[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 11th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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
254/21:27:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 213
3
257/01:13:06
631 6
3 6
5 6
5
N/A -1
3 -0
7 219
3
000/00:02:13
263 -0
6 -0
1 216
9
Coasting Arc #1 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2015/254/10:58:51
840
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5130683
51 A = 6780100
61 meter
Y = 2027015
04 meter E =
0010752
Z = 3934441
82 I = 51
72599
XDOT = -4838
735369 Wp = 77
63861
YDOT = -4364
557310 meter/sec RA = 12
68685 deg
ZDOT = -4049
730713 TA = 54
66126
MA = 54
56080
Ha = 219
423 n
mi
Hp = 213
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16832951
14 X = -5172080
61
Y = 6650311
82 feet Y = 1969409
37 meter
Z = 12908273
69 Z = 3909417
42
XDOT = -15875
116039 XDOT = -4769
898328
YDOT = -14319
413747 feet/sec YDOT = -4418
282830 meter/sec
ZDOT = -13286
518086 ZDOT = -4073
068389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18119509
55 X = 5522826
51
Y = 1429268
21 feet Y = 435640
95 meter
Z = 12799960
45 Z = 3901427
94
XDOT = 8026
605820 XDOT = 2446
509454
YDOT = 18468
577045 feet/sec YDOT = 5629
222283 meter/sec
ZDOT = -13386
309845 ZDOT = -4080
147241
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 15254
49814321
00016717 00000-0 10270-3 0 9006
2 25544 51
6431 13
0700 0000672 309
9031 50
2063 15
55079317 1474
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
49814321 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 13
0700 deg
Eccentricity:
0000672
Arg of perigee: 309
9031 deg
Mean anomaly: 50
2063 deg
Mean motion: 15
55079317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 264
Coasting Arc #2 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2015/254/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3102993
79 A = 6778111
81 meter
Y = 4112248
85 meter E =
0008397
Z = 4399217
39 I = 51
70553
XDOT = -6732
824758 Wp = 104
95005
YDOT = 1457
998362 meter/sec RA = 10
56494 deg
ZDOT = 3378
619474 TA = 310
88468
MA = 310
95740
Ha = 219
161 n
mi
Hp = 213
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10180425
81 X = 3035409
45
Y = 13491630
08 feet Y = 4146571
23 meter
Z = 14433127
90 Z = 4414126
32
XDOT = -22089
320072 XDOT = -6765
039972
YDOT = 4783
459192 feet/sec YDOT = 1382
527779 meter/sec
ZDOT = 11084
709562 ZDOT = 3345
834592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3424598
25 X = -1043817
55
Y = 16495469
59 feet Y = 5027819
13 meter
Z = 14496618
33 Z = 4418569
27
XDOT = -17060
979719 XDOT = -5200
186618
YDOT = -13180
536458 feet/sec YDOT = -4017
427512 meter/sec
ZDOT = 10943
044922 ZDOT = 3335
440092
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 15254
94797224
00016717 00000-0 10270-3 0 9019
2 25544 51
6420 10
8285 0001168 327
1211 32
9869 15
55132999 1543
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
94797224 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 10
8285 deg
Eccentricity:
0001168
Arg of perigee: 327
1211 deg
Mean anomaly: 32
9869 deg
Mean motion: 15
55132999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 306
Coasting Arc #3 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2015/255/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1000370
87 A = 6774943
89 meter
Y = -4233740
53 meter E =
0013957
Z = -5206020
45 I = 51
66355
XDOT = 7553
611261 Wp = 75
43927
YDOT = -253
405836 meter/sec RA = 5
56208 deg
ZDOT = -1244
763330 TA = 182
59994
MA = 182
60720
Ha = 219
332 n
mi
Hp = 213
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3282056
65 X = -927665
06
Y = -13890224
84 feet Y = -4244521
52 meter
Z = -17080119
58 Z = -5210702
86
XDOT = 24782
189175 XDOT = 7561
930063
YDOT = -831
383977 feet/sec YDOT = -168
890035 meter/sec
ZDOT = -4083
869194 ZDOT = -1208
049345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8103928
78 X = 2470077
49
Y = -11720694
35 feet Y = -3572467
64 meter
Z = -17099485
06 Z = -5211923
05
XDOT = 16510
127807 XDOT = 5032
286955
YDOT = 17145
446747 feet/sec YDOT = 5225
932169 meter/sec
ZDOT = -3925
508652 ZDOT = -1196
495037
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 15255
91188747
00016717 00000-0 10270-3 0 9022
2 25544 51
6423 6
0154 0001220 339
7936 20
3169 15
55120540 1699
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
91188747 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 6
0154 deg
Eccentricity:
0001220
Arg of perigee: 339
7936 deg
Mean anomaly: 20
3169 deg
Mean motion: 15
55120540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 285
Coasting Arc #4 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2015/256/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 926984
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1251705
17 A = 6774803
27 meter
Y = 4124600
28 meter E =
0004430
Z = 5224875
23 I = 51
63173
XDOT = -7540
267137 Wp = 39
01213
YDOT = -922
957189 meter/sec RA =
55237 deg
ZDOT = -1073
934403 TA = 61
29468
MA = 61
25015
Ha = 219
361 n
mi
Hp = 213
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4106644
27 X = -1323114
85
Y = 13532153
14 feet Y = 4110204
35 meter
Z = 17141979
09 Z = 5218620
67
XDOT = -24738
409242 XDOT = -7524
169238
YDOT = -3028
074766 feet/sec YDOT = -1007
187566 meter/sec
ZDOT = -3523
406835 ZDOT = -1110
524224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12723569
81 X = -3878144
08
Y = 6248662
41 feet Y = 1904592
30 meter
Z = 17114208
48 Z = 5216410
75
XDOT = -14346
207701 XDOT = -4372
724107
YDOT = -19095
358328 feet/sec YDOT = -5820
265218 meter/sec
ZDOT = -3680
989316 ZDOT = -1121
965543
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 15256
94004823
00016717 00000-0 10270-3 0 9039
2 25544 51
6426
8826 0001350 342
7880 17
3227 15
55145651 1855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
94004823 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node:
8826 deg
Eccentricity:
0001350
Arg of perigee: 342
7880 deg
Mean anomaly: 17
3227 deg
Mean motion: 15
55145651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 288
Coasting Arc #5 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2015/257/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -694714
63 A = 6777900
68 meter
Y = -4187596
42 meter E =
0009388
Z = -5292203
72 I = 51
62852
XDOT = 7621
258011 Wp = 80
17447
YDOT = -504
882929 meter/sec RA = 359
77763 deg
ZDOT = -600
293089 TA = 184
08609
MA = 184
09376
Ha = 219
279 n
mi
Hp = 216
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2279247
47 X = -622128
78
Y = -13738833
40 feet Y = -4194960
08 meter
Z = -17362873
10 Z = -5295401
60
XDOT = 25004
127332 XDOT = 7629
253298
YDOT = -1656
440055 feet/sec YDOT = -419
612382 meter/sec
ZDOT = -1969
465514 ZDOT = -563
251087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4617638
13 X = -1407456
10
Y = -13121634
07 feet Y = -3999474
06 meter
Z = -17375845
65 Z = -5296157
75
XDOT = 23347
210162 XDOT = 7116
229658
YDOT = -5816
895799 feet/sec YDOT = -1772
989839 meter/sec
ZDOT = -1809
657506 ZDOT = -551
583608
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 15257
06857027
00016717 00000-0 10270-3 0 9046
2 25544 51
6454
2401 0005435 274
5847 85
4684 15
53974623 1874
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
06857027 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node:
2401 deg
Eccentricity:
0005435
Arg of perigee: 274
5847 deg
Mean anomaly: 85
4684 deg
Mean motion: 15
53974623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 314
Coasting Arc #6 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062106
98 A = 6778259
95 meter
Y = 4229404
59 meter E =
0003885
Z = 5191685
63 I = 51
59800
XDOT = -7552
341118 Wp = 328
43261
YDOT = -325
925535 meter/sec RA = 354
77766 deg
ZDOT = -1276
725726 TA = 133
85267
MA = 133
82056
Ha = 219
308 n
mi
Hp = 216
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3484602
94 X = -1134541
57
Y = 13875999
30 feet Y = 4217123
14 meter
Z = 17033089
32 Z = 5186349
57
XDOT = -24778
022042 XDOT = -7541
933366
YDOT = -1069
309498 feet/sec YDOT = -410
322777 meter/sec
ZDOT = -4188
732697 ZDOT = -1313
388259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -778071
00 X = -237156
04
Y = 14314034
39 feet Y = 4362917
68 meter
Z = 17009261
33 Z = 5184422
85
XDOT = -23429
758449 XDOT = -7141
390375
YDOT = 3902
562203 feet/sec YDOT = 1189
500960 meter/sec
ZDOT = -4346
729188 ZDOT = -1324
883057
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 15258
09750815
00016717 00000-0 10270-3 0 9058
2 25544 51
6452 355
1122 0005612 279
1289 80
9229 15
54015432 2031
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09750815 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 355
1122 deg
Eccentricity:
0005612
Arg of perigee: 279
1289 deg
Mean anomaly: 80
9229 deg
Mean motion: 15
54015432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 293
Coasting Arc #7 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2015/259/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2724631
68 A = 6780843
07 meter
Y = -4189344
98 meter E =
0004499
Z = -4587696
13 I = 51
57527
XDOT = 6936
934495 Wp = 118
15127
YDOT = 1192
519332 meter/sec RA = 349
77899 deg
ZDOT = 3031
064392 TA = 182
16941
MA = 182
17136
Ha = 219
472 n
mi
Hp = 216
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8939080
31 X = 2793560
87
Y = -13744570
14 feet Y = -4158491
58 meter
Z = -15051496
50 Z = -4574292
34
XDOT = 22758
971439 XDOT = 6908
360036
YDOT = 3912
465001 feet/sec YDOT = 1269
933353 meter/sec
ZDOT = 9944
436981 ZDOT = 3064
693260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5874935
75 X = 1790680
42
Y = -15364439
62 feet Y = -4683081
20 meter
Z = -14992899
56 Z = -4569835
79
XDOT = 21885
713477 XDOT = 6670
765468
YDOT = -1476
088928 feet/sec YDOT = -449
911905 meter/sec
ZDOT = 10089
174139 ZDOT = 3075
180278
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 15259
06212644
00016717 00000-0 10270-3 0 9060
2 25544 51
6456 350
3045 0005574 283
4212 76
6319 15
54003873 2181
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
06212644 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 350
3045 deg
Eccentricity:
0005574
Arg of perigee: 283
4212 deg
Mean anomaly: 76
6319 deg
Mean motion: 15
54003873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 295
Coasting Arc #8 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4173096
07 A = 6784472
76 meter
Y = 4027582
82 meter E =
0007284
Z = 3516319
32 I = 51
55608
XDOT = -5838
282449 Wp = 73
59068
YDOT = -2113
179604 meter/sec RA = 344
78702 deg
ZDOT = -4498
567786 TA = 64
96069
MA = 64
88508
Ha = 219
643 n
mi
Hp = 216
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13691260
06 X = -4234904
41
Y = 13213854
40 feet Y = 3980571
38 meter
Z = 11536480
70 Z = 3495896
43
XDOT = -19154
469978 XDOT = -5792
365928
YDOT = -6933
003949 feet/sec YDOT = -2178
210971 meter/sec
ZDOT = -14759
080662 ZDOT = -4526
817430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10333964
53 X = -3149792
39
Y = 16040795
19 feet Y = 4889234
37 meter
Z = 11447663
69 Z = 3489247
89
XDOT = -18977
317898 XDOT = -5784
286495
YDOT = -1583
174283 feet/sec YDOT = -482
551521 meter/sec
ZDOT = -14880
440619 ZDOT = -4535
558301
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 15260
09103830
00016717 00000-0 10270-3 0 9072
2 25544 51
6452 345
1764 0005515 288
1671 71
8881 15
54023874 2345
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09103830 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 345
1764 deg
Eccentricity:
0005515
Arg of perigee: 288
1671 deg
Mean anomaly: 71
8881 deg
Mean motion: 15
54023874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 301
Coasting Arc #9 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2015/261/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5270489
34 A = 6787744
97 meter
Y = -3717274
68 meter E =
0007134
Z = -2100909
21 I = 51
53707
XDOT = 4358
245122 Wp = 351
72585
YDOT = 3064
836932 meter/sec RA = 339
80161 deg
ZDOT = 5515
163813 TA = 344
97318
MA = 344
99437
Ha = 219
783 n
mi
Hp = 216
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17291631
70 X = 5321870
61
Y = -12195783
07 feet Y = -3658049
55 meter
Z = -6892746
74 Z = -2075180
74
XDOT = 14298
704468 XDOT = 4296
858620
YDOT = 10055
239278 feet/sec YDOT = 3113
231113 meter/sec
ZDOT = 18094
369464 ZDOT = 5536
186041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13768209
40 X = 4196550
22
Y = -16115220
37 feet Y = -4911919
17 meter
Z = -6781127
61 Z = -2066887
70
XDOT = 15059
102564 XDOT = 4590
014461
YDOT = 5220
514115 feet/sec YDOT = 1591
212702 meter/sec
ZDOT = 18184
384783 ZDOT = 5542
600482
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 15261
05562920
00016717 00000-0 10270-3 0 9089
2 25544 51
6454 340
3679 0005661 292
0552 67
9999 15
54049596 2494
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
05562920 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 340
3679 deg
Eccentricity:
0005661
Arg of perigee: 292
0552 deg
Mean anomaly: 67
9999 deg
Mean motion: 15
54049596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 337
Coasting Arc #10 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/262/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5964445
84 A = 6789554
97 meter
Y = 3202888
00 meter E =
0007622
Z = 454240
01 I = 51
51315
XDOT = -2618
718830 Wp = 141
62085
YDOT = -4021
804162 meter/sec RA = 334
82226 deg
ZDOT = -5979
134063 TA = 33
47290
MA = 33
42474
Ha = 219
874 n
mi
Hp = 216
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19568391
85 X = -6002024
56
Y = 10508162
73 feet Y = 3135979
57 meter
Z = 1490288
76 Z = 425174
03
XDOT = -8591
597211 XDOT = -2544
506757
YDOT = -13194
895544 feet/sec YDOT = -4050
674075 meter/sec
ZDOT = -19616
581573 ZDOT = -5991
674730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16098031
08 X = -4906679
87
Y = 15315228
89 feet Y = 4668081
77 meter
Z = 1364391
21 Z = 415866
44
XDOT = -10540
295167 XDOT = -3212
681967
YDOT = -9311
344138 feet/sec YDOT = -2838
097693 meter/sec
ZDOT = -19669
851258 ZDOT = -5995
370663
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 15262
08451431
00016717 00000-0 10270-3 0 9098
2 25544 51
6451 335
2396 0005574 294
6573 65
3999 15
54025195 2653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
08451431 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 335
2396 deg
Eccentricity:
0005574
Arg of perigee: 294
6573 deg
Mean anomaly: 65
3999 deg
Mean motion: 15
54025195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 325
Coasting Arc #11 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2015/263/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6195258
30 A = 6788740
93 meter
Y = -2467543
48 meter E =
0012067
Z = 1229958
00 I = 51
48243
XDOT = 794
152962 Wp = 33
79550
YDOT = 4912
718585 meter/sec RA = 329
84112 deg
ZDOT = 5838
018960 TA = 339
60885
MA = 339
65699
Ha = 219
940 n
mi
Hp = 216
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20325650
59 X = 6216415
80
Y = -8095615
11 feet Y = -2398145
61 meter
Z = 4035295
26 Z = 1260105
20
XDOT = 2605
488720 XDOT = 710
799600
YDOT = 16117
843127 feet/sec YDOT = 4921
133802 meter/sec
ZDOT = 19153
605512 ZDOT = 5841
673924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17203643
53 X = 5243670
55
Y = -13477248
32 feet Y = -4107865
29 meter
Z = 4165704
12 Z = 1269706
61
XDOT = 5933
379880 XDOT = 1808
494187
YDOT = 13516
172092 feet/sec YDOT = 4119
729254 meter/sec
ZDOT = 19168
406024 ZDOT = 5842
530156
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 15263
11338250
00016717 00000-0 10270-3 0 9108
2 25544 51
6447 330
1099 0005785 300
1816 59
8763 15
54097007 2815
Satellite: ISS
Catalog Number: 25544
Epoch time: 15263
11338250 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 330
1099 deg
Eccentricity:
0005785
Arg of perigee: 300
1816 deg
Mean anomaly: 59
8763 deg
Mean motion: 15
54097007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 297
Coasting Arc #12 (Orbit 295)
---------------------------------------
Vector Time (GMT): 2015/264/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5997406
10 A = 6786027
47 meter
Y = 1487378
84 meter E =
0001267
Z = -2805862
32 I = 51
44578
XDOT = 980
131003 Wp = 321
29956
YDOT = -5647
869688 meter/sec RA = 324
85444 deg
ZDOT = -5086
689570 TA = 250
61860
MA = 250
63230
Ha = 220
164 n
mi
Hp = 216
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19676529
21 X = -5999962
69
Y = 4879851
83 feet Y = 1420297
37 meter
Z = -9205585
04 Z = -2835003
04
XDOT = 3215
652898 XDOT = 1067
923372
YDOT = -18529
756194 feet/sec YDOT = -5636
418762 meter/sec
ZDOT = -16688
614074 ZDOT = -5081
714551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17275516
88 X = -5265577
54
Y = 10497708
73 feet Y = 3199701
62 meter
Z = -9331461
81 Z = -2844229
56
XDOT = -1579
547312 XDOT = -481
446021
YDOT = -17420
306837 feet/sec YDOT = -5309
709524 meter/sec
ZDOT = -16666
082692 ZDOT = -5079
822004
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 15264
07793597
00016717 00000-0 10270-3 0 9114
2 25544 51
6442 325
3019 0005842 303
1003 56
9589 15
54084606 2964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15264
07793597 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 325
3019 deg
Eccentricity:
0005842
Arg of perigee: 303
1003 deg
Mean anomaly: 56
9589 deg
Mean motion: 15
54084606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 296
Checksum: 312
Coasting Arc #13 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2015/265/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5401564
90 A = 6782215
11 meter
Y = -290571
22 meter E =
0005784
Z = 4085297
74 I = 51
40743
XDOT = -2558
357849 Wp = 77
34741
YDOT = 6141
964698 meter/sec RA = 319
85526 deg
ZDOT = 3816
176126 TA = 333
10220
MA = 333
13217
Ha = 220
251 n
mi
Hp = 216
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17721669
63 X = 5384567
79
Y = -953317
65 feet Y = -230262
07 meter
Z = 13403207
80 Z = 4111496
29
XDOT = -8393
562496 XDOT = -2645
386247
YDOT = 20150
802816 feet/sec YDOT = 6112
869160 meter/sec
ZDOT = 12520
262882 ZDOT = 3803
536210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16444346
72 X = 5012236
88
Y = -6442743
53 feet Y = -1963748
23 meter
Z = 13516171
25 Z = 4119729
00
XDOT = -2185
331935 XDOT = -666
089174
YDOT = 20594
303780 feet/sec YDOT = 6277
143792 meter/sec
ZDOT = 12464
609830 ZDOT = 3799
213076
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 15265
10677985
00016717 00000-0 10270-3 0 9122
2 25544 51
6439 320
1720 0005846 309
4270 50
6365 15
54097894 3126
Satellite: ISS
Catalog Number: 25544
Epoch time: 15265
10677985 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 320
1720 deg
Eccentricity:
0005846
Arg of perigee: 309
4270 deg
Mean anomaly: 50
6365 deg
Mean motion: 15
54097894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 312
Coasting Arc #14 (Orbit 326)
---------------------------------------
Vector Time (GMT): 2015/266/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4515765
70 A = 6778783
95 meter
Y = -1069338
14 meter E =
0010607
Z = -4950367
74 I = 51
37151
XDOT = 3834
715568 Wp = 46
18328
YDOT = -6277
889365 meter/sec RA = 314
84463 deg
ZDOT = -2137
627988 TA = 202
86554
MA = 202
91281
Ha = 220
397 n
mi
Hp = 216
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14815504
26 X = -4479425
45
Y = -3508327
25 feet Y = -1119633
65 meter
Z = -16241363
98 Z = -4972216
09
XDOT = 12581
087820 XDOT = 3915
015241
YDOT = -20596
749886 feet/sec YDOT = -6234
558254 meter/sec
ZDOT = -7013
215184 ZDOT = -2118
804101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15045027
88 X = -4585724
50
Y = 1547233
03 feet Y = 471596
63 meter
Z = -16335318
69 Z = -4979005
14
XDOT = 5225
221579 XDOT = 1592
647537
YDOT = -22514
785362 feet/sec YDOT = -6862
506578 meter/sec
ZDOT = -6930
895273 ZDOT = -2112
536879
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 15266
07130609
00016717 00000-0 10270-3 0 9137
2 25544 51
6428 315
3632 0005896 311
8797 48
1852 15
54146356 3275
Satellite: ISS
Catalog Number: 25544
Epoch time: 15266
07130609 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 315
3632 deg
Eccentricity:
0005896
Arg of perigee: 311
8797 deg
Mean anomaly: 48
1852 deg
Mean motion: 15
54146356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 327
Checksum: 316
Coasting Arc #15 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2015/267/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3413957
19 A = 6777310
80 meter
Y = 2512263
08 meter E =
0004109
Z = 5289530
12 I = 51
34500
XDOT = -4766
398693 Wp = 336
43503
YDOT = 6002
099603 meter/sec RA = 309
82555 deg
ZDOT = 229
381074 TA = 111
39155
MA = 111
34769
Ha = 220
487 n
mi
Hp = 216
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11200646
95 X = 3359916
21
Y = 8242332
94 feet Y = 2550138
58 meter
Z = 17354101
43 Z = 5305982
91
XDOT = -15637
790989 XDOT = -4834
275624
YDOT = 19691
927830 feet/sec YDOT = 5948
419093 meter/sec
ZDOT = 752
562580 ZDOT = 206
061408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13259272
93 X = 4041426
39
Y = 3890083
49 feet Y = 1185697
45 meter
Z = 17424531
92 Z = 5310997
33
XDOT = -7565
304480 XDOT = -2305
904806
YDOT = 22925
560365 feet/sec YDOT = 6987
710799 meter/sec
ZDOT = 650
932262 ZDOT = 198
404153
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 15267
10012279
00016717 00000-0 10270-3 0 9145
2 25544 51
6430 310
2341 0005817 316
0030 44
0660 15
54145398 3434
Satellite: ISS
Catalog Number: 25544
Epoch time: 15267
10012279 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 310
2341 deg
Eccentricity:
0005817
Arg of perigee: 316
0030 deg
Mean anomaly: 44
0660 deg
Mean motion: 15
54145398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 263
Coasting Arc #16 (Orbit 357)
---------------------------------------
Vector Time (GMT): 2015/268/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2237804
06 A = 6778154
28 meter
Y = -3901847
29 meter E =
0009311
Z = -5078232
83 I = 51
32700
XDOT = 5310
662364 Wp = 81
01530
YDOT = -5254
580996 meter/sec RA = 304
80286 deg
ZDOT = 1701
220280 TA = 205
48411
MA = 205
53005
Ha = 220
570 n
mi
Hp = 215
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7341876
82 X = -2169338
24
Y = -12801336
25 feet Y = -3926489
69 meter
Z = -16660868
85 Z = -5088936
85
XDOT = 17423
432953 XDOT = 5360
761792
YDOT = -17239
438963 feet/sec YDOT = -5194
913341 meter/sec
ZDOT = 5581
431364 ZDOT = 1727
140706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11385470
70 X = -3470291
47
Y = -9307713
76 feet Y = -2836991
15 meter
Z = -16706269
41 Z = -5092070
92
XDOT = 9274
012337 XDOT = 2826
718960
YDOT = -21540
422819 feet/sec YDOT = -6565
520875 meter/sec
ZDOT = 5694
115866 ZDOT = 1735
566516
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 15268
06462425
00016717 00000-0 10270-3 0 9154
2 25544 51
6414 305
4242 0005805 319
5474 40
5247 15
54194465 3586
Satellite: ISS
Catalog Number: 25544
Epoch time: 15268
06462425 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 305
4242 deg
Eccentricity:
0005805
Arg of perigee: 319
5474 deg
Mean anomaly: 40
5247 deg
Mean motion: 15
54194465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 358
Checksum: 304
Coasting Arc #17 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2015/269/01:14:13
263
Vector Time (MET): N/A
Weight (LBS) : 926318
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1038134
47 A = 6781176
28 meter
Y = 5131568
26 meter E =
0009531
Z = 4309563
65 I = 51
32002
XDOT = -5514
473874 Wp = 36
29453
YDOT = 4040
324041 meter/sec RA = 299
78584 deg
ZDOT = -3471
091217 TA = 89
20683
MA = 89
09763
Ha = 220
707 n
mi
Hp = 215
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3405952
97 X = 959740
63
Y = 16835853
87 feet Y = 5142739
65 meter
Z = 14138988
37 Z = 4314415
57
XDOT = -18092
105885 XDOT = -5542
382661
YDOT = 13255
656303 feet/sec YDOT = 3978
501020 meter/sec
ZDOT = -11388
094544 ZDOT = -3497
947795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9443315
26 X = 2878322
49
Y = 14328482
67 feet Y = 4367321
52 meter
Z = 14158949
97 Z = 4315647
95
XDOT = -10614
634219 XDOT = -3235
340510
YDOT = 18401
343608 feet/sec YDOT = 5608
729532 meter/sec
ZDOT = -11504
574960 ZDOT = -3506
594448
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 15269
09341202
00016717 00000-0 10270-3 0 9168
2 25544 51
6415 300
2950 0005913 322
5257 37
5483 15
54216879 3749
Satellite: ISS
Catalog Number: 25544
Epoch time: 15269
09341202 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 300
2950 deg
Eccentricity:
0005913
Arg of perigee: 322
5257 deg
Mean anomaly: 37
5483 deg
Mean motion: 15
54216879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 301
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