[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 9th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
344/13:26:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 216
7
345/20:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
4
348/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 216
1
349/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
9
352/04:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3193)
---------------------------------------
Vector Time (GMT): 2016/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2857619
28 A = 6783813
00 meter
Y = 4783847
88 meter E =
0007942
Z = 3868253
12 I = 51
26908
XDOT = -3557
178328 Wp = 47
33685
YDOT = 5430
289596 meter/sec RA = 272
98037 deg
ZDOT = -4077
147510 TA = 85
69236
MA = 85
60161
Ha = 220
705 n
mi
Hp = 217
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9375391
34 X = 2785122
29
Y = 15695038
98 feet Y = 4815398
22 meter
Z = 12691119
16 Z = 3881958
85
XDOT = -11670
532572 XDOT = -3597
831733
YDOT = 17815
910749 feet/sec YDOT = 5390
283664 meter/sec
ZDOT = -13376
468209 ZDOT = -4094
526031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17493351
62 X = -5331973
57
Y = 5168262
66 feet Y = 1575286
46 meter
Z = 12750232
43 Z = 3886270
84
XDOT = -14060
642714 XDOT = -4285
683899
YDOT = -14315
967472 feet/sec YDOT = -4363
506886 meter/sec
ZDOT = -13453
545734 ZDOT = -4100
640740
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 16342
54056526
00016717 00000-0 10270-3 0 9006
2 25544 51
6415 273
6416 0006404 304
9852 55
0698 15
53825053 31945
Satellite: ISS
Catalog Number: 25544
Epoch time: 16342
54056526 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 273
6416 deg
Eccentricity:
0006404
Arg of perigee: 304
9852 deg
Mean anomaly: 55
0698 deg
Mean motion: 15
53825053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3194
Checksum: 305
Coasting Arc #2 (Orbit 3208)
---------------------------------------
Vector Time (GMT): 2016/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2300840
02 A = 6787300
24 meter
Y = -5821801
22 meter E =
0007081
Z = -2611473
79 I = 51
27928
XDOT = 4036
453657 Wp = 352
57100
YDOT = -3927
438873 meter/sec RA = 267
97548 deg
ZDOT = 5204
496197 TA = 337
85975
MA = 337
89031
Ha = 220
824 n
mi
Hp = 216
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7548687
72 X = -2222882
63
Y = -19100397
70 feet Y = -5847094
80 meter
Z = -8567827
41 Z = -2622461
59
XDOT = 13242
958191 XDOT = 4054
789908
YDOT = -12885
298140 feet/sec YDOT = -3882
198155 meter/sec
ZDOT = 17075
118756 ZDOT = 5224
148847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20306638
22 X = 6189463
33
Y = -2939406
40 feet Y = -895931
07 meter
Z = -8614863
88 Z = -2625810
51
XDOT = 9335
100972 XDOT = 2845
338776
YDOT = 14243
239755 feet/sec YDOT = 4341
339477 meter/sec
ZDOT = 17161
867859 ZDOT = 5230
937324
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 16343
50528600
00016717 00000-0 10270-3 0 9011
2 25544 51
6409 268
8348 0006376 309
0707 50
9878 15
53820028 32099
Satellite: ISS
Catalog Number: 25544
Epoch time: 16343
50528600 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 268
8348 deg
Eccentricity:
0006376
Arg of perigee: 309
0707 deg
Mean anomaly: 50
9878 deg
Mean motion: 15
53820028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3209
Checksum: 314
Coasting Arc #3 (Orbit 3224)
---------------------------------------
Vector Time (GMT): 2016/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1680715
68 A = 6789671
29 meter
Y = 6483818
65 meter E =
0007427
Z = 1092510
92 I = 51
29032
XDOT = -4461
080207 Wp = 115
21322
YDOT = 2147
215591 meter/sec RA = 262
97895 deg
ZDOT = -5852
164634 TA = 52
88125
MA = 52
81340
Ha = 221
009 n
mi
Hp = 216
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5514159
06 X = 1602780
04
Y = 21272370
89 feet Y = 6502177
74 meter
Z = 3584353
42 Z = 1100486
41
XDOT = -14636
089917 XDOT = -4456
331778
YDOT = 7044
670573 feet/sec YDOT = 2097
355529 meter/sec
ZDOT = -19200
015204 ZDOT = -5873
824068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21952571
16 X = -6691143
69
Y = 872534
84 feet Y = 265948
62 meter
Z = 3618094
16 Z = 1102795
10
XDOT = -3754
488688 XDOT = -1144
368152
YDOT = -14070
806344 feet/sec YDOT = -4288
781774 meter/sec
ZDOT = -19295
223146 ZDOT = -5881
184015
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 16344
53431473
00016717 00000-0 10270-3 0 9027
2 25544 51
6418 263
7077 0006360 312
2749 47
7864 15
53833091 32258
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
53431473 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 263
7077 deg
Eccentricity:
0006360
Arg of perigee: 312
2749 deg
Mean anomaly: 47
7864 deg
Mean motion: 15
53833091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3225
Checksum: 309
Coasting Arc #4 (Orbit 3225)
---------------------------------------
Vector Time (GMT): 2016/344/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3103628
28 A = 6786330
90 meter
Y = 5230635
11 meter E =
0008798
Z = 3006491
35 I = 51
27977
XDOT = -3355
486837 Wp = 72
01406
YDOT = 4827
199697 meter/sec RA = 262
66464 deg
ZDOT = -4919
788351 TA = 73
37735
MA = 73
28076
Ha = 220
996 n
mi
Hp = 216
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10182507
48 X = 3030302
91
Y = 17160876
34 feet Y = 5264931
88 meter
Z = 9863816
76 Z = 3021390
23
XDOT = -11008
815081 XDOT = -3385
317973
YDOT = 15837
269348 feet/sec YDOT = 4789
509751 meter/sec
ZDOT = -16141
037898 ZDOT = -4936
160940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15244302
85 X = -4646463
51
Y = 12826464
86 feet Y = 3909506
49 meter
Z = 9928093
78 Z = 3026082
99
XDOT = -16490
623216 XDOT = -5026
341956
YDOT = -7012
548731 feet/sec YDOT = -2137
424853 meter/sec
ZDOT = -16213
586353 ZDOT = -4941
901120
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 16344
59862909
00016717 00000-0 10270-3 0 9036
2 25544 51
6422 263
3883 0006279 312
2878 47
7742 15
53825752 32267
Satellite: ISS
Catalog Number: 25544
Epoch time: 16344
59862909 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 263
3883 deg
Eccentricity:
0006279
Arg of perigee: 312
2878 deg
Mean anomaly: 47
7742 deg
Mean motion: 15
53825752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3226
Checksum: 337
Coasting Arc #5 (Orbit 3240)
---------------------------------------
Vector Time (GMT): 2016/345/13:26:46
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2605010
94 A = 6789037
44 meter
Y = -6064513
88 meter E =
0010989
Z = -1559187
26 I = 51
29567
XDOT = 3995
964336 Wp = 2
19317
YDOT = -3184
169638 meter/sec RA = 257
66507 deg
ZDOT = 5720
807291 TA = 340
67328
MA = 340
71492
Ha = 221
038 n
mi
Hp = 216
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8546623
81 X = -2529428
42
Y = -19896699
09 feet Y = -6093222
19 meter
Z = -5115443
75 Z = -1571658
61
XDOT = 13110
119212 XDOT = 4003
483972
YDOT = -10446
750782 feet/sec YDOT = -3139
442301 meter/sec
ZDOT = 18769
052792 ZDOT = 5740
237055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18004240
58 X = 5487692
53
Y = -12009180
67 feet Y = -3660398
27 meter
Z = -5168953
36 Z = -1575496
99
XDOT = 11768
816553 XDOT = 3587
135285
YDOT = 9545
450565 feet/sec YDOT = 2909
453332 meter/sec
ZDOT = 18854
687053 ZDOT = 5746
908614
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 16345
56333404
00016717 00000-0 10270-3 0 9048
2 25544 51
6436 258
5807 0006462 315
5601 44
5032 15
53866596 32413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
56333404 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 258
5807 deg
Eccentricity:
0006462
Arg of perigee: 315
5601 deg
Mean anomaly: 44
5032 deg
Mean motion: 15
53866596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3241
Checksum: 305
Coasting Arc #6 (Orbit 3245)
---------------------------------------
Vector Time (GMT): 2016/345/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427635
00 A = 6779389
07 meter
Y = -1196231
54 meter E =
0008245
Z = -4999341
80 I = 51
26330
XDOT = -211
061588 Wp = 83
30529
YDOT = -7403
649164 meter/sec RA = 256
09687 deg
ZDOT = 1962
193767 TA = 205
84012
MA = 205
88132
Ha = 220
900 n
mi
Hp = 216
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14526361
55 X = -4389644
39
Y = -3924644
16 feet Y = -1245531
65 meter
Z = -16402040
02 Z = -5020758
22
XDOT = -692
459278 XDOT = -137
788016
YDOT = -24290
187547 feet/sec YDOT = -7405
599803 meter/sec
ZDOT = 6437
643593 ZDOT = 1961
346053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14219224
30 X = -4334019
57
Y = 4599368
47 feet Y = 1401887
51 meter
Z = -16495587
24 Z = -5027854
99
XDOT = -13563
625561 XDOT = -4134
193071
YDOT = -18896
525283 feet/sec YDOT = -5759
660906 meter/sec
ZDOT = 6435
259403 ZDOT = 1961
467066
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 16345
88490142
00016717 00000-0 10270-3 0 9057
2 25544 51
6414 256
9739 0006007 314
6128 45
4533 15
53865205 32461
Satellite: ISS
Catalog Number: 25544
Epoch time: 16345
88490142 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 256
9739 deg
Eccentricity:
0006007
Arg of perigee: 314
6128 deg
Mean anomaly: 45
4533 deg
Mean motion: 15
53865205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3246
Checksum: 312
Coasting Arc #7 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2016/346/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4529224
60 A = 6782490
75 meter
Y = 2756064
74 meter E =
0009185
Z = 4229756
89 I = 51
28182
XDOT = -734
317749 Wp = 37
94806
YDOT = 6733
752493 meter/sec RA = 251
08008 deg
ZDOT = -3590
045200 TA = 88
98862
MA = 88
88339
Ha = 221
114 n
mi
Hp = 216
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14859660
75 X = 4477522
34
Y = 9042207
14 feet Y = 2806424
16 meter
Z = 13877155
16 Z = 4251633
66
XDOT = -2409
178967 XDOT = -792
122596
YDOT = 22092
363822 feet/sec YDOT = 6725
217925 meter/sec
ZDOT = -11778
363517 ZDOT = -3593
752271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17299437
26 X = 5272868
48
Y = -804130
11 feet Y = -245098
86 meter
Z = 13972448
19 Z = 4258802
21
XDOT = 10409
075921 XDOT = 3172
686341
YDOT = 18331
685779 feet/sec YDOT = 5587
497825 meter/sec
ZDOT = -11795
794356 ZDOT = -3595
358120
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 16346
91391300
00016717 00000-0 10270-3 0 9069
2 25544 51
6411 251
8461 0005919 318
5190 41
5512 15
53837187 32627
Satellite: ISS
Catalog Number: 25544
Epoch time: 16346
91391300 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 251
8461 deg
Eccentricity:
0005919
Arg of perigee: 318
5190 deg
Mean anomaly: 41
5512 deg
Mean motion: 15
53837187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 300
Coasting Arc #8 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2016/347/20:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 896210
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4491328
35 A = 6786023
70 meter
Y = -4045883
29 meter E =
0006017
Z = -3076898
09 I = 51
30568
XDOT = 1760
273279 Wp = 5
79878
YDOT = -5653
610483 meter/sec RA = 246
07405 deg
ZDOT = 4871
315115 TA = 318
66625
MA = 318
71177
Ha = 221
192 n
mi
Hp = 216
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14735329
23 X = -4430806
03
Y = -13273895
32 feet Y = -4095769
64 meter
Z = -10094810
00 Z = -3098569
47
XDOT = 5775
174801 XDOT = 1799
699574
YDOT = -18548
590824 feet/sec YDOT = -5633
705962 meter/sec
ZDOT = 15982
004972 ZDOT = 4879
961377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19636093
57 X = -5985081
32
Y = -2416562
81 feet Y = -736568
35 meter
Z = -10188987
52 Z = -3105603
40
XDOT = -6209
530717 XDOT = -1892
664962
YDOT = -17000
647718 feet/sec YDOT = -5181
797425 meter/sec
ZDOT = 16020
866800 ZDOT = 4883
160201
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 16347
87860471
00016717 00000-0 10270-3 0 9076
2 25544 51
6415 247
0399 0006113 321
9045 38
1674 15
53857834 32770
Satellite: ISS
Catalog Number: 25544
Epoch time: 16347
87860471 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 247
0399 deg
Eccentricity:
0006113
Arg of perigee: 321
9045 deg
Mean anomaly: 38
1674 deg
Mean motion: 15
53857834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 330
Coasting Arc #9 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2016/348/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3889326
88 A = 6789343
29 meter
Y = -5403539
57 meter E =
0012593
Z = -1289559
04 I = 51
32503
XDOT = 3307
867009 Wp = 8
53420
YDOT = -3762
631496 meter/sec RA = 243
17372 deg
ZDOT = 5809
220036 TA = 337
36817
MA = 337
42365
Ha = 221
468 n
mi
Hp = 216
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12760258
78 X = -3822349
87
Y = -17728148
20 feet Y = -5446658
01 meter
Z = -4230836
75 Z = -1308290
48
XDOT = 10852
582052 XDOT = 3321
476961
YDOT = -12344
591522 feet/sec YDOT = -3725
565245 meter/sec
ZDOT = 19059
120852 ZDOT = 5825
321600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21415994
62 X = 6527595
16
Y = -4215926
14 feet Y = -1285014
29 meter
Z = -4311909
53 Z = -1314270
03
XDOT = 6462
243366 XDOT = 1969
691778
YDOT = 13325
257983 feet/sec YDOT = 4061
538633 meter/sec
ZDOT = 19130
295143 ZDOT = 5830
913960
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 16348
45741819
00016717 00000-0 10270-3 0 9086
2 25544 51
6419 244
1602 0006537 326
7504 33
3237 15
53871754 32861
Satellite: ISS
Catalog Number: 25544
Epoch time: 16348
45741819 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 244
1602 deg
Eccentricity:
0006537
Arg of perigee: 326
7504 deg
Mean anomaly: 33
3237 deg
Mean motion: 15
53871754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3286
Checksum: 321
Coasting Arc #10 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2016/349/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1453495
73 A = 6787783
22 meter
Y = 6220260
74 meter E =
0001505
Z = -2298539
15 I = 51
32924
XDOT = -5395
878731 Wp = 37
47300
YDOT = -730
767206 meter/sec RA = 240
11069 deg
ZDOT = -5390
400428 TA = 168
22699
MA = 168
22348
Ha = 221
546 n
mi
Hp = 215
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4768686
76 X = 1394996
51
Y = 20407679
61 feet Y = 6236187
89 meter
Z = -7541138
93 Z = -2291619
75
XDOT = -17703
014208 XDOT = -5361
121713
YDOT = -2397
530202 feet/sec YDOT = -790
912576 meter/sec
ZDOT = -17685
040775 ZDOT = -5416
528042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17812173
85 X = 5429150
59
Y = -11062545
92 feet Y = -3371864
00 meter
Z = -7511928
99 Z = -2289635
96
XDOT = 2517
155693 XDOT = 767
229055
YDOT = 16137
892332 feet/sec YDOT = 4918
829583 meter/sec
ZDOT = -17799
336491 ZDOT = -5425
237763
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 16349
10054032
00016717 00000-0 10270-3 0 9094
2 25544 51
6419 240
9542 0006281 329
5230 30
5556 15
53895324 32964
Satellite: ISS
Catalog Number: 25544
Epoch time: 16349
10054032 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 240
9542 deg
Eccentricity:
0006281
Arg of perigee: 329
5230 deg
Mean anomaly: 30
5556 deg
Mean motion: 15
53895324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 302
Coasting Arc #11 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2016/350/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -429044
77 A = 6784416
61 meter
Y = -5703288
36 meter E =
0010278
Z = 3636936
06 I = 51
33370
XDOT = 5872
471535 Wp = 62
40694
YDOT = 2335
502763 meter/sec RA = 235
11171 deg
ZDOT = 4350
425577 TA = 341
00487
MA = 341
04318
Ha = 221
673 n
mi
Hp = 215
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1407627
19 X = -382903
88
Y = -18711575
99 feet Y = -5707828
67 meter
Z = 11932204
91 Z = 3634963
26
XDOT = 19266
638895 XDOT = 5824
786432
YDOT = 7662
410639 feet/sec YDOT = 2400
905543 meter/sec
ZDOT = 14273
049792 ZDOT = 4378
836989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17135418
23 X = -5222875
48
Y = 7659267
32 feet Y = 2334544
68 meter
Z = 11924557
46 Z = 3634605
11
XDOT = 1365
894331 XDOT = 416
324592
YDOT = -19383
156386 feet/sec YDOT = -5907
986066 meter/sec
ZDOT = 14397
085890 ZDOT = 4388
231779
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 16350
12953286
00016717 00000-0 10270-3 0 9109
2 25544 51
6408 235
8270 0006299 333
9507 26
1328 15
53889687 33120
Satellite: ISS
Catalog Number: 25544
Epoch time: 16350
12953286 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 235
8270 deg
Eccentricity:
0006299
Arg of perigee: 333
9507 deg
Mean anomaly: 26
1328 deg
Mean motion: 15
53889687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 323
Coasting Arc #12 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2016/351/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -749398
33 A = 6780881
62 meter
Y = 4894832
91 meter E =
0011834
Z = -4643262
26 I = 51
34136
XDOT = -6073
104969 Wp = 38
57074
YDOT = -3669
120232 meter/sec RA = 230
10431 deg
ZDOT = -2882
649976 TA = 202
58648
MA = 202
63861
Ha = 221
797 n
mi
Hp = 215
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2458655
93 X = -781523
10
Y = 16059163
10 feet Y = 4886273
52 meter
Z = -15233800
06 Z = -4646980
12
XDOT = -19924
885068 XDOT = -6017
621983
YDOT = -12037
796036 feet/sec YDOT = -3736
723236 meter/sec
ZDOT = -9457
513044 ZDOT = -2912
017042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15865358
04 X = 4835761
13
Y = -3421974
34 feet Y = -1043017
78 meter
Z = -15250930
41 Z = -4648483
59
XDOT = -4557
099644 XDOT = -1389
003971
YDOT = 21666
679057 feet/sec YDOT = 6604
003777 meter/sec
ZDOT = -9585
527124 ZDOT = -2921
668667
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 16351
09421020
00016717 00000-0 10270-3 0 9113
2 25544 51
6410 231
0202 0006283 336
6930 23
3937 15
53890940 33274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16351
09421020 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 231
0202 deg
Eccentricity:
0006283
Arg of perigee: 336
6930 deg
Mean anomaly: 23
3937 deg
Mean motion: 15
53890940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 271
Coasting Arc #13 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2016/352/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2032316
93 A = 6778433
40 meter
Y = -3846590
16 meter E =
0004048
Z = 5196349
39 I = 51
35416
XDOT = 5962
278085 Wp = 18
91404
YDOT = 4687
809912 meter/sec RA = 225
08965 deg
ZDOT = 1141
779854 TA = 60
11815
MA = 60
07793
Ha = 221
860 n
mi
Hp = 215
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6667706
47 X = 2049938
07
Y = -12620046
46 feet Y = -3823765
36 meter
Z = 17048390
40 Z = 5206264
24
XDOT = 19561
279806 XDOT = 5903
868443
YDOT = 15379
953780 feet/sec YDOT = 4754
157423 meter/sec
ZDOT = 3745
996896 ZDOT = 1170
601375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14143988
34 X = -4311087
65
Y = -1471750
68 feet Y = -448589
61 meter
Z = 17092484
94 Z = 5209789
41
XDOT = 7035
514959 XDOT = 2144
424960
YDOT = -22784
790397 feet/sec YDOT = -6944
804113 meter/sec
ZDOT = 3871
471541 ZDOT = 1180
024526
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 16352
12319343
00016717 00000-0 10270-3 0 9123
2 25544 51
6402 225
8923 0006383 341
8177 18
2747 15
53912515 33431
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
12319343 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 225
8923 deg
Eccentricity:
0006383
Arg of perigee: 341
8177 deg
Mean anomaly: 18
2747 deg
Mean motion: 15
53912515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 298
Coasting Arc #14 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2016/352/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2616893
80 A = 6778099
11 meter
Y = -3347324
94 meter E =
0005282
Z = 5280338
63 I = 51
35368
XDOT = 5699
248735 Wp = 5
36108
YDOT = 5114
404618 meter/sec RA = 224
43441 deg
ZDOT = 422
763245 TA = 80
62145
MA = 80
56173
Ha = 221
905 n
mi
Hp = 215
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8585609
57 X = 2628480
60
Y = -10982037
21 feet Y = -3317996
75 meter
Z = 17323945
65 Z = 5293078
58
XDOT = 18698
322620 XDOT = 5639
580989
YDOT = 16779
542709 feet/sec YDOT = 5177
803788 meter/sec
ZDOT = 1387
018520 ZDOT = 450
304009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11920740
42 X = -3633441
68
Y = 7089211
16 feet Y = 2160791
56 meter
Z = 17380332
52 Z = 5297525
35
XDOT = -10680
630100 XDOT = -3255
456055
YDOT = -21612
891737 feet/sec YDOT = -6587
609401 meter/sec
ZDOT = 1506
812534 ZDOT = 459
276460
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 16352
25181662
00016717 00000-0 10270-3 0 9139
2 25544 51
6381 225
2516 0006516 341
5576 18
5339 15
53893851 33450
Satellite: ISS
Catalog Number: 25544
Epoch time: 16352
25181662 = yrday
fracday
Element set: 913
Inclination: 51
6381 deg
RA of node: 225
2516 deg
Eccentricity:
0006516
Arg of perigee: 341
5576 deg
Mean anomaly: 18
5339 deg
Mean motion: 15
53893851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 313
Coasting Arc #15 (Orbit 3359)
---------------------------------------
Vector Time (GMT): 2016/353/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3850934
36 A = 6778674
43 meter
Y = 2162480
76 meter E =
0012588
Z = -5152027
74 I = 51
37939
XDOT = -5030
891572 Wp = 72
46561
YDOT = -5599
945052 meter/sec RA = 219
41851 deg
ZDOT = 1416
487187 TA = 211
18788
MA = 211
26264
Ha = 222
112 n
mi
Hp = 215
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12634299
09 X = -3849803
51
Y = 7094753
13 feet Y = 2119423
68 meter
Z = -16902978
16 Z = -5170731
53
XDOT = -16505
549776 XDOT = -4974
778252
YDOT = -18372
523138 feet/sec YDOT = -5655
890207 meter/sec
ZDOT = 4647
267673 ZDOT = 1392
184564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14219919
57 X = 4334231
49
Y = -2228279
30 feet Y = -679179
53 meter
Z = -16985298
50 Z = -5177118
98
XDOT = 8843
780483 XDOT = 2695
584291
YDOT = 21981
315830 feet/sec YDOT = 6699
905065 meter/sec
ZDOT = 4541
719633 ZDOT = 1384
316144
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 16353
21648338
00016717 00000-0 10270-3 0 9145
2 25544 51
6381 220
4446 0006620 345
4393 14
6567 15
53891886 33608
Satellite: ISS
Catalog Number: 25544
Epoch time: 16353
21648338 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 220
4446 deg
Eccentricity:
0006620
Arg of perigee: 345
4393 deg
Mean anomaly: 14
6567 deg
Mean motion: 15
53891886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3360
Checksum: 317
Coasting Arc #16 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2016/354/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4972354
21 A = 6781183
81 meter
Y = -956122
51 meter E =
0011992
Z = 4510067
22 I = 51
41324
XDOT = 3969
809138 Wp = 34
36036
YDOT = 5757
957871 meter/sec RA = 214
40816 deg
ZDOT = -3142
239071 TA = 87
32922
MA = 87
19196
Ha = 222
138 n
mi
Hp = 215
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16313498
07 X = 4960768
52
Y = -3136884
88 feet Y = -900583
30 meter
Z = 14796808
45 Z = 4534193
25
XDOT = 13024
308194 XDOT = 3920
390623
YDOT = 18890
937896 feet/sec YDOT = 5802
074780 meter/sec
ZDOT = -10309
183304 ZDOT = -3123
074674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16327778
69 X = -4976706
94
Y = -2495820
46 feet Y = -760726
08 meter
Z = 14902695
39 Z = 4542341
55
XDOT = -6164
713902 XDOT = -1879
004797
YDOT = -20999
722854 feet/sec YDOT = -6400
715526 meter/sec
ZDOT = -10226
157061 ZDOT = -3116
932672
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 16354
24545778
00016717 00000-0 10270-3 0 9154
2 25544 51
6376 215
3167 0006680 348
3922 11
7075 15
53921814 33765
Satellite: ISS
Catalog Number: 25544
Epoch time: 16354
24545778 = yrday
fracday
Element set: 915
Inclination: 51
6376 deg
RA of node: 215
3167 deg
Eccentricity:
0006680
Arg of perigee: 348
3922 deg
Mean anomaly: 11
7075 deg
Mean motion: 15
53921814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 323
Coasting Arc #17 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2016/355/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5834521
05 A = 6784798
91 meter
Y = -126045
50 meter E =
0007575
Z = -3457880
45 I = 51
45320
XDOT = -2569
009928 Wp = 33
52504
YDOT = -5609
773271 meter/sec RA = 209
40847 deg
ZDOT = 4550
165403 TA = 285
79904
MA = 285
88255
Ha = 222
278 n
mi
Hp = 214
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19142129
45 X = -5815881
18
Y = -413535
12 feet Y = -191186
69 meter
Z = -11344752
13 Z = -3486177
61
XDOT = -8428
510261 XDOT = -2528
191640
YDOT = -18404
767950 feet/sec YDOT = -5638
273613 meter/sec
ZDOT = 14928
364184 ZDOT = 4537
784818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17934439
12 X = 5466417
04
Y = 6489927
82 feet Y = 1978130
00 meter
Z = -11468751
55 Z = -3495675
47
XDOT = 2666
367228 XDOT = 812
708731
YDOT = 18855
411926 feet/sec YDOT = 5747
129555 meter/sec
ZDOT = 14875
028152 ZDOT = 4533
908581
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 16355
21011732
00016717 00000-0 10270-3 0 9161
2 25544 51
6384 210
5096 0006727 352
1881 7
9165 15
53903443 33913
Satellite: ISS
Catalog Number: 25544
Epoch time: 16355
21011732 = yrday
fracday
Element set: 916
Inclination: 51
6384 deg
RA of node: 210
5096 deg
Eccentricity:
0006727
Arg of perigee: 352
1881 deg
Mean anomaly: 7
9165 deg
Mean motion: 15
53903443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 298
Coasting Arc #18 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2016/356/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376085
44 A = 6788059
58 meter
Y = 1114518
85 meter E =
0012674
Z = 2037641
50 I = 51
49380
XDOT = 865
069778 Wp = 81
82130
YDOT = 5230
419191 meter/sec RA = 204
41973 deg
ZDOT = -5536
460044 TA = 75
61450
MA = 75
47386
Ha = 222
448 n
mi
Hp = 214
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20918915
49 X = 6353250
79
Y = 3656557
89 feet Y = 1185692
77 meter
Z = 6685175
52 Z = 2068559
35
XDOT = 2838
155441 XDOT = 833
411192
YDOT = 17160
167951 feet/sec YDOT = 5239
916172 meter/sec
ZDOT = -18164
238990 ZDOT = -5532
334476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18781407
40 X = -5724572
98
Y = -9818469
73 feet Y = -2992669
57 meter
Z = 6820513
24 Z = 2078892
44
XDOT = 1673
382821 XDOT = 510
047084
YDOT = -15876
973182 feet/sec YDOT = -4839
301426 meter/sec
ZDOT = -18147
012734 ZDOT = -5531
209481
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 16356
23908217
00016717 00000-0 10270-3 0 9178
2 25544 51
6393 205
3812 0006823 355
9492 4
1604 15
53935836 34073
Satellite: ISS
Catalog Number: 25544
Epoch time: 16356
23908217 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 205
3812 deg
Eccentricity:
0006823
Arg of perigee: 355
9492 deg
Mean anomaly: 4
1604 deg
Mean motion: 15
53935836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 315
Coasting Arc #19 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2016/357/04:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 930289
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6489925
94 A = 6789775
63 meter
Y = -1909194
64 meter E =
0016727
Z = -452677
20 I = 51
52865
XDOT = 972
305984 Wp = 26
25191
YDOT = -4700
893064 meter/sec RA = 199
44072 deg
ZDOT = 5985
871327 TA = 328
85606
MA = 328
95509
Ha = 222
501 n
mi
Hp = 214
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21292407
95 X = -6465895
59
Y = -6263761
93 feet Y = -1981634
97 meter
Z = -1485161
41 Z = -484145
26
XDOT = 3189
980262 XDOT = 995
723611
YDOT = -15422
877505 feet/sec YDOT = -4689
889393 meter/sec
ZDOT = 19638
685455 ZDOT = 5990
651219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18589574
70 X = 5666102
37
Y = 12107902
27 feet Y = 3690488
61 meter
Z = -1622796
84 Z = -494628
48
XDOT = -6476
109748 XDOT = -1973
918251
YDOT = 12538
028608 feet/sec YDOT = 3821
591120 meter/sec
ZDOT = 19660
406129 ZDOT = 5992
491788
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 16357
20373320
00016717 00000-0 10270-3 0 9188
2 25544 51
6386 200
5746 0006795 359
6107
5039 15
53940235 34228
Satellite: ISS
Catalog Number: 25544
Epoch time: 16357
20373320 = yrday
fracday
Element set: 918
Inclination: 51
6386 deg
RA of node: 200
5746 deg
Eccentricity:
0006795
Arg of perigee: 359
6107 deg
Mean anomaly:
5039 deg
Mean motion: 15
53940235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 300
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