = -2938749
84 I = 51
76823
XDOT = -5317
486063 Wp = 82
21237
YDOT = -2283
418774 meter/sec RA = 160
08885 deg
ZDOT = 5023
804118 TA = 244
32833
MA = 244
38612
Ha = 220
583 n
mi
Hp = 213
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14875854
94 X = -4565448
68
Y = 13467019
50 feet Y = 4053868
84 meter
Z = -9641567
70 Z = -2960851
39
XDOT = -17445
820418 XDOT = -5315
960655
YDOT = -7491
531410 feet/sec YDOT = -2342
874325 meter/sec
ZDOT = 16482
296976 ZDOT = 4997
976526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5818140
50 X = 1773369
23
Y = 19155238
93 feet Y = 5838516
83 meter
Z = -9738458
03 Z = -2968282
01
XDOT = -12892
566322 XDOT = -3929
654215
YDOT = 12223
793173 feet/sec YDOT = 3725
812159 meter/sec
ZDOT = 16370
271755 ZDOT = 4989
658831
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 16148
50606296
00016717 00000-0 10270-3 0 9001
2 25544 51
6409 161
2087 0001609 124
5472 235
5834 15
54704009 1762
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
50606296 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 161
2087 deg
Eccentricity:
0001609
Arg of perigee: 124
5472 deg
Mean anomaly: 235
5834 deg
Mean motion: 15
54704009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 176
Checksum: 297
Coasting Arc #2 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5613646
66 A = 6787057
59 meter
Y = -3617200
68 meter E =
0015310
Z = 1169261
02 I = 51
80753
XDOT = 3481
091814 Wp = 122
33618
YDOT = 3485
773462 meter/sec RA = 155
12127 deg
ZDOT = -5881
187280 TA = 44
98778
MA = 44
86385
Ha = 220
602 n
mi
Hp = 213
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18417475
90 X = 5647998
10
Y = -11867456
30 feet Y = -3554233
16 meter
Z = 3836158
20 Z = 1196613
99
XDOT = 11420
904900 XDOT = 3470
422669
YDOT = 11436
264638 feet/sec YDOT = 3524
642097 meter/sec
ZDOT = -19295
233858 ZDOT = -5864
302623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3212491
55 X = -979167
43
Y = -21651496
27 feet Y = -6599376
06 meter
Z = 3955838
08 Z = 1205739
45
XDOT = 13602
725058 XDOT = 4146
110598
YDOT = -5558
246545 feet/sec YDOT = -1694
153547 meter/sec
ZDOT = -19222
327342 ZDOT = -5858
965374
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 16149
53452301
00016717 00000-0 10270-3 0 9012
2 25544 51
6399 156
0773 0001584 123
1384 236
9921 15
54699194 1921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
53452301 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 156
0773 deg
Eccentricity:
0001584
Arg of perigee: 123
1384 deg
Mean anomaly: 236
9921 deg
Mean motion: 15
54699194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 192
Checksum: 317
Coasting Arc #3 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6108789
65 A = 6787371
00 meter
Y = 2857365
28 meter E =
0013478
Z = 713623
96 I = 51
83669
XDOT = -1439
060440 Wp = 59
23670
YDOT = -4588
097841 meter/sec RA = 150
16214 deg
ZDOT = 5975
276953 TA = 308
45457
MA = 308
57544
Ha = 220
484 n
mi
Hp = 213
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20041960
79 X = -6143753
90
Y = 9374558
01 feet Y = 2788857
19 meter
Z = 2341285
95 Z = 683864
07
XDOT = -4721
326902 XDOT = -1416
673693
YDOT = -15052
814439 feet/sec YDOT = -4604
065540 meter/sec
ZDOT = 19603
927010 ZDOT = 5968
340436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 636105
61 X = 193884
99
Y = 22130294
34 feet Y = 6745313
72 meter
Z = 2211242
19 Z = 673986
62
XDOT = -14124
378593 XDOT = -4305
110595
YDOT = -1576
563799 feet/sec YDOT = -480
536646 meter/sec
ZDOT = 19574
510124 ZDOT = 5966
310686
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 16150
56297941
00016717 00000-0 10270-3 0 9025
2 25544 51
6390 150
9470 0001562 135
4428 224
6851 15
54736909 2080
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
56297941 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 150
9470 deg
Eccentricity:
0001562
Arg of perigee: 135
4428 deg
Mean anomaly: 224
6851 deg
Mean motion: 15
54736909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 309
Coasting Arc #4 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6036673
71 A = 6785024
65 meter
Y = -1760526
89 meter E =
0006796
Z = -2546020
75 I = 51
85532
XDOT = -624
669885 Wp = 130
88222
YDOT = 5503
123801 meter/sec RA = 145
20013 deg
ZDOT = -5299
972172 TA = 77
62050
MA = 77
54445
Ha = 220
606 n
mi
Hp = 213
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19805359
94 X = 6068279
27
Y = -5776006
87 feet Y = -1692843
94 meter
Z = -8353086
44 Z = -2516619
18
XDOT = -2049
441881 XDOT = -660
415582
YDOT = 18054
868115 feet/sec YDOT = 5495
938726 meter/sec
ZDOT = -17388
360145 ZDOT = -5303
093233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2233881
24 X = 680887
00
Y = -20560920
10 feet Y = -6266968
45 meter
Z = -8224775
40 Z = -2506911
54
XDOT = 14450
419586 XDOT = 4404
487890
YDOT = 8513
426440 feet/sec YDOT = 2594
892379 meter/sec
ZDOT = -17402
889650 ZDOT = -5304
400765
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 16151
52715967
00016717 00000-0 10270-3 0 9036
2 25544 51
6386 146
1358 0001493 130
6539 229
4744 15
54691068 2237
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52715967 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 146
1358 deg
Eccentricity:
0001493
Arg of perigee: 130
6539 deg
Mean anomaly: 229
4744 deg
Mean motion: 15
54691068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 317
Coasting Arc #5 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5439723
66 A = 6780863
13 meter
Y = 423033
47 meter E =
0012000
Z = 4018581
46 I = 51
86758
XDOT = 2461
164552 Wp = 105
07194
YDOT = -6092
837906 meter/sec RA = 140
23047 deg
ZDOT = 3960
043353 TA = 303
86026
MA = 303
97440
Ha = 220
528 n
mi
Hp = 213
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17846862
40 X = -5463570
59
Y = 1387905
07 feet Y = 362069
31 meter
Z = 13184322
37 Z = 3992098
44
XDOT = 8074
686849 XDOT = 2509
876868
YDOT = -19989
625676 feet/sec YDOT = -6065
043363 meter/sec
ZDOT = 12992
268219 ZDOT = 3972
117215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5259743
34 X = -1603169
77
Y = 17198870
37 feet Y = 5242215
69 meter
Z = 13068936
17 Z = 3983411
75
XDOT = -14431
644599 XDOT = -4398
765274
YDOT = -14359
078159 feet/sec YDOT = -4376
647023 meter/sec
ZDOT = 13045
889850 ZDOT = 3976
387226
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 16152
55561201
00016717 00000-0 10270-3 0 9041
2 25544 51
6386 141
0051 0001323 138
8136 221
3117 15
54723209 2391
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
55561201 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 141
0051 deg
Eccentricity:
0001323
Arg of perigee: 138
8136 deg
Mean anomaly: 221
3117 deg
Mean motion: 15
54723209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 239
Checksum: 266
Coasting Arc #6 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438668
84 A = 6777193
61 meter
Y = 1131939
37 meter E =
0013272
Z = -5006735
63 I = 51
87840
XDOT = -3944
601527 Wp = 79
75818
YDOT = 6222
752570 meter/sec RA = 135
24863 deg
ZDOT = -2092
595997 TA = 169
93318
MA = 169
90657
Ha = 220
496 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14562561
82 X = 4450002
24
Y = 3713711
84 feet Y = 1181639
20 meter
Z = -16426297
99 Z = -4985145
77
XDOT = -12941
606060 XDOT = -4003
727655
YDOT = 20415
854889 feet/sec YDOT = 6178
310947 meter/sec
ZDOT = -6865
472432 ZDOT = -2111
901388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8602855
92 X = 2622150
48
Y = -12446851
73 feet Y = -3793800
41 meter
Z = -16332479
30 Z = -4978139
69
XDOT = 13715
230014 XDOT = 4180
402108
YDOT = 18589
526316 feet/sec YDOT = 5666
087621 meter/sec
ZDOT = -6950
621984 ZDOT = -2118
549581
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 16153
51978629
00016717 00000-0 10270-3 0 9055
2 25544 51
6379 136
1938 0001343 134
2772 225
8491 15
54694839 2547
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51978629 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 136
1938 deg
Eccentricity:
0001343
Arg of perigee: 134
2772 deg
Mean anomaly: 225
8491 deg
Mean motion: 15
54694839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 336
Coasting Arc #7 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3169257
39 A = 6775694
56 meter
Y = -2725479
99 meter E =
0003346
Z = 5329940
87 I = 51
89549
XDOT = 4975
618300 Wp = 107
54234
YDOT = -5840
206345 meter/sec RA = 130
26097 deg
ZDOT = -28
801929 TA = 342
72531
MA = 342
73669
Ha = 220
545 n
mi
Hp = 213
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10397826
07 X = -3164435
82
Y = -8941863
50 feet Y = -2760894
21 meter
Z = 17486682
64 Z = 5314556
64
XDOT = 16324
207020 XDOT = 5040
695059
YDOT = -19160
781973 feet/sec YDOT = -5784
201801 meter/sec
ZDOT = -94
494517 ZDOT = -4
473628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11931385
37 X = -3636686
26
Y = 6930780
67 feet Y = 2112501
95 meter
Z = 17420163
66 Z = 5309665
88
XDOT = -12121
114629 XDOT = -3694
515739
YDOT = -20905
972912 feet/sec YDOT = -6372
140544 meter/sec
ZDOT = 12
483190 ZDOT = 3
804876
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 16154
54823663
00016717 00000-0 10270-3 0 9067
2 25544 51
6377 131
0626 0001261 141
3673 218
7571 15
54695616 2703
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54823663 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 131
0626 deg
Eccentricity:
0001261
Arg of perigee: 141
3673 deg
Mean anomaly: 218
7571 deg
Mean motion: 15
54695616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 304
Coasting Arc #8 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1793657
42 A = 6777196
25 meter
Y = 4234809
02 meter E =
0013527
Z = -4990374
77 I = 51
92166
XDOT = -5507
770374 Wp = 108
85474
YDOT = 4867
460399 meter/sec RA = 125
27445 deg
ZDOT = 2151
387550 TA = 182
04978
MA = 182
05533
Ha = 220
405 n
mi
Hp = 213
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5884702
82 X = 1770410
90
Y = 13893730
39 feet Y = 4254737
43 meter
Z = -16372620
65 Z = -4981717
52
XDOT = -18070
112776 XDOT = -5572
240867
YDOT = 15969
358265 feet/sec YDOT = 4805
508146 meter/sec
ZDOT = 7058
358105 ZDOT = 2124
475654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15074477
05 X = 4594700
60
Y = -1278370
99 feet Y = -389647
48 meter
Z = -16335669
18 Z = -4979111
97
XDOT = 9312
178757 XDOT = 2838
352085
YDOT = 21143
521970 feet/sec YDOT = 6444
545496 meter/sec
ZDOT = 6940
276742 ZDOT = 2115
396351
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 16155
51240519
00016717 00000-0 10270-3 0 9079
2 25544 51
6388 126
2519 0001191 142
0853 218
0384 15
54693003 2851
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51240519 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 126
2519 deg
Eccentricity:
0001191
Arg of perigee: 142
0853 deg
Mean anomaly: 218
0384 deg
Mean motion: 15
54693003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 294
Coasting Arc #9 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -422155
92 A = 6780862
63 meter
Y = -5462278
76 meter E =
0011419
Z = 3986763
22 I = 51
95201
XDOT = 5605
613431 Wp = 84
24949
YDOT = -3369
575168 meter/sec RA = 120
29776 deg
ZDOT = -4012
138563 TA = 47
40402
MA = 47
30775
Ha = 220
351 n
mi
Hp = 213
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1385025
99 X = -380410
21
Y = -17920862
08 feet Y = -5466766
67 meter
Z = 13079931
83 Z = 3984813
18
XDOT = 18391
120180 XDOT = 5662
365744
YDOT = -11055
036642 feet/sec YDOT = -3306
571648 meter/sec
ZDOT = -13163
184262 ZDOT = -3984
770096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17532635
43 X = -5343947
28
Y = -3984800
80 feet Y = -1214567
28 meter
Z = 13072423
98 Z = 3984474
83
XDOT = -5282
351276 XDOT = -1610
060669
YDOT = -19665
938428 feet/sec YDOT = -5994
178033 meter/sec
ZDOT = -13043
359967 ZDOT = -3975
616118
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 16156
54084961
00016717 00000-0 10270-3 0 9081
2 25544 51
6387 121
1205 0001071 144
0155 216
1070 15
54721197 3016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54084961 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 121
1205 deg
Eccentricity:
0001071
Arg of perigee: 144
0155 deg
Mean anomaly: 216
1070 deg
Mean motion: 15
54721197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 271
Coasting Arc #10 (Orbit 315)
---------------------------------------
Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -803566
21 A = 6785001
39 meter
Y = 6257729
56 meter E =
0005261
Z = -2496103
50 I = 51
98139
XDOT = -5304
131732 Wp = 61
22996
YDOT = 1444
963889 meter/sec RA = 115
33510 deg
ZDOT = 5341
031973 TA = 270
93186
MA = 270
99213
Ha = 220
328 n
mi
Hp = 213
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2636372
07 X = -861356
88
Y = 20530608
81 feet Y = 6248420
77 meter
Z = -8189315
94 Z = -2500146
56
XDOT = -17402
006994 XDOT = -5345
840129
YDOT = 4740
695175 feet/sec YDOT = 1385
415610 meter/sec
ZDOT = 17523
070779 ZDOT = 5315
164486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18949722
17 X = 5775875
32
Y = 8310043
10 feet Y = 2532901
14 meter
Z = -8208073
14 Z = -2501820
69
XDOT = 176
605713 XDOT = 53
829421
YDOT = 16758
328712 feet/sec YDOT = 5107
938591 meter/sec
ZDOT = 17410
115662 ZDOT = 5306
603254
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 16157
50501532
00016717 00000-0 10270-3 0 9097
2 25544 51
6390 116
3104 0001075 148
1513 211
9705 15
54702660 3169
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50501532 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 116
3104 deg
Eccentricity:
0001075
Arg of perigee: 148
1513 deg
Mean anomaly: 211
9705 deg
Mean motion: 15
54702660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 270
Coasting Arc #11 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1868526
65 A = 6787430
88 meter
Y = -6485436
25 meter E =
0014114
Z = 649512
74 I = 52
00445
XDOT = 4720
690321 Wp = 129
97376
YDOT = 751
485067 meter/sec RA = 110
38355 deg
ZDOT = -5999
835757 TA = 43
04440
MA = 42
93409
Ha = 220
276 n
mi
Hp = 213
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6130336
76 X = 1937754
48
Y = -21277677
98 feet Y = -6464154
16 meter
Z = 2130947
30 Z = 658756
82
XDOT = 15487
829137 XDOT = 4741
080905
YDOT = 2465
502188 feet/sec YDOT = 804
389841 meter/sec
ZDOT = -19684
500516 ZDOT = -5976
854094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18864869
34 X = -5750012
17
Y = -11587011
50 feet Y = -3531721
11 meter
Z = 2172421
36 Z = 662154
03
XDOT = 5707
080803 XDOT = 1739
518229
YDOT = -13010
080464 feet/sec YDOT = -3965
472525 meter/sec
ZDOT = -19584
508583 ZDOT = -5969
358216
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 16158
53345608
00016717 00000-0 10270-3 0 9103
2 25544 51
6410 111
1789 0001035 154
7855 205
3349 15
54718635 3320
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
53345608 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 111
1789 deg
Eccentricity:
0001035
Arg of perigee: 154
7855 deg
Mean anomaly: 205
3349 deg
Mean motion: 15
54718635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 297
Coasting Arc #12 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2016/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2693776
94 A = 6786940
20 meter
Y = 6096629
61 meter E =
0013659
Z = 1247088
45 I = 52
01302
XDOT = -3945
511931 Wp = 62
86363
YDOT = -2954
327431 meter/sec RA = 105
43636 deg
ZDOT = 5877
083806 TA = 310
63053
MA = 310
74924
Ha = 220
249 n
mi
Hp = 213
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8837850
85 X = -2767808
59
Y = 20002065
63 feet Y = 6066091
89 meter
Z = 4091497
55 Z = 1233823
79
XDOT = -12944
592949 XDOT = -3940
730990
YDOT = -9692
675298 feet/sec YDOT = -2998
422851 meter/sec
ZDOT = 19281
771017 ZDOT = 5857
928704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17137606
72 X = 5223542
53
Y = 13600421
75 feet Y = 4145408
55 meter
Z = 4032561
65 Z = 1229124
79
XDOT = -11668
811882 XDOT = -3556
653862
YDOT = 8968
480635 feet/sec YDOT = 2733
592897 meter/sec
ZDOT = 19198
854164 ZDOT = 5851
810749
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 16159
56189338
00016717 00000-0 10270-3 0 9114
2 25544 51
6408 106
0482 0001015 155
6402 204
4799 15
54731231 3489
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
56189338 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 106
0482 deg
Eccentricity:
0001015
Arg of perigee: 155
6402 deg
Mean anomaly: 204
4799 deg
Mean motion: 15
54731231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 297
Coasting Arc #13 (Orbit 362)
---------------------------------------
Vector Time (GMT): 2016/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3337260
72 A = 6783743
07 meter
Y = -5076702
00 meter E =
0005193
Z = -3018963
91 I = 52
01054
XDOT = 3043
296080 Wp = 118
11908
YDOT = 4961
245354 meter/sec RA = 100
48408 deg
ZDOT = -4987
583506 TA = 96
25803
MA = 96
19887
Ha = 220
220 n
mi
Hp = 213
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10949018
11 X = 3408446
42
Y = -16655846
45 feet Y = -5038984
13 meter
Z = -9904737
23 Z = -3002580
11
XDOT = 9984
567191 XDOT = 3011
819457
YDOT = 16277
051685 feet/sec YDOT = 4995
102139 meter/sec
ZDOT = -16363
462947 ZDOT = -4972
875818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13613076
23 X = -4149265
64
Y = -14608571
86 feet Y = -4452692
70 meter
Z = -9832386
38 Z = -2996911
37
XDOT = 17121
160700 XDOT = 5218
529781
YDOT = -5003
209420 feet/sec YDOT = -1524
978231 meter/sec
ZDOT = -16300
300799 ZDOT = -4968
331683
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 16160
52605253
00016717 00000-0 10270-3 0 9122
2 25544 51
6412 101
2381 0000908 157
7699 202
3493 15
54738844 3632
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
52605253 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 101
2381 deg
Eccentricity:
0000908
Arg of perigee: 157
7699 deg
Mean anomaly: 202
3493 deg
Mean motion: 15
54738844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 363
Checksum: 298
Coasting Arc #14 (Orbit 363)
---------------------------------------
Vector Time (GMT): 2016/160/13:50:18
153
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3731545
55 A = 6777282
89 meter
Y = 2247720
82 meter E =
0012884
Z = -5203197
38 I = 51
98723
XDOT = -2371
124978 Wp = 105
04620
YDOT = 7149
490631 meter/sec RA = 100
06905 deg
ZDOT = 1387
618037 TA = 178
25012
MA = 178
24561
Ha = 220
201 n
mi
Hp = 214
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12242603
50 X = 3731408
44
Y = 7374412
14 feet Y = 2289449
32 meter
Z = -17070857
55 Z = -5185070
58
XDOT = -7779
281423 XDOT = -2457
636574
YDOT = 23456
334092 feet/sec YDOT = 7122
491248 meter/sec
ZDOT = 4552
552614 ZDOT = 1375
890496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4141068
05 X = 1262197
54
Y = -13776474
39 feet Y = -4199069
39 meter
Z = -16992285
94 Z = -5179248
76
XDOT = 23647
768797 XDOT = 7207
839929
YDOT = 1556
127373 feet/sec YDOT = 474
307623 meter/sec
ZDOT = 4500
102659 ZDOT = 1371
631291
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 16160
59033051
00016717 00000-0 10270-3 0 9131
2 25544 51
6426 100
9178 0001462 236
7783 123
3230 15
54367558 3647
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59033051 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 100
9178 deg
Eccentricity:
0001462
Arg of perigee: 236
7783 deg
Mean anomaly: 123
3230 deg
Mean motion: 15
54367558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 292
Coasting Arc #15 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2016/161/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232008
88 A = 6776977
95 meter
Y = 695583
89 meter E =
0003880
Z = 5246259
31 I = 51
98990
XDOT = 145
062017 Wp = 152
26473
YDOT = -7586
603895 meter/sec RA = 97
71525 deg
ZDOT = 1119
224770 TA = 287
04113
MA = 287
08364
Ha = 220
278 n
mi
Hp = 214
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884543
55 X = -4264956
50
Y = 2282099
38 feet Y = 648073
93 meter
Z = 17212136
86 Z = 5225621
41
XDOT = 475
925251 XDOT = 224
449853
YDOT = -24890
432725 feet/sec YDOT = -7584
537959 meter/sec
ZDOT = 3671
997276 ZDOT = 1120
121397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3882387
55 X = -1183351
72
Y = -13638479
11 feet Y = -4157008
43 meter
Z = 17122065
79 Z = 5218805
65
XDOT = 23781
651700 XDOT = 7248
647438
YDOT = -2137
957882 feet/sec YDOT = -651
649563 meter/sec
ZDOT = 3677
334794 ZDOT = 1120
851645
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 16161
10466597
00016717 00000-0 10270-3 0 9145
2 25544 51
6434 98
3498 0001920 227
4374 132
6617 15
54398239 3724
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10466597 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 98
3498 deg
Eccentricity:
0001920
Arg of perigee: 227
4374 deg
Mean anomaly: 132
6617 deg
Mean motion: 15
54398239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 323
Coasting Arc #16 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2016/162/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075718
27 A = 6776885
80 meter
Y = 1228831
20 meter E =
0013200
Z = -5284483
75 I = 51
99284
XDOT = -1078
128246 Wp = 102
31427
YDOT = 7527
137852 meter/sec RA = 92
73745 deg
ZDOT = 918
002472 TA = 176
43995
MA = 176
43055
Ha = 220
115 n
mi
Hp = 214
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13371779
11 X = 4087343
89
Y = 4031598
44 feet Y = 1274474
11 meter
Z = -17337545
12 Z = -5264656
66
XDOT = -3537
166160 XDOT = -1166
677700
YDOT = 24695
334160 feet/sec YDOT = 7514
586306 meter/sec
ZDOT = 3011
819135 ZDOT = 912
550869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2209476
11 X = -673448
32
Y = 13898103
50 feet Y = 4236141
95 meter
Z = -17251367
13 Z = -5258216
70
XDOT = -23935
617146 XDOT = -7295
576106
YDOT = -94
674385 feet/sec YDOT = -28
856753 meter/sec
ZDOT = 2986
630767 ZDOT = 910
325058
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 16162
06904674
00016717 00000-0 10270-3 0 9155
2 25544 51
6434 93
5415 0001780 234
2112 125
8875 15
54384173 3878
Satellite: ISS
Catalog Number: 25544
Epoch time: 16162
06904674 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 93
5415 deg
Eccentricity:
0001780
Arg of perigee: 234
2112 deg
Mean anomaly: 125
8875 deg
Mean motion: 15
54384173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 387
Checksum: 307
Coasting Arc #17 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2016/163/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798577
74 A = 6779229
52 meter
Y = -3057900
87 meter E =
0006317
Z = 4705683
32 I = 52
00144
XDOT = 1964
900383 Wp = 64
70222
YDOT = -6843
156614 meter/sec RA = 87
76244 deg
ZDOT = -2855
159143 TA = 53
51266
MA = 53
45447
Ha = 220
182 n
mi
Hp = 214
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12462525
40 X = -3786959
32
Y = -10032483
16 feet Y = -3100314
52 meter
Z = 15438593
58 Z = 4687258
81
XDOT = 6446
523566 XDOT = 2055
145327
YDOT = -22451
301227 feet/sec YDOT = -6820
678965 meter/sec
ZDOT = -9367
320022 ZDOT = -2845
395549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8041465
21 X = 2451038
60
Y = -13919596
39 feet Y = -4242692
98 meter
Z = 15358877
01 Z = 4681385
71
XDOT = 22157
330851 XDOT = 6753
554443
YDOT = 2492
563529 feet/sec YDOT = 759
733364 meter/sec
ZDOT = -9323
457420 ZDOT = -2841
789822
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 16163
09771581
00016717 00000-0 10270-3 0 9169
2 25544 51
6434 88
4118 0001720 240
3326 119
7655 15
54401192 4038
Satellite: ISS
Catalog Number: 25544
Epoch time: 16163
09771581 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 88
4118 deg
Eccentricity:
0001720
Arg of perigee: 240
3326 deg
Mean anomaly: 119
7655 deg
Mean motion: 15
54401192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 403
Checksum: 291
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