[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 27th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 35520 9 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
072/03:59:49
025 -1
1 1
6 1
6
N/A -1
1 -0
0 224
2
000/00:03:38
051 0
4 0
1 220
7
Coasting Arc #1 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4507798
78 A = 6790816
54 meter
Y = -2480011
06 meter E =
0010543
Z = 4428556
96 I = 51
30181
XDOT = 566
420114 Wp = 127
31896
YDOT = 6904
381688 meter/sec RA = 287
58766 deg
ZDOT = 3278
248683 TA = 289
38935
MA = 289
50328
Ha = 226
519 n
mi
Hp = 219
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14789366
06 X = 4513683
76
Y = -8136519
22 feet Y = -2429568
72 meter
Z = 14529386
35 Z = 4450469
20
XDOT = 1858
333707 XDOT = 473
247350
YDOT = 22652
170891 feet/sec YDOT = 6910
195052 meter/sec
ZDOT = 10755
409065 ZDOT = 3280
773377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16749952
10 X = 5105385
40
Y = -1288701
14 feet Y = -392796
11 meter
Z = 14622233
59 Z = 4456856
80
XDOT = -7882
310341 XDOT = -2402
528192
YDOT = 20125
946791 feet/sec YDOT = 6134
388582 meter/sec
ZDOT = 10764
969505 ZDOT = 3281
162705
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 14057
55426936
00016717 00000-0 10270-3 0 9004
2 25544 51
6500 288
0276 0003165 183
6912 176
4216 15
50736292 34168
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55426936 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 288
0276 deg
Eccentricity:
0003165
Arg of perigee: 183
6912 deg
Mean anomaly: 176
4216 deg
Mean motion: 15
50736292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 306
Coasting Arc #2 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2014/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4372384
77 A = 6789435
08 meter
Y = 2140860
91 meter E =
0009891
Z = -4741184
08 I = 51
28809
XDOT = -601
067820 Wp = 87
23581
YDOT = -7146
650056 meter/sec RA = 282
60086 deg
ZDOT = -2677
115992 TA = 156
16057
MA = 156
11472
Ha = 226
308 n
mi
Hp = 219
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14345094
40 X = -4372968
79
Y = 7023821
88 feet Y = 2091962
37 meter
Z = -15555065
87 Z = -4762425
63
XDOT = -1972
007285 XDOT = -508
103440
YDOT = -23447
014618 feet/sec YDOT = -7152
852052 meter/sec
ZDOT = -8783
188950 ZDOT = -2679
809319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15867129
54 X = -4836301
08
Y = 737038
18 feet Y = 224649
24 meter
Z = -15645026
55 Z = -4768604
09
XDOT = 7676
128733 XDOT = 2339
684038
YDOT = -21099
868908 feet/sec YDOT = -6431
240043 meter/sec
ZDOT = -8793
439669 ZDOT = -2680
240411
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 14058
52088385
00016717 00000-0 10270-3 0 9015
2 25544 51
6488 283
2332 0003184 192
0876 168
0200 15
50800096 34318
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
52088385 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 283
2332 deg
Eccentricity:
0003184
Arg of perigee: 192
0876 deg
Mean anomaly: 168
0200 deg
Mean motion: 15
50800096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 297
Coasting Arc #3 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2014/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261333
56 A = 6788401
90 meter
Y = -1778456
72 meter E =
0007657
Z = 4974265
43 I = 51
27866
XDOT = 672
120810 Wp = 145
87073
YDOT = 7355
344637 meter/sec RA = 277
61248 deg
ZDOT = 2046
212767 TA = 284
07577
MA = 284
16086
Ha = 226
170 n
mi
Hp = 220
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13980753
16 X = 4256741
11
Y = -5834831
76 feet Y = -1730828
83 meter
Z = 16319768
48 Z = 4994954
99
XDOT = 2205
120767 XDOT = 579
882117
YDOT = 24131
708128 feet/sec YDOT = 7362
345237 meter/sec
ZDOT = 6713
296480 ZDOT = 2049
252828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15054495
85 X = 4588610
34
Y = -53880
65 feet Y = -16422
82 meter
Z = 16407340
29 Z = 5000957
32
XDOT = -7278
154592 XDOT = -2218
381520
YDOT = 22013
468563 feet/sec YDOT = 6709
705218 meter/sec
ZDOT = 6724
995201 ZDOT = 2049
778537
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 14059
55191369
00016717 00000-0 10270-3 0 9027
2 25544 51
6485 278
1192 0003123 194
0599 166
0465 15
50816871 34475
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
55191369 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 278
1192 deg
Eccentricity:
0003123
Arg of perigee: 194
0599 deg
Mean anomaly: 166
0465 deg
Mean motion: 15
50816871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 326
Coasting Arc #4 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2014/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207117
38 A = 6787406
84 meter
Y = 1348550
57 meter E =
0012555
Z = -5163546
81 I = 51
27119
XDOT = -744
343955 Wp = 91
99163
YDOT = -7496
348622 meter/sec RA = 272
62110 deg
ZDOT = -1354
626874 TA = 164
91447
MA = 164
87699
Ha = 226
000 n
mi
Hp = 219
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13802878
55 X = -4196802
11
Y = 4424378
52 feet Y = 1301560
84 meter
Z = -16940770
38 Z = -5183959
15
XDOT = -2442
073344 XDOT = -653
882559
YDOT = -24594
319625 feet/sec YDOT = -7504
166744 meter/sec
ZDOT = -4444
313892 ZDOT = -1358
021956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14362942
23 X = -4377824
79
Y = -931619
05 feet Y = -283957
49 meter
Z = -17027103
67 Z = -5189861
20
XDOT = 6744
471863 XDOT = 2055
715024
YDOT = -22708
015413 feet/sec YDOT = -6921
403098 meter/sec
ZDOT = -4457
505219 ZDOT = -1358
647591
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 14060
51847474
00016717 00000-0 10270-3 0 9031
2 25544 51
6468 273
3235 0003147 200
9583 159
1439 15
50890881 34621
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
51847474 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 273
3235 deg
Eccentricity:
0003147
Arg of perigee: 200
9583 deg
Mean anomaly: 159
1439 deg
Mean motion: 15
50890881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 316
Coasting Arc #5 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2014/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4187297
02 A = 6786893
13 meter
Y = -905405
73 meter E =
0004374
Z = 5263076
75 I = 51
26924
XDOT = 829
531580 Wp = 161
32899
YDOT = 7592
227540 meter/sec RA = 267
62967 deg
ZDOT = 641
895117 TA = 282
48339
MA = 282
53232
Ha = 225
814 n
mi
Hp = 220
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13737851
11 X = 4171544
27
Y = -2970491
24 feet Y = -858667
99 meter
Z = 17267312
18 Z = 5283379
64
XDOT = 2721
560301 XDOT = 741
453856
YDOT = 24908
883004 feet/sec YDOT = 7601
011518 meter/sec
ZDOT = 2105
955107 ZDOT = 645
709749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13801999
34 X = 4206849
40
Y = 2021548
93 feet Y = 616168
11 meter
Z = 17353114
87 Z = 5289229
41
XDOT = -6090
826638 XDOT = -1856
483959
YDOT = 23260
401662 feet/sec YDOT = 7089
770427 meter/sec
ZDOT = 2120
916107 ZDOT = 646
455229
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 14061
54944687
00016717 00000-0 10270-3 0 9040
2 25544 51
6469 268
2089 0003138 204
2971 155
8033 15
50902799 34782
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
54944687 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 268
2089 deg
Eccentricity:
0003138
Arg of perigee: 204
2971 deg
Mean anomaly: 155
8033 deg
Mean motion: 15
50902799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 336
Coasting Arc #6 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231801
34 A = 6786544
91 meter
Y = 422249
14 meter E =
0013644
Z = -5300375
73 I = 51
26962
XDOT = -895
734345 Wp = 102
55448
YDOT = -7600
219425 meter/sec RA = 262
63575 deg
ZDOT = 107
011751 TA = 168
48812
MA = 168
45689
Ha = 225
709 n
mi
Hp = 219
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13883862
67 X = -4210461
23
Y = 1385331
82 feet Y = 375044
97 meter
Z = -17389684
16 Z = -5320881
26
XDOT = -2938
760973 XDOT = -811
200235
YDOT = -24935
103100 feet/sec YDOT = -7609
763427 meter/sec
ZDOT = 351
088422 ZDOT = 102
866881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13438828
15 X = -4096154
82
Y = -3325628
27 feet Y = -1013651
50 meter
Z = -17476269
54 Z = -5326766
95
XDOT = 5367
095975 XDOT = 1635
890853
YDOT = -23493
260388 feet/sec YDOT = -7160
745766 meter/sec
ZDOT = 334
723907 ZDOT = 102
023847
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 14062
51595395
00016717 00000-0 10270-3 0 9057
2 25544 51
6455 263
4123 0003141 209
0909 151
0067 15
50979010 34933
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51595395 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 263
4123 deg
Eccentricity:
0003141
Arg of perigee: 209
0909 deg
Mean anomaly: 151
0067 deg
Mean motion: 15
50979010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 294
Coasting Arc #7 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2014/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4313102
40 A = 6786727
86 meter
Y = 59514
32 meter E =
0001485
Z = 5238484
54 I = 51
27578
XDOT = 945
383289 Wp = 130
65914
YDOT = 7556
791994 meter/sec RA = 257
64357 deg
ZDOT = -865
022210 TA = 327
65387
MA = 327
66298
Ha = 225
457 n
mi
Hp = 220
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14150598
41 X = 4286669
62
Y = 195256
95 feet Y = 107599
11 meter
Z = 17186629
06 Z = 5259372
64
XDOT = 3101
651212 XDOT = 865
013255
YDOT = 24792
624652 feet/sec YDOT = 7566
914384 meter/sec
ZDOT = -2837
999378 ZDOT = -860
625939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13242501
17 X = 4036314
36
Y = 4677246
79 feet Y = 1425624
82 meter
Z = 17274759
17 Z = 5265346
59
XDOT = -4632
036311 XDOT = -1411
844668
YDOT = 23522
325959 feet/sec YDOT = 7169
604952 meter/sec
ZDOT = -2820
558391 ZDOT = -859
706198
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 14063
54686696
00016717 00000-0 10270-3 0 9067
2 25544 51
6459 258
2975 0003168 213
9152 146
1797 15
50995127 35097
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
54686696 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 258
2975 deg
Eccentricity:
0003168
Arg of perigee: 213
9152 deg
Mean anomaly: 146
1797 deg
Mean motion: 15
50995127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 348
Coasting Arc #8 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4455636
11 A = 6787157
48 meter
Y = -548473
37 meter E =
0012519
Z = -5101542
92 I = 51
28464
XDOT = -951
662268 Wp = 115
52803
YDOT = -7418
388761 meter/sec RA = 252
65008 deg
ZDOT = 1626
577011 TA = 170
28888
MA = 170
26466
Ha = 225
424 n
mi
Hp = 219
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14618228
72 X = -4424390
27
Y = -1799453
30 feet Y = -598125
05 meter
Z = -16737345
53 Z = -5123111
70
XDOT = -3122
251534 XDOT = -876
538799
YDOT = -24338
545804 feet/sec YDOT = -7428
610624 meter/sec
ZDOT = 5336
538749 ZDOT = 1622
137349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13282450
44 X = -4048490
90
Y = -6120039
37 feet Y = -1865388
00 meter
Z = -16828279
98 Z = -5129259
74
XDOT = 3932
494587 XDOT = 1198
624350
YDOT = -23179
465450 feet/sec YDOT = -7065
101069 meter/sec
ZDOT = 5318
886184 ZDOT = 1621
196509
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 14064
51331896
00016717 00000-0 10270-3 0 9075
2 25544 51
6451 253
5006 0003127 216
7301 143
3636 15
51066544 35245
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51331896 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 253
5006 deg
Eccentricity:
0003127
Arg of perigee: 216
7301 deg
Mean anomaly: 143
3636 deg
Mean motion: 15
51066544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 284
Coasting Arc #9 (Orbit 3539)
---------------------------------------
Vector Time (GMT): 2014/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4627096
50 A = 6788074
10 meter
Y = 1019332
53 meter E =
0003920
Z = 4858140
97 I = 51
29832
XDOT = 909
241121 Wp = 72
67658
YDOT = 7229
377572 meter/sec RA = 247
65960 deg
ZDOT = -2380
122541 TA = 40
78372
MA = 40
75438
Ha = 225
123 n
mi
Hp = 220
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15180762
81 X = 4591755
03
Y = 3344266
84 feet Y = 1070878
59 meter
Z = 15938782
70 Z = 4880532
68
XDOT = 2983
074543 XDOT = 839
894832
YDOT = 23718
430354 feet/sec YDOT = 7239
157306 meter/sec
ZDOT = -7808
800988 ZDOT = -2375
874781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13486018
04 X = 4110538
30
Y = 7533300
97 feet Y = 2296150
14 meter
Z = 16033127
20 Z = 4886897
17
XDOT = -3353
876441 XDOT = -1022
261539
YDOT = 22606
643625 feet/sec YDOT = 6890
504977 meter/sec
ZDOT = -7791
922653 ZDOT = -2374
978025
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 14065
54417123
00016717 00000-0 10270-3 0 9088
2 25544 51
6453 248
3856 0003155 222
5155 137
5752 15
51090490 35404
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
54417123 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 248
3856 deg
Eccentricity:
0003155
Arg of perigee: 222
5155 deg
Mean anomaly: 137
5752 deg
Mean motion: 15
51090490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3540
Checksum: 296
Coasting Arc #10 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4844215
62 A = 6789192
17 meter
Y = -1464202
97 meter E =
0009088
Z = -4534972
79 I = 51
31525
XDOT = -800
611621 Wp = 128
41174
YDOT = -6954
095987 meter/sec RA = 242
66943 deg
ZDOT = 3099
167613 TA = 172
83454
MA = 172
82154
Ha = 225
134 n
mi
Hp = 219
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15893095
88 X = -4805453
25
Y = -4803815
52 feet Y = -1518157
77 meter
Z = -14878519
64 Z = -4558410
86
XDOT = -2626
678548 XDOT = -737
844516
YDOT = -22815
275547 feet/sec YDOT = -6962
697706 meter/sec
ZDOT = 10167
872745 ZDOT = 3095
431470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13910963
09 X = -4240061
55
Y = -8899739
41 feet Y = -2712640
57 meter
Z = -14977223
76 Z = -4565057
80
XDOT = 2932
419058 XDOT = 893
801329
YDOT = -21677
223088 feet/sec YDOT = -6607
217597 meter/sec
ZDOT = 10153
105243 ZDOT = 3094
666478
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 14066
51056617
00016717 00000-0 10270-3 0 9094
2 25544 51
6452 243
5888 0003073 224
2797 135
8109 15
51157341 35557
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51056617 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 243
5888 deg
Eccentricity:
0003073
Arg of perigee: 224
2797 deg
Mean anomaly: 135
8109 deg
Mean motion: 15
51157341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 315
Coasting Arc #11 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2014/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5070740
53 A = 6790670
12 meter
Y = 1875661
85 meter E =
0007767
Z = 4102447
80 I = 51
33517
XDOT = 613
675588 Wp = 86
51273
YDOT = 6637
166648 meter/sec RA = 237
68278 deg
ZDOT = -3786
386014 TA = 42
75834
MA = 42
69794
Ha = 224
834 n
mi
Hp = 220
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16636287
84 X = 5029461
40
Y = 6153746
22 feet Y = 1932135
67 meter
Z = 13459474
40 Z = 4126980
09
XDOT = 2013
371353 XDOT = 557
804573
YDOT = 21775
481127 feet/sec YDOT = 6643
716443 meter/sec
ZDOT = -12422
526293 ZDOT = -3783
541168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14446676
83 X = 4403347
10
Y = 10155664
14 feet Y = 3095446
43 meter
Z = 13562747
91 Z = 4133925
56
XDOT = -2765
485828 XDOT = -842
920081
YDOT = 20538
371268 feet/sec YDOT = 6260
095563 meter/sec
ZDOT = -12411
466038 ZDOT = -3783
014848
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 14067
54135584
00016717 00000-0 10270-3 0 9101
2 25544 51
6448 238
4733 0003092 230
3389 129
7489 15
51185895 35716
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
54135584 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 238
4733 deg
Eccentricity:
0003092
Arg of perigee: 230
3389 deg
Mean anomaly: 129
7489 deg
Mean motion: 15
51185895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 331
Coasting Arc #12 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2014/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5315340
86 A = 6792141
66 meter
Y = -2233549
21 meter E =
0003978
Z = -3595567
02 I = 51
35874
XDOT = -345
961698 Wp = 131
33607
YDOT = -6258
081898 meter/sec RA = 232
69814 deg
ZDOT = 4399
530948 TA = 186
01666
MA = 186
02144
Ha = 224
829 n
mi
Hp = 219
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17438782
35 X = -5272503
85
Y = -7327917
34 feet Y = -2292749
55 meter
Z = -11796479
72 Z = -3621283
66
XDOT = -1135
044940 XDOT = -297
327973
YDOT = -20531
764758 feet/sec YDOT = -6261
678350 meter/sec
ZDOT = 14434
156654 ZDOT = 4397
969011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15130391
07 X = -4611743
20
Y = -11239016
84 feet Y = -3425652
33 meter
Z = -11904713
47 Z = -3628556
67
XDOT = 2860
492412 XDOT = 871
878087
YDOT = -19131
882642 feet/sec YDOT = -5831
397829 meter/sec
ZDOT = 14428
448234 ZDOT = 4397
791022
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 14068
50769130
00016717 00000-0 10270-3 0 9119
2 25544 51
6454 233
6767 0002991 232
4728 127
6152 15
51253279 35866
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
50769130 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 233
6767 deg
Eccentricity:
0002991
Arg of perigee: 232
4728 deg
Mean anomaly: 127
6152 deg
Mean motion: 15
51253279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 319
Coasting Arc #13 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2014/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5538941
87 A = 6793752
59 meter
Y = 2548187
75 meter E =
0010885
Z = 2983921
30 I = 51
38317
XDOT = -20
300198 Wp = 106
81007
YDOT = 5854
165713 meter/sec RA = 227
71691 deg
ZDOT = -4949
691523 TA = 38
95347
MA = 38
87510
Ha = 224
570 n
mi
Hp = 220
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18172381
46 X = 5495541
06
Y = 8360196
04 feet Y = 2609885
37 meter
Z = 9789768
06 Z = 3010722
68
XDOT = -66
601699 XDOT = -61
717594
YDOT = 19206
580424 feet/sec YDOT = 5853
706654 meter/sec
ZDOT = -16239
145416 ZDOT = -4949
891293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15821688
95 X = 4822450
79
Y = 12148314
43 feet Y = 3702806
24 meter
Z = 9902550
16 Z = 3018297
29
XDOT = -3314
398090 XDOT = -1010
228538
YDOT = 17586
619884 feet/sec YDOT = 5360
401741 meter/sec
ZDOT = -16240
807759 ZDOT = -4950
198205
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 14069
53841630
00016717 00000-0 10270-3 0 9120
2 25544 51
6446 228
5604 0003016 238
7440 121
3416 15
51286808 36026
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
53841630 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 228
5604 deg
Eccentricity:
0003016
Arg of perigee: 238
7440 deg
Mean anomaly: 121
3416 deg
Mean motion: 15
51286808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 290
Coasting Arc #14 (Orbit 3616)
---------------------------------------
Vector Time (GMT): 2014/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5744392
03 A = 6795076
60 meter
Y = -2793118
42 meter E =
0003043
Z = -2314682
24 I = 51
41107
XDOT = 467
676747 Wp = 30
05213
YDOT = -5423
501672 meter/sec RA = 222
73882 deg
ZDOT = 5389
540849 TA = 304
10677
MA = 304
13564
Ha = 224
515 n
mi
Hp = 219
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18846430
56 X = -5701488
00
Y = -9163774
35 feet Y = -2857116
25 meter
Z = -7594101
84 Z = -2342482
77
XDOT = 1534
372529 XDOT = 502
108525
YDOT = -17793
640655 feet/sec YDOT = -5418
078720 meter/sec
ZDOT = 17682
220633 ZDOT = 5391
896930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16538038
26 X = -5040794
06
Y = -12800999
36 feet Y = -3901744
60 meter
Z = -7711082
53 Z = -2350337
95
XDOT = 4084
164917 XDOT = 1244
853467
YDOT = -15923
327501 feet/sec YDOT = -4853
430222 meter/sec
ZDOT = 17692
918038 ZDOT = 5392
801418
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 14070
50469027
00016717 00000-0 10270-3 0 9136
2 25544 51
6459 223
7638 0002907 242
2276 117
8581 15
51351491 36179
Satellite: ISS
Catalog Number: 25544
Epoch time: 14070
50469027 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 223
7638 deg
Eccentricity:
0002907
Arg of perigee: 242
2276 deg
Mean anomaly: 117
8581 deg
Mean motion: 15
51351491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3617
Checksum: 309
Coasting Arc #15 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2014/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5891355
70 A = 6796202
42 meter
Y = 2994474
38 meter E =
0012124
Z = 1556233
87 I = 51
43793
XDOT = -1016
798836 Wp = 127
78368
YDOT = 4990
330151 meter/sec RA = 217
76368 deg
ZDOT = -5729
716482 TA = 35
17050
MA = 35
09053
Ha = 224
312 n
mi
Hp = 219
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19328594
81 X = 5849873
38
Y = 9824391
01 feet Y = 3060123
54 meter
Z = 5105754
17 Z = 1584751
70
XDOT = -3335
954186 XDOT = -1044
693549
YDOT = 16372
474248 feet/sec YDOT = 4978
803003 meter/sec
ZDOT = -18798
282421 ZDOT = -5734
724221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17121377
97 X = 5218596
00
Y = 13256391
26 feet Y = 4040548
05 meter
Z = 5225750
56 Z = 1592808
77
XDOT = -5253
055286 XDOT = -1601
131251
YDOT = 14233
105289 feet/sec YDOT = 4338
250492 meter/sec
ZDOT = -18820
108817 ZDOT = -5736
369168
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 14071
53534867
00016717 00000-0 10270-3 0 9146
2 25544 51
6452 218
6469 0002940 249
1251 110
9586 15
51400005 36336
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
53534867 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 218
6469 deg
Eccentricity:
0002940
Arg of perigee: 249
1251 deg
Mean anomaly: 110
9586 deg
Mean motion: 15
51400005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 296
Coasting Arc #16 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:01:38
051
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4545840
76 A = 6788159
88 meter
Y = 1533726
88 meter E =
0007817
Z = -4809799
21 I = 51
42858
XDOT = -4573
470359 Wp = 116
68745
YDOT = -5591
392228 meter/sec RA = 214
43850 deg
ZDOT = 2539
289343 TA = 178
41227
MA = 178
40979
Ha = 224
221 n
mi
Hp = 220
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14914175
72 X = -4539289
26
Y = 5031912
35 feet Y = 1482928
39 meter
Z = -15780181
14 Z = -4831866
22
XDOT = -15004
824011 XDOT = -4522
941117
YDOT = -18344
462690 feet/sec YDOT = -5642
252854 meter/sec
ZDOT = 8331
001782 ZDOT = 2517
195845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5592708
66 X = 1704657
60
Y = -14612270
31 feet Y = -4453819
99 meter
Z = -15873564
89 Z = -4838262
58
XDOT = 22665
862125 XDOT = 6908
554776
YDOT = -275
284553 feet/sec YDOT = -83
906732 meter/sec
ZDOT = 8238
474476 ZDOT = 2511
087020
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 14072
17949282
00016717 00000-0 10270-3 0 9159
2 25544 51
6486 215
4541 0004018 271
3319 88
7372 15
51138291 36430
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17949282 = yrday
fracday
Element set: 915
Inclination: 51
6486 deg
RA of node: 215
4541 deg
Eccentricity:
0004018
Arg of perigee: 271
3319 deg
Mean anomaly: 88
7372 deg
Mean motion: 15
51138291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 313
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