[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 2nd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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 3958)
---------------------------------------
Vector Time (GMT): 2014/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1540671
48 A = 6791258
37 meter
Y = -4971692
55 meter E =
0010438
Z = 4359328
70 I = 51
96523
XDOT = 5014
548720 Wp = 51
03382
YDOT = -4625
393978 meter/sec RA = 113
71525 deg
ZDOT = -3490
900678 TA = 74
35871
MA = 74
24356
Ha = 226
492 n
mi
Hp = 220
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5054696
45 X = -1506138
84
Y = -16311327
25 feet Y = -4988727
78 meter
Z = 14302259
52 Z = 4351928
66
XDOT = 16451
931495 XDOT = 5082
856088
YDOT = -15175
177093 feet/sec YDOT = -4568
936515 meter/sec
ZDOT = -11453
086215 ZDOT = -3466
374038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7880128
97 X = -2401863
31
Y = -15178490
44 feet Y = -4626403
89 meter
Z = 14271684
40 Z = 4350009
40
XDOT = 12551
286752 XDOT = 3825
632202
YDOT = -17223
927283 feet/sec YDOT = -5249
853036 meter/sec
ZDOT = -11348
675053 ZDOT = -3459
076156
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 14092
54206634
00016717 00000-0 10270-3 0 9003
2 25544 51
6456 114
4709 0003703 344
0182 16
0852 15
50721851 39593
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
54206634 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 114
4709 deg
Eccentricity:
0003703
Arg of perigee: 344
0182 deg
Mean anomaly: 16
0852 deg
Mean motion: 15
50721851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3959
Checksum: 290
Coasting Arc #2 (Orbit 3973)
---------------------------------------
Vector Time (GMT): 2014/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1521733
40 A = 6792479
02 meter
Y = 5268389
20 meter E =
0006008
Z = -4012065
09 I = 51
98203
XDOT = -4804
618869 Wp = 74
84348
YDOT = 4426
059487 meter/sec RA = 108
77742 deg
ZDOT = 3996
187758 TA = 236
60960
MA = 236
66709
Ha = 226
586 n
mi
Hp = 220
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4992563
66 X = 1482197
51
Y = 17284741
46 feet Y = 5285184
79 meter
Z = -13162943
22 Z = -4004769
14
XDOT = -15763
185267 XDOT = -4873
167365
YDOT = 14521
192544 feet/sec YDOT = 4371
948225 meter/sec
ZDOT = 13110
852225 ZDOT = 3972
680483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8256425
97 X = 2516558
63
Y = 16009698
25 feet Y = 4879756
03 meter
Z = -13132861
29 Z = -4002896
12
XDOT = -11640
250641 XDOT = -3547
948395
YDOT = 16658
302378 feet/sec YDOT = 5077
450565 meter/sec
ZDOT = 13010
765400 ZDOT = 3965
681294
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 14093
50872249
00016717 00000-0 10270-3 0 9012
2 25544 51
6467 109
6771 0003748 347
8214 12
2846 15
50724704 39744
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
50872249 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 109
6771 deg
Eccentricity:
0003748
Arg of perigee: 347
8214 deg
Mean anomaly: 12
2846 deg
Mean motion: 15
50724704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3974
Checksum: 320
Coasting Arc #3 (Orbit 3989)
---------------------------------------
Vector Time (GMT): 2014/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1508951
48 A = 6793649
79 meter
Y = -5569522
01 meter E =
0012282
Z = 3579890
68 I = 51
99459
XDOT = 4629
605243 Wp = 69
44462
YDOT = -4146
556057 meter/sec RA = 103
84029 deg
ZDOT = -4483
103508 TA = 68
56118
MA = 68
43022
Ha = 226
554 n
mi
Hp = 220
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4950628
21 X = -1463949
77
Y = -18272709
99 feet Y = -5586144
19 meter
Z = 11745048
16 Z = 3572670
06
XDOT = 15188
993578 XDOT = 4697
406532
YDOT = -13604
186538 feet/sec YDOT = -4094
406069 meter/sec
ZDOT = -14708
344843 ZDOT = -4460
448376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8684679
84 X = -2647090
41
Y = -16842623
68 feet Y = -5133631
70 meter
Z = 11715339
09 Z = 3570835
36
XDOT = 10917
778785 XDOT = 3327
738974
YDOT = -15831
305538 feet/sec YDOT = -4825
381928 meter/sec
ZDOT = -14611
888763 ZDOT = -4453
703695
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 14094
53979685
00016717 00000-0 10270-3 0 9029
2 25544 51
6456 104
5626 0003792 351
8240 8
2848 15
50796501 39907
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
53979685 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 104
5626 deg
Eccentricity:
0003792
Arg of perigee: 351
8240 deg
Mean anomaly: 8
2848 deg
Mean motion: 15
50796501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3990
Checksum: 330
Coasting Arc #4 (Orbit 4004)
---------------------------------------
Vector Time (GMT): 2014/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1556594
87 A = 6794903
37 meter
Y = 5828714
91 meter E =
0006417
Z = -3123965
98 I = 52
00592
XDOT = -4476
496156 Wp = 40
03077
YDOT = 3818
773905 meter/sec RA = 98
90596 deg
ZDOT = 4904
922606 TA = 284
27367
MA = 284
34492
Ha = 226
644 n
mi
Hp = 219
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5106938
56 X = 1506476
48
Y = 19123080
41 feet Y = 5845841
31 meter
Z = -10249232
21 Z = -3116526
35
XDOT = -14686
667177 XDOT = -4542
692507
YDOT = 12528
785777 feet/sec YDOT = 3768
345062 meter/sec
ZDOT = 16092
265767 ZDOT = 4883
015259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9306066
82 X = 2836489
17
Y = 17487029
69 feet Y = 5330046
65 meter
Z = -10218644
72 Z = -3114642
91
XDOT = -10344
414615 XDOT = -3152
977575
YDOT = 14834
177574 feet/sec YDOT = 4521
457325 meter/sec
ZDOT = 15999
008882 ZDOT = 4876
497907
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 14095
50640683
00016717 00000-0 10270-3 0 9031
2 25544 51
6461 99
7689 0003768 356
2563 3
8559 15
50806559 40050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
50640683 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 99
7689 deg
Eccentricity:
0003768
Arg of perigee: 356
2563 deg
Mean anomaly: 3
8559 deg
Mean motion: 15
50806559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4005
Checksum: 335
Coasting Arc #5 (Orbit 4020)
---------------------------------------
Vector Time (GMT): 2014/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1600479
32 A = 6796021
91 meter
Y = -6074325
04 meter E =
0013164
Z = 2583349
29 I = 52
01333
XDOT = 4374
888598 Wp = 87
06322
YDOT = -3411
051118 meter/sec RA = 93
97170 deg
ZDOT = -5286
286918 TA = 64
08285
MA = 63
94723
Ha = 226
596 n
mi
Hp = 219
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5250916
39 X = -1544985
01
Y = -19928887
94 feet Y = -6091912
16 meter
Z = 8475555
42 Z = 2575709
59
XDOT = 14353
309049 XDOT = 4438
385749
YDOT = -11191
112593 feet/sec YDOT = -3361
773649 meter/sec
ZDOT = -17343
461018 ZDOT = -5264
879794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9927752
69 X = -3025979
02
Y = -18074941
23 feet Y = -5509242
09 meter
Z = 8444167
41 Z = 2573782
23
XDOT = 10037
704057 XDOT = 3059
492197
YDOT = -13609
819774 feet/sec YDOT = -4148
273067 meter/sec
ZDOT = -17252
371240 ZDOT = -5258
522754
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 14096
53743141
00016717 00000-0 10270-3 0 9049
2 25544 51
6453 94
6540 0003884 358
7901 1
3240 15
50870513 40212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
53743141 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 94
6540 deg
Eccentricity:
0003884
Arg of perigee: 358
7901 deg
Mean anomaly: 1
3240 deg
Mean motion: 15
50870513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4021
Checksum: 285
Coasting Arc #6 (Orbit 4035)
---------------------------------------
Vector Time (GMT): 2014/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1691328
12 A = 6797015
52 meter
Y = 6257156
97 meter E =
0009958
Z = -2031602
34 I = 52
01798
XDOT = -4315
227863 Wp = 27
51349
YDOT = 2975
045734 meter/sec RA = 89
03981 deg
ZDOT = 5589
890256 TA = 310
18653
MA = 310
27367
Ha = 226
662 n
mi
Hp = 219
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5548976
78 X = 1631102
36
Y = 20528730
23 feet Y = 6275733
59 meter
Z = -6665362
01 Z = -2023532
87
XDOT = -14157
571730 XDOT = -4375
328706
YDOT = 9760
648733 feet/sec YDOT = 2926
454483 meter/sec
ZDOT = 18339
534961 ZDOT = 5568
781247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10668206
82 X = 3251669
44
Y = 18407888
32 feet Y = 5610724
36 meter
Z = -6632191
94 Z = -2021492
10
XDOT = -9948
859251 XDOT = -3032
412300
YDOT = 12317
897358 feet/sec YDOT = 3754
495115 meter/sec
ZDOT = 18249
764746 ZDOT = 5562
528295
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 14097
50399397
00016717 00000-0 10270-3 0 9058
2 25544 51
6451 89
8600 0003759 4
2296 355
8886 15
50894870 40365
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
50399397 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 89
8600 deg
Eccentricity:
0003759
Arg of perigee: 4
2296 deg
Mean anomaly: 355
8886 deg
Mean motion: 15
50894870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4036
Checksum: 347
Coasting Arc #7 (Orbit 4051)
---------------------------------------
Vector Time (GMT): 2014/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1761399
44 A = 6797791
15 meter
Y = -6410008
95 meter E =
0012723
Z = 1401245
00 I = 52
01930
XDOT = 4318
806507 Wp = 103
06917
YDOT = -2469
695233 meter/sec RA = 84
10738 deg
ZDOT = -5827
185462 TA = 61
76137
MA = 61
63298
Ha = 226
628 n
mi
Hp = 219
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5778869
56 X = -1696397
17
Y = -21030213
09 feet Y = -6429342
48 meter
Z = 4597260
50 Z = 1392846
82
XDOT = 14169
312687 XDOT = 4374
408827
YDOT = -8102
674648 feet/sec YDOT = -2421
089192 meter/sec
ZDOT = -19118
062541 ZDOT = -5806
070026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11328944
64 X = -3453062
33
Y = -18645012
67 feet Y = -5682999
86 meter
Z = 4562731
22 Z = 1390720
48
XDOT = 10173
301897 XDOT = 3100
822418
YDOT = -10871
626474 feet/sec YDOT = -3313
671749 meter/sec
ZDOT = -19028
337240 ZDOT = -5799
837191
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 14098
53496732
00016717 00000-0 10270-3 0 9064
2 25544 51
6449 84
7446 0003941 5
6742 354
4453 15
50942276 40525
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
53496732 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 84
7446 deg
Eccentricity:
0003941
Arg of perigee: 5
6742 deg
Mean anomaly: 354
4453 deg
Mean motion: 15
50942276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4052
Checksum: 323
Coasting Arc #8 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2014/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1857149
31 A = 6798229
71 meter
Y = 6485979
75 meter E =
0013743
Z = -776284
18 I = 52
01665
XDOT = -4377
630688 Wp = 32
32972
YDOT = 1961
830619 meter/sec RA = 79
17641 deg
ZDOT = 5978
547784 TA = 319
33146
MA = 319
43401
Ha = 226
632 n
mi
Hp = 219
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6093009
54 X = 1788254
53
Y = 21279461
12 feet Y = 6506362
29 meter
Z = -2546864
09 Z = -767430
38
XDOT = -14362
305408 XDOT = -4428
284858
YDOT = 6436
452162 feet/sec YDOT = 1912
594512 meter/sec
ZDOT = 19614
658084 ZDOT = 5957
158624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12008600
76 X = 3660221
51
Y = 18598871
24 feet Y = 5668935
95 meter
Z = -2510426
98 Z = -765178
14
XDOT = -10643
890571 XDOT = -3244
257846
YDOT = 9480
690064 feet/sec YDOT = 2889
714331 meter/sec
ZDOT = 19523
850108 ZDOT = 5950
869513
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 14099
50148077
00016717 00000-0 10270-3 0 9079
2 25544 51
6444 79
9501 0003726 11
2252 348
8981 15
50986567 40678
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
50148077 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 79
9501 deg
Eccentricity:
0003726
Arg of perigee: 11
2252 deg
Mean anomaly: 348
8981 deg
Mean motion: 15
50986567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 331
Coasting Arc #9 (Orbit 4082)
---------------------------------------
Vector Time (GMT): 2014/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1909619
54 A = 6798394
72 meter
Y = -6520754
15 meter E =
0010715
Z = 86107
74 I = 52
01119
XDOT = 4501
993361 Wp = 115
32326
YDOT = -1405
806221 meter/sec RA = 74
24427 deg
ZDOT = -6036
807551 TA = 63
75547
MA = 63
64538
Ha = 226
635 n
mi
Hp = 219
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6265155
98 X = -1836979
35
Y = -21393550
37 feet Y = -6541702
58 meter
Z = 282505
72 Z = 77008
22
XDOT = 14770
319425 XDOT = 4546
703744
YDOT = -4612
225135 feet/sec YDOT = -1355
212715 meter/sec
ZDOT = -19805
799053 ZDOT = -6014
828703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12512108
78 X = -3813690
76
Y = -18450015
56 feet Y = -5623564
74 meter
Z = 245042
90 Z = 74689
08
XDOT = 11422
567334 XDOT = 3481
598523
YDOT = -8037
342674 feet/sec YDOT = -2449
782047 meter/sec
ZDOT = -19712
581980 ZDOT = -6008
394988
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 14100
53240132
00016717 00000-0 10270-3 0 9081
2 25544 51
6449 74
8342 0003936 12
4163 347
7085 15
51013204 40838
Satellite: ISS
Catalog Number: 25544
Epoch time: 14100
53240132 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 74
8342 deg
Eccentricity:
0003936
Arg of perigee: 12
4163 deg
Mean anomaly: 347
7085 deg
Mean motion: 15
51013204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4083
Checksum: 273
Coasting Arc #10 (Orbit 4098)
---------------------------------------
Vector Time (GMT): 2014/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1961457
25 A = 6798086
88 meter
Y = 6474005
34 meter E =
0016252
Z = 578696
86 I = 52
00114
XDOT = -4685
160658 Wp = 43
80555
YDOT = 874
674927 meter/sec RA = 69
31236 deg
ZDOT = 6005
811365 TA = 322
40398
MA = 322
51749
Ha = 226
582 n
mi
Hp = 218
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6435227
21 X = 1886106
55
Y = 21240174
99 feet Y = 6495518
37 meter
Z = 1898611
75 Z = 588041
59
XDOT = -15371
262000 XDOT = -4723
767696
YDOT = 2869
668397 feet/sec YDOT = 822
067303 meter/sec
ZDOT = 19704
105528 ZDOT = 5982
957536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12926315
24 X = 3939940
88
Y = 18036626
30 feet Y = 5497563
70 meter
Z = 1937110
05 Z = 590431
14
XDOT = -12426
774954 XDOT = -3787
681006
YDOT = 6769
343012 feet/sec YDOT = 2063
295750 meter/sec
ZDOT = 19607
271139 ZDOT = 5976
296243
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 14101
56329313
00016717 00000-0 10270-3 0 9095
2 25544 51
6446 69
7194 0003708 17
2163 342
9113 15
51071886 40999
Satellite: ISS
Catalog Number: 25544
Epoch time: 14101
56329313 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 69
7194 deg
Eccentricity:
0003708
Arg of perigee: 17
2163 deg
Mean anomaly: 342
9113 deg
Mean motion: 15
51071886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4099
Checksum: 308
Coasting Arc #11 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2014/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1945596
06 A = 6797457
23 meter
Y = -6383452
66 meter E =
0007466
Z = -1287168
19 I = 51
98840
XDOT = 4922
540470 Wp = 116
26512
YDOT = -324
967681 meter/sec RA = 64
37856 deg
ZDOT = -5858
452119 TA = 77
64374
MA = 77
56019
Ha = 226
606 n
mi
Hp = 218
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6383189
18 X = -1867817
55
Y = -20943086
17 feet Y = -6404774
84 meter
Z = -4222992
75 Z = -1296429
99
XDOT = 16150
067159 XDOT = 4954
267181
YDOT = -1066
166934 feet/sec YDOT = -269
744004 meter/sec
ZDOT = -19220
643435 ZDOT = -5834
461824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13071490
39 X = -3984190
27
Y = -17554783
40 feet Y = -5350697
98 meter
Z = -4261144
07 Z = -1298796
71
XDOT = 13667
751824 XDOT = 4165
930756
YDOT = -5559
579529 feet/sec YDOT = -1694
559840 meter/sec
ZDOT = -19119
091231 ZDOT = -5827
499007
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 14102
52973042
00016717 00000-0 10270-3 0 9108
2 25544 51
6456 64
9233 0003892 18
7025 341
4268 15
51090332 41148
Satellite: ISS
Catalog Number: 25544
Epoch time: 14102
52973042 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 64
9233 deg
Eccentricity:
0003892
Arg of perigee: 18
7025 deg
Mean anomaly: 341
4268 deg
Mean motion: 15
51090332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 280
Coasting Arc #12 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2014/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1901859
05 A = 6796396
28 meter
Y = 6217519
29 meter E =
0016753
Z = 1947536
68 I = 51
97136
XDOT = -5210
953098 Wp = 58
43805
YDOT = -175
872203 meter/sec RA = 59
44364 deg
ZDOT = 5623
252550 TA = 322
92474
MA = 323
04035
Ha = 226
544 n
mi
Hp = 218
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6239695
03 X = 1822731
37
Y = 20398685
33 feet Y = 6238344
91 meter
Z = 6389556
02 Z = 1956582
80
XDOT = -17096
302815 XDOT = -5235
915438
YDOT = -577
008540 feet/sec YDOT = -234
283318 meter/sec
ZDOT = 18448
991305 ZDOT = 5597
877572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13031656
71 X = 3972048
97
Y = 16874199
85 feet Y = 5143256
11 meter
Z = 6426809
97 Z = 1958891
68
XDOT = -15066
145618 XDOT = -4592
161184
YDOT = 4616
122158 feet/sec YDOT = 1406
994034 meter/sec
ZDOT = 18341
666042 ZDOT = 5590
539810
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 14103
56056765
00016717 00000-0 10270-3 0 9118
2 25544 51
6458 59
8082 0003722 22
7223 337
4093 15
51146068 41309
Satellite: ISS
Catalog Number: 25544
Epoch time: 14103
56056765 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 59
8082 deg
Eccentricity:
0003722
Arg of perigee: 22
7223 deg
Mean anomaly: 337
4093 deg
Mean motion: 15
51146068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 291
Coasting Arc #13 (Orbit 4144)
---------------------------------------
Vector Time (GMT): 2014/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1769447
39 A = 6794994
99 meter
Y = -6016120
25 meter E =
0005676
Z = -2622420
47 I = 51
95141
XDOT = 5526
436422 Wp = 84
69198
YDOT = 662
341645 meter/sec RA = 54
50581 deg
ZDOT = -5257
652104 TA = 124
64363
MA = 124
59011
Ha = 226
556 n
mi
Hp = 218
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5805273
59 X = -1689303
19
Y = -19737927
34 feet Y = -6035459
53 meter
Z = -8603741
71 Z = -2630821
00
XDOT = 18131
353090 XDOT = 5544
159606
YDOT = 2173
036893 feet/sec YDOT = 724
240321 meter/sec
ZDOT = -17249
514776 ZDOT = -5230
762071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12658774
58 X = -3858394
49
Y = -16200210
25 feet Y = -4937824
08 meter
Z = -8638284
70 Z = -2632949
18
XDOT = 16563
139148 XDOT = 5048
444812
YDOT = -3821
322188 feet/sec YDOT = -1164
739003 meter/sec
ZDOT = -17135
865182 ZDOT = -5223
011708
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 14104
52695275
00016717 00000-0 10270-3 0 9121
2 25544 51
6468 55
0122 0003845 24
9877 335
1460 15
51176086 41450
Satellite: ISS
Catalog Number: 25544
Epoch time: 14104
52695275 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 55
0122 deg
Eccentricity:
0003845
Arg of perigee: 24
9877 deg
Mean anomaly: 335
1460 deg
Mean motion: 15
51176086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4145
Checksum: 305
Coasting Arc #14 (Orbit 4160)
---------------------------------------
Vector Time (GMT): 2014/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1585889
05 A = 6793368
96 meter
Y = 5755581
76 meter E =
0015039
Z = 3224564
85 I = 51
92816
XDOT = -5874
011736 Wp = 74
53714
YDOT = -1084
484133 meter/sec RA = 49
56577 deg
ZDOT = 4809
916598 TA = 322
59602
MA = 322
70061
Ha = 226
505 n
mi
Hp = 218
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5203048
05 X = 1505746
78
Y = 18883142
26 feet Y = 5772868
39 meter
Z = 10579281
01 Z = 3232073
82
XDOT = -19271
692047 XDOT = -5884
813672
YDOT = -3558
018808 feet/sec YDOT = -1150
231052 meter/sec
ZDOT = 15780
566267 ZDOT = 4781
354824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12038358
98 X = 3669291
82
Y = 15429517
76 feet Y = 4702917
01 meter
Z = 10610082
57 Z = 3233953
17
XDOT = -18113
783858 XDOT = -5521
081320
YDOT = 3331
024882 feet/sec YDOT = 1015
296384 meter/sec
ZDOT = 15659
921000 ZDOT = 4773
143921
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 14105
55773477
00016717 00000-0 10270-3 0 9137
2 25544 51
6473 49
8971 0003710 29
0218 331
1139 15
51222422 41618
Satellite: ISS
Catalog Number: 25544
Epoch time: 14105
55773477 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 49
8971 deg
Eccentricity:
0003710
Arg of perigee: 29
0218 deg
Mean anomaly: 331
1139 deg
Mean motion: 15
51222422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4161
Checksum: 289
Coasting Arc #15 (Orbit 4175)
---------------------------------------
Vector Time (GMT): 2014/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1302460
12 A = 6791530
27 meter
Y = -5478875
38 meter E =
0009190
Z = -3806941
32 I = 51
90226
XDOT = 6207
222630 Wp = 59
08148
YDOT = 1463
327437 meter/sec RA = 44
62154 deg
ZDOT = -4232
635057 TA = 166
28814
MA = 166
26316
Ha = 226
500 n
mi
Hp = 218
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4273163
13 X = -1222604
04
Y = -17975312
93 feet Y = -5492994
10 meter
Z = -12489964
96 Z = -3813074
25
XDOT = 20364
903641 XDOT = 6210
959220
YDOT = 4800
943036 feet/sec YDOT = 1532
761171 meter/sec
ZDOT = -13886
597955 ZDOT = -4202
471682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11074513
39 X = -3375511
68
Y = -14768258
63 feet Y = -4501365
23 meter
Z = -12514979
55 Z = -3814565
77
XDOT = 19576
924683 XDOT = 5967
046643
YDOT = -3028
814926 feet/sec YDOT = -923
182789 meter/sec
ZDOT = -13759
247848 ZDOT = -4193
818744
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 14106
52406734
00016717 00000-0 10270-3 0 9145
2 25544 51
6479 45
1010 0003796 31
8214 328
3166 15
51264554 41764
Satellite: ISS
Catalog Number: 25544
Epoch time: 14106
52406734 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 45
1010 deg
Eccentricity:
0003796
Arg of perigee: 31
8214 deg
Mean anomaly: 328
3166 deg
Mean motion: 15
51264554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4176
Checksum: 293
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