[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
104/12:17:33
396 1
8 2
0 2
0
N/A 0
1 0
0 221
3
000/00:05:06
793 -0
7 -0
0 214
3
109/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 3351)
---------------------------------------
Vector Time (GMT): 2016/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2894651
80 A = 6788659
60 meter
Y = -6136003
97 meter E =
0011495
Z = 13293
51 I = 51
99489
XDOT = 4261
498152 Wp = 121
82670
YDOT = -2031
706960 meter/sec RA = 64
83219 deg
ZDOT = -6041
447606 TA = 58
03083
MA = 57
91913
Ha = 221
207 n
mi
Hp = 213
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9496889
09 X = -2825886
91
Y = -20131246
61 feet Y = -6167989
40 meter
Z = 43613
87 Z = -600
17
XDOT = 13981
293151 XDOT = 4313
247214
YDOT = -6665
705250 feet/sec YDOT = -1983
763474 meter/sec
ZDOT = -19821
022331 ZDOT = -6020
620384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13593915
55 X = -4143425
46
Y = -17625694
59 feet Y = -5372311
71 meter
Z = -15652
24 Z = -4770
80
XDOT = 11064
694875 XDOT = 3372
518998
YDOT = -8547
146929 feet/sec YDOT = -2605
170384 meter/sec
ZDOT = -19730
114560 ZDOT = -6013
738918
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 16095
53217995
00016717 00000-0 10270-3 0 9009
2 25544 51
6393 65
4007 0002630 25
0873 335
0407 15
54358271 33523
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
53217995 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 65
4007 deg
Eccentricity:
0002630
Arg of perigee: 25
0873 deg
Mean anomaly: 335
0407 deg
Mean motion: 15
54358271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3352
Checksum: 296
Coasting Arc #2 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2016/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2039109
93 A = 6787257
56 meter
Y = 6226594
66 meter E =
0015990
Z = 1739722
48 I = 51
97698
XDOT = -5121
780500 Wp = 59
67600
YDOT = 72
524571 meter/sec RA = 59
88408 deg
ZDOT = 5712
500064 TA = 319
33652
MA = 319
45581
Ha = 221
153 n
mi
Hp = 213
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6689993
22 X = 1960880
20
Y = 20428460
19 feet Y = 6248960
18 meter
Z = 5707750
92 Z = 1749437
11
XDOT = -16803
741797 XDOT = -5149
959766
YDOT = 237
941506 feet/sec YDOT = 15
092648 meter/sec
ZDOT = 18741
798109 ZDOT = 5687
551221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11197212
37 X = 3412910
33
Y = 18336571
78 feet Y = 5588987
08 meter
Z = 5748824
75 Z = 1752241
78
XDOT = -15072
596719 XDOT = -4594
127480
YDOT = 3330
428798 feet/sec YDOT = 1015
114698 meter/sec
ZDOT = 18633
338074 ZDOT = 5679
441445
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 16096
56085880
00016717 00000-0 10270-3 0 9010
2 25544 51
6402 60
2713 0002435 29
4220 330
7069 15
54394933 33686
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
56085880 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 60
2713 deg
Eccentricity:
0002435
Arg of perigee: 29
4220 deg
Mean anomaly: 330
7069 deg
Mean motion: 15
54394933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 300
Coasting Arc #3 (Orbit 3382)
---------------------------------------
Vector Time (GMT): 2016/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -911909
60 A = 6783855
17 meter
Y = -5841145
64 meter E =
0006448
Z = -3334681
26 I = 51
94924
XDOT = 5766
406256 Wp = 71
25304
YDOT = 1789
044652 meter/sec RA = 54
92713 deg
ZDOT = -4716
076315 TA = 147
34802
MA = 147
30814
Ha = 221
252 n
mi
Hp = 213
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2991829
39 X = -830326
11
Y = -19163863
65 feet Y = -5850887
53 meter
Z = -10940555
33 Z = -3338912
14
XDOT = 18918
655697 XDOT = 5768
880978
YDOT = 5869
569068 feet/sec YDOT = 1853
541611 meter/sec
ZDOT = -15472
691322 ZDOT = -4688
058602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7582320
48 X = -2311091
28
Y = -17841925
80 feet Y = -5438218
98 meter
Z = -10957853
98 Z = -3339953
89
XDOT = 18577
863334 XDOT = 5662
532744
YDOT = 1522
176832 feet/sec YDOT = 463
959498 meter/sec
ZDOT = -15351
245245 ZDOT = -4679
059551
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 16097
52523924
00016717 00000-0 10270-3 0 9024
2 25544 51
6408 55
4615 0002710 31
0118 329
1194 15
54385187 33839
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
52523924 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 55
4615 deg
Eccentricity:
0002710
Arg of perigee: 31
0118 deg
Mean anomaly: 329
1194 deg
Mean motion: 15
54385187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3383
Checksum: 297
Coasting Arc #4 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2016/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -398932
07 A = 6779798
82 meter
Y = 5030778
33 meter E =
0009644
Z = 4519887
37 I = 51
91715
XDOT = -6106
613485 Wp = 97
46037
YDOT = -3367
193000 meter/sec RA = 49
95956 deg
ZDOT = 3201
762576 TA = 320
49174
MA = 320
56201
Ha = 221
195 n
mi
Hp = 213
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1308832
24 X = -477113
76
Y = 16505178
26 feet Y = 5025880
67 meter
Z = 14829026
79 Z = 4517758
87
XDOT = -20034
821144 XDOT = -6084
059806
YDOT = -11047
221130 feet/sec YDOT = -3435
354684 meter/sec
ZDOT = 10504
470393 ZDOT = 3172
153057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3013318
06 X = 918459
34
Y = 16289759
87 feet Y = 4965118
81 meter
Z = 14818826
69 Z = 4516778
37
XDOT = -21120
402938 XDOT = -6437
498816
YDOT = -5553
601960 feet/sec YDOT = -1692
737877 meter/sec
ZDOT = 10376
413450 ZDOT = 3162
730819
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 16098
55390188
00016717 00000-0 10270-3 0 9033
2 25544 51
6410 50
3327 0002487 33
5902 326
5408 15
54424708 33994
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
55390188 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 50
3327 deg
Eccentricity:
0002487
Arg of perigee: 33
5902 deg
Mean anomaly: 326
5408 deg
Mean motion: 15
54424708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 311
Coasting Arc #5 (Orbit 3413)
---------------------------------------
Vector Time (GMT): 2016/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1853061
69 A = 6777087
74 meter
Y = -3930943
13 meter E =
0016025
Z = -5214377
83 I = 51
88738
XDOT = 6010
198213 Wp = 73
57306
YDOT = 4561
838543 meter/sec RA = 44
97891 deg
ZDOT = -1302
040141 TA = 183
93902
MA = 183
95165
Ha = 221
251 n
mi
Hp = 213
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6079598
70 X = 1922210
33
Y = -12896795
06 feet Y = -3909834
92 meter
Z = -17107538
81 Z = -5205207
58
XDOT = 19718
498074 XDOT = 5965
064751
YDOT = 14966
661886 feet/sec YDOT = 4628
796073 meter/sec
ZDOT = -4271
785240 ZDOT = -1272
953814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2313634
01 X = 705195
65
Y = -14118200
17 feet Y = -4303227
41 meter
Z = -17066934
38 Z = -5202001
60
XDOT = 22127
244877 XDOT = 6744
384239
YDOT = 8642
723024 feet/sec YDOT = 2634
301978 meter/sec
ZDOT = -4146
243365 ZDOT = -1263
774978
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 16099
51826743
00016717 00000-0 10270-3 0 9042
2 25544 51
6420 45
5233 0002596 36
7259 323
4071 15
54403403 34147
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
51826743 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 45
5233 deg
Eccentricity:
0002596
Arg of perigee: 36
7259 deg
Mean anomaly: 323
4071 deg
Mean motion: 15
54403403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3414
Checksum: 293
Coasting Arc #6 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2016/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312072
47 A = 6776677
29 meter
Y = 2639502
09 meter E =
0005766
Z = 5286789
09 I = 51
86335
XDOT = -5456
013785 Wp = 50
56538
YDOT = -5342
325701 meter/sec RA = 39
99328 deg
ZDOT = -746
744124 TA = 46
56673
MA = 46
51876
Ha = 221
383 n
mi
Hp = 213
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10866379
49 X = -3367023
22
Y = 8659783
77 feet Y = 2602157
52 meter
Z = 17345108
56 Z = 5270565
92
XDOT = -17900
307694 XDOT = -5392
241646
YDOT = -17527
315293 feet/sec YDOT = -5402
981971 meter/sec
ZDOT = -2449
947913 ZDOT = -773
093110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7902639
79 X = -2408724
61
Y = 11535890
97 feet Y = 3516139
57 meter
Z = 17274094
86 Z = 5265144
11
XDOT = -21448
895597 XDOT = -6537
623378
YDOT = -10834
692200 feet/sec YDOT = -3302
414183 meter/sec
ZDOT = -2563
428355 ZDOT = -781
332963
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 16100
54691166
00016717 00000-0 10270-3 0 9058
2 25544 51
6424 40
3944 0002687 38
6735 321
4610 15
54427191 34309
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
54691166 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 40
3944 deg
Eccentricity:
0002687
Arg of perigee: 38
6735 deg
Mean anomaly: 321
4610 deg
Mean motion: 15
54427191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 291
Coasting Arc #7 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2016/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4643403
59 A = 6778934
81 meter
Y = -1322740
14 meter E =
0012356
Z = -4769720
47 I = 51
84528
XDOT = 4386
964754 Wp = 97
18621
YDOT = 5666
259176 meter/sec RA = 35
00804 deg
ZDOT = 2703
908629 TA = 199
46639
MA = 199
51362
Ha = 221
314 n
mi
Hp = 213
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15234263
75 X = 4681019
26
Y = -4339698
63 feet Y = -1270604
51 meter
Z = -15648689
19 Z = -4747072
21
XDOT = 14392
928984 XDOT = 4310
142577
YDOT = 18590
089159 feet/sec YDOT = 5714
887774 meter/sec
ZDOT = 8871
091304 ZDOT = 2725
032730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13196070
31 X = 4022162
23
Y = -8936345
66 feet Y = -2723798
16 meter
Z = -15550006
57 Z = -4739642
00
XDOT = 18796
172763 XDOT = 5729
073458
YDOT = 12187
353535 feet/sec YDOT = 3714
705357 meter/sec
ZDOT = 8961
788643 ZDOT = 2731
553178
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 16101
51125735
00016717 00000-0 10270-3 0 9061
2 25544 51
6420 35
5854 0002679 43
3104 316
8259 15
54433176 34458
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
51125735 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 35
5854 deg
Eccentricity:
0002679
Arg of perigee: 43
3104 deg
Mean anomaly: 316
8259 deg
Mean motion: 15
54433176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 293
Coasting Arc #8 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2016/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5699852
75 A = 6782787
75 meter
Y = 34532
59 meter E =
0013991
Z = 3667182
37 I = 51
83214
XDOT = -2857
115023 Wp = 78
58952
YDOT = -5620
035654 meter/sec RA = 30
03059 deg
ZDOT = -4371
057350 TA = 57
92295
MA = 57
78718
Ha = 221
347 n
mi
Hp = 213
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18700304
30 X = -5717629
06
Y = 113295
91 feet Y = -29306
15 meter
Z = 12031438
21 Z = 3639450
43
XDOT = -9373
736953 XDOT = -2772
825092
YDOT = -18438
437184 feet/sec YDOT = -5651
514746 meter/sec
ZDOT = -14340
739337 ZDOT = -4384
731628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17685881
23 X = -5390656
60
Y = 6309469
26 feet Y = 1923126
23 meter
Z = 11910916
22 Z = 3630447
26
XDOT = -14390
458473 XDOT = -4386
211743
YDOT = -13050
056289 feet/sec YDOT = -3977
657157 meter/sec
ZDOT = -14399
059860 ZDOT = -4388
833445
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 16102
53988290
00016717 00000-0 10270-3 0 9078
2 25544 51
6426 30
4561 0002606 45
1948 314
9416 15
54454861 34615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
53988290 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 30
4561 deg
Eccentricity:
0002606
Arg of perigee: 45
1948 deg
Mean anomaly: 314
9416 deg
Mean motion: 15
54454861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 307
Coasting Arc #9 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2016/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6337237
85 A = 6786433
43 meter
Y = 1083421
99 meter E =
0009002
Z = -2165413
40 I = 51
81634
XDOT = 979
588831 Wp = 43
17640
YDOT = 5240
970253 meter/sec RA = 25
06186 deg
ZDOT = 5508
969331 TA = 292
86484
MA = 292
95987
Ha = 221
332 n
mi
Hp = 213
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20791462
76 X = 6335170
48
Y = 3554534
09 feet Y = 1154277
54 meter
Z = -7104374
68 Z = -2134633
53
XDOT = 3213
874116 XDOT = 894
149790
YDOT = 17194
784296 feet/sec YDOT = 5251
447205 meter/sec
ZDOT = 18074
046363 ZDOT = 5513
520198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20777506
51 X = 6332983
99
Y = -3885166
38 feet Y = -1184198
71 meter
Z = -6970830
72 Z = -2124709
20
XDOT = 8580
181978 XDOT = 2615
239467
YDOT = 13543
110666 feet/sec YDOT = 4127
940131 meter/sec
ZDOT = 18092
786951 ZDOT = 5514
681463
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 16103
50420780
00016717 00000-0 10270-3 0 9082
2 25544 51
6427 25
6466 0002652 48
4297 311
7082 15
54464290 34767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
50420780 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 25
6466 deg
Eccentricity:
0002652
Arg of perigee: 48
4297 deg
Mean anomaly: 311
7082 deg
Mean motion: 15
54464290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 303
Coasting Arc #10 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6453364
48 A = 6788279
39 meter
Y = -2057708
56 meter E =
0013483
Z = 362599
98 I = 51
79371
XDOT = 1128
133993 Wp = 119
87894
YDOT = -4625
665036 meter/sec RA = 20
10020 deg
ZDOT = -6011
467439 TA = 56
22032
MA = 56
09197
Ha = 221
291 n
mi
Hp = 213
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21172455
63 X = -6431636
40
Y = -6751012
34 feet Y = -2129752
87 meter
Z = 1189632
49 Z = 331303
90
XDOT = 3701
227010 XDOT = 1208
976734
YDOT = -15176
066390 feet/sec YDOT = -4612
597776 meter/sec
ZDOT = -19722
662202 ZDOT = -6005
790632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22186257
72 X = -6762371
35
Y = 1386806
76 feet Y = 422698
70 meter
Z = 1054042
77 Z = 321272
24
XDOT = -1833
852500 XDOT = -558
958242
YDOT = -13915
231217 feet/sec YDOT = -4241
362475 meter/sec
ZDOT = -19697
075820 ZDOT = -6003
668710
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 16104
53280949
00016717 00000-0 10270-3 0 9098
2 25544 51
6432 20
5166 0002650 53
4459 306
6938 15
54474640 34929
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53280949 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 20
5166 deg
Eccentricity:
0002650
Arg of perigee: 53
4459 deg
Mean anomaly: 306
6938 deg
Mean motion: 15
54474640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 311
Coasting Arc #11 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:20:06
793
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -350449
78 A = 6778164
06 meter
Y = -4431669
84 meter E =
0014543
Z = -5129787
54 I = 51
75673
XDOT = 7364
056063 Wp = 74
35155
YDOT = 1313
236253 meter/sec RA = 20
04732 deg
ZDOT = -1637
643468 TA = 179
84730
MA = 179
84686
Ha = 221
291 n
mi
Hp = 214
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1149769
61 X = -275949
29
Y = -14539599
20 feet Y = -4435172
50 meter
Z = -16830011
61 Z = -5131308
76
XDOT = 24160
288919 XDOT = 7356
778816
YDOT = 4308
517892 feet/sec YDOT = 1395
545253 meter/sec
ZDOT = -5372
846023 ZDOT = -1601
888316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7376060
71 X = -2248223
31
Y = -12574684
51 feet Y = -3832763
84 meter
Z = -16835743
04 Z = -5131534
48
XDOT = 22681
921606 XDOT = 6913
449706
YDOT = -6319
125736 feet/sec YDOT = -1926
069524 meter/sec
ZDOT = -5217
731691 ZDOT = -1590
364619
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 16104
53281107
00016717 00000-0 10270-3 0 9107
2 25544 51
6436 20
5169 0001251 38
0625 322
0616 15
54138988 34923
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53281107 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 20
5169 deg
Eccentricity:
0001251
Arg of perigee: 38
0625 deg
Mean anomaly: 322
0616 deg
Mean motion: 15
54138988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 284
Coasting Arc #12 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/12:20:06
793
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1405362
03 A = 6777238
46 meter
Y = 3963062
87 meter E =
0003416
Z = 5312528
62 I = 51
72329
XDOT = -7339
915297 Wp = 62
45668
YDOT = -2211
495408 meter/sec RA = 15
05528 deg
ZDOT = -290
253963 TA = 30
31577
MA = 30
29601
Ha = 221
208 n
mi
Hp = 214
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4610767
80 X = -1475379
57
Y = 13002174
78 feet Y = 3946956
01 meter
Z = 17429555
85 Z = 5305531
41
XDOT = -24081
086934 XDOT = -7313
230355
YDOT = -7255
562362 feet/sec YDOT = -2293
426035 meter/sec
ZDOT = -952
276781 ZDOT = -325
844559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1763557
33 X = 537532
27
Y = 13721952
63 feet Y = 4182451
16 meter
Z = 17398362
78 Z = 5303020
98
XDOT = -23721
461267 XDOT = -7230
301394
YDOT = 4458
676311 feet/sec YDOT = 1359
004540 meter/sec
ZDOT = -1106
491436 ZDOT = -337
258590
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 16105
56164145
00016717 00000-0 10270-3 0 9114
2 25544 51
6433 15
3889 0001044 32
7988 327
3230 15
54177665 35087
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56164145 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 15
3889 deg
Eccentricity:
0001044
Arg of perigee: 32
7988 deg
Mean anomaly: 327
3230 deg
Mean motion: 15
54177665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 305
Coasting Arc #13 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:20:06
793
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3118036
04 A = 6778904
73 meter
Y = -3425946
11 meter E =
0012702
Z = -4960769
42 I = 51
69854
XDOT = 6720
280145 Wp = 101
09090
YDOT = 2948
888204 meter/sec RA = 10
06129 deg
ZDOT = 2189
806097 TA = 190
26388
MA = 190
28984
Ha = 221
214 n
mi
Hp = 214
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10229777
03 X = 3180211
40
Y = -11239980
67 feet Y = -3390730
88 meter
Z = -16275490
23 Z = -4945471
50
XDOT = 22048
163206 XDOT = 6676
168327
YDOT = 9674
830066 feet/sec YDOT = 3023
792364 meter/sec
ZDOT = 7184
403204 ZDOT = 2222
344217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3777519
90 X = 1151388
07
Y = -14795176
09 feet Y = -4509569
67 meter
Z = -16208337
17 Z = -4940301
17
XDOT = 22880
988277 XDOT = 6974
125227
YDOT = -2174
298475 feet/sec YDOT = -662
726175 meter/sec
ZDOT = 7325
199969 ZDOT = 2232
720951
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 16106
52616056
00016717 00000-0 10270-3 0 9125
2 25544 51
6445 10
5807 0001114 35
7331 324
3896 15
54162515 35230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52616056 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 10
5807 deg
Eccentricity:
0001114
Arg of perigee: 35
7331 deg
Mean anomaly: 324
3896 deg
Mean motion: 15
54162515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 279
Coasting Arc #14 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/12:20:06
793
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640711
21 A = 6782261
04 meter
Y = 2811170
15 meter E =
0011784
Z = 4061974
50 I = 51
67787
XDOT = -5570
814274 Wp = 74
10225
YDOT = -3572
780937 meter/sec RA = 5
07287 deg
ZDOT = -3879
401849 TA = 56
08871
MA = 55
97670
Ha = 221
326 n
mi
Hp = 214
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15225430
47 X = -4691532
87
Y = 9222999
19 feet Y = 2758990
82 meter
Z = 13326687
98 Z = 4039307
36
XDOT = -18276
949719 XDOT = -5511
604009
YDOT = -11721
722233 feet/sec YDOT = -3634
746758 meter/sec
ZDOT = -12727
696355 ZDOT = -3906
319402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8850126
94 X = -2697518
69
Y = 15530060
30 feet Y = 4733562
38 meter
Z = 13227643
01 Z = 4031785
59
XDOT = -20470
502666 XDOT = -6239
409213
YDOT = -690
566616 feet/sec YDOT = -210
484704 meter/sec
ZDOT = -12843
939856 ZDOT = -3914
832868
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 16107
55496865
00016717 00000-0 10270-3 0 9134
2 25544 51
6441 5
4525 0001240 41
3175 318
8071 15
54186738 35398
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55496865 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 5
4525 deg
Eccentricity:
0001240
Arg of perigee: 41
3175 deg
Mean anomaly: 318
8071 deg
Mean motion: 15
54186738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 306
Coasting Arc #15 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2016/108/12:20:06
793
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5806504
95 A = 6785977
43 meter
Y = -2172420
33 meter E =
0005910
Z = -2758475
29 I = 51
65863
XDOT = 3962
179149 Wp = 53
12806
YDOT = 4074
013898 meter/sec RA =
09207 deg
ZDOT = 5142
888020 TA = 275
65342
MA = 275
72081
Ha = 221
205 n
mi
Hp = 214
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19050213
08 X = 5843765
48
Y = -7127363
27 feet Y = -2107280
05 meter
Z = -9050115
77 Z = -2730177
92
XDOT = 12999
275424 XDOT = 3891
345991
YDOT = 13366
187328 feet/sec YDOT = 4117
926061 meter/sec
ZDOT = 16872
992193 ZDOT = 5161
962938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12917771
50 X = 3937336
75
Y = -15781601
26 feet Y = -4810232
06 meter
Z = -8926744
21 Z = -2720871
64
XDOT = 16717
921881 XDOT = 5095
622589
YDOT = 4114
543957 feet/sec YDOT = 1254
112998 meter/sec
ZDOT = 16955
055264 ZDOT = 5167
900844
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 16108
51946601
00016717 00000-0 10270-3 0 9140
2 25544 51
6442
6445 0001104 39
3331 320
7901 15
54200440 35545
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
51946601 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node:
6445 deg
Eccentricity:
0001104
Arg of perigee: 39
3331 deg
Mean anomaly: 320
7901 deg
Mean motion: 15
54200440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 259
Coasting Arc #16 (Orbit 3564)
---------------------------------------
Vector Time (GMT): 2016/109/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5509592
29 A = 6784564
54 meter
Y = -2263540
99 meter E =
0005608
Z = -3253348
93 I = 51
62863
XDOT = 4458
404218 Wp = 87
66822
YDOT = -4027
433210 meter/sec RA = 356
71083 deg
ZDOT = -4755
121223 TA = 130
02346
MA = 129
97424
Ha = 221
245 n
mi
Hp = 214
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18076090
21 X = -5468067
86
Y = -7426315
58 feet Y = -2324921
06 meter
Z = -10673716
96 Z = -3280012
23
XDOT = 14627
310425 XDOT = 4526
207096
YDOT = -13213
363550 feet/sec YDOT = -3977
197731 meter/sec
ZDOT = -15600
791415 ZDOT = -4733
298196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4720405
53 X = 1438779
60
Y = -18898055
01 feet Y = -5760127
17 meter
Z = -10789102
03 Z = -3288518
30
XDOT = 13844
128320 XDOT = 4219
690312
YDOT = 12297
374888 feet/sec YDOT = 3748
239866 meter/sec
ZDOT = -15505
185097 ZDOT = -4725
980417
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 16109
22675790
00016717 00000-0 10270-3 0 9158
2 25544 51
6408 357
1170 0001176 55
9774 304
1490 15
54190598 35659
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
22675790 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 357
1170 deg
Eccentricity:
0001176
Arg of perigee: 55
9774 deg
Mean anomaly: 304
1490 deg
Mean motion: 15
54190598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3565
Checksum: 321
Coasting Arc #17 (Orbit 3580)
---------------------------------------
Vector Time (GMT): 2016/110/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943970
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213171
43 A = 6780642
17 meter
Y = 2932184
72 meter E =
0009745
Z = 4423675
60 I = 51
58386
XDOT = -5949
706785 Wp = 104
69256
YDOT = 3526
594828 meter/sec RA = 351
72261 deg
ZDOT = 3320
479920 TA = 311
73552
MA = 311
81881
Ha = 221
075 n
mi
Hp = 214
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13822740
91 X = 4158581
36
Y = 9620028
61 feet Y = 2978994
42 meter
Z = 14513371
38 Z = 4444009
43
XDOT = -19520
035383 XDOT = -6004
829467
YDOT = 11570
193004 feet/sec YDOT = 3459
753369 meter/sec
ZDOT = 10893
962993 ZDOT = 3291
443226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7256284
89 X = -2211715
64
Y = 15113064
04 feet Y = 4606461
92 meter
Z = 14601119
49 Z = 4450421
22
XDOT = -13505
792336 XDOT = -4116
565504
YDOT = -16913
888240 feet/sec YDOT = -5155
353135 meter/sec
ZDOT = 10767
128246 ZDOT = 3281
820689
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 16110
25553648
00016717 00000-0 10270-3 0 9161
2 25544 51
6408 351
9887 0001106 49
8276 310
2973 15
54223349 35811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
25553648 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 351
9887 deg
Eccentricity:
0001106
Arg of perigee: 49
8276 deg
Mean anomaly: 310
2973 deg
Mean motion: 15
54223349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3581
Checksum: 316
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