[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 21st 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) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 720)
---------------------------------------
Vector Time (GMT): 2014/141/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1696353
55 A = 6789370
49 meter
Y = -4241335
76 meter E =
0005959
Z = 5017658
37 I = 51
34974
XDOT = 5818
100955 Wp = 89
66596
YDOT = 4606
552966 meter/sec RA = 230
34327 deg
ZDOT = 1924
918979 TA = 341
56978
MA = 341
59136
Ha = 227
453 n
mi
Hp = 219
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5565464
41 X = 1719280
75
Y = -13915143
57 feet Y = -4222238
03 meter
Z = 16462133
76 Z = 5025954
60
XDOT = 19088
257727 XDOT = 5756
806331
YDOT = 15113
362750 feet/sec YDOT = 4671
271923 meter/sec
ZDOT = 6315
350982 ZDOT = 1953
033927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14601337
44 X = -4450487
65
Y = -3198080
26 feet Y = -974774
86 meter
Z = 16497899
57 Z = 5028559
79
XDOT = 11685
436336 XDOT = 3561
720995
YDOT = -20129
923583 feet/sec YDOT = -6135
600708 meter/sec
ZDOT = 6433
573351 ZDOT = 1960
953157
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 14141
66494355
00016717 00000-0 10270-3 0 9000
2 25544 51
6456 231
0747 0003488 19
3183 340
8100 15
50442354 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
66494355 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 231
0747 deg
Eccentricity:
0003488
Arg of perigee: 19
3183 deg
Mean anomaly: 340
8100 deg
Mean motion: 15
50442354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 284
Coasting Arc #2 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2014/142/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1827237
29 A = 6788778
90 meter
Y = 4025657
71 meter E =
0016041
Z = -5166180
58 I = 51
36894
XDOT = -6017
625462 Wp = 68
80138
YDOT = -4515
502538 meter/sec RA = 225
36283 deg
ZDOT = -1388
058056 TA = 187
75610
MA = 187
78093
Ha = 227
602 n
mi
Hp = 219
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5994873
01 X = -1847021
45
Y = 13207538
41 feet Y = 4005113
88 meter
Z = -16949411
35 Z = -5175105
07
XDOT = -19742
865690 XDOT = -5959
942046
YDOT = -14814
640873 feet/sec YDOT = -4582
472929 meter/sec
ZDOT = -4553
996248 ZDOT = -1417
151090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14031942
35 X = 4276936
03
Y = 3489899
44 feet Y = 1063721
35 meter
Z = -16987798
98 Z = -5177881
13
XDOT = -10887
211589 XDOT = -3318
422092
YDOT = 20976
483033 feet/sec YDOT = 6393
632029 meter/sec
ZDOT = -4676
385628 ZDOT = -1425
362339
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 14142
63176777
00016717 00000-0 10270-3 0 9014
2 25544 51
6462 226
2813 0003565 22
8939 337
2370 15
50444992 7366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
63176777 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 226
2813 deg
Eccentricity:
0003565
Arg of perigee: 22
8939 deg
Mean anomaly: 337
2370 deg
Mean motion: 15
50444992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 314
Coasting Arc #3 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2014/143/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1999230
16 A = 6788186
07 meter
Y = -3804095
48 meter E =
0004885
Z = 5250447
98 I = 51
38937
XDOT = 6213
728896 Wp = 71
16679
YDOT = 4412
852765 meter/sec RA = 220
38373 deg
ZDOT = 832
123567 TA = 10
85411
MA = 10
84358
Ha = 227
547 n
mi
Hp = 219
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6559154
08 X = 2016114
53
Y = -12480628
21 feet Y = -3781644
54 meter
Z = 17225879
20 Z = 5260200
98
XDOT = 20386
249660 XDOT = 6159
879316
YDOT = 14477
863401 feet/sec YDOT = 4482
037560 meter/sec
ZDOT = 2730
064197 ZDOT = 862
178684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13484265
73 X = -4110004
19
Y = -3939456
40 feet Y = -1200746
31 meter
Z = 17267737
49 Z = 5263206
39
XDOT = 10018
158258 XDOT = 3053
534637
YDOT = -21782
897548 feet/sec YDOT = -6639
427173 meter/sec
ZDOT = 2856
553221 ZDOT = 870
677422
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 14143
66302668
00016717 00000-0 10270-3 0 9029
2 25544 51
6456 221
1688 0003712 27
6826 332
4522 15
50497390 7529
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
66302668 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 221
1688 deg
Eccentricity:
0003712
Arg of perigee: 27
6826 deg
Mean anomaly: 332
4522 deg
Mean motion: 15
50497390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 302
Coasting Arc #4 (Orbit 766)
---------------------------------------
Vector Time (GMT): 2014/144/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2212647
75 A = 6787970
05 meter
Y = 3625116
32 meter E =
0017083
Z = -5309835
64 I = 51
41409
XDOT = -6349
362340 Wp = 77
36487
YDOT = -4259
444450 meter/sec RA = 215
40565 deg
ZDOT = -259
220570 TA = 190
13341
MA = 190
16790
Ha = 227
661 n
mi
Hp = 219
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7259343
00 X = -2227226
29
Y = 11893426
26 feet Y = 3600291
77 meter
Z = -17420720
59 Z = -5320619
81
XDOT = -20831
241274 XDOT = -6300
001134
YDOT = -13974
555281 feet/sec YDOT = -4330
171094 meter/sec
ZDOT = -850
461189 ZDOT = -289
945632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13121475
91 X = 3999425
86
Y = 4512965
91 feet Y = 1375552
01 meter
Z = -17466916
26 Z = -5323916
08
XDOT = -8995
552026 XDOT = -2741
844258
YDOT = 22324
985570 feet/sec YDOT = 6804
655602 meter/sec
ZDOT = -979
820923 ZDOT = -298
649417
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 14144
62981550
00016717 00000-0 10270-3 0 9030
2 25544 51
6467 216
3756 0003737 29
8689 330
2675 15
50501232 7673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
62981550 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 216
3756 deg
Eccentricity:
0003737
Arg of perigee: 29
8689 deg
Mean anomaly: 330
2675 deg
Mean motion: 15
50501232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 767
Checksum: 317
Coasting Arc #5 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2014/145/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2465186
13 A = 6787804
27 meter
Y = -3449276
70 meter E =
0006016
Z = 5297007
75 I = 51
43860
XDOT = 6466
260203 Wp = 51
41304
YDOT = 4105
230534 meter/sec RA = 210
42884 deg
ZDOT = -332
190380 TA = 41
78650
MA = 41
74057
Ha = 227
604 n
mi
Hp = 219
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8087881
00 X = 2477841
89
Y = -11316524
60 feet Y = -3421638
93 meter
Z = 17378634
35 Z = 5309014
04
XDOT = 21214
764447 XDOT = 6421
487696
YDOT = 13468
604113 feet/sec YDOT = 4177
290089 meter/sec
ZDOT = -1089
863453 ZDOT = -300
886162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12821841
53 X = -3908097
30
Y = -5224050
66 feet Y = -1592290
64 meter
Z = 17429978
61 Z = 5312657
48
XDOT = 7959
581138 XDOT = 2426
080331
YDOT = -22775
250157 feet/sec YDOT = -6941
896248 meter/sec
ZDOT = -958
016689 ZDOT = -292
003487
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 14145
66103786
00016717 00000-0 10270-3 0 9043
2 25544 51
6454 211
2626 0003888 34
8512 325
2893 15
50552264 7832
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
66103786 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 211
2626 deg
Eccentricity:
0003888
Arg of perigee: 34
8512 deg
Mean anomaly: 325
2893 deg
Mean motion: 15
50552264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 309
Coasting Arc #6 (Orbit 797)
---------------------------------------
Vector Time (GMT): 2014/146/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2740592
69 A = 6788041
74 meter
Y = 3330867
69 meter E =
0016696
Z = -5255647
48 I = 51
46739
XDOT = -6510
704428 Wp = 85
52530
YDOT = -3910
784991 meter/sec RA = 205
45432 deg
ZDOT = 920
322713 TA = 193
29874
MA = 193
34281
Ha = 227
701 n
mi
Hp = 219
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8991445
82 X = -2752104
80
Y = 10928043
61 feet Y = 3300156
64 meter
Z = -17242937
93 Z = -5268988
86
XDOT = -21360
578832 XDOT = -6470
959962
YDOT = -12830
659419 feet/sec YDOT = -3983
369712 meter/sec
ZDOT = 3019
431473 ZDOT = 888
790297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12751790
88 X = 3886745
86
Y = 5974255
48 feet Y = 1820953
07 meter
Z = -17299920
36 Z = -5273015
72
XDOT = -6838
434098 XDOT = -2084
354713
YDOT = 22919
076577 feet/sec YDOT = 6985
734541 meter/sec
ZDOT = 2886
575429 ZDOT = 879
828191
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 14146
62779231
00016717 00000-0 10270-3 0 9055
2 25544 51
6461 206
4697 0003876 36
2671 323
8742 15
50553485 7982
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
62779231 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 206
4697 deg
Eccentricity:
0003876
Arg of perigee: 36
2671 deg
Mean anomaly: 323
8742 deg
Mean motion: 15
50553485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 798
Checksum: 331
Coasting Arc #7 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2014/147/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3048496
15 A = 6788351
40 meter
Y = -3221853
20 meter E =
0008589
Z = 5134564
24 I = 51
49571
XDOT = 6521
938992 Wp = 48
75485
YDOT = 3730
391031 meter/sec RA = 200
48069 deg
ZDOT = -1524
240163 TA = 56
00393
MA = 55
92236
Ha = 227
620 n
mi
Hp = 219
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10001627
79 X = 3059354
58
Y = -10570384
52 feet Y = -3187702
71 meter
Z = 16845683
20 Z = 5149399
75
XDOT = 21397
437639 XDOT = 6487
144581
YDOT = 12238
815719 feet/sec YDOT = 3803
129132 meter/sec
ZDOT = -5000
787935 ZDOT = -1492
641124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12769190
45 X = -3892049
25
Y = -6824717
42 feet Y = -2080173
87 meter
Z = 16908980
97 Z = 5153857
40
XDOT = 5780
494994 XDOT = 1761
894874
YDOT = -22933
849589 feet/sec YDOT = -6990
237355 meter/sec
ZDOT = -4867
606874 ZDOT = -1483
646575
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 14147
65897877
00016717 00000-0 10270-3 0 9067
2 25544 51
6444 201
3560 0003992 40
7106 319
4343 15
50606333 8146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
65897877 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 201
3560 deg
Eccentricity:
0003992
Arg of perigee: 40
7106 deg
Mean anomaly: 319
4343 deg
Mean motion: 15
50606333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 307
Coasting Arc #8 (Orbit 828)
---------------------------------------
Vector Time (GMT): 2014/148/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3356177
82 A = 6789047
50 meter
Y = 3179488
93 meter E =
0014889
Z = -4984794
83 I = 51
52746
XDOT = -6456
763098 Wp = 91
85110
YDOT = -3526
238281 meter/sec RA = 195
51043 deg
ZDOT = 2103
044058 TA = 198
67396
MA = 198
72865
Ha = 227
726 n
mi
Hp = 219
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11011082
08 X = -3367267
25
Y = 10431394
14 feet Y = 3141896
52 meter
Z = -16354313
76 Z = -5001125
52
XDOT = -21183
605966 XDOT = -6427
068083
YDOT = -11569
023232 feet/sec YDOT = -3598
276139 meter/sec
ZDOT = 6899
750847 ZDOT = 2071
749288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13029836
96 X = 3971494
31
Y = 7615701
00 feet Y = 2321265
66 meter
Z = -16423944
04 Z = -5006018
14
XDOT = -4722
886356 XDOT = -1439
535761
YDOT = 22640
759497 feet/sec YDOT = 6900
903495 meter/sec
ZDOT = 6767
809388 ZDOT = 2062
828302
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 14148
62569976
00016717 00000-0 10270-3 0 9072
2 25544 51
6444 196
5629 0003993 42
3456 317
8002 15
50602641 8292
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
62569976 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 196
5629 deg
Eccentricity:
0003993
Arg of perigee: 42
3456 deg
Mean anomaly: 317
8002 deg
Mean motion: 15
50602641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 829
Checksum: 328
Coasting Arc #9 (Orbit 844)
---------------------------------------
Vector Time (GMT): 2014/149/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685940
34 A = 6789802
50 meter
Y = -3148182
22 meter E =
0011485
Z = 4748822
27 I = 51
55932
XDOT = 6346
539470 Wp = 56
60839
YDOT = 3354
093919 meter/sec RA = 190
54113 deg
ZDOT = -2691
595628 TA = 60
07996
MA = 59
96594
Ha = 227
613 n
mi
Hp = 218
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12092980
13 X = 3697801
55
Y = -10328681
82 feet Y = -3106897
90 meter
Z = 15580125
56 Z = 4766756
72
XDOT = 20821
979888 XDOT = 6321
636603
YDOT = 11004
245142 feet/sec YDOT = 3424
926070 meter/sec
ZDOT = -8830
694316 ZDOT = -2660
824751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13377809
51 X = -4077556
34
Y = -8459831
15 feet Y = -2578556
53 meter
Z = 15656551
94 Z = 4772117
03
XDOT = 3816
368202 XDOT = 1163
229028
YDOT = -22203
547849 feet/sec YDOT = -6767
641384 meter/sec
ZDOT = -8700
926179 ZDOT = -2652
042300
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 14149
65685076
00016717 00000-0 10270-3 0 9087
2 25544 51
6430 191
4486 0004045 45
7624 314
3858 15
50659504 8454
Satellite: ISS
Catalog Number: 25544
Epoch time: 14149
65685076 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 191
4486 deg
Eccentricity:
0004045
Arg of perigee: 45
7624 deg
Mean anomaly: 314
3858 deg
Mean motion: 15
50659504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 845
Checksum: 325
Coasting Arc #10 (Orbit 859)
---------------------------------------
Vector Time (GMT): 2014/150/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3990402
77 A = 6790870
50 meter
Y = 3185412
28 meter E =
0012059
Z = -4488077
00 I = 51
59330
XDOT = -6165
935743 Wp = 93
36557
YDOT = -3177
716855 meter/sec RA = 185
57583 deg
ZDOT = 3233
655847 TA = 209
22889
MA = 209
29642
Ha = 227
740 n
mi
Hp = 218
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13091872
62 X = -4003924
37
Y = 10450827
70 feet Y = 3140713
97 meter
Z = -14724662
06 Z = -4507494
45
XDOT = -20229
447977 XDOT = -6145
651723
YDOT = -10425
580234 feet/sec YDOT = -3246
555280 meter/sec
ZDOT = 10609
107108 ZDOT = 3203
751215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13947111
15 X = 4251079
48
Y = 9146147
76 feet Y = 2787745
84 meter
Z = -14807385
75 Z = -4513291
18
XDOT = -2995
474623 XDOT = -913
020665
YDOT = 21503
409777 feet/sec YDOT = 6554
239300 meter/sec
ZDOT = 10482
961138 ZDOT = 3195
206555
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 14150
62353898
00016717 00000-0 10270-3 0 9091
2 25544 51
6427 186
6550 0004104 48
3723 311
7779 15
50652093 8609
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
62353898 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 186
6550 deg
Eccentricity:
0004104
Arg of perigee: 48
3723 deg
Mean anomaly: 311
7779 deg
Mean motion: 15
50652093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 860
Checksum: 314
Coasting Arc #11 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2014/151/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4304234
55 A = 6791952
27 meter
Y = -3229397
73 meter E =
0014131
Z = 4136391
88 I = 51
62778
XDOT = 5933
006651 Wp = 69
04603
YDOT = 3052
668721 meter/sec RA = 180
61216 deg
ZDOT = -3775
072852 TA = 59
93447
MA = 59
79440
Ha = 227
607 n
mi
Hp = 218
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14121504
42 X = 4319933
13
Y = -10595136
91 feet Y = -3181177
72 meter
Z = 13570839
51 Z = 4157339
13
XDOT = 19465
244918 XDOT = 5916
768257
YDOT = 10015
317326 feet/sec YDOT = 3118
925057 meter/sec
ZDOT = -12385
409618 ZDOT = -3746
290054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14575428
54 X = -4442590
62
Y = -9838755
56 feet Y = -2998852
69 meter
Z = 13660061
13 Z = 4163586
63
XDOT = 2413
202633 XDOT = 735
544163
YDOT = -20671
782808 feet/sec YDOT = -6300
759400 meter/sec
ZDOT = -12263
977176 ZDOT = -3738
060243
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 14151
65465492
00016717 00000-0 10270-3 0 9101
2 25544 51
6420 181
5404 0004089 50
7769 309
3744 15
50712236 8761
Satellite: ISS
Catalog Number: 25544
Epoch time: 14151
65465492 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 181
5404 deg
Eccentricity:
0004089
Arg of perigee: 50
7769 deg
Mean anomaly: 309
3744 deg
Mean motion: 15
50712236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 306
Coasting Arc #12 (Orbit 890)
---------------------------------------
Vector Time (GMT): 2014/152/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4569058
82 A = 6793214
29 meter
Y = 3335741
14 meter E =
0009334
Z = -3768078
00 I = 51
66305
XDOT = -5645
912187 Wp = 83
97707
YDOT = -2942
409566 meter/sec RA = 175
65266 deg
ZDOT = 4251
287420 TA = 231
05187
MA = 231
13508
Ha = 227
736 n
mi
Hp = 218
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14990350
44 X = -4587716
07
Y = 10944032
61 feet Y = 3284543
08 meter
Z = -12362460
62 Z = -3790318
88
XDOT = -18523
333947 XDOT = -5633
241336
YDOT = -9653
574691 feet/sec YDOT = -3005
475393 meter/sec
ZDOT = 13947
793374 ZDOT = 4223
890733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15369244
24 X = 4684545
64
Y = 10291628
67 feet Y = 3136888
42 meter
Z = -12457190
68 Z = -3796951
72
XDOT = -1983
213255 XDOT = -604
483400
YDOT = 19664
914960 feet/sec YDOT = 5993
866080 meter/sec
ZDOT = 13832
198086 ZDOT = 4216
053977
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 14152
62131056
00016717 00000-0 10270-3 0 9116
2 25544 51
6420 176
7463 0004198 54
4768 305
6774 15
50705902 8914
Satellite: ISS
Catalog Number: 25544
Epoch time: 14152
62131056 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 176
7463 deg
Eccentricity:
0004198
Arg of perigee: 54
4768 deg
Mean anomaly: 305
6774 deg
Mean motion: 15
50705902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 891
Checksum: 304
Coasting Arc #13 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2014/153/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4830268
26 A = 6794425
53 meter
Y = -3437920
74 meter E =
0016115
Z = 3306836
87 I = 51
69851
XDOT = 5305
465261 Wp = 83
30262
YDOT = 2901
527244 meter/sec RA = 170
69548 deg
ZDOT = -4711
537862 TA = 58
32909
MA = 58
17203
Ha = 227
616 n
mi
Hp = 218
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15847336
82 X = 4852289
29
Y = -11279267
51 feet Y = -3383782
76 meter
Z = 10849202
35 Z = 3330354
85
XDOT = 17406
382090 XDOT = 5295
512595
YDOT = 9519
446337 feet/sec YDOT = 2960
801168 meter/sec
ZDOT = -15457
801386 ZDOT = -4685
788493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16166482
26 X = -4927543
79
Y = -10715469
28 feet Y = -3266075
04 meter
Z = 10949370
80 Z = 3337368
22
XDOT = 1864
133952 XDOT = 568
188029
YDOT = -18568
274187 feet/sec YDOT = -5659
609972 meter/sec
ZDOT = -15349
163276 ZDOT = -4678
424966
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 14153
65239163
00016717 00000-0 10270-3 0 9129
2 25544 51
6420 171
6316 0004139 56
3733 303
7813 15
50763675 9075
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
65239163 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 171
6316 deg
Eccentricity:
0004139
Arg of perigee: 56
3733 deg
Mean anomaly: 303
7813 deg
Mean motion: 15
50763675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 298
Coasting Arc #14 (Orbit 921)
---------------------------------------
Vector Time (GMT): 2014/154/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5023651
24 A = 6795632
14 meter
Y = 3588741
27 meter E =
0008867
Z = -2840945
27 I = 51
73335
XDOT = -4935
536817 Wp = 62
42601
YDOT = -2890
448360 meter/sec RA = 165
74232 deg
ZDOT = 5092
441507 TA = 265
40466
MA = 265
50594
Ha = 227
700 n
mi
Hp = 218
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16481795
39 X = -5049607
56
Y = 11774085
52 feet Y = 3532418
68 meter
Z = -9320686
58 Z = -2865412
26
XDOT = -16192
706091 XDOT = -4927
585838
YDOT = -9483
098293 feet/sec YDOT = -2945
596676 meter/sec
ZDOT = 16707
485259 ZDOT = 5068
484381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17047806
38 X = 5196171
38
Y = 10848834
42 feet Y = 3306724
73 meter
Z = -9424911
51 Z = -2872713
03
XDOT = -1930
116455 XDOT = -588
299495
YDOT = 17414
144778 feet/sec YDOT = 5307
831328 meter/sec
ZDOT = 16606
426162 ZDOT = 5061
638694
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 14154
61901427
00016717 00000-0 10270-3 0 9136
2 25544 51
6422 166
8375 0004238 60
6911 299
4663 15
50766414 9229
Satellite: ISS
Catalog Number: 25544
Epoch time: 14154
61901427 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 166
8375 deg
Eccentricity:
0004238
Arg of perigee: 60
6911 deg
Mean anomaly: 299
4663 deg
Mean motion: 15
50766414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 922
Checksum: 309
Coasting Arc #15 (Orbit 937)
---------------------------------------
Vector Time (GMT): 2014/155/14:42:57
854
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5202569
82 A = 6796724
61 meter
Y = -3718206
35 meter E =
0017020
Z = 2284170
69 I = 51
76777
XDOT = 4518
460713 Wp = 97
83859
YDOT = 2962
075817 meter/sec RA = 160
79171 deg
ZDOT = -5437
393128 TA = 56
80572
MA = 56
64262
Ha = 227
626 n
mi
Hp = 218
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17068798
61 X = 5232665
18
Y = -12198839
74 feet Y = -3659859
77 meter
Z = 7493998
31 Z = 2309516
94
XDOT = 14824
346172 XDOT = 4511
415468
YDOT = 9718
096513 feet/sec YDOT = 3012
565157 meter/sec
ZDOT = -17839
216299 ZDOT = -5415
459910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17856045
77 X = -5442522
75
Y = -10940159
83 feet Y = -3334560
72 meter
Z = 7601981
32 Z = 2317083
91
XDOT = 2347
751756 XDOT = 715
594735
YDOT = -16236
428642 feet/sec YDOT = -4948
863450 meter/sec
ZDOT = -17746
734093 ZDOT = -5409
204552
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 14155
65006024
00016717 00000-0 10270-3 0 9141
2 25544 51
6427 161
7228 0004169 62
7904 297
3671 15
50811708 9383
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
65006024 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 161
7228 deg
Eccentricity:
0004169
Arg of perigee: 62
7904 deg
Mean anomaly: 297
3671 deg
Mean motion: 15
50811708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 938
Checksum: 308
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