[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 2nd 2014
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) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
317/02:00:25
047 0
3 1
0 1
0
N/A 0
9 0
0 226
9
000/00:02:04
695 -0
3 -0
0 218
9
Coasting Arc #1 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2014/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2600729
50 A = 6794040
83 meter
Y = -5293944
87 meter E =
0011596
Z = 3366666
93 I = 51
86183
XDOT = 6071
186947 Wp = 69
89770
YDOT = -1
169967 meter/sec RA = 142
78958 deg
ZDOT = -4674
850297 TA = 71
03250
MA = 70
90687
Ha = 226
246 n
mi
Hp = 220
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8532577
10 X = 2643379
94
Y = -17368585
54 feet Y = -5264623
19 meter
Z = 11045495
17 Z = 3379404
91
XDOT = 19918
592346 XDOT = 6093
458003
YDOT = -3
838475 feet/sec YDOT = 66
846277 meter/sec
ZDOT = -15337
435359 ZDOT = -4645
302870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4314117
31 X = 1314942
96
Y = 18831899
51 feet Y = 5739962
97 meter
Z = 11100610
43 Z = 3383466
06
XDOT = -14203
999245 XDOT = -4329
378970
YDOT = 12253
085699 feet/sec YDOT = 3734
740521 meter/sec
ZDOT = -15211
517867 ZDOT = -4636
470646
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 14304
53931470
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 143
6797 0004475 339
1928 20
9040 15
50851332 32480
Satellite: ISS
Catalog Number: 25544
Epoch time: 14304
53931470 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 143
6797 deg
Eccentricity:
0004475
Arg of perigee: 339
1928 deg
Mean anomaly: 20
9040 deg
Mean motion: 15
50851332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 295
Coasting Arc #2 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2014/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2725223
36 A = 6795341
64 meter
Y = 5515309
51 meter E =
0006757
Z = -2880762
06 I = 51
88903
XDOT = -5732
633305 Wp = 26
13800
YDOT = -184
901090 meter/sec RA = 137
84524 deg
ZDOT = 5079
549861 TA = 301
24758
MA = 301
31377
Ha = 226
339 n
mi
Hp = 220
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8941021
52 X = -2772700
29
Y = 18094847
49 feet Y = 5484568
65 meter
Z = -9451319
08 Z = -2894116
66
XDOT = -18807
852051 XDOT = -5754
814778
YDOT = -606
630874 feet/sec YDOT = -249
130805 meter/sec
ZDOT = 16665
189834 ZDOT = 5051
647309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4781842
64 X = -1457505
64
Y = -19580696
69 feet Y = -5968196
35 meter
Z = -9509106
27 Z = -2898375
59
XDOT = 13476
072230 XDOT = 4107
506816
YDOT = -11309
989641 feet/sec YDOT = -3447
284843 meter/sec
ZDOT = 16546
300491 ZDOT = 5043
312390
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 14305
50590243
00016717 00000-0 10270-3 0 9019
2 25544 51
6426 138
8839 0004272 343
5401 16
5611 15
50844267 32637
Satellite: ISS
Catalog Number: 25544
Epoch time: 14305
50590243 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 138
8839 deg
Eccentricity:
0004272
Arg of perigee: 343
5401 deg
Mean anomaly: 16
5611 deg
Mean motion: 15
50844267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 290
Coasting Arc #3 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2014/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2839250
83 A = 6796384
53 meter
Y = -5720284
58 meter E =
0012088
Z = 2315530
92 I = 51
91598
XDOT = 5382
829183 Wp = 88
69597
YDOT = 462
449434 meter/sec RA = 132
90488 deg
ZDOT = -5433
126729 TA = 65
64162
MA = 65
51548
Ha = 226
347 n
mi
Hp = 219
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9315127
39 X = 2891757
07
Y = -18767337
87 feet Y = -5688240
48 meter
Z = 7596886
21 Z = 2329451
79
XDOT = 17660
200733 XDOT = 5403
650701
YDOT = 1517
222553 feet/sec YDOT = 522
759726 meter/sec
ZDOT = -17825
218928 ZDOT = -5406
926754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5266134
54 X = 1605117
81
Y = 20256688
90 feet Y = 6174238
78 meter
Z = 7657129
42 Z = 2333893
05
XDOT = -12957
075673 XDOT = -3949
316665
YDOT = 10094
731224 feet/sec YDOT = 3076
874077 meter/sec
ZDOT = -17713
621842 ZDOT = -5399
111937
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 14306
53690578
00016717 00000-0 10270-3 0 9026
2 25544 51
6429 133
7694 0004531 346
0902 14
0124 15
50916448 32795
Satellite: ISS
Catalog Number: 25544
Epoch time: 14306
53690578 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 133
7694 deg
Eccentricity:
0004531
Arg of perigee: 346
0902 deg
Mean anomaly: 14
0124 deg
Mean motion: 15
50916448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 305
Coasting Arc #4 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2014/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2875655
33 A = 6797412
21 meter
Y = 5901511
47 meter E =
0010839
Z = -1741235
30 I = 51
93866
XDOT = -5054
880794 Wp = 21
93252
YDOT = -785
594876 meter/sec RA = 127
96539 deg
ZDOT = 5706
771906 TA = 319
06478
MA = 319
14611
Ha = 226
441 n
mi
Hp = 219
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9434564
72 X = -2932975
14
Y = 19361914
27 feet Y = 5869033
40 meter
Z = -5712714
22 Z = -1755344
79
XDOT = -16584
254574 XDOT = -5073
442608
YDOT = -2577
411012 feet/sec YDOT = -842
225171 meter/sec
ZDOT = 18723
004942 ZDOT = 5682
170502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5912674
87 X = -1802183
30
Y = -20693799
17 feet Y = -6307469
99 meter
Z = -5773802
18 Z = -1759854
90
XDOT = 12652
570266 XDOT = 3856
503417
YDOT = -8790
612154 feet/sec YDOT = -2679
378584 meter/sec
ZDOT = 18618
267401 ZDOT = 5674
847904
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 14307
50345518
00016717 00000-0 10270-3 0 9036
2 25544 51
6416 128
9732 0004262 351
2811 8
8265 15
50902428 32945
Satellite: ISS
Catalog Number: 25544
Epoch time: 14307
50345518 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 128
9732 deg
Eccentricity:
0004262
Arg of perigee: 351
2811 deg
Mean anomaly: 8
8265 deg
Mean motion: 15
50902428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 295
Coasting Arc #5 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2014/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2905753
67 A = 6797961
92 meter
Y = -6043174
35 meter E =
0011331
Z = 1096297
69 I = 51
95972
XDOT = 4732
923359 Wp = 104
82945
YDOT = 1195
863576 meter/sec RA = 123
02916 deg
ZDOT = -5904
609618 TA = 63
34868
MA = 63
23268
Ha = 226
455 n
mi
Hp = 219
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9533312
57 X = 2967788
30
Y = -19826687
51 feet Y = -6010333
40 meter
Z = 3596777
20 Z = 1110564
87
XDOT = 15527
963777 XDOT = 4747
882547
YDOT = 3923
436928 feet/sec YDOT = 1248
873421 meter/sec
ZDOT = -19372
078798 ZDOT = -5881
580949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6501604
81 X = 1981689
15
Y = 21006245
75 feet Y = 6402703
71 meter
Z = 3658574
44 Z = 1115133
49
XDOT = -12612
273690 XDOT = -3844
221021
YDOT = 7287
494471 feet/sec YDOT = 2221
228315 meter/sec
ZDOT = -19274
107621 ZDOT = -5874
748003
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 14308
53441689
00016717 00000-0 10270-3 0 9047
2 25544 51
6416 123
8580 0004561 354
0845 6
0251 15
50983227 33100
Satellite: ISS
Catalog Number: 25544
Epoch time: 14308
53441689 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 123
8580 deg
Eccentricity:
0004561
Arg of perigee: 354
0845 deg
Mean anomaly: 6
0251 deg
Mean motion: 15
50983227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 291
Coasting Arc #6 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2014/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2867883
30 A = 6798439
04 meter
Y = 6137794
32 meter E =
0014506
Z = -460861
80 I = 51
97709
XDOT = -4458
612649 Wp = 30
59951
YDOT = -1638
629493 meter/sec RA = 118
09343 deg
ZDOT = 6017
102264 TA = 324
45807
MA = 324
55461
Ha = 226
543 n
mi
Hp = 219
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9409065
94 X = -2934065
61
Y = 20137120
48 feet Y = 6105353
72 meter
Z = -1512013
79 Z = -474955
04
XDOT = -14627
994255 XDOT = -4469
187667
YDOT = -5376
081015 feet/sec YDOT = -1688
547387 meter/sec
ZDOT = 19741
149161 ZDOT = 5995
416778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7157178
97 X = -2181508
15
Y = -21038547
21 feet Y = -6412549
19 meter
Z = -1573101
82 Z = -479481
44
XDOT = 12832
143670 XDOT = 3911
237391
YDOT = -5812
182080 feet/sec YDOT = -1771
553098 meter/sec
ZDOT = 19648
973870 ZDOT = 5989
007235
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 14309
50092701
00016717 00000-0 10270-3 0 9053
2 25544 51
6412 119
0617 0004259 359
6386
4761 15
50966816 33254
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
50092701 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 119
0617 deg
Eccentricity:
0004259
Arg of perigee: 359
6386 deg
Mean anomaly:
4761 deg
Mean motion: 15
50966816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 301
Coasting Arc #7 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2014/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2835542
85 A = 6798289
53 meter
Y = -6171782
51 meter E =
0009148
Z = -229922
98 I = 51
99131
XDOT = 4206
032532 Wp = 115
14787
YDOT = 2149
930553 meter/sec RA = 113
15977 deg
ZDOT = -6030
012547 TA = 67
31313
MA = 67
21644
Ha = 226
567 n
mi
Hp = 219
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9302962
09 X = 2905463
33
Y = -20248630
29 feet Y = -6139682
69 meter
Z = -754340
48 Z = -215977
86
XDOT = 13799
319331 XDOT = 4210
971592
YDOT = 7053
577930 feet/sec YDOT = 2196
992534 meter/sec
ZDOT = -19783
505730 ZDOT = -6009
567739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7661868
82 X = 2335337
62
Y = 20926908
20 feet Y = 6378521
62 meter
Z = -693859
46 Z = -211488
36
XDOT = -13323
275453 XDOT = -4060
934358
YDOT = 4247
507378 feet/sec YDOT = 1294
640249 meter/sec
ZDOT = -19696
703343 ZDOT = -6003
555179
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 14310
53184681
00016717 00000-0 10270-3 0 9068
2 25544 51
6413 113
9460 0004561 2
9364 357
1813 15
51043157 33417
Satellite: ISS
Catalog Number: 25544
Epoch time: 14310
53184681 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 113
9460 deg
Eccentricity:
0004561
Arg of perigee: 2
9364 deg
Mean anomaly: 357
1813 deg
Mean motion: 15
51043157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 279
Coasting Arc #8 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2014/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2754193
04 A = 6798004
39 meter
Y = 6140677
12 meter E =
0016627
Z = 890124
62 I = 52
00246
XDOT = -4019
268986 Wp = 43
81130
YDOT = -2674
184185 meter/sec RA = 108
22635 deg
ZDOT = 5957
406759 TA = 325
76654
MA = 325
87361
Ha = 226
624 n
mi
Hp = 219
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9036066
40 X = -2826978
88
Y = 20146578
49 feet Y = 6109471
00 meter
Z = 2920356
37 Z = 876567
88
XDOT = -13186
578037 XDOT = -4018
006880
YDOT = -8773
570160 feet/sec YDOT = -2719
123105 meter/sec
ZDOT = 19545
297765 ZDOT = 5937
884285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8124307
93 X = -2476289
06
Y = -20539497
21 feet Y = -6260438
75 meter
Z = 2861516
57 Z = 872190
25
XDOT = 14070
985086 XDOT = 4288
836254
YDOT = -2828
760260 feet/sec YDOT = -862
206127 meter/sec
ZDOT = 19462
515961 ZDOT = 5932
174865
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 14311
56274690
00016717 00000-0 10270-3 0 9073
2 25544 51
6420 108
8302 0004271 8
1066 352
0153 15
51040734 33574
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
56274690 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 108
8302 deg
Eccentricity:
0004271
Arg of perigee: 8
1066 deg
Mean anomaly: 352
0153 deg
Mean motion: 15
51040734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 271
Coasting Arc #9 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2014/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2696713
88 A = 6797130
56 meter
Y = -6034871
10 meter E =
0006157
Z = -1583572
26 I = 52
00931
XDOT = 3863
718937 Wp = 108
51692
YDOT = 3234
409350 meter/sec RA = 103
29344 deg
ZDOT = -5766
668873 TA = 88
67770
MA = 88
60717
Ha = 226
661 n
mi
Hp = 218
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8847486
47 X = 2771689
46
Y = -19799445
86 feet Y = -6004295
48 meter
Z = -5195447
06 Z = -1570289
57
XDOT = 12676
243230 XDOT = 3855
277194
YDOT = 10611
579231 feet/sec YDOT = 3277
568772 meter/sec
ZDOT = -18919
517299 ZDOT = -5747
919489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8342989
80 X = 2542943
29
Y = 20032137
65 feet Y = 6105795
56 meter
Z = -5137774
38 Z = -1565993
63
XDOT = -15033
725717 XDOT = -4582
279599
YDOT = 1446
412952 feet/sec YDOT = 440
866668 meter/sec
ZDOT = -18840
128457 ZDOT = -5742
471154
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 14312
52919417
00016717 00000-0 10270-3 0 9084
2 25544 51
6423 104
0342 0004530 11
4942 348
6312 15
51091484 33720
Satellite: ISS
Catalog Number: 25544
Epoch time: 14312
52919417 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 104
0342 deg
Eccentricity:
0004530
Arg of perigee: 11
4942 deg
Mean anomaly: 348
6312 deg
Mean motion: 15
51091484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 278
Coasting Arc #10 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2014/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2615720
34 A = 6796042
97 meter
Y = 5854109
98 meter E =
0016664
Z = 2224037
24 I = 52
01332
XDOT = -3780
757320 Wp = 58
79857
YDOT = -3785
147173 meter/sec RA = 98
36006 deg
ZDOT = 5494
756707 TA = 325
77051
MA = 325
87782
Ha = 226
683 n
mi
Hp = 218
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8581759
66 X = -2691791
85
Y = 19206397
56 feet Y = 5824433
92 meter
Z = 7296710
11 Z = 2211145
47
XDOT = -12404
059448 XDOT = -3764
842283
YDOT = -12418
461855 feet/sec YDOT = -3827
337149 meter/sec
ZDOT = 18027
417019 ZDOT = 5476
428512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8417216
00 X = -2565567
44
Y = -19300175
32 feet Y = -5882693
44 meter
Z = 7240717
65 Z = 2206970
74
XDOT = 16200
130587 XDOT = 4937
799803
YDOT = -303
896875 feet/sec YDOT = -92
627767 meter/sec
ZDOT = 17949
921405 ZDOT = 5471
136044
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 14313
56004994
00016717 00000-0 10270-3 0 9095
2 25544 51
6434 98
9187 0004323 15
3932 344
7350 15
51117216 33880
Satellite: ISS
Catalog Number: 25544
Epoch time: 14313
56004994 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 98
9187 deg
Eccentricity:
0004323
Arg of perigee: 15
3932 deg
Mean anomaly: 344
7350 deg
Mean motion: 15
51117216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3388
Checksum: 309
Coasting Arc #11 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2014/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2580179
73 A = 6794601
78 meter
Y = -5596163
42 meter E =
0005951
Z = -2869882
28 I = 52
01275
XDOT = 3727
806401 Wp = 69
21497
YDOT = 4328
957713 meter/sec RA = 93
42576 deg
ZDOT = -5096
277717 TA = 143
17342
MA = 143
13253
Ha = 226
721 n
mi
Hp = 218
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8465156
59 X = 2656506
79
Y = -18360116
19 feet Y = -5566883
35 meter
Z = -9415624
28 Z = -2857162
61
XDOT = 12230
335961 XDOT = 3703
878471
YDOT = 14202
617168 feet/sec YDOT = 4370
510770 meter/sec
ZDOT = -16720
071251 ZDOT = -5078
226254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8180034
67 X = 2493274
57
Y = 18516931
67 feet Y = 5643960
77 meter
Z = -9360395
18 Z = -2853048
45
XDOT = -17460
085581 XDOT = -5321
834085
YDOT = -689
586518 feet/sec YDOT = -210
185971 meter/sec
ZDOT = -16643
853738 ZDOT = -5073
046619
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 14314
52645739
00016717 00000-0 10270-3 0 9102
2 25544 51
6438 94
1231 0004519 18
7498 341
3818 15
51136750 34037
Satellite: ISS
Catalog Number: 25544
Epoch time: 14314
52645739 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 94
1231 deg
Eccentricity:
0004519
Arg of perigee: 18
7498 deg
Mean anomaly: 341
3818 deg
Mean motion: 15
51136750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 303
Coasting Arc #12 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2014/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2548891
58 A = 6792928
61 meter
Y = 5263181
66 meter E =
0014599
Z = 3440039
12 I = 52
00962
XDOT = -3740
593313 Wp = 73
74311
YDOT = -4842
006881 meter/sec RA = 88
48973 deg
ZDOT = 4624
335616 TA = 326
29875
MA = 326
39149
Ha = 226
743 n
mi
Hp = 218
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8362505
19 X = -2624267
13
Y = 17267656
37 feet Y = 5234256
80 meter
Z = 11286217
59 Z = 3427473
77
XDOT = -12272
287772 XDOT = -3708
634743
YDOT = -15885
849348 feet/sec YDOT = -4883
658000 meter/sec
ZDOT = 15171
704777 ZDOT = 4606
241607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7722724
35 X = -2353886
38
Y = -17598033
23 feet Y = -5363880
53 meter
Z = 11231692
31 Z = 3423419
82
XDOT = 18831
017772 XDOT = 5739
694217
YDOT = 1396
365550 feet/sec YDOT = 425
612220 meter/sec
ZDOT = 15095
400229 ZDOT = 4601
077990
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 14315
55726859
00016717 00000-0 10270-3 0 9110
2 25544 51
6448 89
0075 0004441 21
8811 338
2529 15
51189900 34191
Satellite: ISS
Catalog Number: 25544
Epoch time: 14315
55726859 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 89
0075 deg
Eccentricity:
0004441
Arg of perigee: 21
8811 deg
Mean anomaly: 338
2529 deg
Mean motion: 15
51189900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 315
Coasting Arc #13 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2014/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2582761
82 A = 6791247
76 meter
Y = -4865079
82 meter E =
0010368
Z = -3984543
60 I = 52
00247
XDOT = 3769
044522 Wp = 53
80852
YDOT = 5301
936891 meter/sec RA = 83
55186 deg
ZDOT = -4031
883892 TA = 174
24443
MA = 174
23250
Ha = 226
760 n
mi
Hp = 218
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8473628
00 X = 2656328
21
Y = -15961547
97 feet Y = -4835786
35 meter
Z = -13072649
61 Z = -3971818
07
XDOT = 12365
631633 XDOT = 3729
062767
YDOT = 17394
806074 feet/sec YDOT = 5343
861261 meter/sec
ZDOT = -13227
965525 ZDOT = -4013
671241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6936057
73 X = 2114110
40
Y = 16730311
13 feet Y = 5099398
83 meter
Z = -13017501
51 Z = -3967734
46
XDOT = -20124
972887 XDOT = -6134
091736
YDOT = -1885
801514 feet/sec YDOT = -574
792301 meter/sec
ZDOT = -13151
241728 ZDOT = -4008
498479
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 14316
52363518
00016717 00000-0 10270-3 0 9128
2 25544 51
6450 84
2118 0004581 24
9706 335
1666 15
51190144 34348
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
52363518 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 84
2118 deg
Eccentricity:
0004581
Arg of perigee: 24
9706 deg
Mean anomaly: 335
1666 deg
Mean motion: 15
51190144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 290
Coasting Arc #14 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2014/317/02:01:27
395
Vector Time (MET): N/A
Weight (LBS) : 931416
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3640345
16 A = 6787304
72 meter
Y = -2576878
20 meter E =
0016255
Z = -5130542
21 I = 51
98676
XDOT = 2523
273052 Wp = 62
81918
YDOT = 7013
094636 meter/sec RA = 80
65895 deg
ZDOT = -1729
033539 TA = 190
49560
MA = 190
52958
Ha = 226
897 n
mi
Hp = 218
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11943389
63 X = 3693812
70
Y = -8454324
79 feet Y = -2535870
55 meter
Z = -16832487
57 Z = -5112727
83
XDOT = 8278
454895 XDOT = 2453
062658
YDOT = 23008
840669 feet/sec YDOT = 7040
918939 meter/sec
ZDOT = -5672
682216 ZDOT = -1716
946223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6616178
73 X = -2016611
28
Y = -13149677
11 feet Y = -4008021
58 meter
Z = -16756042
86 Z = -5107241
87
XDOT = 23012
991244 XDOT = 7014
359731
YDOT = -4401
850889 feet/sec YDOT = -1341
684151 meter/sec
ZDOT = -5622
395414 ZDOT = -1713
706122
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 14317
10344595
00016717 00000-0 10270-3 0 9138
2 25544 51
6460 81
3385 0004674 18
6060 341
5261 15
51052459 34437
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
10344595 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 81
3385 deg
Eccentricity:
0004674
Arg of perigee: 18
6060 deg
Mean anomaly: 341
5261 deg
Mean motion: 15
51052459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 289
Coasting Arc #15 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2014/318/02:01:27
395
Vector Time (MET): N/A
Weight (LBS) : 931416
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3729921
46 A = 6786473
32 meter
Y = 2066839
36 meter E =
0005246
Z = 5275087
03 I = 51
97826
XDOT = -2598
913309 Wp = 61
28712
YDOT = -7148
909849 meter/sec RA = 75
71514 deg
ZDOT = 965
106904 TA = 19
52906
MA = 19
50897
Ha = 226
984 n
mi
Hp = 218
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12237275
12 X = -3778381
12
Y = 6780969
03 feet Y = 2024858
07 meter
Z = 17306715
98 Z = 5256849
64
XDOT = -8526
618469 XDOT = -2523
467617
YDOT = -23454
428640 feet/sec YDOT = -7177
550729 meter/sec
ZDOT = 3166
361234 ZDOT = 952
664932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5143826
32 X = 1567838
26
Y = 13113841
10 feet Y = 3997098
77 meter
Z = 17228554
31 Z = 5251263
36
XDOT = -23399
960512 XDOT = -7132
307964
YDOT = 5094
120729 feet/sec YDOT = 1552
687998 meter/sec
ZDOT = 3114
595599 ZDOT = 949
328739
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 14318
13431882
00016717 00000-0 10270-3 0 9149
2 25544 51
6458 76
2233 0004631 20
6103 339
5234 15
51099459 34598
Satellite: ISS
Catalog Number: 25544
Epoch time: 14318
13431882 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 76
2233 deg
Eccentricity:
0004631
Arg of perigee: 20
6103 deg
Mean anomaly: 339
5234 deg
Mean motion: 15
51099459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 301
Coasting Arc #16 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2014/319/02:01:27
395
Vector Time (MET): N/A
Weight (LBS) : 931416
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3886644
61 A = 6786149
02 meter
Y = -1567622
12 meter E =
0017476
Z = -5352070
09 I = 51
96940
XDOT = 2648
008027 Wp = 74
29193
YDOT = 7176
075765 meter/sec RA = 70
76974 deg
ZDOT = -174
782682 TA = 194
02185
MA = 194
07044
Ha = 226
949 n
mi
Hp = 218
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12751458
70 X = 3929884
25
Y = -5143117
18 feet Y = -1523917
49 meter
Z = -17559285
08 Z = -5333084
00
XDOT = 8687
690378 XDOT = 2568
415721
YDOT = 23543
555661 feet/sec YDOT = 7205
242478 meter/sec
ZDOT = -573
433997 ZDOT = -162
112339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3683642
74 X = -1122774
31
Y = -13354007
14 feet Y = -4070301
38 meter
Z = -17478018
05 Z = -5327299
90
XDOT = 23389
650938 XDOT = 7129
165606
YDOT = -5752
632891 feet/sec YDOT = -1753
402505 meter/sec
ZDOT = -520
709357 ZDOT = -158
712212
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 14319
10074353
00016717 00000-0 10270-3 0 9154
2 25544 51
6465 71
4275 0004802 24
6761 335
4619 15
51117125 34743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14319
10074353 = yrday
fracday
Element set: 915
Inclination: 51
6465 deg
RA of node: 71
4275 deg
Eccentricity:
0004802
Arg of perigee: 24
6761 deg
Mean anomaly: 335
4619 deg
Mean motion: 15
51117125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 291
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