[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
265/11:30:45
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 219
8
Coasting Arc #1 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2014/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3334540
28 A = 6790068
99 meter
Y = -3398438
20 meter E =
0013072
Z = -4853283
82 I = 51
58533
XDOT = 6609
759280 Wp = 77
88886
YDOT = -2957
625534 meter/sec RA = 351
60840 deg
ZDOT = -2473
301199 TA = 167
76399
MA = 167
73221
Ha = 227
390 n
mi
Hp = 219
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10940092
78 X = -3272714
75
Y = -11149731
62 feet Y = -3435382
02 meter
Z = -15922847
17 Z = -4869331
93
XDOT = 21685
561942 XDOT = 6654
355323
YDOT = -9703
495847 feet/sec YDOT = -2883
461843 meter/sec
ZDOT = -8114
505246 ZDOT = -2441
083446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10340009
10 X = 3151634
77
Y = 11615831
06 feet Y = 3540505
31 meter
Z = -15990493
67 Z = -4873902
47
XDOT = -21293
950814 XDOT = -6490
396208
YDOT = 7987
388038 feet/sec YDOT = 2434
555874 meter/sec
ZDOT = -7976
916745 ZDOT = -2431
364224
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 14262
52042369
00016717 00000-0 10270-3 0 9003
2 25544 51
6475 352
0341 0001801 119
7772 240
3558 15
50440897 25964
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
52042369 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 352
0341 deg
Eccentricity:
0001801
Arg of perigee: 119
7772 deg
Mean anomaly: 240
3558 deg
Mean motion: 15
50440897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 301
Coasting Arc #2 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2014/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3075828
59 A = 6789100
33 meter
Y = 3369103
77 meter E =
0007489
Z = 5023694
48 I = 51
55235
XDOT = -6693
021395 Wp = 122
67026
YDOT = 3185
112482 meter/sec RA = 346
64303 deg
ZDOT = 1955
741200 TA = 308
28493
MA = 308
35227
Ha = 227
195 n
mi
Hp = 219
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10091301
15 X = 3013522
50
Y = 11053490
08 feet Y = 3403151
91 meter
Z = 16481937
27 Z = 5038484
61
XDOT = -21958
731612 XDOT = -6737
640941
YDOT = 10449
844100 feet/sec YDOT = 3110
017539 meter/sec
ZDOT = 6416
473753 ZDOT = 1923
118826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9688857
16 X = -2953163
66
Y = -11317354
98 feet Y = -3449529
80 meter
Z = 16544237
10 Z = 5042683
47
XDOT = 21444
355613 XDOT = 6536
239591
YDOT = -9153
368193 feet/sec YDOT = -2789
946625 meter/sec
ZDOT = 6277
132818 ZDOT = 1913
270083
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 14263
55168243
00016717 00000-0 10270-3 0 9018
2 25544 51
6477 346
9213 0001805 120
2827 239
8503 15
50515188 26126
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
55168243 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 346
9213 deg
Eccentricity:
0001805
Arg of perigee: 120
2827 deg
Mean anomaly: 239
8503 deg
Mean motion: 15
50515188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 298
Coasting Arc #3 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2793115
55 A = 6788535
09 meter
Y = -3409551
54 meter E =
0015257
Z = -5176616
91 I = 51
51939
XDOT = 6716
056973 Wp = 83
50822
YDOT = -3390
357812 meter/sec RA = 341
67551 deg
ZDOT = -1392
556269 TA = 173
05789
MA = 173
03673
Ha = 227
271 n
mi
Hp = 219
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9163764
94 X = -2729635
29
Y = -11186192
71 feet Y = -3440431
72 meter
Z = -16983651
29 Z = -5190030
79
XDOT = 22034
307653 XDOT = 6760
234159
YDOT = -11123
221167 feet/sec YDOT = -3315
007693 meter/sec
ZDOT = -4568
754165 ZDOT = -1359
822940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8950201
65 X = 2728021
46
Y = 11272939
11 feet Y = 3435991
84 meter
Z = -17040089
22 Z = -5193819
20
XDOT = -21345
007032 XDOT = -6505
958143
YDOT = 10261
423557 feet/sec YDOT = 3127
681900 meter/sec
ZDOT = -4428
915865 ZDOT = -1349
933556
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 14264
51846888
00016717 00000-0 10270-3 0 9024
2 25544 51
6470 342
1291 0001732 120
4779 239
6543 15
50503346 26271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51846888 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 342
1291 deg
Eccentricity:
0001732
Arg of perigee: 120
4779 deg
Mean anomaly: 239
6543 deg
Mean motion: 15
50503346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 309
Coasting Arc #4 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4466201
49 A = 6796605
36 meter
Y = -4311758
16 meter E =
0005808
Z = -2769137
95 I = 51
51809
XDOT = 5263
459422 Wp = 72
13777
YDOT = 2170
486062 meter/sec RA = 336
77610 deg
ZDOT = 5120
170274 TA = 256
50289
MA = 256
56761
Ha = 227
227 n
mi
Hp = 219
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14652892
04 X = 4527536
22
Y = -14146188
20 feet Y = -4261471
66 meter
Z = -9085098
27 Z = -2747292
17
XDOT = 17268
567656 XDOT = 5213
925202
YDOT = 7121
017263 feet/sec YDOT = 2229
069252 meter/sec
ZDOT = 16798
458905 ZDOT = 5145
618789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16300661
13 X = -4968441
51
Y = 12280221
89 feet Y = 3743011
63 meter
Z = -8991412
18 Z = -2740582
43
XDOT = -15288
584432 XDOT = -4659
960535
YDOT = -7941
138443 feet/sec YDOT = -2420
458998 meter/sec
ZDOT = 16906
302535 ZDOT = 5153
041013
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 14265
48523419
00016717 00000-0 10270-3 0 9034
2 25544 51
6473 337
3359 0001703 119
9019 240
2301 15
50540793 26427
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48523419 = yrday
fracday
Element set: 903
Inclination: 51
6473 deg
RA of node: 337
3359 deg
Eccentricity:
0001703
Arg of perigee: 119
9019 deg
Mean anomaly: 240
2301 deg
Mean motion: 15
50540793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 295
Coasting Arc #5 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4549762
34 A = 6797480
49 meter
Y = 4495663
08 meter E =
0015609
Z = 2278895
40 I = 51
49276
XDOT = -4940
444179 Wp = 109
04238
YDOT = -2241
453812 meter/sec RA = 331
81061 deg
ZDOT = -5416
255217 TA = 45
56016
MA = 45
43255
Ha = 227
185 n
mi
Hp = 219
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14927041
81 X = -4610765
92
Y = 14749550
79 feet Y = 4444443
95 meter
Z = 7476690
95 Z = 2256644
37
XDOT = -16208
806361 XDOT = -4888
702013
YDOT = -7353
851089 feet/sec YDOT = -2296
412572 meter/sec
ZDOT = -17769
866198 ZDOT = -5440
129262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16411675
29 X = 5002278
63
Y = -13131666
42 feet Y = -4002531
92 meter
Z = 7381259
01 Z = 2249807
75
XDOT = 14296
981954 XDOT = 4357
720100
YDOT = 7775
345795 feet/sec YDOT = 2369
925398 meter/sec
ZDOT = -17870
995424 ZDOT = -5447
079405
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 14266
51642915
00016717 00000-0 10270-3 0 9043
2 25544 51
6468 332
2231 0001803 118
6984 241
4348 15
50597001 26587
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51642915 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 332
2231 deg
Eccentricity:
0001803
Arg of perigee: 118
6984 deg
Mean anomaly: 241
4348 deg
Mean motion: 15
50597001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 304
Coasting Arc #6 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4575005
02 A = 6798314
67 meter
Y = -4695058
67 meter E =
0007906
Z = -1793696
37 I = 51
46790
XDOT = 4616
106786 Wp = 49
90828
YDOT = 2350
916003 meter/sec RA = 326
84351 deg
ZDOT = 5641
752742 TA = 290
37452
MA = 290
45942
Ha = 227
135 n
mi
Hp = 219
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15009858
99 X = 4635879
49
Y = -15403735
81 feet Y = -4643557
91 meter
Z = -5884830
62 Z = -1771322
91
XDOT = 15144
707304 XDOT = 4562
069194
YDOT = 7712
979013 feet/sec YDOT = 2402
235018 meter/sec
ZDOT = 18509
687473 ZDOT = 5664
045683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16311962
00 X = -4971886
02
Y = 14057427
01 feet Y = 4284703
75 meter
Z = -5788852
79 Z = -1764442
33
XDOT = -13285
950174 XDOT = -4049
557613
YDOT = -7785
126526 feet/sec YDOT = -2372
906565 meter/sec
ZDOT = 18604
068202 ZDOT = 5670
519988
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 14267
48315369
00016717 00000-0 10270-3 0 9051
2 25544 51
6463 327
4298 0001649 118
9982 241
1334 15
50590217 26731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48315369 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 327
4298 deg
Eccentricity:
0001649
Arg of perigee: 118
9982 deg
Mean anomaly: 241
1334 deg
Mean motion: 15
50590217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 326
Coasting Arc #7 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4585226
16 A = 6798788
43 meter
Y = 4854180
73 meter E =
0015448
Z = 1239364
98 I = 51
44440
XDOT = -4280
959202 Wp = 120
99105
YDOT = -2544
169618 meter/sec RA = 321
87505 deg
ZDOT = -5827
176250 TA = 45
51387
MA = 45
38769
Ha = 227
028 n
mi
Hp = 219
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15043392
90 X = -4645186
44
Y = 15925789
80 feet Y = 4802570
69 meter
Z = 4066158
07 Z = 1216944
01
XDOT = -14045
141740 XDOT = -4223
884679
YDOT = -8347
013184 feet/sec YDOT = -2591
723812 meter/sec
ZDOT = -19118
032315 ZDOT = -5847
833760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16125562
87 X = 4915071
56
Y = -14855091
29 feet Y = -4527831
82 meter
Z = 3969959
36 Z = 1210043
61
XDOT = 12235
773021 XDOT = 3729
463617
YDOT = 8108
137545 feet/sec YDOT = 2471
360324 meter/sec
ZDOT = -19205
420022 ZDOT = -5853
812023
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 14268
51430530
00016717 00000-0 10270-3 0 9065
2 25544 51
6461 322
3163 0001757 118
6956 241
4372 15
50669322 26898
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51430530 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 322
3163 deg
Eccentricity:
0001757
Arg of perigee: 118
6956 deg
Mean anomaly: 241
4372 deg
Mean motion: 15
50669322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 307
Coasting Arc #8 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535878
96 A = 6799283
77 meter
Y = -5010604
59 meter E =
0011100
Z = -701880
26 I = 51
42116
XDOT = 3969
954391 Wp = 48
53136
YDOT = 2771
674993 meter/sec RA = 316
90487 deg
ZDOT = 5937
498087 TA = 303
87596
MA = 303
98152
Ha = 227
059 n
mi
Hp = 219
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14881492
66 X = 4594981
14
Y = -16438991
43 feet Y = -4959551
09 meter
Z = -2302756
76 Z = -679701
06
XDOT = 13024
784748 XDOT = 3909
822969
YDOT = 9093
421893 feet/sec YDOT = 2815
734187 meter/sec
ZDOT = 19479
980599 ZDOT = 5956
637391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15721252
74 X = -4791837
84
Y = 15651543
51 feet Y = 4770590
46 meter
Z = -2207566
45 Z = -672866
25
XDOT = -11275
777122 XDOT = -3436
856867
YDOT = -8600
016075 feet/sec YDOT = -2621
284900 meter/sec
ZDOT = 19560
869417 ZDOT = 5962
152998
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 14269
48098959
00016717 00000-0 10270-3 0 9078
2 25544 51
6454 317
5223 0001673 116
9452 243
1870 15
50643451 27047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
48098959 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 317
5223 deg
Eccentricity:
0001673
Arg of perigee: 116
9452 deg
Mean anomaly: 243
1870 deg
Mean motion: 15
50643451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 319
Coasting Arc #9 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/270/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4477035
63 A = 6799213
36 meter
Y = 5107548
44 meter E =
0013970
Z = 103484
52 I = 51
40001
XDOT = -3661
317879 Wp = 131
60789
YDOT = -3077
558757 meter/sec RA = 311
93318 deg
ZDOT = -5988
261192 TA = 47
27515
MA = 47
15763
Ha = 226
912 n
mi
Hp = 219
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14688437
11 X = -4534319
38
Y = 16757048
67 feet Y = 5057163
05 meter
Z = 339516
15 Z = 81595
62
XDOT = -12012
197766 XDOT = -3597
542286
YDOT = -10096
977549 feet/sec YDOT = -3118
146118 meter/sec
ZDOT = -19646
526219 ZDOT = -6005
892348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15255282
27 X = 4649810
04
Y = -16244389
94 feet Y = -4951290
05 meter
Z = 245549
56 Z = 74843
50
XDOT = 10350
983408 XDOT = 3154
979743
YDOT = 9387
250012 feet/sec YDOT = 2861
233804 meter/sec
ZDOT = -19720
947042 ZDOT = -6010
944658
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 14270
51209780
00016717 00000-0 10270-3 0 9081
2 25544 51
6457 312
4081 0001792 119
7497 240
3832 15
50733850 27206
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51209780 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 312
4081 deg
Eccentricity:
0001792
Arg of perigee: 119
7497 deg
Mean anomaly: 240
3832 deg
Mean motion: 15
50733850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 301
Coasting Arc #10 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2014/271/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4365237
01 A = 6799186
60 meter
Y = -5184563
11 meter E =
0013731
Z = 464171
82 I = 51
37886
XDOT = 3399
075303 Wp = 56
86903
YDOT = 3406
671314 meter/sec RA = 306
95988 deg
ZDOT = 5963
664966 TA = 308
14811
MA = 308
27177
Ha = 226
979 n
mi
Hp = 219
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14321643
74 X = 4420632
73
Y = -17009721
50 feet Y = -5135438
42 meter
Z = 1522873
43 Z = 485512
96
XDOT = 11151
821859 XDOT = 3331
758457
YDOT = 11176
743156 feet/sec YDOT = 3444
306208 meter/sec
ZDOT = 19565
829940 ZDOT = 5980
013588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14599437
79 X = -4449908
64
Y = 16763322
82 feet Y = 5109460
79 meter
Z = 1614519
46 Z = 492105
53
XDOT = -9613
921873 XDOT = -2930
323387
YDOT = -10300
052819 feet/sec YDOT = -3139
456099 meter/sec
ZDOT = 19634
740110 ZDOT = 5984
668785
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 14271
54318544
00016717 00000-0 10270-3 0 9095
2 25544 51
6451 307
2941 0001778 116
7349 243
3984 15
50709130 27366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
54318544 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 307
2941 deg
Eccentricity:
0001778
Arg of perigee: 116
7349 deg
Mean anomaly: 243
3984 deg
Mean motion: 15
50709130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 315
Coasting Arc #11 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255523
65 A = 6798524
69 meter
Y = 5184876
27 meter E =
0011203
Z = -1079635
28 I = 51
36030
XDOT = -3151
816488 Wp = 138
40908
YDOT = -3798
233297 meter/sec RA = 301
98481 deg
ZDOT = -5860
762804 TA = 53
32958
MA = 53
22667
Ha = 226
814 n
mi
Hp = 219
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13961691
76 X = -4307941
25
Y = 17010748
91 feet Y = 5136995
07 meter
Z = -3542110
48 Z = -1100436
10
XDOT = -10340
605277 XDOT = -3080
639390
YDOT = -12461
395331 feet/sec YDOT = -3833
081499 meter/sec
ZDOT = -19228
224421 ZDOT = -5875
900881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13936259
77 X = 4247771
98
Y = -17012764
63 feet Y = -5185490
66 meter
Z = -3631454
96 Z = -1106867
47
XDOT = 8980
752562 XDOT = 2737
333381
YDOT = 11445
092956 feet/sec YDOT = 3488
464333 meter/sec
ZDOT = -19291
921435 ZDOT = -5880
177653
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 14272
50980579
00016717 00000-0 10270-3 0 9107
2 25544 51
6459 302
4992 0001855 123
1302 237
0027 15
50792210 27510
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
50980579 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 302
4992 deg
Eccentricity:
0001855
Arg of perigee: 123
1302 deg
Mean anomaly: 237
0027 deg
Mean motion: 15
50792210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 291
Coasting Arc #12 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2014/273/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4106655
06 A = 6797877
50 meter
Y = -5151714
70 meter E =
0015049
Z = 1649214
30 I = 51
34155
XDOT = 2966
380421 Wp = 69
73432
YDOT = 4196
857367 meter/sec RA = 297
00816 deg
ZDOT = 5686
199767 TA = 308
38362
MA = 308
51870
Ha = 226
857 n
mi
Hp = 219
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13473277
75 X = 4155946
05
Y = -16901951
11 feet Y = -5105515
69 meter
Z = 5410808
07 Z = 1669284
22
XDOT = 9732
219228 XDOT = 2891
607654
YDOT = 13769
217084 feet/sec YDOT = 4229
611722 meter/sec
ZDOT = 18655
511047 ZDOT = 5700
428248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13143344
84 X = -4006091
51
Y = 17132340
80 feet Y = 5221937
48 meter
Z = 5497034
96 Z = 1675496
25
XDOT = -8602
905945 XDOT = -2622
165732
YDOT = -12643
329883 feet/sec YDOT = -3853
686948 meter/sec
ZDOT = 18715
275849 ZDOT = 5704
416079
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 14273
54084885
00016717 00000-0 10270-3 0 9118
2 25544 51
6451 297
3851 0001882 119
9636 240
1702 15
50787370 27674
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
54084885 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 297
3851 deg
Eccentricity:
0001882
Arg of perigee: 119
9636 deg
Mean anomaly: 240
1702 deg
Mean motion: 15
50787370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 326
Coasting Arc #13 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2014/274/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3976708
95 A = 6796683
53 meter
Y = 5030125
33 meter E =
0007792
Z = -2248404
59 I = 51
32562
XDOT = -2804
536797 Wp = 133
84571
YDOT = -4631
540346 meter/sec RA = 292
02943 deg
ZDOT = -5418
415540 TA = 71
23123
MA = 71
14671
Ha = 226
699 n
mi
Hp = 219
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13046945
39 X = -4021739
30
Y = 16503035
88 feet Y = 4985403
25 meter
Z = -7376655
49 Z = -2267832
81
XDOT = -9201
236211 XDOT = -2726
216250
YDOT = -15195
342341 feet/sec YDOT = -4662
464985 meter/sec
ZDOT = -17776
953873 ZDOT = -5431
849115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12422045
76 X = 3786239
55
Y = -16941879
83 feet Y = -5163884
97 meter
Z = -7460128
03 Z = -2273847
02
XDOT = 8373
466772 XDOT = 2552
232672
YDOT = 13967
804148 feet/sec YDOT = 4257
386704 meter/sec
ZDOT = -17833
270728 ZDOT = -5435
580918
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 14274
50742780
00016717 00000-0 10270-3 0 9121
2 25544 51
6458 292
5902 0001880 128
0397 232
0924 15
50851913 27826
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
50742780 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 292
5902 deg
Eccentricity:
0001880
Arg of perigee: 128
0397 deg
Mean anomaly: 232
0924 deg
Mean motion: 15
50851913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 311
Coasting Arc #14 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2014/275/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826605
22 A = 6795481
15 meter
Y = -4867387
03 meter E =
0014758
Z = 2786217
54 I = 51
30981
XDOT = 2710
226271 Wp = 85
20656
YDOT = 5054
623816 meter/sec RA = 287
04878 deg
ZDOT = 5085
807681 TA = 306
51251
MA = 306
64834
Ha = 226
677 n
mi
Hp = 219
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12554479
06 X = 3867214
44
Y = -15969117
54 feet Y = -4824368
16 meter
Z = 9141133
67 Z = 2804905
78
XDOT = 8891
818475 XDOT = 2628
797514
YDOT = 16583
411469 feet/sec YDOT = 5084
476441 meter/sec
ZDOT = 16685
720738 ZDOT = 5098
775449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11653521
32 X = -3551993
30
Y = 16593635
16 feet Y = 5057740
00 meter
Z = 9221425
99 Z = 2810690
64
XDOT = -8422
977917 XDOT = -2567
323669
YDOT = -15258
131212 feet/sec YDOT = -4650
678393 meter/sec
ZDOT = 16739
993946 ZDOT = 5102
350155
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 14275
53842507
00016717 00000-0 10270-3 0 9134
2 25544 51
6447 287
4759 0001900 126
2770 233
8556 15
50871125 27989
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
53842507 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 287
4759 deg
Eccentricity:
0001900
Arg of perigee: 126
2770 deg
Mean anomaly: 233
8556 deg
Mean motion: 15
50871125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 327
Coasting Arc #15 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2014/276/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3715307
92 A = 6793928
78 meter
Y = 4613400
57 meter E =
0006289
Z = -3330931
89 I = 51
29693
XDOT = -2640
632634 Wp = 103
79261
YDOT = -5479
200711 meter/sec RA = 282
06575 deg
ZDOT = -4652
339713 TA = 115
11584
MA = 115
05057
Ha = 226
564 n
mi
Hp = 219
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12189330
44 X = -3750439
25
Y = 15135828
63 feet Y = 4571656
83 meter
Z = -10928254
23 Z = -3349066
16
XDOT = -8663
492895 XDOT = -2556
567041
YDOT = -17976
380284 feet/sec YDOT = -5508
260386 meter/sec
ZDOT = -15263
581737 ZDOT = -4664
962854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11048296
27 X = 3367520
70
Y = -15934234
87 feet Y = -4856754
79 meter
Z = -11006140
74 Z = -3354671
70
XDOT = 8623
867948 XDOT = 2628
554951
YDOT = 16538
833283 feet/sec YDOT = 5041
036385 meter/sec
ZDOT = -15316
329118 ZDOT = -4668
417115
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 14276
50496170
00016717 00000-0 10270-3 0 9144
2 25544 51
6448 282
6809 0001863 133
1427 226
9880 15
50917056 28132
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
50496170 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 282
6809 deg
Eccentricity:
0001863
Arg of perigee: 133
1427 deg
Mean anomaly: 226
9880 deg
Mean motion: 15
50917056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 320
Coasting Arc #16 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2014/277/11:30:45
000
Vector Time (MET): N/A
Weight (LBS) : 929559
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604885
77 A = 6792409
25 meter
Y = -4317767
18 meter E =
0012934
Z = 3799003
20 I = 51
28531
XDOT = 2632
962558 Wp = 102
25875
YDOT = 5874
046837 meter/sec RA = 277
08045 deg
ZDOT = 4162
988677 TA = 303
57479
MA = 303
69820
Ha = 226
461 n
mi
Hp = 219
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11827053
06 X = 3634445
73
Y = -14165902
82 feet Y = -4277289
29 meter
Z = 12463921
25 Z = 3816587
57
XDOT = 8638
328603 XDOT = 2546
859398
YDOT = 19271
807208 feet/sec YDOT = 5903
009382 meter/sec
ZDOT = 13658
099335 ZDOT = 4175
569452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10485496
49 X = -3195979
33
Y = 15123452
97 feet Y = 4609628
47 meter
Z = 12539412
00 Z = 3822012
78
XDOT = -9076
384190 XDOT = -2766
481901
YDOT = -17700
754343 feet/sec YDOT = -5395
189924 meter/sec
ZDOT = 13710
613260 ZDOT = 4178
994922
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 14277
53591194
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 277
5659 0001836 133
9338 226
1965 15
50951021 28285
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
53591194 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 277
5659 deg
Eccentricity:
0001836
Arg of perigee: 133
9338 deg
Mean anomaly: 226
1965 deg
Mean motion: 15
50951021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 330
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