[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 16th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 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
048/10:50:01
363 1
7 3
1 3
1
N/A -2
5 -0
4 222
1
000/00:11:58
727 0
9 0
2 213
5
Coasting Arc #1 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2349548
21 A = 6785261
83 meter
Y = 5892796
76 meter E =
0020136
Z = 2379301
68 I = 51
37211
XDOT = -5501
339430 Wp = 109
20526
YDOT = -19
932918 meter/sec RA = 309
17744 deg
ZDOT = -5352
602195 TA = 44
08239
MA = 43
92204
Ha = 222
323 n
mi
Hp = 211
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7708491
52 X = -2426825
80
Y = 19333322
71 feet Y = 5866090
60 meter
Z = 7806107
88 Z = 2367700
27
XDOT = -18049
013877 XDOT = -5474
707306
YDOT = -65
396713 feet/sec YDOT = -81
303930 meter/sec
ZDOT = -17561
030822 ZDOT = -5379
261351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17623425
56 X = -5371620
11
Y = 11109155
55 feet Y = 3386070
61 meter
Z = 7754680
08 Z = 2363626
49
XDOT = -13677
695765 XDOT = -4168
961669
YDOT = -9288
616985 feet/sec YDOT = -2831
170457 meter/sec
ZDOT = -17676
567874 ZDOT = -5387
817888
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 16046
53691242
00016717 00000-0 10270-3 0 9006
2 25544 51
6424 309
6731 0006390 115
9329 244
2483 15
54713674 25907
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53691242 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 309
6731 deg
Eccentricity:
0006390
Arg of perigee: 115
9329 deg
Mean anomaly: 244
2483 deg
Mean motion: 15
54713674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 307
Coasting Arc #2 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3412466
47 A = 6787357
46 meter
Y = -5836281
95 meter E =
0013649
Z = -570404
76 I = 51
36073
XDOT = 4395
585054 Wp = 67
37983
YDOT = 1999
829946 meter/sec RA = 304
18213 deg
ZDOT = 5954
160921 TA = 286
44124
MA = 286
59122
Ha = 222
163 n
mi
Hp = 211
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11195756
12 X = 3480246
34
Y = -19147906
67 feet Y = -5797742
54 meter
Z = -1871406
70 Z = -553663
19
XDOT = 14421
210806 XDOT = 4343
973405
YDOT = 6561
121869 feet/sec YDOT = 2048
695983 meter/sec
ZDOT = 19534
648691 ZDOT = 5975
387843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20151221
11 X = 6142092
20
Y = -9283638
25 feet Y = -2829652
94 meter
Z = -1797719
81 Z = -547945
00
XDOT = 7286
918805 XDOT = 2221
052852
YDOT = 12095
522922 feet/sec YDOT = 3686
715387 meter/sec
ZDOT = 19626
259491 ZDOT = 5982
083893
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 16047
50105928
00016717 00000-0 10270-3 0 9016
2 25544 51
6430 304
8618 0006216 119
1602 241
0174 15
54761266 26051
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
50105928 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 304
8618 deg
Eccentricity:
0006216
Arg of perigee: 119
1602 deg
Mean anomaly: 241
0174 deg
Mean motion: 15
54761266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 281
Coasting Arc #3 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1037977
98 A = 6781374
51 meter
Y = -5158791
91 meter E =
0012061
Z = -4290251
37 I = 51
31844
XDOT = 5489
414084 Wp = 117
35393
YDOT = -4022
376464 meter/sec RA = 299
37271 deg
ZDOT = 3510
773900 TA = 188
60180
MA = 188
62249
Ha = 222
113 n
mi
Hp = 213
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3405439
58 X = -959374
10
Y = -16925170
31 feet Y = -5169959
95 meter
Z = -14075627
84 Z = -4295102
39
XDOT = 18009
888728 XDOT = 5516
931765
YDOT = -13196
773175 feet/sec YDOT = -3960
836186 meter/sec
ZDOT = 11518
287073 ZDOT = 3537
506663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10830645
95 X = 3301180
89
Y = -13423528
31 feet Y = -4091491
43 meter
Z = -14095662
59 Z = -4296357
96
XDOT = 20660
324248 XDOT = 6297
266831
YDOT = 4459
619130 feet/sec YDOT = 1359
291911 meter/sec
ZDOT = 11634
920242 ZDOT = 3546
323690
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 16048
46519360
00016717 00000-0 10270-3 0 9022
2 25544 51
6429 300
0492 0003871 133
5657 226
5818 15
54178661 26202
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46519360 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 300
0492 deg
Eccentricity:
0003871
Arg of perigee: 133
5657 deg
Mean anomaly: 226
5818 deg
Mean motion: 15
54178661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 308
Coasting Arc #4 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -69894
84 A = 6785256
99 meter
Y = 6055885
76 meter E =
0016246
Z = 3040722
82 I = 51
31621
XDOT = -5395
234728 Wp = 105
18683
YDOT = 2406
159625 meter/sec RA = 294
36492 deg
ZDOT = -4898
372924 TA = 39
72711
MA = 39
60824
Ha = 222
065 n
mi
Hp = 213
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -229313
79 X = -152378
29
Y = 19868391
60 feet Y = 6054643
10 meter
Z = 9976124
73 Z = 3040182
67
XDOT = -17700
901338 XDOT = -5397
946310
YDOT = 7894
224493 feet/sec YDOT = 2345
811140 meter/sec
ZDOT = -16070
777310 ZDOT = -4924
587795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15186519
61 X = -4628851
18
Y = 12815804
35 feet Y = 3906257
17 meter
Z = 9972633
32 Z = 3039658
64
XDOT = -16568
022989 XDOT = -5049
933407
YDOT = -6993
277249 feet/sec YDOT = -2131
550906 meter/sec
ZDOT = -16184
853313 ZDOT = -4933
143290
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 16049
49398858
00016717 00000-0 10270-3 0 9034
2 25544 51
6426 294
9201 0003925 137
4808 222
6649 15
54181034 26363
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49398858 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 294
9201 deg
Eccentricity:
0003925
Arg of perigee: 137
4808 deg
Mean anomaly: 222
6649 deg
Mean motion: 15
54181034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 331
Coasting Arc #5 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2016/050/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1029873
37 A = 6788083
25 meter
Y = -6539870
63 meter E =
0008253
Z = -1494828
68 I = 51
31438
XDOT = 5051
819133 Wp = 63
80418
YDOT = -510
162034 meter/sec RA = 289
36548 deg
ZDOT = 5740
739837 TA = 279
80710
MA = 279
90028
Ha = 221
909 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3378849
64 X = 1110188
35
Y = -21456268
46 feet Y = -6527904
92 meter
Z = -4904293
58 Z = -1489630
48
XDOT = 16574
209753 XDOT = 5029
263028
YDOT = -1673
759955 feet/sec YDOT = -453
795025 meter/sec
ZDOT = 18834
448285 ZDOT = 5765
224992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18228944
81 X = 5556182
38
Y = -11820580
31 feet Y = -3602912
88 meter
Z = -4880535
72 Z = -1487587
29
XDOT = 11388
247132 XDOT = 3471
137726
YDOT = 9780
431677 feet/sec YDOT = 2981
075575 meter/sec
ZDOT = 18940
668386 ZDOT = 5773
115724
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 16050
45846876
00016717 00000-0 10270-3 0 9041
2 25544 51
6431 290
1111 0003777 141
8907 218
2514 15
54232148 26513
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
45846876 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 290
1111 deg
Eccentricity:
0003777
Arg of perigee: 141
8907 deg
Mean anomaly: 218
2514 deg
Mean motion: 15
54232148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 298
Coasting Arc #6 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2016/051/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1883141
87 A = 6789075
95 meter
Y = 6509617
28 meter E =
0015336
Z = -260280
26 I = 51
30750
XDOT = -4548
330320 Wp = 139
24225
YDOT = -1546
446119 meter/sec RA = 284
37154 deg
ZDOT = -5980
300756 TA = 43
57634
MA = 43
45530
Ha = 221
868 n
mi
Hp = 213
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6178286
97 X = -1954529
76
Y = 21357012
09 feet Y = 6488159
57 meter
Z = -853937
88 Z = -269601
74
XDOT = -14922
343570 XDOT = -4501
650520
YDOT = -5073
642124 feet/sec YDOT = -1597
048008 meter/sec
ZDOT = -19620
409303 ZDOT = -6002
281373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19833087
15 X = -6045124
96
Y = 10043358
83 feet Y = 3061215
77 meter
Z = -895546
00 Z = -272962
42
XDOT = -5641
051033 XDOT = -1719
392355
YDOT = -12838
753020 feet/sec YDOT = -3913
251921 meter/sec
ZDOT = -19715
393732 ZDOT = -6009
252010
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 16051
48723491
00016717 00000-0 10270-3 0 9053
2 25544 51
6429 284
9816 0003834 147
3886 212
7504 15
54205371 26677
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
48723491 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 284
9816 deg
Eccentricity:
0003834
Arg of perigee: 147
3886 deg
Mean anomaly: 212
7504 deg
Mean motion: 15
54205371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 324
Coasting Arc #7 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2016/052/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2568942
15 A = 6787326
02 meter
Y = -5966196
83 meter E =
0014918
Z = 1950263
18 I = 51
29465
XDOT = 3934
545869 Wp = 81
40570
YDOT = 3523
125305 meter/sec RA = 279
37508 deg
ZDOT = 5560
807311 TA = 300
21651
MA = 300
36415
Ha = 221
700 n
mi
Hp = 213
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8428287
90 X = 2625993
41
Y = -19574136
58 feet Y = -5937150
04 meter
Z = 6398501
26 Z = 1962881
27
XDOT = 12908
615055 XDOT = 3867
845641
YDOT = 11558
810056 feet/sec YDOT = 3566
751580 meter/sec
ZDOT = 18244
118475 ZDOT = 5579
757551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19910947
17 X = 6068856
70
Y = -7551165
23 feet Y = -2301595
16 meter
Z = 6454282
65 Z = 1967265
35
XDOT = 7
985611 XDOT = 2
434014
YDOT = 15780
196526 feet/sec YDOT = 4809
803901 meter/sec
ZDOT = 18325
612471 ZDOT = 5585
646681
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 16052
51598493
00016717 00000-0 10270-3 0 9061
2 25544 51
6424 279
8517 0003558 149
2057 210
9305 15
54254447 26832
Satellite: ISS
Catalog Number: 25544
Epoch time: 16052
51598493 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 279
8517 deg
Eccentricity:
0003558
Arg of perigee: 149
2057 deg
Mean anomaly: 210
9305 deg
Mean motion: 15
54254447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 327
Coasting Arc #8 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2016/053/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3166415
43 A = 6783753
82 meter
Y = 4894205
65 meter E =
0007083
Z = -3472539
00 I = 51
27816
XDOT = -3227
207850 Wp = 114
33528
YDOT = -5284
685139 meter/sec RA = 274
37094 deg
ZDOT = -4515
700817 TA = 106
65838
MA = 106
58061
Ha = 221
536 n
mi
Hp = 213
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10388502
08 X = -3204040
61
Y = 16057105
16 feet Y = 4858585
93 meter
Z = -11392844
49 Z = -3488012
22
XDOT = -10587
952264 XDOT = -3145
938520
YDOT = -17338
205837 feet/sec YDOT = -5320
320017 meter/sec
ZDOT = -14815
291393 ZDOT = -4531
179442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18650827
59 X = -5684772
25
Y = 4042938
68 feet Y = 1232287
71 meter
Z = -11460793
35 Z = -3493249
81
XDOT = 5153
814501 XDOT = 1570
882660
YDOT = -18315
938511 feet/sec YDOT = -5582
698058 meter/sec
ZDOT = -14881
430762 ZDOT = -4535
860096
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 16053
48042434
00016717 00000-0 10270-3 0 9078
2 25544 51
6420 275
0425 0003523 156
6131 203
5182 15
54266186 26981
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
48042434 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 275
0425 deg
Eccentricity:
0003523
Arg of perigee: 156
6131 deg
Mean anomaly: 203
5182 deg
Mean motion: 15
54266186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2698
Checksum: 293
Coasting Arc #9 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2016/054/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3634496
76 A = 6779873
13 meter
Y = -3428215
36 meter E =
0011260
Z = 4578503
93 I = 51
26358
XDOT = 2469
507984 Wp = 126
27795
YDOT = 6620
758872 meter/sec RA = 269
35507 deg
ZDOT = 2985
343809 TA = 293
73482
MA = 293
85289
Ha = 221
444 n
mi
Hp = 213
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11924201
96 X = 3650321
85
Y = -11247425
72 feet Y = -3387482
94 meter
Z = 15021338
36 Z = 4596197
91
XDOT = 8102
060316 XDOT = 2380
788267
YDOT = 21721
649844 feet/sec YDOT = 6647
878866 meter/sec
ZDOT = 9794
435068 ZDOT = 2997
123487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16319982
63 X = 4974330
71
Y = 144874
72 feet Y = 44157
82 meter
Z = 15098641
06 Z = 4602065
80
XDOT = -9320
550236 XDOT = -2840
903712
YDOT = 20009
553424 feet/sec YDOT = 6098
911883 meter/sec
ZDOT = 9844
317941 ZDOT = 3000
548108
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 16054
50914675
00016717 00000-0 10270-3 0 9088
2 25544 51
6417 269
9121 0003464 156
6901 203
4409 15
54288275 27144
Satellite: ISS
Catalog Number: 25544
Epoch time: 16054
50914675 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 269
9121 deg
Eccentricity:
0003464
Arg of perigee: 156
6901 deg
Mean anomaly: 203
4409 deg
Mean motion: 15
54288275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 316
Coasting Arc #10 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/055/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4032934
45 A = 6777131
02 meter
Y = 1647846
20 meter E =
0015109
Z = -5204215
23 I = 51
25526
XDOT = -1617
986605 Wp = 94
19468
YDOT = -7404
590390 meter/sec RA = 264
32860 deg
ZDOT = -1094
572574 TA = 165
26759
MA = 165
22351
Ha = 221
292 n
mi
Hp = 213
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13231412
23 X = -4025781
94
Y = 5406319
57 feet Y = 1602786
54 meter
Z = -17074196
96 Z = -5223788
72
XDOT = -5308
355003 XDOT = -1529
749520
YDOT = -24293
275558 feet/sec YDOT = -7422
190576 meter/sec
ZDOT = -3591
117370 ZDOT = -1102
216889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13275522
04 X = -4046379
12
Y = -5014455
89 feet Y = -1528406
16 meter
Z = -17159327
19 Z = -5230162
93
XDOT = 12366
874682 XDOT = 3769
423403
YDOT = -20385
967525 feet/sec YDOT = -6213
642902 meter/sec
ZDOT = -3622
953828 ZDOT = -1104
276327
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 16055
47355820
00016717 00000-0 10270-3 0 9097
2 25544 51
6407 265
1016 0003341 163
0404 197
0861 15
54344285 27298
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
47355820 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 265
1016 deg
Eccentricity:
0003341
Arg of perigee: 163
0404 deg
Mean anomaly: 197
0861 deg
Mean motion: 15
54344285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 299
Coasting Arc #11 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2016/056/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4308719
59 A = 6776946
86 meter
Y = 236894
79 meter E =
0003967
Z = 5222110
07 I = 51
25921
XDOT = 688
183356 Wp = 112
51727
YDOT = 7586
533969 meter/sec RA = 259
29928 deg
ZDOT = -912
906422 TA = 346
25223
MA = 346
26303
Ha = 221
073 n
mi
Hp = 213
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14136219
12 X = 4280383
93
Y = 777213
86 feet Y = 284920
04 meter
Z = 17132907
04 Z = 5242971
59
XDOT = 2257
819410 XDOT = 607
732151
YDOT = 24890
203309 feet/sec YDOT = 7593
779736 meter/sec
ZDOT = -2995
099809 ZDOT = -909
759901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9885802
52 X = 3013192
61
Y = 9980099
69 feet Y = 3041934
39 meter
Z = 17223291
63 Z = 5249659
29
XDOT = -14267
520896 XDOT = -4348
740369
YDOT = 19274
995104 feet/sec YDOT = 5875
018508 meter/sec
ZDOT = -2982
775033 ZDOT = -909
149830
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 16056
50225061
00016717 00000-0 10270-3 0 9107
2 25544 51
6409 259
9715 0003354 167
6618 192
4618 15
54358621 27454
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
50225061 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 259
9715 deg
Eccentricity:
0003354
Arg of perigee: 167
6618 deg
Mean anomaly: 192
4618 deg
Mean motion: 15
54358621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 315
Coasting Arc #12 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/057/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4471619
19 A = 6779272
17 meter
Y = -2077151
87 meter E =
0012578
Z = -4665178
60 I = 51
27296
XDOT = 352
530975 Wp = 122
93260
YDOT = -7109
010074 meter/sec RA = 254
27174 deg
ZDOT = 2826
205006 TA = 175
30532
MA = 175
29352
Ha = 221
098 n
mi
Hp = 213
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14670666
64 X = -4425398
44
Y = -6814802
73 feet Y = -2126898
68 meter
Z = -15305704
05 Z = -4686787
82
XDOT = 1156
597688 XDOT = 418
271148
YDOT = -23323
523866 feet/sec YDOT = -7104
699881 meter/sec
ZDOT = 9272
326136 ZDOT = 2828
078129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6498018
17 X = -1980595
94
Y = -14716678
18 feet Y = -4485643
51 meter
Z = -15399016
71 Z = -4693620
29
XDOT = 15087
725178 XDOT = 4598
738634
YDOT = -16377
777643 feet/sec YDOT = -4991
946626 meter/sec
ZDOT = 9281
663746 ZDOT = 2829
051110
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 16057
46663586
00016717 00000-0 10270-3 0 9112
2 25544 51
6398 255
1602 0003291 171
9916 188
1290 15
54381890 27602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
46663586 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 255
1602 deg
Eccentricity:
0003291
Arg of perigee: 171
9916 deg
Mean anomaly: 188
1290 deg
Mean motion: 15
54381890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 328
Coasting Arc #13 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2016/058/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438650
84 A = 6783000
79 meter
Y = 3690423
47 meter E =
0012387
Z = 3549109
87 I = 51
29613
XDOT = -1498
590097 Wp = 101
72082
YDOT = 6079
133529 meter/sec RA = 249
25584 deg
ZDOT = -4436
302992 TA = 36
12303
MA = 36
03941
Ha = 220
763 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14562502
76 X = 4379813
82
Y = 12107688
55 feet Y = 3739730
89 meter
Z = 11644061
26 Z = 3570528
17
XDOT = -4916
634177 XDOT = -1544
907624
YDOT = 19944
663808 feet/sec YDOT = 6062
115755 meter/sec
ZDOT = -14554
799844 ZDOT = -4443
695983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3274814
06 X = 998163
33
Y = 18595217
70 feet Y = 5667822
36 meter
Z = 11736278
92 Z = 3577217
82
XDOT = -15184
061703 XDOT = -4628
102007
YDOT = 11903
097692 feet/sec YDOT = 3628
064176 meter/sec
ZDOT = -14587
878955 ZDOT = -4446
385506
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 16058
49529734
00016717 00000-0 10270-3 0 9123
2 25544 51
6404 250
0299 0003121 178
1484 181
9681 15
54436249 27768
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
49529734 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 250
0299 deg
Eccentricity:
0003121
Arg of perigee: 178
1484 deg
Mean anomaly: 181
9681 deg
Mean motion: 15
54436249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 325
Coasting Arc #14 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2016/059/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192936
85 A = 6786676
37 meter
Y = -4930557
57 meter E =
0004554
Z = -2041679
77 I = 51
31907
XDOT = 2699
974351 Wp = 68
17542
YDOT = -4577
645598 meter/sec RA = 244
25060 deg
ZDOT = 5521
535758 TA = 269
15788
MA = 269
21006
Ha = 220
870 n
mi
Hp = 214
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13756354
50 X = -4127572
97
Y = -16176369
99 feet Y = -4977080
55 meter
Z = -6698424
43 Z = -2061888
52
XDOT = 8858
183567 XDOT = 2724
140985
YDOT = -15018
522303 feet/sec YDOT = -4547
316915 meter/sec
ZDOT = 18115
274796 ZDOT = 5534
710707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -425784
18 X = -129779
02
Y = -21202851
15 feet Y = -6462629
03 meter
Z = -6785199
76 Z = -2068128
89
XDOT = 14712
535192 XDOT = 4484
380726
YDOT = -6099
082509 feet/sec YDOT = -1859
000349 meter/sec
ZDOT = 18173
158822 ZDOT = 5539
178809
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 16059
45965555
00016717 00000-0 10270-3 0 9136
2 25544 51
6390 245
2189 0003237 180
9307 179
1841 15
54415497 27915
Satellite: ISS
Catalog Number: 25544
Epoch time: 16059
45965555 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 245
2189 deg
Eccentricity:
0003237
Arg of perigee: 180
9307 deg
Mean anomaly: 179
1841 deg
Mean motion: 15
54415497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 335
Coasting Arc #15 (Orbit 2806)
---------------------------------------
Vector Time (GMT): 2016/060/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639785
41 A = 6788320
82 meter
Y = 5714565
13 meter E =
0014694
Z = 258689
43 I = 51
33998
XDOT = -3919
035611 Wp = 141
57840
YDOT = 2774
795420 meter/sec RA = 239
25606 deg
ZDOT = -5983
376221 TA = 35
62098
MA = 35
52300
Ha = 220
690 n
mi
Hp = 214
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11941553
17 X = 3574356
61
Y = 18748573
27 feet Y = 5754901
82 meter
Z = 848718
59 Z = 276210
95
XDOT = -12857
728382 XDOT = -3920
708303
YDOT = 9103
659514 feet/sec YDOT = 2730
960166 meter/sec
ZDOT = -19630
499412 ZDOT = -6002
418156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2195739
48 X = -669261
39
Y = 22116859
52 feet Y = 6741218
78 meter
Z = 923725
20 Z = 281551
44
XDOT = -14021
519596 XDOT = -4273
759173
YDOT = -547
054300 feet/sec YDOT = -166
742151 meter/sec
ZDOT = -19713
515029 ZDOT = -6008
679381
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 16060
48828719
00016717 00000-0 10270-3 0 9142
2 25544 51
6393 240
0885 0003071 184
3779 175
7348 15
54465039 28070
Satellite: ISS
Catalog Number: 25544
Epoch time: 16060
48828719 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 240
0885 deg
Eccentricity:
0003071
Arg of perigee: 184
3779 deg
Mean anomaly: 175
7348 deg
Mean motion: 15
54465039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2807
Checksum: 336
Coasting Arc #16 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2016/061/10:56:00
727
Vector Time (MET): N/A
Weight (LBS) : 922145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2800127
74 A = 6787372
61 meter
Y = -5985586
82 meter E =
0012281
Z = 1529699
29 I = 51
35281
XDOT = 5018
301241 Wp = 74
51988
YDOT = -873
677075 meter/sec RA = 234
26199 deg
ZDOT = 5732
129880 TA = 302
26377
MA = 302
38271
Ha = 220
669 n
mi
Hp = 214
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9186770
81 X = -2740417
89
Y = -19637752
04 feet Y = -6016565
70 meter
Z = 5018698
46 Z = 1516242
67
XDOT = 16464
242916 XDOT = 4999
853915
YDOT = -2866
394602 feet/sec YDOT = -817
661692 meter/sec
ZDOT = 18806
200395 ZDOT = 5756
462640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4517003
44 X = 1376782
65
Y = -21218084
50 feet Y = -6467272
15 meter
Z = 4961347
35 Z = 1512218
67
XDOT = 13207
016644 XDOT = 4025
498673
YDOT = 7261
041557 feet/sec YDOT = 2213
165467 meter/sec
ZDOT = 18911
843094 ZDOT = 5764
329775
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 16061
51690334
00016717 00000-0 10270-3 0 9158
2 25544 51
6381 234
9565 0003230 188
0786 172
0315 15
54468864 28220
Satellite: ISS
Catalog Number: 25544
Epoch time: 16061
51690334 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 234
9565 deg
Eccentricity:
0003230
Arg of perigee: 188
0786 deg
Mean anomaly: 172
0315 deg
Mean motion: 15
54468864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 312
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