[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 26th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 68 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
160/13:47:39
077 -0
3 1
9 2
0
N/A 1
9 -0
2 220
2
000/00:05:18
153 0
2 -0
0 214
8
161/01:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
7
Coasting Arc #1 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2016/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1081240
15 A = 6776592
42 meter
Y = 4307113
08 meter E =
0015082
Z = -5132298
32 I = 51
68134
XDOT = -7488
616798 Wp = 104
11474
YDOT = 27
311705 meter/sec RA = 170
06445 deg
ZDOT = 1600
931743 TA = 181
33690
MA = 181
34093
Ha = 220
651 n
mi
Hp = 213
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3547375
82 X = -1104392
31
Y = 14130948
41 feet Y = 4294892
99 meter
Z = -16838249
08 Z = -5137606
56
XDOT = -24568
952749 XDOT = -7496
142332
YDOT = 89
605331 feet/sec YDOT = -56
473228 meter/sec
ZDOT = 5252
400732 ZDOT = 1564
535340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10970366
59 X = 3343767
74
Y = 9545455
67 feet Y = 2909454
89 meter
Z = -16862074
11 Z = -5139560
19
XDOT = -10526
089249 XDOT = -3208
352003
YDOT = 21093
937963 feet/sec YDOT = 6429
432291 meter/sec
ZDOT = 5094
029718 ZDOT = 1552
660258
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 16146
51341461
00016717 00000-0 10270-3 0 9000
2 25544 51
6412 171
1494 0001530 120
7050 239
4254 15
54665671 1457
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
51341461 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 171
1494 deg
Eccentricity:
0001530
Arg of perigee: 120
7050 deg
Mean anomaly: 239
4254 deg
Mean motion: 15
54665671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 271
Coasting Arc #2 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2016/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984797
98 A = 6779718
58 meter
Y = -4304629
42 meter E =
0010883
Z = 4296221
29 I = 51
72196
XDOT = 6714
052713 Wp = 79
07514
YDOT = 1106
208548 meter/sec RA = 165
06953 deg
ZDOT = -3546
581803 TA = 47
04037
MA = 46
94916
Ha = 220
556 n
mi
Hp = 213
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9792644
31 X = 3011842
29
Y = -14122799
92 feet Y = -4271100
61 meter
Z = 14095214
22 Z = 4310786
06
XDOT = 22027
731998 XDOT = 6718
411664
YDOT = 3629
293137 feet/sec YDOT = 1181
314256 meter/sec
ZDOT = -11635
767069 ZDOT = -3513
955749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8344876
29 X = -2543518
29
Y = -14963320
48 feet Y = -4560820
08 meter
Z = 14159325
68 Z = 4315762
47
XDOT = 11974
211081 XDOT = 3649
739538
YDOT = -17584
034275 feet/sec YDOT = -5359
613647 meter/sec
ZDOT = -11493
972218 ZDOT = -3503
362732
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 16147
54187760
00016717 00000-0 10270-3 0 9015
2 25544 51
6393 166
0186 0001637 120
9463 239
1851 15
54711862 1616
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
54187760 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 166
0186 deg
Eccentricity:
0001637
Arg of perigee: 120
9463 deg
Mean anomaly: 239
1851 deg
Mean motion: 15
54711862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 305
Coasting Arc #3 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535780
14 A = 6783909
25 meter
Y = 4104062
33 meter E =
0005598
Z = -2937203
97 I = 51
76807
XDOT = -5315
719590 Wp = 82
32117
YDOT = -2285
025603 meter/sec RA = 160
08876 deg
ZDOT = 5024
938588 TA = 244
23935
MA = 244
29713
Ha = 220
580 n
mi
Hp = 213
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14881168
45 X = -4567067
97
Y = 13464771
43 feet Y = 4053165
52 meter
Z = -9636495
95 Z = -2959313
39
XDOT = -17440
024900 XDOT = -5314
181856
YDOT = -7496
803161 feet/sec YDOT = -2344
461332 meter/sec
ZDOT = 16486
018988 ZDOT = 4999
119607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5813818
62 X = 1772051
91
Y = 19159105
90 feet Y = 5839695
48 meter
Z = -9733420
41 Z = -2966746
54
XDOT = -12894
573631 XDOT = -3930
266043
YDOT = 12216
634637 feet/sec YDOT = 3723
630237 meter/sec
ZDOT = 16374
031518 ZDOT = 4990
804807
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 16148
50605941
00016717 00000-0 10270-3 0 9029
2 25544 51
6407 161
2085 0001624 124
8859 235
2447 15
54707989 1764
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
50605941 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 161
2085 deg
Eccentricity:
0001624
Arg of perigee: 124
8859 deg
Mean anomaly: 235
2447 deg
Mean motion: 15
54707989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 176
Checksum: 317
Coasting Arc #4 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5615569
18 A = 6787045
85 meter
Y = -3615242
33 meter E =
0015321
Z = 1165950
09 I = 51
80737
XDOT = 3477
078509 Wp = 122
41605
YDOT = 3488
392929 meter/sec RA = 155
12114 deg
ZDOT = -5882
032947 TA = 44
94432
MA = 44
82039
Ha = 220
597 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18423783
38 X = 5649914
66
Y = -11861031
26 feet Y = -3552253
34 meter
Z = 3825295
58 Z = 1193312
39
XDOT = 11407
737889 XDOT = 3466
384479
YDOT = 11444
858692 feet/sec YDOT = 3527
216546 meter/sec
ZDOT = -19298
008355 ZDOT = -5865
167845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3204007
28 X = -976581
42
Y = -21654651
49 feet Y = -6600337
78 meter
Z = 3945015
72 Z = 1202440
79
XDOT = 13604
891711 XDOT = 4146
770993
YDOT = -5543
341007 feet/sec YDOT = -1689
610339 meter/sec
ZDOT = -19225
187410 ZDOT = -5859
837123
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 16149
53451640
00016717 00000-0 10270-3 0 9039
2 25544 51
6397 156
0770 0001597 123
5579 236
5727 15
54704398 1923
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
53451640 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 156
0770 deg
Eccentricity:
0001597
Arg of perigee: 123
5579 deg
Mean anomaly: 236
5727 deg
Mean motion: 15
54704398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 192
Checksum: 326
Coasting Arc #5 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6110051
76 A = 6787349
23 meter
Y = 2853300
05 meter E =
0013480
Z = 718929
95 I = 51
83651
XDOT = -1432
131390 Wp = 59
36178
YDOT = -4591
356027 meter/sec RA = 150
16198 deg
ZDOT = 5974
443792 TA = 308
38706
MA = 308
50807
Ha = 220
477 n
mi
Hp = 213
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20046101
57 X = -6144996
23
Y = 9361220
62 feet Y = 2784777
95 meter
Z = 2358694
07 Z = 689163
99
XDOT = -4698
593799 XDOT = -1409
704677
YDOT = -15063
504024 feet/sec YDOT = -4607
246017 meter/sec
ZDOT = 19601
193544 ZDOT = 5967
541032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 622177
78 X = 189639
79
Y = 22128899
77 feet Y = 6744888
65 meter
Z = 2228624
53 Z = 679284
76
XDOT = -14125
253239 XDOT = -4305
377187
YDOT = -1600
672823 feet/sec YDOT = -487
885076 meter/sec
ZDOT = 19571
924170 ZDOT = 5965
522487
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 16150
56296886
00016717 00000-0 10270-3 0 9044
2 25544 51
6388 150
9467 0001578 135
8093 224
3186 15
54743356 2084
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
56296886 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 150
9467 deg
Eccentricity:
0001578
Arg of perigee: 135
8093 deg
Mean anomaly: 224
3186 deg
Mean motion: 15
54743356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 332
Coasting Arc #6 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6035827
80 A = 6784987
44 meter
Y = -1753420
67 meter E =
0006794
Z = -2552848
59 I = 51
85511
XDOT = -634
598104 Wp = 130
84199
YDOT = 5506
054973 meter/sec RA = 145
19988 deg
ZDOT = -5295
760725 TA = 77
74442
MA = 77
66835
Ha = 220
596 n
mi
Hp = 213
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19802584
65 X = 6067387
13
Y = -5752692
49 feet Y = -1685747
44 meter
Z = -8375487
51 Z = -2523451
25
XDOT = -2082
014777 XDOT = -670
396297
YDOT = 18064
484818 feet/sec YDOT = 5498
758580 meter/sec
ZDOT = -17374
543060 ZDOT = -5298
930142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2254427
99 X = 687149
65
Y = -20549596
89 feet Y = -6263517
13 meter
Z = -8247196
06 Z = -2513745
36
XDOT = 14447
679478 XDOT = 4403
652705
YDOT = 8545
788846 feet/sec YDOT = 2604
756440 meter/sec
ZDOT = -17389
283605 ZDOT = -5300
253643
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 16151
52714459
00016717 00000-0 10270-3 0 9053
2 25544 51
6384 146
1355 0001508 131
1667 228
9616 15
54698855 2230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52714459 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 146
1355 deg
Eccentricity:
0001508
Arg of perigee: 131
1667 deg
Mean anomaly: 228
9616 deg
Mean motion: 15
54698855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 317
Coasting Arc #7 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5435370
49 A = 6780813
13 meter
Y = 412318
80 meter E =
0011986
Z = 4025526
66 I = 51
86733
XDOT = 2473
392749 Wp = 105
29978
YDOT = -6093
804715 meter/sec RA = 140
23008 deg
ZDOT = 3950
940373 TA = 303
74673
MA = 303
86088
Ha = 220
516 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17832580
33 X = -5459131
67
Y = 1352751
97 feet Y = 351403
81 meter
Z = 13207108
46 Z = 3999064
99
XDOT = 8114
805608 XDOT = 2522
159187
YDOT = -19992
797620 feet/sec YDOT = -6065
873125 meter/sec
ZDOT = 12962
402800 ZDOT = 3963
073769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5287297
71 X = -1611568
34
Y = 17172867
59 feet Y = 5234290
04 meter
Z = 13091817
08 Z = 3990385
85
XDOT = -14421
765036 XDOT = -4395
753983
YDOT = -14395
751352 feet/sec YDOT = -4387
825012 meter/sec
ZDOT = 13016
283822 ZDOT = 3967
363309
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 16152
55559127
00016717 00000-0 10270-3 0 9067
2 25544 51
6385 141
0047 0001339 139
3519 220
7734 15
54732255 2392
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
55559127 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 141
0047 deg
Eccentricity:
0001339
Arg of perigee: 139
3519 deg
Mean anomaly: 220
7734 deg
Mean motion: 15
54732255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 239
Checksum: 303
Coasting Arc #8 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429519
18 A = 6777142
56 meter
Y = 1146314
60 meter E =
0013302
Z = -5011522
43 I = 51
87816
XDOT = -3957
619289 Wp = 79
92789
YDOT = 6219
447116 meter/sec RA = 135
24808 deg
ZDOT = -2077
818018 TA = 169
91325
MA = 169
88653
Ha = 220
481 n
mi
Hp = 213
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14532543
24 X = 4440715
76
Y = 3760874
67 feet Y = 1195911
35 meter
Z = -16442002
74 Z = -4989977
36
XDOT = -12984
315253 XDOT = -4016
779273
YDOT = 20405
010222 feet/sec YDOT = 6174
859729 meter/sec
ZDOT = -6816
988249 ZDOT = -2097
186729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8636593
35 X = 2632433
65
Y = -12402343
39 feet Y = -3780234
27 meter
Z = -16348381
55 Z = -4982986
70
XDOT = 13693
288401 XDOT = 4173
714305
YDOT = 18623
588640 feet/sec YDOT = 5676
469818 meter/sec
ZDOT = -6902
412964 ZDOT = -2103
855471
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 16153
51975941
00016717 00000-0 10270-3 0 9071
2 25544 51
6377 136
1934 0001358 134
9659 225
1604 15
54705343 2540
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51975941 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 136
1934 deg
Eccentricity:
0001358
Arg of perigee: 134
9659 deg
Mean anomaly: 225
1604 deg
Mean motion: 15
54705343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 315
Coasting Arc #9 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3154694
60 A = 6775660
23 meter
Y = -2742531
74 meter E =
0003339
Z = 5329789
10 I = 51
89533
XDOT = 4987
431290 Wp = 107
28929
YDOT = -5830
014718 meter/sec RA = 130
26024 deg
ZDOT = -48
820099 TA = 343
16850
MA = 343
17957
Ha = 220
527 n
mi
Hp = 213
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10350047
89 X = -3149682
70
Y = -8997807
54 feet Y = -2777782
04 meter
Z = 17486184
71 Z = 5314476
08
XDOT = 16362
963549 XDOT = 5052
490447
YDOT = -19127
344874 feet/sec YDOT = -5773
878169 meter/sec
ZDOT = -160
170928 ZDOT = -24
434455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11968212
06 X = -3647911
04
Y = 6867090
02 feet Y = 2093089
04 meter
Z = 17419978
82 Z = 5309609
55
XDOT = -12081
183994 XDOT = -3682
344881
YDOT = -20929
088265 feet/sec YDOT = -6379
186103 meter/sec
ZDOT = -52
945280 ZDOT = -16
137721
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 16154
54820232
00016717 00000-0 10270-3 0 9088
2 25544 51
6375 131
0621 0001278 142
1322 217
9921 15
54707455 2709
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54820232 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 131
0621 deg
Eccentricity:
0001278
Arg of perigee: 142
1322 deg
Mean anomaly: 217
9921 deg
Mean motion: 15
54707455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 281
Coasting Arc #10 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1773684
46 A = 6777190
31 meter
Y = 4252416
61 meter E =
0013482
Z = -4982485
03 I = 51
92160
XDOT = -5515
982386 Wp = 109
10390
YDOT = 4847
923723 meter/sec RA = 125
27362 deg
ZDOT = 2174
471458 TA = 182
03559
MA = 182
04108
Ha = 220
385 n
mi
Hp = 213
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5819174
74 X = 1750204
20
Y = 13951498
06 feet Y = 4272120
36 meter
Z = -16346735
66 Z = -4973925
36
XDOT = -18097
055071 XDOT = -5580
345937
YDOT = 15905
261559 feet/sec YDOT = 4785
880233 meter/sec
ZDOT = 7134
092709 ZDOT = 2147
519926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15108448
46 X = 4605055
09
Y = -1197754
85 feet Y = -365075
68 meter
Z = -16310212
39 Z = -4971352
74
XDOT = 9248
578339 XDOT = 2818
966678
YDOT = 21146
748248 feet/sec YDOT = 6445
528866 meter/sec
ZDOT = 7015
842198 ZDOT = 2138
428702
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 16155
51236309
00016717 00000-0 10270-3 0 9093
2 25544 51
6386 126
2513 0001208 142
9433 217
1804 15
54706213 2850
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51236309 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 126
2513 deg
Eccentricity:
0001208
Arg of perigee: 142
9433 deg
Mean anomaly: 217
1804 deg
Mean motion: 15
54706213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 287
Coasting Arc #11 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -397582
49 A = 6780879
71 meter
Y = -5476976
37 meter E =
0011472
Z = 3969047
94 I = 51
95203
XDOT = 5607
922368 Wp = 84
68789
YDOT = -3338
861623 meter/sec RA = 120
29694 deg
ZDOT = -4034
592900 TA = 47
25085
MA = 47
15437
Ha = 220
327 n
mi
Hp = 213
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1304404
48 X = -355588
20
Y = -17969082
57 feet Y = -5481188
09 meter
Z = 13021810
82 Z = 3967217
87
XDOT = 18398
695434 XDOT = 5664
440138
YDOT = -10954
270417 feet/sec YDOT = -3275
833591 meter/sec
ZDOT = -13236
853348 ZDOT = -4007
213783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17554286
69 X = -5350546
58
Y = -4076545
28 feet Y = -1242531
00 meter
Z = 13014828
23 Z = 3966919
65
XDOT = -5190
521755 XDOT = -1582
071031
YDOT = -19641
751734 feet/sec YDOT = -5986
805928 meter/sec
ZDOT = -13116
988205 ZDOT = -3998
058005
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 16156
54079831
00016717 00000-0 10270-3 0 9104
2 25544 51
6386 121
1199 0001089 145
0708 215
0516 15
54735718 3018
Satellite: ISS
Catalog Number: 25544
Epoch time: 16156
54079831 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 121
1199 deg
Eccentricity:
0001089
Arg of perigee: 145
0708 deg
Mean anomaly: 215
0516 deg
Mean motion: 15
54735718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 296
Coasting Arc #12 (Orbit 315)
---------------------------------------
Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -831316
53 A = 6785012
75 meter
Y = 6265186
72 meter E =
0005293
Z = -2468004
41 I = 51
98141
XDOT = -5298
660601 Wp = 60
53247
YDOT = 1403
064876 meter/sec RA = 115
33435 deg
ZDOT = 5357
704285 TA = 271
96920
MA = 272
02982
Ha = 220
301 n
mi
Hp = 213
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2727416
45 X = -889325
03
Y = 20555074
55 feet Y = 6255566
39 meter
Z = -8097127
34 Z = -2472182
80
XDOT = -17384
057090 XDOT = -5339
981867
YDOT = 4603
231220 feet/sec YDOT = 1343
579941 meter/sec
ZDOT = 17577
769965 ZDOT = 5331
864310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18947151
98 X = 5775091
92
Y = 8404856
88 feet Y = 2561800
38 meter
Z = -8116475
48 Z = -2473901
73
XDOT = 56
725485 XDOT = 17
289928
YDOT = 16702
589275 feet/sec YDOT = 5090
949211 meter/sec
ZDOT = 17464
942361 ZDOT = 5323
314432
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 16157
50495452
00016717 00000-0 10270-3 0 9113
2 25544 51
6389 116
3097 0001096 149
2786 210
8432 15
54718993 3166
Satellite: ISS
Catalog Number: 25544
Epoch time: 16157
50495452 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 116
3097 deg
Eccentricity:
0001096
Arg of perigee: 149
2786 deg
Mean anomaly: 210
8432 deg
Mean motion: 15
54718993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 316
Checksum: 323
Coasting Arc #13 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1897503
21 A = 6787400
63 meter
Y = -6480601
02 meter E =
0014078
Z = 612473
67 I = 52
00435
XDOT = 4705
867814 Wp = 130
46541
YDOT = 802
662494 meter/sec RA = 110
38283 deg
ZDOT = -6004
860671 TA = 42
95268
MA = 42
84284
Ha = 220
246 n
mi
Hp = 213
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6225404
23 X = 1966854
74
Y = -21261814
36 feet Y = -6458994
19 meter
Z = 2009428
04 Z = 621858
82
XDOT = 15439
198865 XDOT = 4725
711630
YDOT = 2633
407133 feet/sec YDOT = 855
398457 meter/sec
ZDOT = -19700
986452 ZDOT = -5981
952332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18823947
33 X = -5737539
15
Y = -11675123
06 feet Y = -3558577
51 meter
Z = 2051515
83 Z = 625302
02
XDOT = 5849
451995 XDOT = 1782
912968
YDOT = -12921
382184 feet/sec YDOT = -3938
437290 meter/sec
ZDOT = -19601
323446 ZDOT = -5974
483386
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 16158
53338423
00016717 00000-0 10270-3 0 9122
2 25544 51
6408 111
1781 0001056 156
0269 204
0934 15
54735960 3322
Satellite: ISS
Catalog Number: 25544
Epoch time: 16158
53338423 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 111
1781 deg
Eccentricity:
0001056
Arg of perigee: 156
0269 deg
Mean anomaly: 204
0934 deg
Mean motion: 15
54735960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 288
Coasting Arc #14 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2016/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2721917
60 A = 6786841
07 meter
Y = 6075226
81 meter E =
0013671
Z = 1289229
55 I = 52
01270
XDOT = -3920
693705 Wp = 63
44127
YDOT = -3010
199375 meter/sec RA = 105
43551 deg
ZDOT = 5865
390076 TA = 310
51821
MA = 310
63722
Ha = 220
216 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8930175
85 X = -2795912
53
Y = 19931846
50 feet Y = 6044374
61 meter
Z = 4229755
74 Z = 1275828
27
XDOT = -12863
168323 XDOT = -3915
233031
YDOT = -9875
982200 feet/sec YDOT = -3054
013459 meter/sec
ZDOT = 19243
405760 ZDOT = 5846
357177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17046253
31 X = 5195698
01
Y = 13673032
64 feet Y = 4167540
35 meter
Z = 4170228
54 Z = 1271085
66
XDOT = -11820
463367 XDOT = -3602
877234
YDOT = 8850
079869 feet/sec YDOT = 2697
504344 meter/sec
ZDOT = 19161
031815 ZDOT = 5840
282497
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 16159
56180952
00016717 00000-0 10270-3 0 9139
2 25544 51
6406 106
0473 0001036 156
9897 203
1303 15
54750040 3488
Satellite: ISS
Catalog Number: 25544
Epoch time: 16159
56180952 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 106
0473 deg
Eccentricity:
0001036
Arg of perigee: 156
9897 deg
Mean anomaly: 203
1303 deg
Mean motion: 15
54750040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 291
Coasting Arc #15 (Orbit 362)
---------------------------------------
Vector Time (GMT): 2016/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3362154
55 A = 6783579
32 meter
Y = -5035469
75 meter E =
0005157
Z = -3060007
02 I = 52
01002
XDOT = 3008
073776 Wp = 116
72776
YDOT = 5014
582239 meter/sec RA = 100
48286 deg
ZDOT = -4955
450971 TA = 98
18453
MA = 98
12603
Ha = 220
184 n
mi
Hp = 213
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11030690
80 X = 3433076
70
Y = -16520570
05 feet Y = -4997474
97 meter
Z = -10039393
12 Z = -3043502
93
XDOT = 9869
008452 XDOT = 2975
847259
YDOT = 16452
041467 feet/sec YDOT = 5048
040948 meter/sec
ZDOT = -16258
041243 ZDOT = -4940
916198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13462239
48 X = -4103290
59
Y = -14657123
19 feet Y = -4467491
15 meter
Z = -9966525
80 Z = -3037797
06
XDOT = 17260
516907 XDOT = 5261
005553
YDOT = -4860
207937 feet/sec YDOT = -1481
391379 meter/sec
ZDOT = -16195
642647 ZDOT = -4936
431879
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 16160
52595650
00016717 00000-0 10270-3 0 9143
2 25544 51
6411 101
2371 0000930 159
3973 200
7217 15
54759193 3634
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
52595650 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 101
2371 deg
Eccentricity:
0000930
Arg of perigee: 159
3973 deg
Mean anomaly: 200
7217 deg
Mean motion: 15
54759193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 363
Checksum: 291
Coasting Arc #16 (Orbit 363)
---------------------------------------
Vector Time (GMT): 2016/160/13:50:18
153
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3711583
16 A = 6777275
60 meter
Y = 2307279
34 meter E =
0012799
Z = -5191307
29 I = 51
98723
XDOT = -2410
576147 Wp = 105
58757
YDOT = 7125
365763 meter/sec RA = 100
06722 deg
ZDOT = 1443
012423 TA = 178
24966
MA = 178
24518
Ha = 220
164 n
mi
Hp = 214
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12177110
10 X = 3710723
78
Y = 7569814
12 feet Y = 2348780
57 meter
Z = -17031848
08 Z = -5173279
21
XDOT = -7908
714392 XDOT = -2497
084122
YDOT = 23377
184262 feet/sec YDOT = 7097
925224 meter/sec
ZDOT = 4734
292728 ZDOT = 1431
093245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4346603
04 X = 1324844
61
Y = -13760321
14 feet Y = -4194145
88 meter
Z = -16953717
86 Z = -5167493
20
XDOT = 23604
018701 XDOT = 7194
504900
YDOT = 1687
085679 feet/sec YDOT = 514
223715 meter/sec
ZDOT = 4681
012173 ZDOT = 1426
772510
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 16160
59023361
00016717 00000-0 10270-3 0 9156
2 25544 51
6425 100
9167 0001484 236
6937 123
4073 15
54387626 3642
Satellite: ISS
Catalog Number: 25544
Epoch time: 16160
59023361 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 100
9167 deg
Eccentricity:
0001484
Arg of perigee: 236
6937 deg
Mean anomaly: 123
4073 deg
Mean motion: 15
54387626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 364
Checksum: 302
Coasting Arc #17 (Orbit 371)
---------------------------------------
Vector Time (GMT): 2016/161/01:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 923904
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230478
45 A = 6776872
42 meter
Y = 628088
80 meter E =
0003758
Z = 5255905
60 I = 51
98959
XDOT = 193
045671 Wp = 153
03959
YDOT = -7594
152101 meter/sec RA = 97
71328 deg
ZDOT = 1059
339335 TA = 286
84413
MA = 286
88534
Ha = 220
240 n
mi
Hp = 214
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13879522
48 X = -4262718
30
Y = 2060658
80 feet Y = 580599
91 meter
Z = 17243784
77 Z = 5235276
84
XDOT = 633
351938 XDOT = 272
805244
YDOT = -24915
197181 feet/sec YDOT = -7591
547494 meter/sec
ZDOT = 3475
522752 ZDOT = 1060
469955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3661871
78 X = -1116138
52
Y = -13659230
20 feet Y = -4163333
36 meter
Z = 17153766
28 Z = 5228467
96
XDOT = 23823
055973 XDOT = 7261
267461
YDOT = -1999
264901 feet/sec YDOT = -609
375942 meter/sec
ZDOT = 3481
881443 ZDOT = 1061
277464
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 16161
10456219
00016717 00000-0 10270-3 0 9167
2 25544 51
6433 98
3487 0001944 227
4991 132
5998 15
54419677 3723
Satellite: ISS
Catalog Number: 25544
Epoch time: 16161
10456219 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 98
3487 deg
Eccentricity:
0001944
Arg of perigee: 227
4991 deg
Mean anomaly: 132
5998 deg
Mean motion: 15
54419677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 372
Checksum: 334
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