[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 27th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 185 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 80)
---------------------------------------
Vector Time (GMT): 2013/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1948581
99 A = 6799388
78 meter
Y = -6176141
51 meter E =
0009850
Z = 2058138
12 I = 51
30813
XDOT = 4263
623577 Wp = 76
45325
YDOT = 3187
749607 meter/sec RA = 272
76480 deg
ZDOT = 5509
209209 TA = 306
37927
MA = 306
47010
Ha = 226
604 n
mi
Hp = 222
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6392985
53 X = 2007502
40
Y = -20262931
46 feet Y = -6154021
83 meter
Z = 6752421
66 Z = 2067747
00
XDOT = 13988
266330 XDOT = 4200
898765
YDOT = 10458
496085 feet/sec YDOT = 3235
077320 meter/sec
ZDOT = 18074
833362 ZDOT = 5529
768889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20398917
16 X = -6217589
95
Y = 5897820
44 feet Y = 1797655
67 meter
Z = 6793507
66 Z = 2070661
13
XDOT = 1485
090906 XDOT = 452
655708
YDOT = -15857
167070 feet/sec YDOT = -4833
264523 meter/sec
ZDOT = 18160
406637 ZDOT = 5535
291943
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 13207
56037746
00016717 00000-0 10270-3 0 9008
2 25544 51
6490 273
2446 0004304 232
6799 127
3960 15
50055295 818
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
56037746 = yrday
fracday
Element set: 900
Inclination: 51
6490 deg
RA of node: 273
2446 deg
Eccentricity:
0004304
Arg of perigee: 232
6799 deg
Mean anomaly: 127
3960 deg
Mean motion: 15
50055295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 81
Checksum: 300
Coasting Arc #2 (Orbit 95)
---------------------------------------
Vector Time (GMT): 2013/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1689688
30 A = 6798665
07 meter
Y = 6127307
08 meter E =
0006128
Z = -2403105
56 I = 51
30492
XDOT = -4400
963509 Wp = 174
85286
YDOT = -3301
693202 meter/sec RA = 267
78813 deg
ZDOT = -5331
089456 TA = 32
09101
MA = 32
05372
Ha = 226
414 n
mi
Hp = 222
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5543596
80 X = -1746406
11
Y = 20102713
52 feet Y = 6108094
84 meter
Z = -7884204
60 Z = -2411451
46
XDOT = -14438
856658 XDOT = -4337
819497
YDOT = -10832
326777 feet/sec YDOT = -3350
554398 meter/sec
ZDOT = -17490
450971 ZDOT = -5352
315371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19677116
93 X = 5997585
24
Y = -6862657
25 feet Y = -2091737
93 meter
Z = -7919990
09 Z = -2414012
98
XDOT = -1307
575507 XDOT = -398
549015
YDOT = 16511
430773 feet/sec YDOT = 5032
684100 meter/sec
ZDOT = -17578
802049 ZDOT = -5358
018864
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 13208
52743529
00016717 00000-0 10270-3 0 9019
2 25544 51
6484 268
4534 0004210 236
4825 123
5924 15
50079132 963
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
52743529 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node: 268
4534 deg
Eccentricity:
0004210
Arg of perigee: 236
4825 deg
Mean anomaly: 123
5924 deg
Mean motion: 15
50079132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 96
Checksum: 296
Coasting Arc #3 (Orbit 111)
---------------------------------------
Vector Time (GMT): 2013/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1432168
04 A = 6797960
14 meter
Y = -6058847
88 meter E =
0009638
Z = 2720476
29 I = 51
30464
XDOT = 4569
764275 Wp = 86
34444
YDOT = 3390
584027 meter/sec RA = 262
81080 deg
ZDOT = 5130
369269 TA = 304
52134
MA = 304
61230
Ha = 226
326 n
mi
Hp = 222
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4698714
03 X = 1486597
74
Y = -19878109
83 feet Y = -6042528
21 meter
Z = 8925447
15 Z = 2727565
61
XDOT = 14992
664944 XDOT = 4506
588685
YDOT = 11123
963342 feet/sec YDOT = 3441
332650 meter/sec
ZDOT = 16831
920175 ZDOT = 5152
415203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18878872
78 X = -5754280
42
Y = 7762715
28 feet Y = 2366075
62 meter
Z = 8955958
04 Z = 2729776
01
XDOT = 977
812031 XDOT = 298
037107
YDOT = -17204
371089 feet/sec YDOT = -5243
892308 meter/sec
ZDOT = 16923
696659 ZDOT = 5158
342742
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 13209
55895193
00016717 00000-0 10270-3 0 9029
2 25544 51
6483 263
3425 0004106 241
0510 119
0229 15
50087482 1126
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
55895193 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 263
3425 deg
Eccentricity:
0004106
Arg of perigee: 241
0510 deg
Mean anomaly: 119
0229 deg
Mean motion: 15
50087482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 112
Checksum: 279
Coasting Arc #4 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2013/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1215212
11 A = 6797063
76 meter
Y = 5950418
80 meter E =
0003149
Z = -3048922
25 I = 51
30730
XDOT = -4758
390767 Wp = 168
30456
YDOT = -3476
723692 meter/sec RA = 257
83327 deg
ZDOT = -4892
695772 TA = 46
78324
MA = 46
75695
Ha = 226
153 n
mi
Hp = 222
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3986916
38 X = -1266849
96
Y = 19522371
38 feet Y = 5936540
92 meter
Z = -10003025
75 Z = -3054950
79
XDOT = -15611
518263 XDOT = -4695
392435
YDOT = -11406
573792 feet/sec YDOT = -3529
582595 meter/sec
ZDOT = -16052
151483 ZDOT = -4915
658534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18029250
72 X = 5495315
62
Y = -8452380
88 feet Y = -2576285
69 meter
Z = -10029077
06 Z = -3056862
69
XDOT = -564
747229 XDOT = -172
134955
YDOT = 17940
108362 feet/sec YDOT = 5468
145029 meter/sec
ZDOT = -16147
760163 ZDOT = -4921
837298
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 13210
52598841
00016717 00000-0 10270-3 0 9039
2 25544 51
6488 258
5510 0004030 245
1503 114
9228 15
50119685 1275
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
52598841 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 258
5510 deg
Eccentricity:
0004030
Arg of perigee: 245
1503 deg
Mean anomaly: 114
9228 deg
Mean motion: 15
50119685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 127
Checksum: 288
Coasting Arc #5 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2013/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1008437
01 A = 6796262
71 meter
Y = -5824492
98 meter E =
0008940
Z = 3347247
91 I = 51
31126
XDOT = 4974
323503 Wp = 97
43235
YDOT = 3531
921525 meter/sec RA = 252
85566 deg
ZDOT = 4635
388653 TA = 301
71200
MA = 301
79912
Ha = 226
103 n
mi
Hp = 222
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3308520
36 X = 1057232
91
Y = -19109228
92 feet Y = -5812943
33 meter
Z = 10981784
47 Z = 3352264
99
XDOT = 16319
959000 XDOT = 4911
941808
YDOT = 11587
669046 feet/sec YDOT = 3587
198525 meter/sec
ZDOT = 15207
968023 ZDOT = 4659
401932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17136838
59 X = -5223308
40
Y = 9053093
42 feet Y = 2759382
88 meter
Z = 11003580
77 Z = 3353891
42
XDOT = -13
135360 XDOT = -4
003658
YDOT = -18677
981329 feet/sec YDOT = -5693
048709 meter/sec
ZDOT = 15307
974572 ZDOT = 4665
870650
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 13211
55748293
00016717 00000-0 10270-3 0 9042
2 25544 51
6481 253
4401 0003900 249
5793 110
4939 15
50119846 1432
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
55748293 = yrday
fracday
Element set: 904
Inclination: 51
6481 deg
RA of node: 253
4401 deg
Eccentricity:
0003900
Arg of perigee: 249
5793 deg
Mean anomaly: 110
4939 deg
Mean motion: 15
50119846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 143
Checksum: 298
Coasting Arc #6 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2013/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -849817
68 A = 6795263
72 meter
Y = 5669245
59 meter E =
0001703
Z = -3649981
53 I = 51
31932
XDOT = -5201
915522 Wp = 97
25772
YDOT = -3572
066162 meter/sec RA = 247
87818 deg
ZDOT = -4339
033749 TA = 126
21438
MA = 126
19863
Ha = 225
953 n
mi
Hp = 222
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2788115
76 X = -895418
81
Y = 18599887
11 feet Y = 5659487
64 meter
Z = -11975005
02 Z = -3654220
24
XDOT = -17066
651974 XDOT = -5140
507634
YDOT = -11719
377172 feet/sec YDOT = -3629
893656 meter/sec
ZDOT = -14235
675030 ZDOT = -4364
155010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16252183
71 X = 4953665
59
Y = -9442043
91 feet Y = -2877934
98 meter
Z = -11993517
69 Z = -3655624
19
XDOT = 692
500717 XDOT = 211
074219
YDOT = 19399
252523 feet/sec YDOT = 5912
892169 meter/sec
ZDOT = -14340
324396 ZDOT = -4370
930876
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 13212
52449803
00016717 00000-0 10270-3 0 9056
2 25544 51
6492 248
6488 0003908 253
7885 106
2836 15
50156343 1580
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
52449803 = yrday
fracday
Element set: 905
Inclination: 51
6492 deg
RA of node: 248
6488 deg
Eccentricity:
0003908
Arg of perigee: 253
7885 deg
Mean anomaly: 106
2836 deg
Mean motion: 15
50156343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 158
Checksum: 320
Coasting Arc #7 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2013/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 709294
29 A = 6794408
48 meter
Y = -5501076
69 meter E =
0007725
Z = 3919914
73 I = 51
32745
XDOT = 5450
037619 Wp = 109
85486
YDOT = 3577
705277 meter/sec RA = 242
90061 deg
ZDOT = 4025
599633 TA = 297
81120
MA = 297
88947
Ha = 225
933 n
mi
Hp = 222
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2327081
00 X = 751714
15
Y = -18048151
86 feet Y = -5492907
99 meter
Z = 12860612
64 Z = 3923463
05
XDOT = 17880
700850 XDOT = 5390
070840
YDOT = 11737
878204 feet/sec YDOT = 3638
315483 meter/sec
ZDOT = 13207
347877 ZDOT = 4051
929699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15364842
03 X = -4683203
85
Y = 9729920
63 feet Y = 2965679
81 meter
Z = 12876207
64 Z = 3924668
09
XDOT = -1532
362919 XDOT = -467
064218
YDOT = -20082
429821 feet/sec YDOT = -6121
124609 meter/sec
ZDOT = 13317
069338 ZDOT = 4059
042734
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 13213
55597034
00016717 00000-0 10270-3 0 9061
2 25544 51
6477 243
5377 0003765 258
4062 101
6667 15
50153831 1742
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
55597034 = yrday
fracday
Element set: 906
Inclination: 51
6477 deg
RA of node: 243
5377 deg
Eccentricity:
0003765
Arg of perigee: 258
4062 deg
Mean anomaly: 101
6667 deg
Mean motion: 15
50153831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 174
Checksum: 307
Coasting Arc #8 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2013/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -621238
16 A = 6793401
16 meter
Y = 5316803
24 meter E =
0004128
Z = -4187333
87 I = 51
34010
XDOT = -5698
302251 Wp = 59
38864
YDOT = -3558
365010 meter/sec RA = 237
92372 deg
ZDOT = -3673
423788 TA = 172
70657
MA = 172
70056
Ha = 225
813 n
mi
Hp = 222
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2038182
94 X = -660305
00
Y = 17443580
20 feet Y = 5309638
01 meter
Z = -13737972
00 Z = -4190446
28
XDOT = -18695
217360 XDOT = -5640
244090
YDOT = -11674
425885 feet/sec YDOT = -3621
762163 meter/sec
ZDOT = -12051
915315 ZDOT = -3700
964450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14544060
22 X = 4433029
56
Y = -9824728
57 feet Y = -2994577
27 meter
Z = -13751711
72 Z = -4191521
73
XDOT = 2471
047036 XDOT = 753
175137
YDOT = 20684
841177 feet/sec YDOT = 6304
739591 meter/sec
ZDOT = -12166
722271 ZDOT = -3708
416948
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 13214
52296400
00016717 00000-0 10270-3 0 9073
2 25544 51
6486 238
7464 0003856 262
4257 97
6456 15
50188064 1899
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
52296400 = yrday
fracday
Element set: 907
Inclination: 51
6486 deg
RA of node: 238
7464 deg
Eccentricity:
0003856
Arg of perigee: 262
4257 deg
Mean anomaly: 97
6456 deg
Mean motion: 15
50188064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 189
Checksum: 326
Coasting Arc #9 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2013/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 557645
16 A = 6792548
44 meter
Y = -5126091
05 meter E =
0006032
Z = 4419258
03 I = 51
35271
XDOT = 5958
212824 Wp = 124
19131
YDOT = 3504
049284 meter/sec RA = 232
94648 deg
ZDOT = 3306
088910 TA = 292
24008
MA = 292
30406
Ha = 225
805 n
mi
Hp = 222
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1829544
48 X = 593457
58
Y = -16817884
04 feet Y = -5119655
15 meter
Z = 14498878
05 Z = 4422053
64
XDOT = 19547
942336 XDOT = 5902
527145
YDOT = 11496
224686 feet/sec YDOT = 3570
366228 meter/sec
ZDOT = 10846
748392 ZDOT = 3334
897843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13762488
45 X = -4194806
48
Y = 9819530
30 feet Y = 2992992
84 meter
Z = 14511259
68 Z = 4423031
95
XDOT = -3547
718888 XDOT = -1081
344717
YDOT = -21210
940991 feet/sec YDOT = -6465
094814 meter/sec
ZDOT = 10966
889130 ZDOT = 3342
707807
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 13215
55441365
00016717 00000-0 10270-3 0 9080
2 25544 51
6469 233
6348 0003748 267
4234 92
6488 15
50188710 2052
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
55441365 = yrday
fracday
Element set: 908
Inclination: 51
6469 deg
RA of node: 233
6348 deg
Eccentricity:
0003748
Arg of perigee: 267
4234 deg
Mean anomaly: 92
6488 deg
Mean motion: 15
50188710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 205
Checksum: 316
Coasting Arc #10 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2013/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -546461
00 A = 6791632
01 meter
Y = 4934211
44 meter E =
0006904
Z = -4641646
87 I = 51
36945
XDOT = -6204
494441 Wp = 59
08161
YDOT = -3418
361979 meter/sec RA = 227
97049 deg
ZDOT = -2903
113870 TA = 181
87646
MA = 181
87906
Ha = 225
743 n
mi
Hp = 222
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1792851
06 X = -579048
39
Y = 16188357
75 feet Y = 4927918
61 meter
Z = -15228500
23 Z = -4644380
37
XDOT = -20355
952892 XDOT = -6151
706174
YDOT = -11215
098355 feet/sec YDOT = -3487
449253 meter/sec
ZDOT = -9524
651804 ZDOT = -2933
126128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13098823
75 X = 3992521
48
Y = -9660730
09 feet Y = -2944590
53 meter
Z = -15240589
60 Z = -4645331
71
XDOT = 4698
818539 XDOT = 1432
199891
YDOT = 21595
803066 feet/sec YDOT = 6582
400775 meter/sec
ZDOT = -9649
860154 ZDOT = -2941
277375
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 13216
52138581
00016717 00000-0 10270-3 0 9092
2 25544 51
6472 228
8434 0003852 271
1327 88
9382 15
50216282 2203
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
52138581 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 228
8434 deg
Eccentricity:
0003852
Arg of perigee: 271
1327 deg
Mean anomaly: 88
9382 deg
Mean motion: 15
50216282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 220
Checksum: 299
Coasting Arc #11 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2013/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 564078
01 A = 6790857
66 meter
Y = -4743509
60 meter E =
0004005
Z = 4825775
86 I = 51
38693
XDOT = 6452
209177 Wp = 142
05153
YDOT = 3300
833276 meter/sec RA = 222
99421 deg
ZDOT = 2486
173695 TA = 283
39028
MA = 283
43492
Ha = 225
731 n
mi
Hp = 222
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1850649
65 X = 593637
22
Y = -15562695
53 feet Y = -4737036
63 meter
Z = 15832597
98 Z = 4828587
66
XDOT = 21168
665278 XDOT = 6402
742092
YDOT = 10829
505500 feet/sec YDOT = 3372
709282 meter/sec
ZDOT = 8156
737845 ZDOT = 2517
397271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12513096
24 X = -3813991
73
Y = 9415544
67 feet Y = 2869858
02 meter
Z = 15844983
31 Z = 4829550
91
XDOT = -5948
180139 XDOT = -1813
005306
YDOT = -21874
094872 feet/sec YDOT = -6667
224117 meter/sec
ZDOT = 8287
052219 ZDOT = 2525
893516
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 13217
55281225
00016717 00000-0 10270-3 0 9102
2 25544 51
6459 223
7313 0003826 276
3595 83
7120 15
50223222 2365
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
55281225 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 223
7313 deg
Eccentricity:
0003826
Arg of perigee: 276
3595 deg
Mean anomaly: 83
7120 deg
Mean motion: 15
50223222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 281
Coasting Arc #12 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2013/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -628997
10 A = 6790121
10 meter
Y = 4567031
79 meter E =
0009245
Z = -4993720
95 I = 51
40775
XDOT = -6671
761035 Wp = 64
71455
YDOT = -3150
022525 meter/sec RA = 218
01954 deg
ZDOT = -2039
610751 TA = 185
34866
MA = 185
35855
Ha = 225
754 n
mi
Hp = 222
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2063638
77 X = -655762
27
Y = 14983700
08 feet Y = 4559848
39 meter
Z = -16383598
90 Z = -4996841
41
XDOT = -21888
979772 XDOT = -6626
133272
YDOT = -10334
719570 feet/sec YDOT = -3224
375220 meter/sec
ZDOT = -6691
636321 ZDOT = -2071
910115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12081918
35 X = 3682568
71
Y = -9074674
46 feet Y = -2765960
77 meter
Z = -16397247
29 Z = -4997880
97
XDOT = 7227
842969 XDOT = 2203
046537
YDOT = 21963
346012 feet/sec YDOT = 6694
427865 meter/sec
ZDOT = -6826
493423 ZDOT = -2080
715195
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 13218
51976272
00016717 00000-0 10270-3 0 9113
2 25544 51
6458 218
9395 0003870 279
9819 80
0895 15
50244226 2510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
51976272 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 218
9395 deg
Eccentricity:
0003870
Arg of perigee: 279
9819 deg
Mean anomaly: 80
0895 deg
Mean motion: 15
50244226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 327
Coasting Arc #13 (Orbit 266)
---------------------------------------
Vector Time (GMT): 2013/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 724662
91 A = 6789513
73 meter
Y = -4399625
28 meter E =
0001872
Z = 5120325
43 I = 51
43008
XDOT = 6882
151495 Wp = 171
61452
YDOT = 2974
243870 meter/sec RA = 213
04523 deg
ZDOT = 1579
714261 TA = 263
08489
MA = 263
10618
Ha = 225
737 n
mi
Hp = 222
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2377503
00 X = 748933
98
Y = -14434466
13 feet Y = -4391385
94 meter
Z = 16798967
94 Z = 5123904
65
XDOT = 22579
237189 XDOT = 6840
707691
YDOT = 9758
017947 feet/sec YDOT = 3050
972719 meter/sec
ZDOT = 5182
789570 ZDOT = 1613
045786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11759539
27 X = -3584307
57
Y = 8671628
34 feet Y = 2643112
32 meter
Z = 16814510
24 Z = 5125062
72
XDOT = -8552
109157 XDOT = -2606
682871
YDOT = -21928
972330 feet/sec YDOT = -6683
950766 meter/sec
ZDOT = 5322
009005 ZDOT = 1622
148345
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 13219
55116543
00016717 00000-0 10270-3 0 9126
2 25544 51
6453 213
8272 0003932 285
0689 75
0026 15
50257553 2679
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
55116543 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 213
8272 deg
Eccentricity:
0003932
Arg of perigee: 285
0689 deg
Mean anomaly: 75
0026 deg
Mean motion: 15
50257553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 267
Checksum: 299
Coasting Arc #14 (Orbit 281)
---------------------------------------
Vector Time (GMT): 2013/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -857449
08 A = 6789029
65 meter
Y = 4260680
79 meter E =
0010855
Z = -5225092
45 I = 51
45503
XDOT = -7050
906092 Wp = 72
03403
YDOT = -2768
282841 meter/sec RA = 208
07265 deg
ZDOT = -1098
873308 TA = 187
38081
MA = 187
39680
Ha = 225
835 n
mi
Hp = 222
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2813153
14 X = -879647
60
Y = 13978611
52 feet Y = 4250968
05 meter
Z = -17142691
77 Z = -5229311
77
XDOT = -23132
894001 XDOT = -7014
088582
YDOT = -9082
292786 feet/sec YDOT = -2846
924699 meter/sec
ZDOT = -3605
227389 ZDOT = -1133
035862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11607547
42 X = 3537980
45
Y = -8243536
84 feet Y = -2512630
03 meter
Z = -17160892
60 Z = -5230640
07
XDOT = 9848
126792 XDOT = 3001
709046
YDOT = 21678
712197 feet/sec YDOT = 6607
671478 meter/sec
ZDOT = -3747
969178 ZDOT = -1142
381005
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 13220
51809368
00016717 00000-0 10270-3 0 9139
2 25544 51
6454 209
0349 0003908 288
8763 71
1964 15
50275233 2829
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
51809368 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 209
0349 deg
Eccentricity:
0003908
Arg of perigee: 288
8763 deg
Mean anomaly: 71
1964 deg
Mean motion: 15
50275233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 282
Checksum: 312
Coasting Arc #15 (Orbit 297)
---------------------------------------
Vector Time (GMT): 2013/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924479
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1020285
85 A = 6788676
03 meter
Y = -4138085
67 meter E =
0001054
Z = 5284912
51 I = 51
48161
XDOT = 7200
474308 Wp = 287
63116
YDOT = 2547
755480 meter/sec RA = 203
10141 deg
ZDOT = 605
207361 TA = 156
57696
MA = 156
57216
Ha = 225
819 n
mi
Hp = 222
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3347394
53 X = 1040810
73
Y = -13576396
54 feet Y = -4126561
27 meter
Z = 17338951
80 Z = 5289918
86
XDOT = 23623
603373 XDOT = 7168
509709
YDOT = 8358
777820 feet/sec YDOT = 2628
097039 meter/sec
ZDOT = 1985
588455 ZDOT = 640
108346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11583287
55 X = -3530586
05
Y = 7784969
02 feet Y = 2372858
56 meter
Z = 17360430
57 Z = 5291459
24
XDOT = -11126
140878 XDOT = -3391
247740
YDOT = -21304
770493 feet/sec YDOT = -6493
694046 meter/sec
ZDOT = 2131
464995 ZDOT = 649
670531
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 13221
54947209
00016717 00000-0 10270-3 0 9141
2 25544 51
6454 203
9230 0004022 293
5152 66
5575 15
50293464 2983
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
54947209 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 203
9230 deg
Eccentricity:
0004022
Arg of perigee: 293
5152 deg
Mean anomaly: 66
5575 deg
Mean motion: 15
50293464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 298
Checksum: 298
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