[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 12th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 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
104/12:22:07
990 1
5 1
5 1
5
N/A 0
3 -0
1 221
2
000/00:04:11
979 -0
1 0
0 214
3
Coasting Arc #1 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2016/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5694930
89 A = 6782789
91 meter
Y = 44261
19 meter E =
0013978
Z = 3674778
07 I = 51
83247
XDOT = -2869
766054 Wp = 78
28998
YDOT = -5619
873706 meter/sec RA = 30
03032 deg
ZDOT = -4362
906582 TA = 58
11032
MA = 57
97440
Ha = 221
362 n
mi
Hp = 213
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18684156
47 X = -5712853
26
Y = 145213
87 feet Y = -19523
34 meter
Z = 12056358
49 Z = 3647069
69
XDOT = -9415
242958 XDOT = -2785
516586
YDOT = -18437
905859 feet/sec YDOT = -5651
494496 meter/sec
ZDOT = -14313
997971 ZDOT = -4376
642414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17660248
89 X = -5382843
86
Y = 6334318
30 feet Y = 1930700
22 meter
Z = 11935936
95 Z = 3638073
58
XDOT = -14427
808704 XDOT = -4397
596093
YDOT = -13037
657093 feet/sec YDOT = -3973
877882 meter/sec
ZDOT = -14372
586023 ZDOT = -4380
764220
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 16102
53990315
00016717 00000-0 10270-3 0 9002
2 25544 51
6430 30
4559 0002631 44
4619 315
6744 15
54446052 34617
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
53990315 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 30
4559 deg
Eccentricity:
0002631
Arg of perigee: 44
4619 deg
Mean anomaly: 315
6744 deg
Mean motion: 15
54446052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 283
Coasting Arc #2 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2016/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6335258
41 A = 6786431
30 meter
Y = 1072929
77 meter E =
0008944
Z = -2176334
73 I = 51
81648
XDOT = 995
785583 Wp = 42
69005
YDOT = 5243
712494 meter/sec RA = 25
06107 deg
ZDOT = 5503
485339 TA = 293
22268
MA = 293
31684
Ha = 221
315 n
mi
Hp = 213
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20784968
53 X = 6333361
56
Y = 3520110
79 feet Y = 1143764
13 meter
Z = -7140205
80 Z = -2145564
06
XDOT = 3267
013067 XDOT = 910
341313
YDOT = 17203
781148 feet/sec YDOT = 5254
370539 meter/sec
ZDOT = 18056
054262 ZDOT = 5508
114873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20759703
58 X = 6327557
65
Y = -3915290
71 feet Y = -1193380
61 meter
Z = -7006699
76 Z = -2135642
09
XDOT = 8631
057131 XDOT = 2630
746213
YDOT = 13534
397119 feet/sec YDOT = 4125
284242 meter/sec
ZDOT = 18075
136167 ZDOT = 5509
301504
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 16103
50423071
00016717 00000-0 10270-3 0 9011
2 25544 51
6429 25
6460 0002619 46
4303 313
7067 15
54458248 34763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
50423071 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 25
6460 deg
Eccentricity:
0002619
Arg of perigee: 46
4303 deg
Mean anomaly: 313
7067 deg
Mean motion: 15
54458248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 288
Coasting Arc #3 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6455907
90 A = 6788292
57 meter
Y = -2047379
99 meter E =
0013427
Z = 375774
82 I = 51
79410
XDOT = 1109
947495 Wp = 119
90744
YDOT = -4631
376789 meter/sec RA = 20
09844 deg
ZDOT = -6010
447300 TA = 56
04989
MA = 55
92233
Ha = 221
271 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21180800
21 X = -6434359
13
Y = -6717125
95 feet Y = -2119453
74 meter
Z = 1232857
02 Z = 344465
94
XDOT = 3641
560024 XDOT = 1190
850503
YDOT = -15194
805737 feet/sec YDOT = -4618
512566 meter/sec
ZDOT = -19719
315290 ZDOT = -6004
858692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22182006
99 X = -6761075
73
Y = 1421517
41 feet Y = 433278
51 meter
Z = 1097209
67 Z = 334429
51
XDOT = -1893
741677 XDOT = -577
212463
YDOT = -13911
366470 feet/sec YDOT = -4240
184500 meter/sec
ZDOT = -19694
111045 ZDOT = -6002
765046
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 16104
53283450
00016717 00000-0 10270-3 0 9021
2 25544 51
6436 20
5151 0002591 52
0358 308
1023 15
54468853 34925
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53283450 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 20
5151 deg
Eccentricity:
0002591
Arg of perigee: 52
0358 deg
Mean anomaly: 308
1023 deg
Mean motion: 15
54468853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 280
Coasting Arc #4 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1443920
16 A = 6777124
53 meter
Y = -3946013
71 meter E =
0015777
Z = -5330838
29 I = 51
75399
XDOT = 7192
845588 Wp = 84
45376
YDOT = 2625
665388 meter/sec RA = 20
01752 deg
ZDOT = 6
189006 TA = 185
59638
MA = 185
61403
Ha = 221
246 n
mi
Hp = 214
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4737270
87 X = 1513833
18
Y = -12946239
20 feet Y = -3929476
20 meter
Z = -17489626
95 Z = -5323654
05
XDOT = 23598
574765 XDOT = 7162
920092
YDOT = 8614
387755 feet/sec YDOT = 2705
933247 meter/sec
ZDOT = 20
305138 ZDOT = 41
057380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1636451
81 X = -498790
51
Y = -13729066
02 feet Y = -4184619
32 meter
Z = -17457624
91 Z = -5321084
07
XDOT = 23917
684266 XDOT = 7290
110164
YDOT = -3062
445230 feet/sec YDOT = -933
433306 meter/sec
ZDOT = 171
305554 ZDOT = 52
213933
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 16104
53283479
00016717 00000-0 10270-3 0 9033
2 25544 51
6438 20
5148 0001725 29
1025 331
0223 15
54208672 34925
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53283479 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 20
5148 deg
Eccentricity:
0001725
Arg of perigee: 29
1025 deg
Mean anomaly: 331
0223 deg
Mean motion: 15
54208672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 282
Coasting Arc #5 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3157079
74 A = 6778321
11 meter
Y = 3261858
02 meter E =
0007454
Z = 5030304
67 I = 51
72764
XDOT = -6608
063348 Wp = 49
48539
YDOT = -3370
646820 meter/sec RA = 15
02422 deg
ZDOT = -1954
999451 TA = 59
49339
MA = 59
41982
Ha = 221
273 n
mi
Hp = 214
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10357873
16 X = -3217755
11
Y = 10701633
93 feet Y = 3226214
51 meter
Z = 16503624
26 Z = 5014820
77
XDOT = -21679
997860 XDOT = -6560
384243
YDOT = -11058
552559 feet/sec YDOT = -3444
276108 meter/sec
ZDOT = -6414
040193 ZDOT = -1986
983823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4134749
04 X = -1260271
51
Y = 14385825
39 feet Y = 4384799
58 meter
Z = 16435692
78 Z = 5009599
16
XDOT = -23245
854906 XDOT = -7085
336575
YDOT = 829
697208 feet/sec YDOT = 252
891709 meter/sec
ZDOT = -6552
354051 ZDOT = -1997
157515
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 16105
56161377
00016717 00000-0 10270-3 0 9040
2 25544 51
6436 15
3855 0001721 27
7543 332
3701 15
54248190 35087
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56161377 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 15
3855 deg
Eccentricity:
0001721
Arg of perigee: 27
7543 deg
Mean anomaly: 332
3701 deg
Mean motion: 15
54248190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 291
Coasting Arc #6 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4672506
01 A = 6781608
02 meter
Y = -2548975
99 meter E =
0008335
Z = -4210326
15 I = 51
70803
XDOT = 5454
185458 Wp = 97
51111
YDOT = 3919
768590 meter/sec RA = 10
03491 deg
ZDOT = 3685
028855 TA = 210
26093
MA = 210
30909
Ha = 221
249 n
mi
Hp = 214
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15329744
11 X = 4721114
00
Y = -8362782
13 feet Y = -2496453
45 meter
Z = -13813405
99 Z = -4187510
00
XDOT = 17894
309246 XDOT = 5392
047954
YDOT = 12860
133169 feet/sec YDOT = 3980
413760 meter/sec
ZDOT = 12089
989682 ZDOT = 3711
372743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9352019
80 X = 2850495
64
Y = -14839807
62 feet Y = -4523173
36 meter
Z = -13713759
51 Z = -4179953
90
XDOT = 20748
962258 XDOT = 6324
283696
YDOT = 1814
150243 feet/sec YDOT = 552
952994 meter/sec
ZDOT = 12203
678437 ZDOT = 3719
681188
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 16106
52608413
00016717 00000-0 10270-3 0 9055
2 25544 51
6443 10
5764 0001724 31
6829 328
4427 15
54238703 35232
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52608413 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 10
5764 deg
Eccentricity:
0001724
Arg of perigee: 31
6829 deg
Mean anomaly: 328
4427 deg
Mean motion: 15
54238703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 291
Coasting Arc #7 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5862306
52 A = 6785528
21 meter
Y = 1783110
51 meter E =
0014245
Z = 2901863
78 I = 51
68928
XDOT = -3824
464688 Wp = 92
54751
YDOT = -4336
336827 meter/sec RA = 5
05420 deg
ZDOT = -5040
841132 TA = 54
39556
MA = 54
26293
Ha = 221
328 n
mi
Hp = 214
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19233289
12 X = -5895906
05
Y = 5850100
09 feet Y = 1717366
68 meter
Z = 9520550
47 Z = 2873304
35
XDOT = -12547
456327 XDOT = -3751
204159
YDOT = -14226
826860 feet/sec YDOT = -4378
695346 meter/sec
ZDOT = -16538
192691 ZDOT = -5059
241147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13709635
10 X = -4178696
78
Y = 14783200
36 feet Y = 4505919
47 meter
Z = 9396108
52 Z = 2863933
88
XDOT = -16840
647789 XDOT = -5133
029446
YDOT = -5012
013900 feet/sec YDOT = -1527
661837 meter/sec
ZDOT = -16617
276618 ZDOT = -5064
945913
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 16107
55484069
00016717 00000-0 10270-3 0 9069
2 25544 51
6442 5
4470 0001722 38
2105 321
9169 15
54240115 35394
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55484069 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 5
4470 deg
Eccentricity:
0001722
Arg of perigee: 38
2105 deg
Mean anomaly: 321
9169 deg
Mean motion: 15
54240115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 287
Coasting Arc #8 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2016/108/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6577391
57 A = 6788189
14 meter
Y = -1023904
96 meter E =
0010675
Z = -1306660
45 I = 51
66733
XDOT = 1870
258296 Wp = 36
98514
YDOT = 4613
892918 meter/sec RA =
08053 deg
ZDOT = 5832
027707 TA = 308
80020
MA = 308
89548
Ha = 221
207 n
mi
Hp = 214
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21579368
68 X = 6594699
51
Y = -3359268
23 feet Y = -950255
54 meter
Z = -4286943
72 Z = -1274666
86
XDOT = 6136
018030 XDOT = 1790
195994
YDOT = 15137
443956 feet/sec YDOT = 4634
360293 meter/sec
ZDOT = 19133
949169 ZDOT = 5840
918087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16722989
39 X = 5097167
17
Y = -14087923
40 feet Y = -4293999
05 meter
Z = -4147741
84 Z = -1264231
71
XDOT = 11970
937750 XDOT = 3648
741826
YDOT = 8598
590301 feet/sec YDOT = 2620
850324 meter/sec
ZDOT = 19171
657488 ZDOT = 5843
521202
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 16108
51928701
00016717 00000-0 10270-3 0 9073
2 25544 51
6448
6378 0001684 35
5800 324
5465 15
54286296 35548
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
51928701 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node:
6378 deg
Eccentricity:
0001684
Arg of perigee: 35
5800 deg
Mean anomaly: 324
5465 deg
Mean motion: 15
54286296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 315
Coasting Arc #9 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2016/109/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6764963
79 A = 6788850
32 meter
Y = 201349
61 meter E =
0010877
Z = -475002
91 I = 51
63720
XDOT = 271
343089 Wp = 130
13950
YDOT = -4780
514832 meter/sec RA = 355
11058 deg
ZDOT = -5988
362936 TA = 54
98325
MA = 54
88122
Ha = 221
182 n
mi
Hp = 214
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22194763
08 X = -6764405
17
Y = 660595
84 feet Y = 125702
36 meter
Z = -1558408
49 Z = -507864
30
XDOT = 890
233232 XDOT = 353
868929
YDOT = -15684
103781 feet/sec YDOT = -4777
019663 meter/sec
ZDOT = -19646
860027 ZDOT = -5986
843886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18407475
08 X = -5610598
40
Y = 12399326
27 feet Y = 3779314
65 meter
Z = -1701205
87 Z = -518527
55
XDOT = -6608
463993 XDOT = -2014
259825
YDOT = -12464
966354 feet/sec YDOT = -3799
321745 meter/sec
ZDOT = -19639
311916 ZDOT = -5986
062272
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 16109
54801989
00016717 00000-0 10270-3 0 9086
2 25544 51
6448 355
5084 0001527 40
4954 319
6312 15
54253245 35707
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
54801989 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 355
5084 deg
Eccentricity:
0001527
Arg of perigee: 40
4954 deg
Mean anomaly: 319
6312 deg
Mean motion: 15
54253245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 317
Coasting Arc #10 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2016/110/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6391054
29 A = 6786753
10 meter
Y = 634407
00 meter E =
0015331
Z = 2169920
93 I = 51
59848
XDOT = -2349
651699 Wp = 67
05725
YDOT = 4821
940891 meter/sec RA = 350
13534 deg
ZDOT = 5485
641815 TA = 317
04990
MA = 317
16950
Ha = 221
104 n
mi
Hp = 213
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20968025
90 X = 6372944
54
Y = 2081387
81 feet Y = 705774
98 meter
Z = 7119163
15 Z = 2200923
34
XDOT = -7708
831032 XDOT = -2430
044381
YDOT = 15820
016048 feet/sec YDOT = 4795
216561 meter/sec
ZDOT = 17997
512517 ZDOT = 5474
031935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18639079
78 X = 5681191
52
Y = -9728370
74 feet Y = -2965207
40 meter
Z = 7253707
79 Z = 2210930
13
XDOT = 1420
396292 XDOT = 432
936790
YDOT = 16162
518410 feet/sec YDOT = 4926
335611 meter/sec
ZDOT = 17946
123962 ZDOT = 5469
978583
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 16110
57673933
00016717 00000-0 10270-3 0 9098
2 25544 51
6444 350
3783 0001730 36
5869 323
5402 15
54302883 35863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
57673933 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 350
3783 deg
Eccentricity:
0001730
Arg of perigee: 36
5869 deg
Mean anomaly: 323
5402 deg
Mean motion: 15
54302883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 315
Coasting Arc #11 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2016/111/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5501516
24 A = 6783014
95 meter
Y = -1548157
33 meter E =
0006893
Z = -3660954
23 I = 51
55407
XDOT = 4212
950395 Wp = 70
04468
YDOT = -4691
127389 meter/sec RA = 345
15013 deg
ZDOT = -4351
604255 TA = 153
48307
MA = 153
44779
Ha = 221
083 n
mi
Hp = 213
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18049593
97 X = -5466011
89
Y = -5079256
34 feet Y = -1609480
77 meter
Z = -12011004
69 Z = -3687593
21
XDOT = 13822
015732 XDOT = 4286
233150
YDOT = -15390
837889 feet/sec YDOT = -4643
606023 meter/sec
ZDOT = -14276
916848 ZDOT = -4330
960088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17716715
05 X = -5400054
75
Y = 5909250
49 feet Y = 1801139
55 meter
Z = -12126404
58 Z = -3696128
12
XDOT = 3276
025667 XDOT = 998
532623
YDOT = -19260
693623 feet/sec YDOT = -5870
659416 meter/sec
ZDOT = -14186
317946 ZDOT = -4323
989710
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 16111
54115318
00016717 00000-0 10270-3 0 9106
2 25544 51
6437 345
5692 0001553 36
6853 323
4406 15
54309637 36012
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
54115318 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 345
5692 deg
Eccentricity:
0001553
Arg of perigee: 36
6853 deg
Mean anomaly: 323
4406 deg
Mean motion: 15
54309637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 292
Coasting Arc #12 (Orbit 3616)
---------------------------------------
Vector Time (GMT): 2016/112/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190781
57 A = 6779228
91 meter
Y = 2472548
29 meter E =
0008312
Z = 4714410
52 I = 51
51044
XDOT = -5676
030344 Wp = 105
47757
YDOT = 4371
100770 meter/sec RA = 340
15092 deg
ZDOT = 2746
885536 TA = 317
27115
MA = 317
33575
Ha = 221
070 n
mi
Hp = 213
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13749283
37 X = 4139920
49
Y = 8112035
09 feet Y = 2519128
40 meter
Z = 15467226
12 Z = 4734644
90
XDOT = -18622
146799 XDOT = -5737
830640
YDOT = 14340
881791 feet/sec YDOT = 4307
282294 meter/sec
ZDOT = 9012
091653 ZDOT = 2719
161883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15830127
04 X = 4825022
72
Y = -1242554
10 feet Y = -378730
49 meter
Z = 15554617
56 Z = 4741047
43
XDOT = -7081
397822 XDOT = -2158
410056
YDOT = 21334
430629 feet/sec YDOT = 6502
734456 meter/sec
ZDOT = 8890
815428 ZDOT = 2709
920542
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 16112
56985141
00016717 00000-0 10270-3 0 9119
2 25544 51
6435 340
4388 0001755 42
4989 317
6299 15
54317621 36179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
56985141 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 340
4388 deg
Eccentricity:
0001755
Arg of perigee: 42
4989 deg
Mean anomaly: 317
6299 deg
Mean motion: 15
54317621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3617
Checksum: 322
Coasting Arc #13 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2016/113/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2598456
37 A = 6776848
37 meter
Y = -3412512
47 meter E =
0015820
Z = -5260582
95 I = 51
47168
XDOT = 6610
618222 Wp = 79
57650
YDOT = -3777
463459 meter/sec RA = 335
13972 deg
ZDOT = -814
171166 TA = 182
60772
MA = 182
61598
Ha = 221
058 n
mi
Hp = 213
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8525119
32 X = -2534549
55
Y = -11195907
04 feet Y = -3441213
15 meter
Z = -17259130
41 Z = -5273050
39
XDOT = 21688
379992 XDOT = 6656
322410
YDOT = -12393
252817 feet/sec YDOT = -3703
283633 meter/sec
ZDOT = -2671
165243 ZDOT = -781
946576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13403099
73 X = -4085264
80
Y = -4066254
08 feet Y = -1239394
24 meter
Z = -17312598
64 Z = -5276880
06
XDOT = 9898
378720 XDOT = 3017
025834
YDOT = -21843
115255 feet/sec YDOT = -6657
781530 meter/sec
ZDOT = -2530
467549 ZDOT = -771
286509
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 16113
53424296
00016717 00000-0 10270-3 0 9127
2 25544 51
6421 335
6285 0001644 41
6019 318
5258 15
54371296 36328
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
53424296 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 335
6285 deg
Eccentricity:
0001644
Arg of perigee: 41
6019 deg
Mean anomaly: 318
5258 deg
Mean motion: 15
54371296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 299
Coasting Arc #14 (Orbit 3647)
---------------------------------------
Vector Time (GMT): 2016/114/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 870205
22 A = 6777143
15 meter
Y = 4268824
17 meter E =
0005706
Z = 5188020
44 I = 51
44416
XDOT = -6996
496907 Wp = 52
10112
YDOT = 2904
882042 meter/sec RA = 330
12434 deg
ZDOT = -1212
306584 TA = 49
58171
MA = 49
53194
Ha = 221
019 n
mi
Hp = 213
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2855004
00 X = 797203
82
Y = 14005328
65 feet Y = 4278147
46 meter
Z = 17021064
42 Z = 5192070
24
XDOT = -22954
386178 XDOT = -7022
571045
YDOT = 9530
452894 feet/sec YDOT = 2826
496712 meter/sec
ZDOT = -3977
383806 ZDOT = -1246
357958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10653246
34 X = 3247109
48
Y = 9499392
09 feet Y = 2895414
71 meter
Z = 17037805
17 Z = 5193123
01
XDOT = -11813
326422 XDOT = -3600
701894
YDOT = 20673
784507 feet/sec YDOT = 6301
369518 meter/sec
ZDOT = -4125
833890 ZDOT = -1257
554170
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 16114
56291761
00016717 00000-0 10270-3 0 9131
2 25544 51
6423 330
4984 0001575 44
5812 315
5467 15
54378029 36482
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
56291761 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 330
4984 deg
Eccentricity:
0001575
Arg of perigee: 44
5812 deg
Mean anomaly: 315
5467 deg
Mean motion: 15
54378029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3648
Checksum: 317
Coasting Arc #15 (Orbit 3662)
---------------------------------------
Vector Time (GMT): 2016/115/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 803006
48 A = 6779828
91 meter
Y = -4977449
99 meter E =
0010598
Z = -4542968
34 I = 51
42451
XDOT = 6790
812080 Wp = 102
37912
YDOT = -1725
918471 meter/sec RA = 325
10973 deg
ZDOT = 3095
210213 TA = 198
72362
MA = 198
76263
Ha = 221
032 n
mi
Hp = 213
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2634535
68 X = 880674
10
Y = -16330216
51 feet Y = -4968036
12 meter
Z = -14904751
77 Z = -4538878
66
XDOT = 22279
567190 XDOT = 6794
571528
YDOT = -5662
462176 feet/sec YDOT = -1649
957977 meter/sec
ZDOT = 10154
889151 ZDOT = 3128
208107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7946998
11 X = -2422245
02
Y = -14526541
34 feet Y = -4427689
80 meter
Z = -14886006
61 Z = -4537254
82
XDOT = 12905
069827 XDOT = 3933
465283
YDOT = -17600
191942 feet/sec YDOT = -5364
538504 meter/sec
ZDOT = 10298
524525 ZDOT = 3138
990275
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 16115
52728964
00016717 00000-0 10270-3 0 9149
2 25544 51
6408 325
6872 0001572 47
8245 312
3041 15
54398196 36637
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
52728964 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 325
6872 deg
Eccentricity:
0001572
Arg of perigee: 47
8245 deg
Mean anomaly: 312
3041 deg
Mean motion: 15
54398196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3663
Checksum: 320
Coasting Arc #16 (Orbit 3678)
---------------------------------------
Vector Time (GMT): 2016/116/12:24:13
979
Vector Time (MET): N/A
Weight (LBS) : 945061
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2321109
16 A = 6783703
26 meter
Y = 5419332
95 meter E =
0013657
Z = 3345017
90 I = 51
41265
XDOT = -6098
705185 Wp = 86
17982
YDOT = 266
358541 meter/sec RA = 320
10474 deg
ZDOT = -4646
120132 TA = 54
67166
MA = 54
54406
Ha = 220
948 n
mi
Hp = 213
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7615187
55 X = -2397785
94
Y = 17779963
74 feet Y = 5392948
09 meter
Z = 10974468
19 Z = 3333556
00
XDOT = -20008
875279 XDOT = -6078
661143
YDOT = 873
879727 feet/sec YDOT = 198
270759 meter/sec
ZDOT = -15243
176285 ZDOT = -4675
697969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5268606
00 X = 1605871
11
Y = 18640636
99 feet Y = 5681666
15 meter
Z = 10923625
19 Z = 3329520
96
XDOT = -13528
353916 XDOT = -4123
442274
YDOT = 12865
066579 feet/sec YDOT = 3921
272293 meter/sec
ZDOT = -15371
667547 ZDOT = -4685
284268
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 16116
55594064
00016717 00000-0 10270-3 0 9156
2 25544 51
6413 320
5567 0001544 43
1304 316
9970 15
54446093 36790
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
55594064 = yrday
fracday
Element set: 915
Inclination: 51
6413 deg
RA of node: 320
5567 deg
Eccentricity:
0001544
Arg of perigee: 43
1304 deg
Mean anomaly: 316
9970 deg
Mean motion: 15
54446093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3679
Checksum: 310
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