[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 12th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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 3197)
---------------------------------------
Vector Time (GMT): 2014/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6262524
89 A = 6799125
71 meter
Y = -1828627
74 meter E =
0008288
Z = -1913208
05 I = 51
64833
XDOT = 2959
724905 Wp = 65
54127
YDOT = 4293
737718 meter/sec RA = 357
13898 deg
ZDOT = 5606
694090 TA = 273
43007
MA = 273
52487
Ha = 228
359 n
mi
Hp = 219
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20546341
49 X = 6291801
09
Y = -5999434
83 feet Y = -1758432
57 meter
Z = -6276929
28 Z = -1882715
13
XDOT = 9710
383548 XDOT = 2884
256538
YDOT = 14087
066005 feet/sec YDOT = 4326
413541 meter/sec
ZDOT = 18394
665651 ZDOT = 5620
888171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19864510
04 X = 6054702
66
Y = 8071535
12 feet Y = 2460203
90 meter
Z = -6147907
78 Z = -1873882
29
XDOT = -631
843868 XDOT = -192
586011
YDOT = 15553
438615 feet/sec YDOT = 4740
688090 meter/sec
ZDOT = 18453
830945 ZDOT = 5624
727672
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 14043
50369111
00016717 00000-0 10270-3 0 9005
2 25544 51
6474 357
6758 0003760 125
1008 235
0495 15
50254671 31988
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
50369111 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 357
6758 deg
Eccentricity:
0003760
Arg of perigee: 125
1008 deg
Mean anomaly: 235
0495 deg
Mean motion: 15
50254671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 297
Coasting Arc #2 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2014/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6304730
84 A = 6799665
42 meter
Y = 2046075
66 meter E =
0017524
Z = 1476924
55 I = 51
62058
XDOT = -2737
454687 Wp = 120
64418
YDOT = -4238
380031 meter/sec RA = 352
18452 deg
ZDOT = -5771
750931 TA = 43
24884
MA = 43
11138
Ha = 228
270 n
mi
Hp = 219
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20684812
46 X = -6334316
18
Y = 6712846
66 feet Y = 1975406
80 meter
Z = 4845553
00 Z = 1446225
84
XDOT = -8981
150547 XDOT = -2661
820102
YDOT = -13905
446295 feet/sec YDOT = -4268
569459 meter/sec
ZDOT = -18936
190720 ZDOT = -5784
864802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20536353
23 X = -6259480
46
Y = -7240453
99 feet Y = -2206890
37 meter
Z = 4715631
73 Z = 1437324
55
XDOT = 871
748411 XDOT = 265
708916
YDOT = -14933
892315 feet/sec YDOT = -4551
850378 meter/sec
ZDOT = -18990
807958 ZDOT = -5788
398266
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 14044
53508303
00016717 00000-0 10270-3 0 9018
2 25544 51
6485 352
5641 0003745 129
1118 231
0366 15
50282351 32142
Satellite: ISS
Catalog Number: 25544
Epoch time: 14044
53508303 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 352
5641 deg
Eccentricity:
0003745
Arg of perigee: 129
1118 deg
Mean anomaly: 231
0366 deg
Mean motion: 15
50282351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 274
Coasting Arc #3 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2014/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6308240
02 A = 6799987
26 meter
Y = -2297247
18 meter E =
0010067
Z = -1066910
77 I = 51
59134
XDOT = 2519
814863 Wp = 59
51029
YDOT = 4209
712076 meter/sec RA = 347
22846 deg
ZDOT = 5880
912107 TA = 288
93555
MA = 289
04465
Ha = 228
160 n
mi
Hp = 219
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20696325
54 X = 6338642
10
Y = -7536900
19 feet Y = -2226534
50 meter
Z = -3500363
43 Z = -1036192
95
XDOT = 8267
109131 XDOT = 2443
986748
YDOT = 13811
391324 feet/sec YDOT = 4237
466745 meter/sec
ZDOT = 19294
331061 ZDOT = 5892
968206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21149210
00 X = 6446279
21
Y = 6224718
05 feet Y = 1897294
06 meter
Z = -3370326
57 Z = -1027275
54
XDOT = -1183
759838 XDOT = -360
809999
YDOT = 14410
189984 feet/sec YDOT = 4392
225907 meter/sec
ZDOT = 19344
490812 ZDOT = 5896
200799
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 14045
50199399
00016717 00000-0 10270-3 0 9028
2 25544 51
6483 347
7725 0003674 132
9146 227
2313 15
50314544 32298
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
50199399 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 347
7725 deg
Eccentricity:
0003674
Arg of perigee: 132
9146 deg
Mean anomaly: 227
2313 deg
Mean motion: 15
50314544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3229
Checksum: 310
Coasting Arc #4 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2014/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285495
05 A = 6800248
91 meter
Y = 2504196
01 meter E =
0016689
Z = 593698
21 I = 51
56354
XDOT = -2264
934236 Wp = 130
33514
YDOT = -4246
770849 meter/sec RA = 342
27048 deg
ZDOT = -5966
021880 TA = 43
25762
MA = 43
12669
Ha = 228
066 n
mi
Hp = 219
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20621702
94 X = -6315914
32
Y = 8215866
16 feet Y = 2433737
55 meter
Z = 1947828
76 Z = 563090
71
XDOT = -7430
886600 XDOT = -2188
297182
YDOT = -13932
975225 feet/sec YDOT = -4271
670862 meter/sec
ZDOT = -19573
562597 ZDOT = -5976
837817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21577723
79 X = -6576890
21
Y = -5257850
73 feet Y = -1602592
90 meter
Z = 1818231
90 Z = 554197
08
XDOT = 1733
059006 XDOT = 528
236385
YDOT = -14018
380223 feet/sec YDOT = -4272
802292 meter/sec
ZDOT = -19618
484191 ZDOT = -5979
713981
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 14046
53334727
00016717 00000-0 10270-3 0 9039
2 25544 51
6494 342
6608 0003716 137
0800 223
0641 15
50336346 32454
Satellite: ISS
Catalog Number: 25544
Epoch time: 14046
53334727 = yrday
fracday
Element set: 903
Inclination: 51
6494 deg
RA of node: 342
6608 deg
Eccentricity:
0003716
Arg of perigee: 137
0800 deg
Mean anomaly: 223
0641 deg
Mean motion: 15
50336346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 287
Coasting Arc #5 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2014/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6221160
74 A = 6800265
02 meter
Y = -2732618
98 meter E =
0012037
Z = -152820
41 I = 51
53432
XDOT = 2032
703267 Wp = 61
60403
YDOT = 4312
883681 meter/sec RA = 337
31052 deg
ZDOT = 5995
522857 TA = 296
75038
MA = 296
87350
Ha = 227
964 n
mi
Hp = 219
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20410632
34 X = 6251997
46
Y = -8965285
35 feet Y = -2662877
57 meter
Z = -501379
31 Z = -122524
29
XDOT = 6668
973973 XDOT = 1955
200797
YDOT = 14149
880842 feet/sec YDOT = 4335
181978 meter/sec
ZDOT = 19670
350581 ZDOT = 6005
208540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21906958
52 X = 6677240
96
Y = 4143383
10 feet Y = 1262903
17 meter
Z = -373068
34 Z = -113711
23
XDOT = -2297
422203 XDOT = -700
254288
YDOT = 13776
385648 feet/sec YDOT = 4199
042346 meter/sec
ZDOT = 19710
493245 ZDOT = 6007
758341
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 14047
50022193
00016717 00000-0 10270-3 0 9049
2 25544 51
6490 337
8689 0003617 140
5222 219
6192 15
50370784 32605
Satellite: ISS
Catalog Number: 25544
Epoch time: 14047
50022193 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 337
8689 deg
Eccentricity:
0003617
Arg of perigee: 140
5222 deg
Mean anomaly: 219
6192 deg
Mean motion: 15
50370784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3260
Checksum: 298
Coasting Arc #6 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2014/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6131777
74 A = 6800151
68 meter
Y = 2902768
30 meter E =
0014939
Z = -345150
53 I = 51
50679
XDOT = -1775
785727 Wp = 138
97389
YDOT = -4444
120074 meter/sec RA = 332
34849 deg
ZDOT = -5986
439404 TA = 44
74827
MA = 44
62785
Ha = 227
849 n
mi
Hp = 219
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20117381
04 X = -6162104
82
Y = 9523518
03 feet Y = 2834029
22 meter
Z = -1132383
64 Z = -375011
36
XDOT = -5826
068659 XDOT = -1696
878861
YDOT = -14580
446438 feet/sec YDOT = -4463
537539 meter/sec
ZDOT = -19640
549225 ZDOT = -5994
873618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22029259
15 X = -6714518
19
Y = -3132998
91 feet Y = -954938
07 meter
Z = -1258875
54 Z = -383705
26
XDOT = 3046
745666 XDOT = 928
648079
YDOT = -13704
893682 feet/sec YDOT = -4177
251594 meter/sec
ZDOT = -19675
390767 ZDOT = -5997
059106
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 14048
53153635
00016717 00000-0 10270-3 0 9050
2 25544 51
6498 332
7570 0003684 145
1186 215
0206 15
50391837 32765
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
53153635 = yrday
fracday
Element set: 905
Inclination: 51
6498 deg
RA of node: 332
7570 deg
Eccentricity:
0003684
Arg of perigee: 145
1186 deg
Mean anomaly: 215
0206 deg
Mean motion: 15
50391837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 309
Coasting Arc #7 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2014/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6002772
26 A = 6799812
86 meter
Y = -3081432
54 meter E =
0013593
Z = 803990
67 I = 51
47847
XDOT = 1558
454690 Wp = 68
91194
YDOT = 4601
558415 meter/sec RA = 327
38415 deg
ZDOT = 5924
155428 TA = 299
78619
MA = 299
92131
Ha = 227
760 n
mi
Hp = 219
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19694134
72 X = 6032877
91
Y = -10109686
82 feet Y = -3014137
28 meter
Z = 2637764
67 Z = 833224
40
XDOT = 5113
040323 XDOT = 1478
105915
YDOT = 15096
976426 feet/sec YDOT = 4618
537470 meter/sec
ZDOT = 19436
205474 ZDOT = 5931
530405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22029242
12 X = 6714513
00
Y = 2026919
58 feet Y = 617805
09 meter
Z = 2761630
22 Z = 841744
89
XDOT = -3741
291538 XDOT = -1140
345661
YDOT = 13812
947289 feet/sec YDOT = 4210
186334 meter/sec
ZDOT = 19466
553048 ZDOT = 5933
405369
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 14049
56283054
00016717 00000-0 10270-3 0 9064
2 25544 51
6492 327
6452 0003577 148
1872 211
9496 15
50426884 32922
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
56283054 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 327
6452 deg
Eccentricity:
0003577
Arg of perigee: 148
1872 deg
Mean anomaly: 211
9496 deg
Mean motion: 15
50426884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 330
Coasting Arc #8 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2014/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5854478
27 A = 6799283
55 meter
Y = 3187966
87 meter E =
0012323
Z = -1310573
19 I = 51
45195
XDOT = -1330
740021 Wp = 145
15013
YDOT = -4816
760530 meter/sec RA = 322
41754 deg
ZDOT = -5809
181386 TA = 49
12968
MA = 49
02296
Ha = 227
618 n
mi
Hp = 219
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19207605
88 X = -5883325
43
Y = 10459208
89 feet Y = 3122336
91 meter
Z = -4299780
80 Z = -1339083
56
XDOT = -4365
944952 XDOT = -1248
560145
YDOT = -15803
020113 feet/sec YDOT = -4831
182841 meter/sec
ZDOT = -19058
994049 ZDOT = -5815
445753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21819367
36 X = -6650543
17
Y = -1090305
00 feet Y = -332324
96 meter
Z = -4420603
16 Z = -1347399
84
XDOT = 4547
520240 XDOT = 1386
084169
YDOT = -14106
359077 feet/sec YDOT = -4299
618247 meter/sec
ZDOT = -19084
621704 ZDOT = -5816
992695
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 14050
52965035
00016717 00000-0 10270-3 0 9079
2 25544 51
6498 322
8524 0003639 153
5025 206
6312 15
50446983 33071
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
52965035 = yrday
fracday
Element set: 907
Inclination: 51
6498 deg
RA of node: 322
8524 deg
Eccentricity:
0003639
Arg of perigee: 153
5025 deg
Mean anomaly: 206
6312 deg
Mean motion: 15
50446983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 304
Coasting Arc #9 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2014/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5673449
46 A = 6798571
87 meter
Y = -3290938
17 meter E =
0014366
Z = 1770855
86 I = 51
42555
XDOT = 1156
152411 Wp = 79
56344
YDOT = 5050
578324 meter/sec RA = 317
44838 deg
ZDOT = 5645
287816 TA = 299
91263
MA = 300
05524
Ha = 227
532 n
mi
Hp = 219
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18613679
33 X = 5701225
62
Y = -10797041
24 feet Y = -3227338
55 meter
Z = 5809894
56 Z = 1798484
25
XDOT = 3793
150954 XDOT = 1072
166987
YDOT = 16570
138857 feet/sec YDOT = 5063
038104 meter/sec
ZDOT = 18521
285485 ZDOT = 5650
699729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21486199
51 X = 6548993
61
Y = 117748
54 feet Y = 35889
75 meter
Z = 5927005
86 Z = 1806551
39
XDOT = -5227
550189 XDOT = -1593
357298
YDOT = 14580
187461 feet/sec YDOT = 4444
041138 meter/sec
ZDOT = 18543
280003 ZDOT = 5651
991745
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 14051
56090611
00016717 00000-0 10270-3 0 9084
2 25544 51
6494 317
7399 0003522 155
8560 204
2756 15
50483341 33233
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
56090611 = yrday
fracday
Element set: 908
Inclination: 51
6494 deg
RA of node: 317
7399 deg
Eccentricity:
0003522
Arg of perigee: 155
8560 deg
Mean anomaly: 204
2756 deg
Mean motion: 15
50483341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 301
Coasting Arc #10 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2014/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5483716
26 A = 6797651
10 meter
Y = 3310440
90 meter E =
0009168
Z = -2266160
37 I = 51
40104
XDOT = -985
039591 Wp = 145
26373
YDOT = -5327
287747 meter/sec RA = 312
47701 deg
ZDOT = -5416
785014 TA = 59
99843
MA = 59
90748
Ha = 227
364 n
mi
Hp = 219
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17991195
07 X = -5509318
58
Y = 10861026
57 feet Y = 3248975
14 meter
Z = -7434909
34 Z = -2292861
75
XDOT = -3231
757189 XDOT = -899
082634
YDOT = -17477
978173 feet/sec YDOT = -5337
822912 meter/sec
ZDOT = -17771
604377 ZDOT = -5421
360955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20965827
40 X = -6390384
19
Y = 618889
52 feet Y = 188637
53 meter
Z = -7548107
85 Z = -2300663
27
XDOT = 5934
215261 XDOT = 1808
748811
YDOT = -15221
892095 feet/sec YDOT = -4639
632710 meter/sec
ZDOT = -17790
029149 ZDOT = -5422
400885
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 14052
52768968
00016717 00000-0 10270-3 0 9099
2 25544 51
6499 312
9468 0003563 162
5182 197
6092 15
50502850 33383
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
52768968 = yrday
fracday
Element set: 909
Inclination: 51
6499 deg
RA of node: 312
9468 deg
Eccentricity:
0003563
Arg of perigee: 162
5182 deg
Mean anomaly: 197
6092 deg
Mean motion: 15
50502850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 336
Coasting Arc #11 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2014/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5272411
48 A = 6796613
65 meter
Y = -3316757
57 meter E =
0014173
Z = 2707954
32 I = 51
37751
XDOT = 875
157855 Wp = 92
61487
YDOT = 5611
430049 meter/sec RA = 307
50293 deg
ZDOT = 5145
032281 TA = 298
06967
MA = 298
21291
Ha = 227
272 n
mi
Hp = 219
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17297937
91 X = 5295954
08
Y = -10881750
56 feet Y = -3257666
28 meter
Z = 8884364
55 Z = 2733624
13
XDOT = 2871
252804 XDOT = 787
351836
YDOT = 18410
203572 feet/sec YDOT = 5620
726013 meter/sec
ZDOT = 16880
027169 ZDOT = 5149
069995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20344756
25 X = 6201081
71
Y = -1332731
79 feet Y = -406216
65 meter
Z = 8993208
75 Z = 2741130
03
XDOT = -6454
045524 XDOT = -1967
193076
YDOT = 16015
746100 feet/sec YDOT = 4881
599411 meter/sec
ZDOT = 16896
138627 ZDOT = 5149
943054
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 14053
55890738
00016717 00000-0 10270-3 0 9106
2 25544 51
6497 307
8339 0003430 164
1226 196
0033 15
50539644 33548
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
55890738 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 307
8339 deg
Eccentricity:
0003430
Arg of perigee: 164
1226 deg
Mean anomaly: 196
0033 deg
Mean motion: 15
50539644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 308
Coasting Arc #12 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2014/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5067192
64 A = 6795387
13 meter
Y = 3233246
01 meter E =
0006536
Z = -3169092
23 I = 51
35589
XDOT = -779
439013 Wp = 130
25495
YDOT = -5916
643666 meter/sec RA = 302
52686 deg
ZDOT = -4800
852746 TA = 86
40933
MA = 86
33458
Ha = 227
083 n
mi
Hp = 219
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16624647
77 X = -5087576
66
Y = 10607762
51 feet Y = 3176467
27 meter
Z = -10397284
23 Z = -3193757
35
XDOT = -2557
214611 XDOT = -689
899111
YDOT = -19411
560584 feet/sec YDOT = -5924
859474 meter/sec
ZDOT = -15750
829220 ZDOT = -4804
421294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19586681
92 X = -5970020
65
Y = 1754877
56 feet Y = 534886
68 meter
Z = -10501873
86 Z = -3200971
15
XDOT = 6917
781975 XDOT = 2108
539946
YDOT = -16923
894998 feet/sec YDOT = -5158
403195 meter/sec
ZDOT = -15764
917446 ZDOT = -4805
146838
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 14054
52565504
00016717 00000-0 10270-3 0 9115
2 25544 51
6500 303
0407 0003453 172
0424 188
0782 15
50562746 33697
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
52565504 = yrday
fracday
Element set: 911
Inclination: 51
6500 deg
RA of node: 303
0407 deg
Eccentricity:
0003453
Arg of perigee: 172
0424 deg
Mean anomaly: 188
0782 deg
Mean motion: 15
50562746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 286
Coasting Arc #13 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2014/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4854499
13 A = 6794154
66 meter
Y = -3130741
52 meter E =
0013000
Z = 3569674
54 I = 51
33607
XDOT = 746
117048 Wp = 107
62429
YDOT = 6216
107124 meter/sec RA = 297
54813 deg
ZDOT = 4419
889273 TA = 294
69415
MA = 294
82944
Ha = 226
990 n
mi
Hp = 219
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15926834
41 X = 4871806
92
Y = -10271461
68 feet Y = -3076358
44 meter
Z = 11711530
65 Z = 3593298
86
XDOT = 2447
890579 XDOT = 655
081617
YDOT = 20394
052243 feet/sec YDOT = 6223
941908 meter/sec
ZDOT = 14500
949060 ZDOT = 4423
292305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18771660
82 X = 5721602
22
Y = -2105984
72 feet Y = -641904
14 meter
Z = 11811710
63 Z = 3600209
40
XDOT = -7156
407539 XDOT = -2181
273018
YDOT = 17930
953551 feet/sec YDOT = 5465
354642 meter/sec
ZDOT = 14514
299034 ZDOT = 4423
958346
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 14055
55683521
00016717 00000-0 10270-3 0 9120
2 25544 51
6499 297
9276 0003315 173
0942 187
0255 15
50593328 33854
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
55683521 = yrday
fracday
Element set: 912
Inclination: 51
6499 deg
RA of node: 297
9276 deg
Eccentricity:
0003315
Arg of perigee: 173
0942 deg
Mean anomaly: 187
0255 deg
Mean motion: 15
50593328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 328
Coasting Arc #14 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2014/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4665236
29 A = 6792771
87 meter
Y = 2939094
63 meter E =
0006610
Z = -3971938
28 I = 51
31797
XDOT = -731
806039 Wp = 100
82420
YDOT = -6509
998447 meter/sec RA = 292
56739 deg
ZDOT = -3964
486264 TA = 127
65803
MA = 127
59804
Ha = 226
790 n
mi
Hp = 220
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15305893
33 X = -4678461
15
Y = 9642698
92 feet Y = 2886850
79 meter
Z = -13031293
57 Z = -3994633
20
XDOT = -2400
938447 XDOT = -639
697558
YDOT = -21358
262621 feet/sec YDOT = -6517
667200 meter/sec
ZDOT = -13006
844697 ZDOT = -3967
817094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17893770
43 X = -5454021
23
Y = 2132568
00 feet Y = 650006
73 meter
Z = -13127519
14 Z = -4001267
83
XDOT = 7275
076483 XDOT = 2217
443312
YDOT = -18966
155978 feet/sec YDOT = -5780
884342 meter/sec
ZDOT = -13019
854504 ZDOT = -3968
451653
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 14056
52354711
00016717 00000-0 10270-3 0 9135
2 25544 51
6496 293
1343 0003335 181
6402 178
4738 15
50627018 34004
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
52354711 = yrday
fracday
Element set: 913
Inclination: 51
6496 deg
RA of node: 293
1343 deg
Eccentricity:
0003335
Arg of perigee: 181
6402 deg
Mean anomaly: 178
4738 deg
Mean motion: 15
50627018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 293
Coasting Arc #15 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4483578
34 A = 6791539
04 meter
Y = -2727400
03 meter E =
0010985
Z = 4306847
05 I = 51
30268
XDOT = 773
366467 Wp = 124
29418
YDOT = 6784
786709 meter/sec RA = 287
58431 deg
ZDOT = 3479
045227 TA = 290
08017
MA = 290
19837
Ha = 226
698 n
mi
Hp = 220
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14709902
69 X = 4492822
70
Y = -8948162
82 feet Y = -2677209
77 meter
Z = 14130075
62 Z = 4328649
81
XDOT = 2537
291557 XDOT = 680
540277
YDOT = 22259
798913 feet/sec YDOT = 6792
916233 meter/sec
ZDOT = 11414
190378 ZDOT = 3482
576066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17017381
38 X = 5186897
84
Y = -2058911
18 feet Y = -627556
13 meter
Z = 14222500
06 Z = 4335018
02
XDOT = -7161
631698 XDOT = -2182
865342
YDOT = 20030
172361 feet/sec YDOT = 6105
196536 meter/sec
ZDOT = 11428
014995 ZDOT = 3483
258970
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14057
55468987
00016717 00000-0 10270-3 0 9141
2 25544 51
6492 288
0210 0003214 182
6538 177
4597 15
50644397 34161
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55468987 = yrday
fracday
Element set: 914
Inclination: 51
6492 deg
RA of node: 288
0210 deg
Eccentricity:
0003214
Arg of perigee: 182
6538 deg
Mean anomaly: 177
4597 deg
Mean motion: 15
50644397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 336
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