[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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
119/07:49:45
098 -0
3 4
0 4
0
N/A -2
5 0
0 227
2
000/00:09:30
196 -3
1 0
2 222
3
Coasting Arc #1 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2014/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924085
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380936
40 A = 6789477
37 meter
Y = -3186862
33 meter E =
0012500
Z = -4961934
19 I = 51
54623
XDOT = 6464
129632 Wp = 52
36994
YDOT = -3475
748808 meter/sec RA = 345
30282 deg
ZDOT = -2168
448490 TA = 196
39763
MA = 196
43810
Ha = 226
719 n
mi
Hp = 220
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11092311
01 X = -3320944
92
Y = -10455585
08 feet Y = -3224334
92 meter
Z = -16279311
64 Z = -4978212
78
XDOT = 21207
774383 XDOT = 6513
049653
YDOT = -11403
375354 feet/sec YDOT = -3403
189329 meter/sec
ZDOT = -7114
332317 ZDOT = -2136
927033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15021779
48 X = -4578638
38
Y = -2116008
04 feet Y = -644959
25 meter
Z = -16347576
63 Z = -4982741
36
XDOT = 10503
075633 XDOT = 3201
337453
YDOT = -20540
544013 feet/sec YDOT = -6260
757815 meter/sec
ZDOT = -6980
428792 ZDOT = -2127
634696
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 14118
51984687
00016717 00000-0 10270-3 0 9000
2 25544 51
6484 345
7355 0004667 333
7498 26
3415 15
50488295 3621
Satellite: ISS
Catalog Number: 25544
Epoch time: 14118
51984687 = yrday
fracday
Element set: 900
Inclination: 51
6484 deg
RA of node: 345
7355 deg
Eccentricity:
0004667
Arg of perigee: 333
7498 deg
Mean anomaly: 26
3415 deg
Mean motion: 15
50488295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 335
Coasting Arc #2 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2014/119/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6475903
89 A = 6800383
87 meter
Y = 528239
84 meter E =
0004634
Z = -2000616
72 I = 51
55024
XDOT = 1297
948240 Wp = 150
05417
YDOT = -5105
132782 meter/sec RA = 341
18548 deg
ZDOT = -5558
852266 TA = 52
01695
MA = 51
97511
Ha = 227
208 n
mi
Hp = 222
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21246403
82 X = -6471610
91
Y = 1733070
35 feet Y = 455846
07 meter
Z = -6563703
15 Z = -2032066
01
XDOT = 4258
360369 XDOT = 1381
942220
YDOT = -16749
123301 feet/sec YDOT = -5090
148816 meter/sec
ZDOT = -18237
704285 ZDOT = -5552
342714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19950493
30 X = -6080910
36
Y = -7390972
12 feet Y = -2252768
30 meter
Z = -6696772
04 Z = -2041176
12
XDOT = 10502
717122 XDOT = 3201
228179
YDOT = -11878
773612 feet/sec YDOT = -3620
650197 meter/sec
ZDOT = -18209
269554 ZDOT = -5550
185360
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 14119
35775386
00016717 00000-0 10270-3 0 9018
2 25544 51
6481 341
5815 0002250 296
1326 63
9593 15
49730542 3752
Satellite: ISS
Catalog Number: 25544
Epoch time: 14119
35775386 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 341
5815 deg
Eccentricity:
0002250
Arg of perigee: 296
1326 deg
Mean anomaly: 63
9593 deg
Mean motion: 15
49730542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 314
Coasting Arc #3 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2014/120/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6359698
73 A = 6799927
12 meter
Y = -869459
20 meter E =
0012438
Z = 2224313
01 I = 51
51933
XDOT = -1192
881326 Wp = 63
47861
YDOT = 5256
972874 meter/sec RA = 336
22631 deg
ZDOT = 5447
342228 TA = 321
24654
MA = 321
33569
Ha = 227
182 n
mi
Hp = 222
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20865153
30 X = 6358143
32
Y = -2852556
44 feet Y = -798349
65 meter
Z = 7297614
87 Z = 2255204
41
XDOT = -3913
652643 XDOT = -1278
039318
YDOT = 17247
286333 feet/sec YDOT = 5243
157215 meter/sec
ZDOT = 17871
857703 ZDOT = 5441
340362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20177774
83 X = 6150185
77
Y = 5867148
33 feet Y = 1788306
81 meter
Z = 7428381
84 Z = 2264170
79
XDOT = -10268
605951 XDOT = -3129
871094
YDOT = 12646
388737 feet/sec YDOT = 3854
619287 meter/sec
ZDOT = 17845
541228 ZDOT = 5439
320966
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 14120
38949947
00016717 00000-0 10270-3 0 9020
2 25544 51
6476 336
4720 0002296 301
2853 58
8072 15
49750167 3915
Satellite: ISS
Catalog Number: 25544
Epoch time: 14120
38949947 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 336
4720 deg
Eccentricity:
0002296
Arg of perigee: 301
2853 deg
Mean anomaly: 58
8072 deg
Mean motion: 15
49750167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 319
Coasting Arc #4 (Orbit 405)
---------------------------------------
Vector Time (GMT): 2014/121/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6223631
14 A = 6799317
27 meter
Y = 1165378
41 meter E =
0002936
Z = -2476051
53 I = 51
49042
XDOT = 1094
250190 Wp = 135
28634
YDOT = -5413
230969 meter/sec RA = 331
26487 deg
ZDOT = -5304
108261 TA = 72
45115
MA = 72
41907
Ha = 227
181 n
mi
Hp = 222
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20418737
33 X = -6224172
01
Y = 3823419
99 feet Y = 1095778
77 meter
Z = -8123528
64 Z = -2506286
93
XDOT = 3590
059678 XDOT = 1180
466977
YDOT = -17759
944124 feet/sec YDOT = -5400
512250 meter/sec
ZDOT = -17401
929991 ZDOT = -5298
583075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20239862
64 X = -6169110
13
Y = -4449112
33 feet Y = -1356089
44 meter
Z = -8251572
70 Z = -2515079
36
XDOT = 10027
602548 XDOT = 3056
413256
YDOT = -13423
268409 feet/sec YDOT = -4091
412211 meter/sec
ZDOT = -17377
600618 ZDOT = -5296
692668
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 14121
35674229
00016717 00000-0 10270-3 0 9037
2 25544 51
6483 331
6817 0002380 303
6366 56
4558 15
49784294 4064
Satellite: ISS
Catalog Number: 25544
Epoch time: 14121
35674229 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 331
6817 deg
Eccentricity:
0002380
Arg of perigee: 303
6366 deg
Mean anomaly: 56
4558 deg
Mean motion: 15
49784294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 406
Checksum: 315
Coasting Arc #5 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2014/122/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6059079
63 A = 6798749
36 meter
Y = -1450354
94 meter E =
0012050
Z = 2705648
04 I = 51
46173
XDOT = -972
273353 Wp = 69
69600
YDOT = 5585
649614 meter/sec RA = 326
30094 deg
ZDOT = 5156
896225 TA = 320
91823
MA = 321
00522
Ha = 227
152 n
mi
Hp = 222
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19878870
19 X = 6061704
12
Y = -4758382
34 feet Y = -1382583
80 meter
Z = 8876798
03 Z = 2735089
02
XDOT = -3189
873205 XDOT = -1059
712038
YDOT = 18325
622093 feet/sec YDOT = 5574
288024 meter/sec
ZDOT = 16918
950871 ZDOT = 5151
960713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20159478
67 X = 6144609
10
Y = 3029364
66 feet Y = 923350
35 meter
Z = 9001532
94 Z = 2743667
24
XDOT = -9711
863842 XDOT = -2960
176099
YDOT = 14280
606156 feet/sec YDOT = 4352
728756 meter/sec
ZDOT = 16897
084889 ZDOT = 5150
231474
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 14122
38845017
00016717 00000-0 10270-3 0 9047
2 25544 51
6481 326
5718 0002417 309
6801 50
4136 15
49806191 4221
Satellite: ISS
Catalog Number: 25544
Epoch time: 14122
38845017 = yrday
fracday
Element set: 904
Inclination: 51
6481 deg
RA of node: 326
5718 deg
Eccentricity:
0002417
Arg of perigee: 309
6801 deg
Mean anomaly: 50
4136 deg
Mean motion: 15
49806191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 292
Coasting Arc #6 (Orbit 436)
---------------------------------------
Vector Time (GMT): 2014/123/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5884226
94 A = 6798049
21 meter
Y = 1686614
97 meter E =
0002286
Z = -2959190
83 I = 51
43517
XDOT = 849
207991 Wp = 88
76044
YDOT = -5758
320654 meter/sec RA = 321
33516 deg
ZDOT = -4973
907812 TA = 125
06369
MA = 125
04224
Ha = 227
168 n
mi
Hp = 222
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19305206
51 X = -5888274
74
Y = 5533513
67 feet Y = 1620791
20 meter
Z = -9708631
33 Z = -2987785
74
XDOT = 2786
115455 XDOT = 937
697683
YDOT = -18892
128130 feet/sec YDOT = -5748
329366 meter/sec
ZDOT = -16318
595183 ZDOT = -4969
567631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19946859
88 X = -6079802
89
Y = -1750861
03 feet Y = -533662
44 meter
Z = -9829830
15 Z = -2996132
23
XDOT = 9355
917982 XDOT = 2851
683801
YDOT = -15139
681154 feet/sec YDOT = -4614
574816 meter/sec
ZDOT = -16299
218397 ZDOT = -4968
001768
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 14123
35565745
00016717 00000-0 10270-3 0 9053
2 25544 51
6488 321
7815 0002555 310
4805 49
6122 15
49836358 4379
Satellite: ISS
Catalog Number: 25544
Epoch time: 14123
35565745 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 321
7815 deg
Eccentricity:
0002555
Arg of perigee: 310
4805 deg
Mean anomaly: 49
6122 deg
Mean motion: 15
49836358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 437
Checksum: 316
Coasting Arc #7 (Orbit 452)
---------------------------------------
Vector Time (GMT): 2014/124/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5685617
15 A = 6797374
04 meter
Y = -1904266
38 meter E =
0011300
Z = 3189187
90 I = 51
40945
XDOT = -700
208151 Wp = 76
15436
YDOT = 5945
000147 meter/sec RA = 316
36689 deg
ZDOT = 4786
426621 TA = 320
77207
MA = 320
85390
Ha = 227
144 n
mi
Hp = 221
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18653599
59 X = 5690996
31
Y = -6247593
09 feet Y = -1840656
15 meter
Z = 10463214
88 Z = 3216821
14
XDOT = -2297
270837 XDOT = -789
885614
YDOT = 19504
593657 feet/sec YDOT = 5936
668451 meter/sec
ZDOT = 15703
499414 ZDOT = 4782
807379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19602596
35 X = 5974871
37
Y = 511599
44 feet Y = 155935
51 meter
Z = 10580384
91 Z = 3224901
32
XDOT = -8906
847346 XDOT = -2714
807071
YDOT = 16069
761625 feet/sec YDOT = 4898
063343 meter/sec
ZDOT = 15687
142517 ZDOT = 4781
441039
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 14124
38732769
00016717 00000-0 10270-3 0 9060
2 25544 51
6488 316
6714 0002590 317
7437 42
3514 15
49861470 4536
Satellite: ISS
Catalog Number: 25544
Epoch time: 14124
38732769 = yrday
fracday
Element set: 906
Inclination: 51
6488 deg
RA of node: 316
6714 deg
Eccentricity:
0002590
Arg of perigee: 317
7437 deg
Mean anomaly: 42
3514 deg
Mean motion: 15
49861470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 453
Checksum: 320
Coasting Arc #8 (Orbit 467)
---------------------------------------
Vector Time (GMT): 2014/125/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5487483
76 A = 6796593
90 meter
Y = 2072193
59 meter E =
0003817
Z = -3438240
19 I = 51
38568
XDOT = 543
625842 Wp = 54
00118
YDOT = -6124
690699 meter/sec RA = 311
39710 deg
ZDOT = -4560
292294 TA = 166
32872
MA = 166
31837
Ha = 227
175 n
mi
Hp = 221
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18003555
64 X = -5493545
64
Y = 6798535
40 feet Y = 2010795
18 meter
Z = -11280315
59 Z = -3464912
55
XDOT = 1783
549350 XDOT = 634
225745
YDOT = -20094
129590 feet/sec YDOT = -6118
104892 meter/sec
ZDOT = -14961
588890 ZDOT = -4557
431431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19169475
08 X = -5842856
00
Y = 560477
75 feet Y = 170833
62 meter
Z = -11393450
26 Z = -3472723
64
XDOT = 8385
571127 XDOT = 2555
922080
YDOT = -16979
167418 feet/sec YDOT = -5175
250229 meter/sec
ZDOT = -14948
413459 ZDOT = -4556
276422
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 14125
35449935
00016717 00000-0 10270-3 0 9079
2 25544 51
6491 311
8811 0002764 317
1688 42
9247 15
49890594 4684
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
35449935 = yrday
fracday
Element set: 907
Inclination: 51
6491 deg
RA of node: 311
8811 deg
Eccentricity:
0002764
Arg of perigee: 317
1688 deg
Mean anomaly: 42
9247 deg
Mean motion: 15
49890594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 468
Checksum: 337
Coasting Arc #9 (Orbit 483)
---------------------------------------
Vector Time (GMT): 2014/126/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5272135
41 A = 6795842
88 meter
Y = -2214643
93 meter E =
0010171
Z = 3662013
21 I = 51
36347
XDOT = -360
126595 Wp = 82
60476
YDOT = 6315
115849 meter/sec RA = 306
42480 deg
ZDOT = 4328
526564 TA = 321
05708
MA = 321
13030
Ha = 227
163 n
mi
Hp = 221
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17297032
19 X = 5278719
20
Y = -7265892
16 feet Y = -2155650
73 meter
Z = 12014479
02 Z = 3687640
69
XDOT = -1181
517700 XDOT = -451
743645
YDOT = 20718
884019 feet/sec YDOT = 6310
576407 meter/sec
ZDOT = 14201
202639 ZDOT = 4326
554594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18626247
02 X = 5677280
09
Y = -1555227
72 feet Y = -474033
41 meter
Z = 12123217
65 Z = 3695156
74
XDOT = -7758
082095 XDOT = -2364
663423
YDOT = 17941
887559 feet/sec YDOT = 5468
687328 meter/sec
ZDOT = 14191
760286 ZDOT = 4325
648535
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 14126
38613188
00016717 00000-0 10270-3 0 9087
2 25544 51
6490 306
7707 0002804 325
2850 34
8117 15
49914592 4845
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
38613188 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 306
7707 deg
Eccentricity:
0002804
Arg of perigee: 325
2850 deg
Mean anomaly: 34
8117 deg
Mean motion: 15
49914592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 484
Checksum: 316
Coasting Arc #10 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2014/127/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5068729
45 A = 6794996
52 meter
Y = 2309344
65 meter E =
0006227
Z = -3899283
00 I = 51
34299
XDOT = 164
629138 Wp = 46
82378
YDOT = -6488
667233 meter/sec RA = 301
45108 deg
ZDOT = -4056
844496 TA = 180
43240
MA = 180
43294
Ha = 227
206 n
mi
Hp = 221
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16629689
80 X = -5075234
72
Y = 7576590
06 feet Y = 2252626
47 meter
Z = -12792923
24 Z = -3923922
20
XDOT = 540
121843 XDOT = 256
881660
YDOT = -21288
278323 feet/sec YDOT = -6486
310456 meter/sec
ZDOT = -13309
857271 ZDOT = -4055
820626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18045705
51 X = -5500331
04
Y = 2370084
40 feet Y = 722401
72 meter
Z = -12897495
78 Z = -3931156
71
XDOT = 7033
600318 XDOT = 2143
841377
YDOT = -18847
357978 feet/sec YDOT = -5744
674712 meter/sec
ZDOT = -13304
402476 ZDOT = -4055
181875
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 14127
35326759
00016717 00000-0 10270-3 0 9091
2 25544 51
6486 301
9802 0002973 324
0618 36
0332 15
49948938 4999
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
35326759 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 301
9802 deg
Eccentricity:
0002973
Arg of perigee: 324
0618 deg
Mean anomaly: 36
0332 deg
Mean motion: 15
49948938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 334
Coasting Arc #11 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2014/128/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4856205
13 A = 6794220
40 meter
Y = -2373136
61 meter E =
0008682
Z = 4108966
80 I = 51
32493
XDOT = 56
784688 Wp = 88
64426
YDOT = 6668
848928 meter/sec RA = 296
47499 deg
ZDOT = 3777
749136 TA = 322
17758
MA = 322
23856
Ha = 227
204 n
mi
Hp = 221
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15932431
53 X = 4862420
92
Y = -7785881
26 feet Y = -2318796
59 meter
Z = 13480862
21 Z = 4132572
92
XDOT = 186
301469 XDOT = -36
143381
YDOT = 21879
425618 feet/sec YDOT = 6668
964398 meter/sec
ZDOT = 12394
190080 ZDOT = 3777
799172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17386445
02 X = 5299388
44
Y = -3076027
00 feet Y = -937573
03 meter
Z = 13581073
41 Z = 4139511
18
XDOT = -6198
093272 XDOT = -1889
178829
YDOT = 19781
651021 feet/sec YDOT = 6029
447231 meter/sec
ZDOT = 12393
254175 ZDOT = 3777
463873
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 14128
38486218
00016717 00000-0 10270-3 0 9104
2 25544 51
6484 296
8695 0003024 332
1183 27
9805 15
49965877 5158
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
38486218 = yrday
fracday
Element set: 910
Inclination: 51
6484 deg
RA of node: 296
8695 deg
Eccentricity:
0003024
Arg of perigee: 332
1183 deg
Mean anomaly: 27
9805 deg
Mean motion: 15
49965877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 336
Coasting Arc #12 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2014/129/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4667005
38 A = 6793340
54 meter
Y = 2394529
91 meter E =
0008789
Z = -4326138
45 I = 51
30846
XDOT = -291
588901 Wp = 48
60762
YDOT = -6820
520555 meter/sec RA = 291
49744 deg
ZDOT = -3459
508086 TA = 185
99727
MA = 186
00780
Ha = 227
258 n
mi
Hp = 221
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15311697
45 X = -4672419
46
Y = 7856069
26 feet Y = 2342310
09 meter
Z = -14193367
60 Z = -4348823
57
XDOT = -956
656499 XDOT = -198
493244
YDOT = -22377
035940 feet/sec YDOT = -6823
260836 meter/sec
ZDOT = -11350
092146 ZDOT = -3460
698327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16745800
06 X = -5104119
86
Y = 3605648
22 feet Y = 1099001
58 meter
Z = -14289683
99 Z = -4355495
68
XDOT = 5253
810337 XDOT = 1601
361391
YDOT = -20611
197071 feet/sec YDOT = -6282
292867 meter/sec
ZDOT = -11353
960273 ZDOT = -3460
687091
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 14129
35196166
00016717 00000-0 10270-3 0 9113
2 25544 51
6474 292
0783 0003150 331
2052 28
8924 15
50010011 5300
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
35196166 = yrday
fracday
Element set: 911
Inclination: 51
6474 deg
RA of node: 292
0783 deg
Eccentricity:
0003150
Arg of perigee: 331
2052 deg
Mean anomaly: 28
8924 deg
Mean motion: 15
50010011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 267
Coasting Arc #13 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2014/130/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477831
65 A = 6792598
38 meter
Y = -2381650
50 meter E =
0006908
Z = 4512629
87 I = 51
29541
XDOT = 548
998855 Wp = 93
23027
YDOT = 6974
264440 meter/sec RA = 286
51798 deg
ZDOT = 3131
526888 TA = 325
17692
MA = 325
22211
Ha = 227
257 n
mi
Hp = 221
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14691048
73 X = 4482209
77
Y = -7813813
98 feet Y = -2331551
92 meter
Z = 14805216
12 Z = 4534393
56
XDOT = 1801
177345 XDOT = 455
758068
YDOT = 22881
445014 feet/sec YDOT = 6979
882433 meter/sec
ZDOT = 10274
038347 ZDOT = 3133
967244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16065447
46 X = 4896748
39
Y = -4004875
52 feet Y = -1220686
06 meter
Z = 14897630
55 Z = 4540797
79
XDOT = -4204
594437 XDOT = -1281
560385
YDOT = 21440
629134 feet/sec YDOT = 6535
103760 meter/sec
ZDOT = 10283
174138 ZDOT = 3134
311477
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 14130
38351801
00016717 00000-0 10270-3 0 9128
2 25544 51
6473 286
9671 0003213 338
3823 21
7192 15
50016583 5467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
38351801 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 286
9671 deg
Eccentricity:
0003213
Arg of perigee: 338
3823 deg
Mean anomaly: 21
7192 deg
Mean motion: 15
50016583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 289
Coasting Arc #14 (Orbit 560)
---------------------------------------
Vector Time (GMT): 2014/131/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322321
84 A = 6791742
11 meter
Y = 2335284
01 meter E =
0011210
Z = -4700432
54 I = 51
28388
XDOT = -817
535325 Wp = 53
81171
YDOT = -7087
401917 meter/sec RA = 281
53711 deg
ZDOT = -2767
564356 TA = 188
56451
MA = 188
58365
Ha = 227
325 n
mi
Hp = 221
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180845
92 X = -4325280
66
Y = 7661692
96 feet Y = 2286932
41 meter
Z = -15421366
61 Z = -4721437
38
XDOT = -2682
202510 XDOT = -724
777446
YDOT = -23252
630961 feet/sec YDOT = -7096
025532 meter/sec
ZDOT = -9079
935552 ZDOT = -2771
310467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15458974
75 X = -4711895
50
Y = 4249593
66 feet Y = 1295276
15 meter
Z = -15510561
93 Z = -4727619
28
XDOT = 3052
345411 XDOT = 930
354881
YDOT = -22112
589267 feet/sec YDOT = -6739
917209 meter/sec
ZDOT = -9094
579998 ZDOT = -2772
027983
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 14131
35058127
00016717 00000-0 10270-3 0 9132
2 25544 51
6460 282
1751 0003271 338
6286 21
4728 15
50071174 5616
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
35058127 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 282
1751 deg
Eccentricity:
0003271
Arg of perigee: 338
6286 deg
Mean anomaly: 21
4728 deg
Mean motion: 15
50071174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 561
Checksum: 282
Coasting Arc #15 (Orbit 576)
---------------------------------------
Vector Time (GMT): 2014/132/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4176260
79 A = 6791097
22 meter
Y = -2253794
27 meter E =
0005036
Z = 4853539
20 I = 51
27662
XDOT = 1102
793260 Wp = 93
32771
YDOT = 7198
150951 meter/sec RA = 276
55505 deg
ZDOT = 2391
192289 TA = 333
08864
MA = 333
11475
Ha = 227
318 n
mi
Hp = 221
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13701643
01 X = 4177575
40
Y = -7394338
17 feet Y = -2207085
28 meter
Z = 15923685
02 Z = 4873830
51
XDOT = 3618
088124 XDOT = 1010
604053
YDOT = 23615
980810 feet/sec YDOT = 7209
967642 meter/sec
ZDOT = 7845
119059 ZDOT = 2396
325667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14855670
61 X = 4528008
40
Y = -4355318
90 feet Y = -1327501
20 meter
Z = 16009848
56 Z = 4879801
84
XDOT = -1814
226421 XDOT = -552
976213
YDOT = 22754
559301 feet/sec YDOT = 6935
589675 meter/sec
ZDOT = 7865
615981 ZDOT = 2397
439751
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 14132
38209921
00016717 00000-0 10270-3 0 9147
2 25544 51
6462 277
0635 0003342 344
6367 15
4681 15
50067782 5776
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
38209921 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 277
0635 deg
Eccentricity:
0003342
Arg of perigee: 344
6367 deg
Mean anomaly: 15
4681 deg
Mean motion: 15
50067782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 577
Checksum: 307
Coasting Arc #16 (Orbit 591)
---------------------------------------
Vector Time (GMT): 2014/133/07:54:30
196
Vector Time (MET): N/A
Weight (LBS) : 923661
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4072070
19 A = 6790338
14 meter
Y = 2151178
49 meter E =
0013274
Z = -5002001
39 I = 51
27093
XDOT = -1393
084724 Wp = 60
65127
YDOT = -7257
301200 meter/sec RA = 271
57191 deg
ZDOT = -1984
626380 TA = 189
91623
MA = 189
94245
Ha = 227
398 n
mi
Hp = 221
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13359810
35 X = -4071523
84
Y = 7057672
23 feet Y = 2105645
13 meter
Z = -16410765
73 Z = -5021782
03
XDOT = -4570
487940 XDOT = -1302
187499
YDOT = -23810
043306 feet/sec YDOT = -7272
371297 meter/sec
ZDOT = -6511
241403 ZDOT = -1991
173285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14374840
98 X = -4381451
53
Y = 4346902
24 feet Y = 1324935
80 meter
Z = -16494753
39 Z = -5027600
83
XDOT = 498
581922 XDOT = 151
967770
YDOT = -23188
707949 feet/sec YDOT = -7067
918183 meter/sec
ZDOT = -6537
709766 ZDOT = -1992
693937
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 14133
34912653
00016717 00000-0 10270-3 0 9158
2 25544 51
6451 272
2712 0003333 346
5188 13
5873 15
50131088 5929
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
34912653 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 272
2712 deg
Eccentricity:
0003333
Arg of perigee: 346
5188 deg
Mean anomaly: 13
5873 deg
Mean motion: 15
50131088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 592
Checksum: 291
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