[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 9th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
016/01:58:23
490 -1
1 2
9 2
9
N/A 2
6 -0
2 228
6
000/00:06:46
980 -0
8 -0
1 220
8
Coasting Arc #1 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/008/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -878055
92 A = 6788570
87 meter
Y = -4115228
75 meter E =
0005876
Z = 5324673
26 I = 51
68966
XDOT = 7517
170056 Wp = 28
39649
YDOT = -1494
765097 meter/sec RA = 169
28145 deg
ZDOT = 89
370077 TA = 60
78147
MA = 60
72271
Ha = 228
037 n
mi
Hp = 220
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2880760
89 X = -857838
78
Y = -13501406
66 feet Y = -4124934
87 meter
Z = 17469400
46 Z = 5320456
76
XDOT = 24662
631417 XDOT = 7532
892028
YDOT = -4904
084964 feet/sec YDOT = -1410
615401 meter/sec
ZDOT = 293
208914 ZDOT = 125
925525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2260740
93 X = 689073
84
Y = -13640958
79 feet Y = -4157764
24 meter
Z = 17452220
81 Z = 5319436
90
XDOT = 23715
384542 XDOT = 7228
449208
YDOT = 4481
880744 feet/sec YDOT = 1366
077251 meter/sec
ZDOT = 447
501515 ZDOT = 136
398462
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 14008
68978099
00016717 00000-0 10270-3 0 9006
2 25544 51
6487 170
1384 0005472 3
6800 356
4390 15
50282239 26580
Satellite: ISS
Catalog Number: 25544
Epoch time: 14008
68978099 = yrday
fracday
Element set: 900
Inclination: 51
6487 deg
RA of node: 170
1384 deg
Eccentricity:
0005472
Arg of perigee: 3
6800 deg
Mean anomaly: 356
4390 deg
Mean motion: 15
50282239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 320
Coasting Arc #2 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/009/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 715361
48 A = 6788604
76 meter
Y = 4164900
62 meter E =
0016257
Z = -5326103
39 I = 51
71986
XDOT = -7433
999471 Wp = 73
10796
YDOT = 1766
965509 meter/sec RA = 164
32801 deg
ZDOT = 388
839292 TA = 200
57131
MA = 200
63684
Ha = 228
158 n
mi
Hp = 220
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2346986
49 X = 694607
95
Y = 13664372
10 feet Y = 4172784
45 meter
Z = -17474092
48 Z = -5322678
48
XDOT = -24389
762045 XDOT = -7455
094416
YDOT = 5797
130935 feet/sec YDOT = 1683
715817 meter/sec
ZDOT = 1275
719462 ZDOT = 352
674830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2582504
19 X = -787147
28
Y = 13639552
12 feet Y = 4157335
49 meter
Z = -17460257
97 Z = -5321886
63
XDOT = -23864
818116 XDOT = -7273
996562
YDOT = -3104
438721 feet/sec YDOT = -946
232922 meter/sec
ZDOT = 1123
017014 ZDOT = 342
295586
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 14009
65672047
00016717 00000-0 10270-3 0 9019
2 25544 51
6485 165
3475 0005574 7
7571 352
3665 15
50286139 26738
Satellite: ISS
Catalog Number: 25544
Epoch time: 14009
65672047 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 165
3475 deg
Eccentricity:
0005574
Arg of perigee: 7
7571 deg
Mean anomaly: 352
3665 deg
Mean motion: 15
50286139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 321
Coasting Arc #3 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/010/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -519023
08 A = 6788644
07 meter
Y = -4244064
62 meter E =
0008197
Z = 5270447
18 I = 51
75015
XDOT = 7341
903246 Wp = 29
13008
YDOT = -2013
218407 meter/sec RA = 159
37453 deg
ZDOT = -890
570481 TA = 69
42211
MA = 69
33419
Ha = 228
163 n
mi
Hp = 219
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1702831
64 X = -497128
53
Y = -13924096
53 feet Y = -4249746
56 meter
Z = 17291493
36 Z = 5267978
77
XDOT = 24087
609076 XDOT = 7368
195935
YDOT = -6605
047267 feet/sec YDOT = -1930
969498 meter/sec
ZDOT = -2921
819163 ZDOT = -854
840851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3042669
85 X = 927405
77
Y = -13706227
81 feet Y = -4177658
24 meter
Z = 17281704
83 Z = 5267463
63
XDOT = 23913
909920 XDOT = 7288
959744
YDOT = 1783
627686 feet/sec YDOT = 543
649719 meter/sec
ZDOT = -2770
893823 ZDOT = -844
568437
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 14010
68810258
00016717 00000-0 10270-3 0 9023
2 25544 51
6486 160
2353 0005644 11
0011 349
1262 15
50337121 26895
Satellite: ISS
Catalog Number: 25544
Epoch time: 14010
68810258 = yrday
fracday
Element set: 902
Inclination: 51
6486 deg
RA of node: 160
2353 deg
Eccentricity:
0005644
Arg of perigee: 11
0011 deg
Mean anomaly: 349
1262 deg
Mean motion: 15
50337121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 272
Coasting Arc #4 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/011/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 366488
49 A = 6788977
43 meter
Y = 4364318
25 meter E =
0015518
Z = -5199907
20 I = 51
77967
XDOT = -7186
535493 Wp = 78
89342
YDOT = 2236
908692 meter/sec RA = 154
42481 deg
ZDOT = 1377
348498 TA = 204
31536
MA = 204
38866
Ha = 228
279 n
mi
Hp = 219
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1202390
04 X = 342917
86
Y = 14318629
44 feet Y = 4368285
13 meter
Z = -17060062
98 Z = -5198183
80
XDOT = -23577
872354 XDOT = -7217
705678
YDOT = 7338
939279 feet/sec YDOT = 2156
369890 meter/sec
ZDOT = 4518
859903 ZDOT = 1342
361886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3409217
00 X = -1039129
34
Y = 13966825
04 feet Y = 4257088
27 meter
Z = -17053435
95 Z = -5197887
28
XDOT = -23691
274101 XDOT = -7221
100346
YDOT = -471
558947 feet/sec YDOT = -143
731167 meter/sec
ZDOT = 4371
013257 ZDOT = 1332
284841
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 14011
65500767
00016717 00000-0 10270-3 0 9033
2 25544 51
6483 155
4441 0005752 15
0928 345
0394 15
50345136 27041
Satellite: ISS
Catalog Number: 25544
Epoch time: 14011
65500767 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 155
4441 deg
Eccentricity:
0005752
Arg of perigee: 15
0928 deg
Mean anomaly: 345
0394 deg
Mean motion: 15
50345136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 288
Coasting Arc #5 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/012/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -186570
40 A = 6789375
40 meter
Y = -4514784
67 meter E =
0010723
Z = 5064241
85 I = 51
80930
XDOT = 7024
195332 Wp = 36
52109
YDOT = -2418
529577 meter/sec RA = 149
47508 deg
ZDOT = -1886
888455 TA = 71
79055
MA = 71
67385
Ha = 228
271 n
mi
Hp = 219
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -612107
61 X = -160671
50
Y = -14812285
65 feet Y = -4516726
58 meter
Z = 16614966
70 Z = 5063398
09
XDOT = 23045
260276 XDOT = 7059
883652
YDOT = -7934
808324 feet/sec YDOT = -2339
780858 meter/sec
ZDOT = -6190
578922 ZDOT = -1852
679620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3884815
31 X = 1184091
71
Y = -14310234
22 feet Y = -4361759
39 meter
Z = 16612074
13 Z = 5063360
19
XDOT = 23361
959338 XDOT = 7120
725206
YDOT = -716
221993 feet/sec YDOT = -218
304463 meter/sec
ZDOT = -6045
963644 ZDOT = -1842
809719
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 14012
68635297
00016717 00000-0 10270-3 0 9045
2 25544 51
6486 150
3316 0005819 17
8178 342
3176 15
50392657 27206
Satellite: ISS
Catalog Number: 25544
Epoch time: 14012
68635297 = yrday
fracday
Element set: 904
Inclination: 51
6486 deg
RA of node: 150
3316 deg
Eccentricity:
0005819
Arg of perigee: 17
8178 deg
Mean anomaly: 342
3176 deg
Mean motion: 15
50392657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 315
Coasting Arc #6 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/013/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 67266
08 A = 6790001
48 meter
Y = 4695395
43 meter E =
0013940
Z = -4915588
38 I = 51
83720
XDOT = -6809
392324 Wp = 82
08889
YDOT = 2567
691212 meter/sec RA = 144
52928 deg
ZDOT = 2367
106017 TA = 211
03626
MA = 211
11869
Ha = 228
394 n
mi
Hp = 219
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 220689
23 X = 38634
23
Y = 15404840
65 feet Y = 4695987
92 meter
Z = -16127258
47 Z = -4915330
81
XDOT = -22340
525998 XDOT = -6849
097257
YDOT = 8424
183768 feet/sec YDOT = 2491
322062 meter/sec
ZDOT = 7766
095856 ZDOT = 2333
931024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4188314
71 X = -1276598
32
Y = 14826612
36 feet Y = 4519151
45 meter
Z = -16126867
98 Z = -4915469
36
XDOT = -22791
484684 XDOT = -6946
844532
YDOT = 1829
101523 feet/sec YDOT = 557
510144 meter/sec
ZDOT = 7625
797519 ZDOT = 2324
343084
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 14013
65322348
00016717 00000-0 10270-3 0 9054
2 25544 51
6482 145
5402 0005944 22
3771 337
7638 15
50404179 27353
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
65322348 = yrday
fracday
Element set: 905
Inclination: 51
6482 deg
RA of node: 145
5402 deg
Eccentricity:
0005944
Arg of perigee: 22
3771 deg
Mean anomaly: 337
7638 deg
Mean motion: 15
50404179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 301
Coasting Arc #7 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/014/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73603
69 A = 6790735
04 meter
Y = -4902767
75 meter E =
0013191
Z = 4693854
71 I = 51
86545
XDOT = 6592
755631 Wp = 47
21894
YDOT = -2658
466813 meter/sec RA = 139
58376 deg
ZDOT = -2866
330516 TA = 71
24071
MA = 71
09762
Ha = 228
371 n
mi
Hp = 219
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 241481
92 X = 105621
12
Y = -16085196
02 feet Y = -4901765
97 meter
Z = 15399785
81 Z = 4694289
69
XDOT = 21629
775692 XDOT = 6635
916742
YDOT = -8722
003979 feet/sec YDOT = -2584
500886 meter/sec
ZDOT = -9403
971510 ZDOT = -2834
199605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4568674
26 X = 1392531
92
Y = -15422064
20 feet Y = -4700645
17 meter
Z = 15402350
43 Z = 4694636
41
XDOT = 22126
941218 XDOT = 6744
291683
YDOT = -2746
588763 feet/sec YDOT = -837
160255 meter/sec
ZDOT = -9268
043818 ZDOT = -2824
899756
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 14014
68453158
00016717 00000-0 10270-3 0 9063
2 25544 51
6489 140
4276 0006004 24
4093 335
7341 15
50448901 27519
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
68453158 = yrday
fracday
Element set: 906
Inclination: 51
6489 deg
RA of node: 140
4276 deg
Eccentricity:
0006004
Arg of perigee: 24
4093 deg
Mean anomaly: 335
7341 deg
Mean motion: 15
50448901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 296
Coasting Arc #8 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/015/15:23:17
517
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -140532
03 A = 6791602
01 meter
Y = 5124750
08 meter E =
0011935
Z = -4463554
34 I = 51
89079
XDOT = -6340
226710 Wp = 80
25914
YDOT = 2711
484611 meter/sec RA = 134
64184 deg
ZDOT = 3322
287678 TA = 223
17295
MA = 223
26659
Ha = 228
502 n
mi
Hp = 219
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -461063
09 X = -176145
52
Y = 16813484
52 feet Y = 5122979
70 meter
Z = -14644207
15 Z = -4464323
21
XDOT = -20801
268735 XDOT = -6386
214267
YDOT = 8895
946888 feet/sec YDOT = 2640
326823 meter/sec
ZDOT = 10899
893958 ZDOT = 3291
376697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4707854
17 X = -1434953
95
Y = 16143869
00 feet Y = 4920651
27 meter
Z = -14648216
50 Z = -4464776
39
XDOT = -21283
154209 XDOT = -6487
105403
YDOT = 3536
462440 feet/sec YDOT = 1077
913752 meter/sec
ZDOT = 10769
086803 ZDOT = 3282
417657
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 14015
65136748
00016717 00000-0 10270-3 0 9075
2 25544 51
6482 135
6359 0006149 29
6588 330
4910 15
50463466 27669
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
65136748 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 135
6359 deg
Eccentricity:
0006149
Arg of perigee: 29
6588 deg
Mean anomaly: 330
4910 deg
Mean motion: 15
50463466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 328
Coasting Arc #9 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2014/016/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3846342
01 A = 6790009
93 meter
Y = 1920276
29 meter E =
0016635
Z = -5269883
99 I = 51
89085
XDOT = -4484
533387 Wp = 66
47828
YDOT = 6108
573121 meter/sec RA = 132
48371 deg
ZDOT = -1043
408336 TA = 193
51642
MA = 193
56103
Ha = 228
629 n
mi
Hp = 220
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12619232
33 X = 3850182
16
Y = 6300119
07 feet Y = 1963310
29 meter
Z = -17289645
64 Z = -5251189
89
XDOT = -14713
036048 XDOT = -4547
439058
YDOT = 20041
250397 feet/sec YDOT = 6058
072536 meter/sec
ZDOT = -3423
255696 ZDOT = -1065
345671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6825908
74 X = -2080536
98
Y = -12452090
68 feet Y = -3795397
24 meter
Z = -17211065
59 Z = -5245932
79
XDOT = 22612
863535 XDOT = 6892
400805
YDOT = -7517
514071 feet/sec YDOT = -2291
338289 meter/sec
ZDOT = -3516
719936 ZDOT = -1071
896236
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 14016
10255498
00016717 00000-0 10270-3 0 9081
2 25544 51
6494 133
3994 0004810 13
5393 346
5886 15
49923878 27735
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
10255498 = yrday
fracday
Element set: 908
Inclination: 51
6494 deg
RA of node: 133
3994 deg
Eccentricity:
0004810
Arg of perigee: 13
5393 deg
Mean anomaly: 346
5886 deg
Mean motion: 15
49923878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 340
Coasting Arc #10 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3770289
10 A = 6789680
46 meter
Y = -1919789
32 meter E =
0005167
Z = 5306457
89 I = 51
91038
XDOT = 4211
147650 Wp = 51
89405
YDOT = -6367
678940 meter/sec RA = 127
54614 deg
ZDOT = 690
987770 TA = 31
54469
MA = 31
51372
Ha = 228
727 n
mi
Hp = 220
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12369714
88 X = -3774317
97
Y = -6298521
37 feet Y = -1961973
82 meter
Z = 17409638
73 Z = 5288132
83
XDOT = 13816
101214 XDOT = 4278
682940
YDOT = -20891
335106 feet/sec YDOT = -6320
209613 meter/sec
ZDOT = 2267
020242 ZDOT = 711
608363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6833643
34 X = 2082894
49
Y = 12192568
97 feet Y = 3716295
02 meter
Z = 17332608
55 Z = 5282979
08
XDOT = -22227
264552 XDOT = -6774
870235
YDOT = 9122
485887 feet/sec YDOT = 2780
533698 meter/sec
ZDOT = 2354
980288 ZDOT = 717
797992
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 14017
13418356
00016717 00000-0 10270-3 0 9090
2 25544 51
6495 128
2896 0004797 16
0092 344
1209 15
49958300 27896
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13418356 = yrday
fracday
Element set: 909
Inclination: 51
6495 deg
RA of node: 128
2896 deg
Eccentricity:
0004797
Arg of perigee: 16
0092 deg
Mean anomaly: 344
1209 deg
Mean motion: 15
49958300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 330
Coasting Arc #11 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2014/018/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3730289
78 A = 6789505
03 meter
Y = 1939074
48 meter E =
0017269
Z = -5345691
16 I = 51
92863
XDOT = -3897
637669 Wp = 72
11503
YDOT = 6573
536024 meter/sec RA = 122
60963 deg
ZDOT = -331
088051 TA = 194
70806
MA = 194
75837
Ha = 228
699 n
mi
Hp = 220
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12238483
53 X = 3734296
55
Y = 6361792
93 feet Y = 1980811
47 meter
Z = -17538356
81 Z = -5327560
50
XDOT = -12787
525160 XDOT = -3969
246445
YDOT = 21566
719239 feet/sec YDOT = 6529
549770 meter/sec
ZDOT = -1086
246888 ZDOT = -350
195685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6898514
48 X = -2102667
21
Y = -12055325
42 feet Y = -3674463
19 meter
Z = -17462144
06 Z = -5322461
51
XDOT = 21579
174960 XDOT = 6577
332528
YDOT = -10636
369680 feet/sec YDOT = -3241
965478 meter/sec
ZDOT = -1167
864863 ZDOT = -355
965210
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 14018
10131950
00016717 00000-0 10270-3 0 9102
2 25544 51
6500 123
4992 0004943 19
5745 340
5595 15
49980256 28044
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
10131950 = yrday
fracday
Element set: 910
Inclination: 51
6500 deg
RA of node: 123
4992 deg
Eccentricity:
0004943
Arg of perigee: 19
5745 deg
Mean anomaly: 340
5595 deg
Mean motion: 15
49980256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 300
Coasting Arc #12 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2014/019/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3677799
72 A = 6789346
27 meter
Y = -1994065
71 meter E =
0006304
Z = 5343543
78 I = 51
94434
XDOT = 3593
743097 Wp = 42
95999
YDOT = -6770
701196 meter/sec RA = 117
67371 deg
ZDOT = -48
652402 TA = 47
52848
MA = 47
47521
Ha = 228
800 n
mi
Hp = 220
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12066272
05 X = -3681185
06
Y = -6542210
32 feet Y = -2035212
15 meter
Z = 17531311
62 Z = 5325669
63
XDOT = 11790
495726 XDOT = 3669
423828
YDOT = -22213
586602 feet/sec YDOT = -6730
090511 meter/sec
ZDOT = -159
620743 ZDOT = -31
011001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6863197
87 X = 2091902
71
Y = 11996684
18 feet Y = 3656589
34 meter
Z = 17456185
37 Z = 5320645
30
XDOT = -20892
096302 XDOT = -6367
910953
YDOT = 12096
325661 feet/sec YDOT = 3686
960061 meter/sec
ZDOT = -84
150247 ZDOT = -25
648995
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 14019
13291164
00016717 00000-0 10270-3 0 9111
2 25544 51
6500 118
3891 0004943 22
4162 337
7204 15
50014664 28207
Satellite: ISS
Catalog Number: 25544
Epoch time: 14019
13291164 = yrday
fracday
Element set: 911
Inclination: 51
6500 deg
RA of node: 118
3891 deg
Eccentricity:
0004943
Arg of perigee: 22
4162 deg
Mean anomaly: 337
7204 deg
Mean motion: 15
50014664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 272
Coasting Arc #13 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2014/020/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670362
49 A = 6789357
67 meter
Y = 2057616
79 meter E =
0017314
Z = -5342589
55 I = 51
95788
XDOT = -3257
621580 Wp = 77
64702
YDOT = 6907
986287 meter/sec RA = 112
73837 deg
ZDOT = 427
282838 TA = 196
39206
MA = 196
44812
Ha = 228
755 n
mi
Hp = 220
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12041871
68 X = 3673033
16
Y = 6750711
25 feet Y = 2098676
00 meter
Z = -17528180
95 Z = -5324753
26
XDOT = -10687
734841 XDOT = -3336
701681
YDOT = 22663
997006 feet/sec YDOT = 6871
115325 meter/sec
ZDOT = 1401
846583 ZDOT = 411
265860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6940236
79 X = -2115384
17
Y = -12043009
51 feet Y = -3670709
30 meter
Z = -17453221
44 Z = -5319741
90
XDOT = 19962
196166 XDOT = 6084
477391
YDOT = -13413
338300 feet/sec YDOT = -4088
385514 meter/sec
ZDOT = 1333
200583 ZDOT = 406
359538
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 14020
10001327
00016717 00000-0 10270-3 0 9121
2 25544 51
6498 113
5981 0005052 25
4010 334
7388 15
50034334 28359
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
10001327 = yrday
fracday
Element set: 912
Inclination: 51
6498 deg
RA of node: 113
5981 deg
Eccentricity:
0005052
Arg of perigee: 25
4010 deg
Mean anomaly: 334
7388 deg
Mean motion: 15
50034334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 264
Coasting Arc #14 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2014/021/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3656546
36 A = 6789405
42 meter
Y = -2157281
02 meter E =
0007994
Z = 5294471
14 I = 51
96950
XDOT = 2938
759563 Wp = 41
14656
YDOT = -7031
186764 meter/sec RA = 107
80364 deg
ZDOT = -828
743649 TA = 56
78073
MA = 56
70411
Ha = 228
854 n
mi
Hp = 220
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11996543
18 X = -3657869
92
Y = -7077693
63 feet Y = -2198178
15 meter
Z = 17370312
14 Z = 5276705
20
XDOT = 9641
599615 XDOT = 3021
191167
YDOT = -23068
198046 feet/sec YDOT = -6997
862792 meter/sec
ZDOT = -2718
975225 ZDOT = -814
267398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6942713
98 X = 2116139
22
Y = 12181842
31 feet Y = 3713025
54 meter
Z = 17295663
61 Z = 5271718
27
XDOT = -19013
027933 XDOT = -5795
170914
YDOT = 14638
795268 feet/sec YDOT = 4461
904798 meter/sec
ZDOT = -2656
802197 ZDOT = -809
793310
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 14021
13156912
00016717 00000-0 10270-3 0 9137
2 25544 51
6497 108
4877 0005061 28
5792 331
5636 15
50069501 28519
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
13156912 = yrday
fracday
Element set: 913
Inclination: 51
6497 deg
RA of node: 108
4877 deg
Eccentricity:
0005061
Arg of perigee: 28
5792 deg
Mean anomaly: 331
5636 deg
Mean motion: 15
50069501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 300
Coasting Arc #15 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2014/022/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3693910
46 A = 6789629
42 meter
Y = 2251569
06 meter E =
0016730
Z = -5246962
62 I = 51
97816
XDOT = -2597
995228 Wp = 82
82167
YDOT = 7091
216724 meter/sec RA = 102
86883 deg
ZDOT = 1219
319521 TA = 198
82050
MA = 198
88242
Ha = 228
805 n
mi
Hp = 219
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12119128
82 X = 3693946
19
Y = 7387037
60 feet Y = 2292876
82 meter
Z = -17214444
28 Z = -5229018
25
XDOT = -8523
606392 XDOT = -2683
020713
YDOT = 23265
146732 feet/sec YDOT = 7061
688902 meter/sec
ZDOT = 4000
392128 ZDOT = 1206
492284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7107473
63 X = -2166357
96
Y = -12390126
40 feet Y = -3776510
53 meter
Z = -17139057
33 Z = -5223984
67
XDOT = 17859
418652 XDOT = 5443
550805
YDOT = -15677
720040 feet/sec YDOT = -4778
569068 meter/sec
ZDOT = 3945
157669 ZDOT = 1202
484057
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 14022
09863684
00016717 00000-0 10270-3 0 9145
2 25544 51
6490 103
6959 0005130 31
5246 328
6211 15
50085634 28662
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
09863684 = yrday
fracday
Element set: 914
Inclination: 51
6490 deg
RA of node: 103
6959 deg
Eccentricity:
0005130
Arg of perigee: 31
5246 deg
Mean anomaly: 328
6211 deg
Mean motion: 15
50085634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 301
Coasting Arc #16 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2014/023/02:01:46
980
Vector Time (MET): N/A
Weight (LBS) : 900891
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3729782
61 A = 6789908
73 meter
Y = -2380100
84 meter E =
0009956
Z = 5146084
87 I = 51
98563
XDOT = 2284
175425 Wp = 44
71438
YDOT = -7132
497767 meter/sec RA = 97
93495 deg
ZDOT = -1634
502711 TA = 61
03786
MA = 60
93807
Ha = 228
889 n
mi
Hp = 219
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12236819
59 X = -3727888
44
Y = -7808729
80 feet Y = -2421798
98 meter
Z = 16883480
56 Z = 5127970
88
XDOT = 7494
013863 XDOT = 2371
702676
YDOT = -23400
583224 feet/sec YDOT = -7106
465291 meter/sec
ZDOT = -5362
541703 ZDOT = -1623
193879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7223362
92 X = 2201681
02
Y = 12692608
35 feet Y = 3868707
02 meter
Z = 16807398
73 Z = 5122895
13
XDOT = -16718
489731 XDOT = -5095
795670
YDOT = 16589
237563 feet/sec YDOT = 5056
399609 meter/sec
ZDOT = -5313
696090 ZDOT = -1619
614568
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 14023
13015679
00016717 00000-0 10270-3 0 9155
2 25544 51
6491 98
5852 0005133 34
7528 325
3957 15
50121493 28821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
13015679 = yrday
fracday
Element set: 915
Inclination: 51
6491 deg
RA of node: 98
5852 deg
Eccentricity:
0005133
Arg of perigee: 34
7528 deg
Mean anomaly: 325
3957 deg
Mean motion: 15
50121493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2882
Checksum: 310
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