[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 31215 34 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
There are no maneuvers
Coasting Arc #1 (Orbit 8)
---------------------------------------
Vector Time (GMT): 2014/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2110790
31 A = 6788183
13 meter
Y = -5241247
73 meter E =
0016833
Z = 3755465
38 I = 51
28907
XDOT = 4289
758317 Wp = 116
54759
YDOT = 4759
966478 meter/sec RA = 259
74855 deg
ZDOT = 4209
986171 TA = 288
63667
MA = 288
81938
Ha = 225
674 n
mi
Hp = 215
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6925165
05 X = 2150999
30
Y = -17195694
66 feet Y = -5217419
01 meter
Z = 12321080
66 Z = 3765816
59
XDOT = 14074
010225 XDOT = 4215
761520
YDOT = 15616
687921 feet/sec YDOT = 4807
523232 meter/sec
ZDOT = 13812
290588 ZDOT = 4230
646054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16836417
00 X = 5131739
90
Y = 7685793
45 feet Y = 2342629
84 meter
Z = 12366183
56 Z = 3769212
75
XDOT = -15727
475889 XDOT = -4793
734651
YDOT = 11972
452178 feet/sec YDOT = 3649
203424 meter/sec
ZDOT = 13899
513956 ZDOT = 4236
571854
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 14353
55630475
00016717 00000-0 10270-3 0 9008
2 25544 51
6466 260
3224 0007153 150
1250 210
0312 15
52456825 90
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
55630475 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 260
3224 deg
Eccentricity:
0007153
Arg of perigee: 150
1250 deg
Mean anomaly: 210
0312 deg
Mean motion: 15
52456825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 9
Checksum: 262
Coasting Arc #2 (Orbit 23)
---------------------------------------
Vector Time (GMT): 2014/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2539249
66 A = 6785348
28 meter
Y = 4404950
41 meter E =
0012518
Z = -4502211
29 I = 51
28756
XDOT = -4151
027273 Wp = 103
96209
YDOT = -5608
037347 meter/sec RA = 254
74870 deg
ZDOT = -3156
080184 TA = 134
20653
MA = 134
10364
Ha = 225
443 n
mi
Hp = 215
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8330871
58 X = -2566447
72
Y = 14451937
05 feet Y = 4376403
27 meter
Z = -14771034
42 Z = -4514612
27
XDOT = -13618
855884 XDOT = -4072
677082
YDOT = -18399
072662 feet/sec YDOT = -5654
018419 meter/sec
ZDOT = -10354
593780 ZDOT = -3176
055659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14178975
08 X = -4321751
60
Y = -8696526
68 feet Y = -2650701
33 meter
Z = -14824724
38 Z = -4518575
99
XDOT = 18191
042523 XDOT = 5544
629761
YDOT = -11922
163923 feet/sec YDOT = -3633
875564 meter/sec
ZDOT = -10438
756139 ZDOT = -3181
732871
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 14354
52185305
00016717 00000-0 10270-3 0 9014
2 25544 51
6473 255
5211 0007081 153
9962 206
1547 15
52531076 246
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
52185305 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 255
5211 deg
Eccentricity:
0007081
Arg of perigee: 153
9962 deg
Mean anomaly: 206
1547 deg
Mean motion: 15
52531076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 24
Checksum: 284
Coasting Arc #3 (Orbit 39)
---------------------------------------
Vector Time (GMT): 2014/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2985540
69 A = 6783191
90 meter
Y = -3477527
00 meter E =
0012412
Z = 4996965
80 I = 51
28944
XDOT = 3982
353024 Wp = 142
83001
YDOT = 6253
485095 meter/sec RA = 249
74495 deg
ZDOT = 1960
353832 TA = 287
97913
MA = 288
11438
Ha = 225
274 n
mi
Hp = 215
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9795081
00 X = 2999931
66
Y = -11409209
32 feet Y = -3444060
84 meter
Z = 16394244
76 Z = 5011503
71
XDOT = 13065
462677 XDOT = 3902
606344
YDOT = 20516
683384 feet/sec YDOT = 6297
572241 meter/sec
ZDOT = 6431
607062 ZDOT = 1979
506550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11262303
79 X = 3432750
19
Y = 9859844
02 feet Y = 3005280
46 meter
Z = 16456880
62 Z = 5016057
21
XDOT = -19989
718058 XDOT = -6092
866064
YDOT = 11896
732096 feet/sec YDOT = 3626
123943 meter/sec
ZDOT = 6512
159099 ZDOT = 1984
906093
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 14355
55173794
00016717 00000-0 10270-3 0 9028
2 25544 51
6468 250
3997 0007118 158
4236 201
7218 15
52572759 406
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
55173794 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 250
3997 deg
Eccentricity:
0007118
Arg of perigee: 158
4236 deg
Mean anomaly: 201
7218 deg
Mean motion: 15
52572759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 40
Checksum: 318
Coasting Arc #4 (Orbit 54)
---------------------------------------
Vector Time (GMT): 2014/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3521965
15 A = 6781841
84 meter
Y = 2436025
90 meter E =
0017590
Z = -5272834
37 I = 51
29730
XDOT = -3698
022339 Wp = 108
10284
YDOT = -6672
829412 meter/sec RA = 244
73747 deg
ZDOT = -619
811345 TA = 155
98232
MA = 155
90018
Ha = 225
093 n
mi
Hp = 215
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11555003
78 X = -3523330
00
Y = 7992210
94 feet Y = 2396633
95 meter
Z = -17299325
37 Z = -5289946
55
XDOT = -12132
619223 XDOT = -3620
119527
YDOT = -21892
484949 feet/sec YDOT = -6713
747449 meter/sec
ZDOT = -2033
501789 ZDOT = -637
587246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8017253
59 X = -2443658
90
Y = -11426774
93 feet Y = -3482881
00 meter
Z = -17372756
43 Z = -5295216
16
XDOT = 21031
124859 XDOT = 6410
286857
YDOT = -11585
879699 feet/sec YDOT = -3531
376132 meter/sec
ZDOT = -2108
124529 ZDOT = -642
556357
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 14356
51722317
00016717 00000-0 10270-3 0 9037
2 25544 51
6468 245
5978 0007010 162
3148 197
8249 15
52635516 554
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51722317 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 245
5978 deg
Eccentricity:
0007010
Arg of perigee: 162
3148 deg
Mean anomaly: 197
8249 deg
Mean motion: 15
52635516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 55
Checksum: 315
Coasting Arc #5 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2014/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4057985
55 A = 6781679
00 meter
Y = -1386861
58 meter E =
0006879
Z = 5249311
53 I = 51
31124
XDOT = 3315
960884 Wp = 141
52337
YDOT = 6875
566729 meter/sec RA = 239
73000 deg
ZDOT = -751
650350 TA = 315
66132
MA = 315
71640
Ha = 224
779 n
mi
Hp = 215
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13313600
87 X = 4047692
94
Y = -4550070
79 feet Y = -1341540
62 meter
Z = 17222150
68 Z = 5268999
32
XDOT = 10879
136760 XDOT = 3242
481481
YDOT = 22557
633626 feet/sec YDOT = 6912
237183 meter/sec
ZDOT = -2466
044457 ZDOT = -735
719826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4805503
31 X = 1464717
41
Y = 13113111
53 feet Y = 3996876
40 meter
Z = 17306386
98 Z = 5274986
75
XDOT = -21384
102605 XDOT = -6517
874474
YDOT = 10982
581417 feet/sec YDOT = 3347
490816 meter/sec
ZDOT = -2399
309199 ZDOT = -731
309444
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 14357
54704006
00016717 00000-0 10270-3 0 9047
2 25544 51
6464 240
4758 0006975 167
3193 192
8135 15
52700024 718
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
54704006 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 240
4758 deg
Eccentricity:
0006975
Arg of perigee: 167
3193 deg
Mean anomaly: 192
8135 deg
Mean motion: 15
52700024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 299
Coasting Arc #6 (Orbit 85)
---------------------------------------
Vector Time (GMT): 2014/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4629070
53 A = 6782897
82 meter
Y = 331307
87 meter E =
0016665
Z = -4961474
19 I = 51
33171
XDOT = -2756
201975 Wp = 127
90728
YDOT = -6821
014222 meter/sec RA = 234
72327 deg
ZDOT = 2110
893384 TA = 162
80659
MA = 162
75008
Ha = 224
732 n
mi
Hp = 215
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15187239
27 X = -4608330
32
Y = 1086968
07 feet Y = 279658
97 meter
Z = -16277802
45 Z = -4983910
86
XDOT = -9042
657398 XDOT = -2689
976859
YDOT = -22378
655584 feet/sec YDOT = -6851
465749 meter/sec
ZDOT = 6925
503228 ZDOT = 2097
664610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1638707
09 X = -499477
92
Y = -15033989
60 feet Y = -4582360
03 meter
Z = -16373588
01 Z = -4990669
63
XDOT = 20932
923155 XDOT = 6380
354978
YDOT = -9782
496171 feet/sec YDOT = -2981
704833 meter/sec
ZDOT = 6870
263989 ZDOT = 2094
056464
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 14358
51246389
00016717 00000-0 10270-3 0 9051
2 25544 51
6459 235
6730 0006911 171
1164 189
0111 15
52727517 863
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51246389 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 235
6730 deg
Eccentricity:
0006911
Arg of perigee: 171
1164 deg
Mean anomaly: 189
0111 deg
Mean motion: 15
52727517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 86
Checksum: 308
Coasting Arc #7 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2014/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5136412
10 A = 6784929
15 meter
Y = 651305
76 meter E =
0010003
Z = 4374772
60 I = 51
35813
XDOT = 2041
359058 Wp = 111
27865
YDOT = 6581
213807 meter/sec RA = 229
72178 deg
ZDOT = -3373
879133 TA = 12
99907
MA = 12
97330
Ha = 224
324 n
mi
Hp = 216
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16851745
75 X = 5107496
37
Y = 2136829
93 feet Y = 708582
51 meter
Z = 14352928
47 Z = 4399654
01
XDOT = 6697
372237 XDOT = 1984
003651
YDOT = 21591
908815 feet/sec YDOT = 6603
721127 meter/sec
ZDOT = -11069
157259 ZDOT = -3364
101539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1231472
94 X = -375352
95
Y = 16851563
31 feet Y = 5136356
50 meter
Z = 14458984
09 Z = 4407098
35
XDOT = -19965
833981 XDOT = -6085
586197
YDOT = 8011
158642 feet/sec YDOT = 2441
801154 meter/sec
ZDOT = -11028
582746 ZDOT = -3361
512021
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 14359
54221495
00016717 00000-0 10270-3 0 9067
2 25544 51
6458 230
5504 0006780 175
5675 184
5538 15
52807875 1022
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
54221495 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 230
5504 deg
Eccentricity:
0006780
Arg of perigee: 175
5675 deg
Mean anomaly: 184
5538 deg
Mean motion: 15
52807875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 323
Coasting Arc #8 (Orbit 116)
---------------------------------------
Vector Time (GMT): 2014/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5584203
56 A = 6787718
10 meter
Y = -1541247
78 meter E =
0009119
Z = -3549335
07 I = 51
38784
XDOT = -1137
388362 Wp = 145
02904
YDOT = -6126
725175 meter/sec RA = 224
72551 deg
ZDOT = 4448
279439 TA = 173
01219
MA = 172
99947
Ha = 224
345 n
mi
Hp = 216
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18320877
83 X = -5549312
65
Y = -5056587
22 feet Y = -1603498
73 meter
Z = -11644800
10 Z = -3576377
30
XDOT = -3731
589113 XDOT = -1090
401372
YDOT = -20100
804379 feet/sec YDOT = -6139
181669 meter/sec
ZDOT = 14594
092648 ZDOT = 4442
868095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3747904
79 X = 1142361
38
Y = -18560230
38 feet Y = -5657158
22 meter
Z = -11759934
79 Z = -3584428
13
XDOT = 18423
402587 XDOT = 5615
453108
YDOT = -5516
065138 feet/sec YDOT = -1681
296654 meter/sec
ZDOT = 14572
056256 ZDOT = 4441
562747
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 14360
50757768
00016717 00000-0 10270-3 0 9073
2 25544 51
6451 225
7468 0006812 179
9205 180
1949 15
52815982 1175
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50757768 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 225
7468 deg
Eccentricity:
0006812
Arg of perigee: 179
9205 deg
Mean anomaly: 180
1949 deg
Mean motion: 15
52815982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 117
Checksum: 332
Coasting Arc #9 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2014/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5872469
21 A = 6790273
12 meter
Y = 2305288
22 meter E =
0016377
Z = 2483797
58 I = 51
42015
XDOT = 67
202804 Wp = 128
43672
YDOT = 5550
979239 meter/sec RA = 219
73734 deg
ZDOT = -5297
198157 TA = 23
61865
MA = 23
54355
Ha = 224
032 n
mi
Hp = 216
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19266631
25 X = 5834189
12
Y = 7563281
55 feet Y = 2370743
86 meter
Z = 8148942
19 Z = 2512231
99
XDOT = 220
481641 XDOT = 30
857258
YDOT = 18211
874145 feet/sec YDOT = 5551
527700 meter/sec
ZDOT = -17379
259046 ZDOT = -5296
959796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5839299
98 X = -1779818
63
Y = 19807142
36 feet Y = 6037216
99 meter
Z = 8269900
46 Z = 2520665
66
XDOT = -16665
760212 XDOT = -5079
723713
YDOT = 2361
506332 feet/sec YDOT = 719
787130 meter/sec
ZDOT = -17379
190148 ZDOT = -5297
177157
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 14361
53726504
00016717 00000-0 10270-3 0 9082
2 25544 51
6453 220
6237 0006729 183
1898 176
9212 15
52879388 1331
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
53726504 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 220
6237 deg
Eccentricity:
0006729
Arg of perigee: 183
1898 deg
Mean anomaly: 176
9212 deg
Mean motion: 15
52879388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 327
Coasting Arc #10 (Orbit 147)
---------------------------------------
Vector Time (GMT): 2014/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5997827
62 A = 6792145
61 meter
Y = -2920464
16 meter E =
0004457
Z = -1279590
74 I = 51
45045
XDOT = 1128
185451 Wp = 86
11069
YDOT = -4856
958829 meter/sec RA = 214
75425 deg
ZDOT = 5814
943753 TA = 259
95134
MA = 260
00163
Ha = 223
940 n
mi
Hp = 216
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19677912
14 X = -5958508
75
Y = -9581575
32 feet Y = -2987315
88 meter
Z = -4198132
36 Z = -1308631
70
XDOT = 3701
395835 XDOT = 1154
166353
YDOT = -15934
904295 feet/sec YDOT = -4844
197637 meter/sec
ZDOT = 19077
899452 ZDOT = 5820
487232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7458471
05 X = 2273341
98
Y = -20551063
51 feet Y = -6263964
16 meter
Z = -4321588
29 Z = -1317220
11
XDOT = 14723
100100 XDOT = 4487
600911
YDOT = 1338
372510 feet/sec YDOT = 407
935941 meter/sec
ZDOT = 19102
384397 ZDOT = 5822
406764
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 14362
50256641
00016717 00000-0 10270-3 0 9091
2 25544 51
6443 215
8195 0006722 188
2308 171
8734 15
52905321 1480
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
50256641 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 215
8195 deg
Eccentricity:
0006722
Arg of perigee: 188
2308 deg
Mean anomaly: 171
8734 deg
Mean motion: 15
52905321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 148
Checksum: 305
Coasting Arc #11 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5868444
00 A = 6792788
34 meter
Y = 3400249
87 meter E =
0016778
Z = -46298
75 I = 51
47910
XDOT = -2426
105071 Wp = 154
82771
YDOT = 4116
560866 meter/sec RA = 209
77719 deg
ZDOT = -6002
142786 TA = 25
67220
MA = 25
58900
Ha = 223
793 n
mi
Hp = 216
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19253425
19 X = 5830210
35
Y = 11155675
41 feet Y = 3465660
84 meter
Z = -151898
78 Z = -17883
56
XDOT = -7959
662307 XDOT = -2442
800779
YDOT = 13505
777120 feet/sec YDOT = 4089
337457 meter/sec
ZDOT = -19692
069509 ZDOT = -6013
968800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8714326
66 X = -2656126
77
Y = 20475011
28 feet Y = 6240783
44 meter
Z = -31181
40 Z = -9504
09
XDOT = -12868
598021 XDOT = -3922
348677
YDOT = -5487
190364 feet/sec YDOT = -1672
495623 meter/sec
ZDOT = -19743
245628 ZDOT = -6017
741267
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 14363
53219000
00016717 00000-0 10270-3 0 9105
2 25544 51
6442 210
6962 0006805 191
7835 168
3159 15
52941109 1644
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
53219000 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 210
6962 deg
Eccentricity:
0006805
Arg of perigee: 191
7835 deg
Mean anomaly: 168
3159 deg
Mean motion: 15
52941109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 293
Coasting Arc #12 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2014/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5507079
82 A = 6791793
45 meter
Y = -3732859
15 meter E =
0009994
Z = 1356211
81 I = 51
50319
XDOT = 3715
857007 Wp = 87
82216
YDOT = -3362
386881 meter/sec RA = 204
79994 deg
ZDOT = 5797
385148 TA = 286
96417
MA = 287
07369
Ha = 223
528 n
mi
Hp = 216
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18067847
18 X = -5471516
83
Y = -12246913
21 feet Y = -3794244
11 meter
Z = 4449513
81 Z = 1329545
48
XDOT = 12191
131914 XDOT = 3725
018105
YDOT = -11031
453022 feet/sec YDOT = -3320
782825 meter/sec
ZDOT = 19020
292479 ZDOT = 5815
458274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9602600
71 X = 2926872
70
Y = -19626988
60 feet Y = -5982306
13 meter
Z = 4336304
42 Z = 1321705
59
XDOT = 11174
386328 XDOT = 3405
952953
YDOT = 9713
827459 feet/sec YDOT = 2960
774609 meter/sec
ZDOT = 19098
014385 ZDOT = 5821
074784
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 14364
56177819
00016717 00000-0 10270-3 0 9111
2 25544 51
6431 205
5712 0006795 196
5399 163
5533 15
53026960 1805
Satellite: ISS
Catalog Number: 25544
Epoch time: 14364
56177819 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 205
5712 deg
Eccentricity:
0006795
Arg of perigee: 196
5399 deg
Mean anomaly: 163
5533 deg
Mean motion: 15
53026960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 320
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