[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 21st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
There are no maneuvers
Coasting Arc #1 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2016/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963234
92 A = 6785032
52 meter
Y = 662139
40 meter E =
0011779
Z = 3155630
70 I = 51
83190
XDOT = 1954
963450 Wp = 78
74178
YDOT = -5606
351783 meter/sec RA = 149
24498 deg
ZDOT = 4857
600931 TA = 317
56279
MA = 317
65381
Ha = 220
568 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19564419
02 X = -5985524
44
Y = 2172373
37 feet Y = 595330
28 meter
Z = 10353119
09 Z = 3126608
94
XDOT = 6413
922081 XDOT = 1993
913921
YDOT = -18393
542596 feet/sec YDOT = -5584
271745 meter/sec
ZDOT = 15937
010929 ZDOT = 4867
192782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19739086
66 X = -6016473
61
Y = 671274
95 feet Y = 204604
61 meter
Z = 10226955
57 Z = 3117176
06
XDOT = 7743
291059 XDOT = 2360
155115
YDOT = -16418
375440 feet/sec YDOT = -5004
320834 meter/sec
ZDOT = 15979
555906 ZDOT = 4870
568640
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 16078
55789319
00016717 00000-0 10270-3 0 9006
2 25544 51
6424 150
0323 0001863 312
5236 47
5759 15
54189115 30884
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
55789319 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 150
0323 deg
Eccentricity:
0001863
Arg of perigee: 312
5236 deg
Mean anomaly: 47
5759 deg
Mean motion: 15
54189115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 314
Coasting Arc #2 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2016/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5156486
38 A = 6781170
84 meter
Y = 530350
16 meter E =
0008226
Z = -4380556
55 I = 51
84527
XDOT = -3526
038674 Wp = 57
50618
YDOT = 5866
169737 meter/sec RA = 144
27273 deg
ZDOT = -3440
793933 TA = 177
66203
MA = 177
65818
Ha = 220
551 n
mi
Hp = 215
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16917606
24 X = 5171451
24
Y = 1739993
97 feet Y = 588096
53 meter
Z = -14371904
69 Z = -4355471
66
XDOT = -11568
368354 XDOT = -3574
659886
YDOT = 19245
963703 feet/sec YDOT = 5826
466927 meter/sec
ZDOT = -11288
694006 ZDOT = -3458
041187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16877341
32 X = 5144213
64
Y = 2739759
93 feet Y = 835078
83 meter
Z = -14263018
25 Z = -4347367
96
XDOT = -12411
757100 XDOT = -3783
103564
YDOT = 17302
094425 feet/sec YDOT = 5273
678381 meter/sec
ZDOT = -11364
542036 ZDOT = -3463
912413
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 16079
52238756
00016717 00000-0 10270-3 0 9019
2 25544 51
6417 145
2238 0001885 319
0876 41
0135 15
54182550 31034
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
52238756 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 145
2238 deg
Eccentricity:
0001885
Arg of perigee: 319
0876 deg
Mean anomaly: 41
0135 deg
Mean motion: 15
54182550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 297
Coasting Arc #3 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2016/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4041662
00 A = 6778001
82 meter
Y = -1828545
77 meter E =
0003370
Z = 5122402
81 I = 51
86105
XDOT = 4736
425097 Wp = 114
07958
YDOT = -5799
430844 meter/sec RA = 139
29208 deg
ZDOT = 1664
691592 TA = 319
89063
MA = 319
91551
Ha = 220
657 n
mi
Hp = 214
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13260045
94 X = -4045796
53
Y = -5999165
90 feet Y = -1873764
70 meter
Z = 16805783
51 Z = 5102759
87
XDOT = 15539
452418 XDOT = 4792
837486
YDOT = -19027
004083 feet/sec YDOT = -5746
149330 meter/sec
ZDOT = 5461
586588 ZDOT = 1687
837559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13105088
78 X = -3994431
06
Y = -6551855
86 feet Y = -1997005
66 meter
Z = 16720735
69 Z = 5096480
24
XDOT = 15808
923975 XDOT = 4818
560027
YDOT = -17405
363716 feet/sec YDOT = -5305
154861 meter/sec
ZDOT = 5563
060302 ZDOT = 1695
620780
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 16080
55116674
00016717 00000-0 10270-3 0 9029
2 25544 51
6421 140
0945 0001969 324
6210 35
4812 15
54230308 31195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
55116674 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 140
0945 deg
Eccentricity:
0001969
Arg of perigee: 324
6210 deg
Mean anomaly: 35
4812 deg
Mean motion: 15
54230308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 278
Coasting Arc #4 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2016/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2757406
16 A = 6777129
12 meter
Y = 3165064
77 meter E =
0013921
Z = -5332482
81 I = 51
88121
XDOT = -5512
356699 Wp = 85
18517
YDOT = 5308
127111 meter/sec RA = 134
30685 deg
ZDOT = 302
005526 TA = 187
67722
MA = 187
69856
Ha = 220
643 n
mi
Hp = 214
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9046608
14 X = 2747711
38
Y = 10384070
77 feet Y = 3195844
88 meter
Z = -17495022
34 Z = -5319112
17
XDOT = -18085
159772 XDOT = -5572
770807
YDOT = 17415
115193 feet/sec YDOT = 5246
146525 meter/sec
ZDOT = 990
831777 ZDOT = 275
080541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8900093
21 X = 2712748
41
Y = 10605191
43 feet Y = 3232462
35 meter
Z = -17437434
06 Z = -5314929
90
XDOT = -17741
720942 XDOT = -5407
676543
YDOT = 16314
817213 feet/sec YDOT = 4972
756286 meter/sec
ZDOT = 873
005659 ZDOT = 266
092125
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 16081
51563729
00016717 00000-0 10270-3 0 9034
2 25544 51
6416 135
2855 0002028 331
5760 28
5281 15
54214517 31343
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
51563729 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 135
2855 deg
Eccentricity:
0002028
Arg of perigee: 331
5760 deg
Mean anomaly: 28
5281 deg
Mean motion: 15
54214517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 291
Coasting Arc #5 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2016/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1397208
78 A = 6778520
98 meter
Y = -4414947
40 meter E =
0007062
Z = 4948036
84 I = 51
90805
XDOT = 5874
652867 Wp = 41
06772
YDOT = -4388
390343 meter/sec RA = 129
32431 deg
ZDOT = -2249
726061 TA = 70
85172
MA = 70
77529
Ha = 220
636 n
mi
Hp = 214
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4584018
29 X = -1371771
21
Y = -14484735
56 feet Y = -4430428
88 meter
Z = 16233716
68 Z = 4941312
09
XDOT = 19273
795494 XDOT = 5934
216470
YDOT = -14397
606113 feet/sec YDOT = -4322
363393 meter/sec
ZDOT = -7380
991013 ZDOT = -2221
043233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4580137
97 X = -1396026
05
Y = -14517851
65 feet Y = -4425041
18 meter
Z = 16205204
87 Z = 4939346
44
XDOT = 18369
020749 XDOT = 5598
877524
YDOT = -13919
780230 feet/sec YDOT = -4242
749014 meter/sec
ZDOT = -7255
661792 ZDOT = -2211
525714
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 16082
54439090
00016717 00000-0 10270-3 0 9042
2 25544 51
6414 130
1560 0002087 336
7240 23
3818 15
54283162 31502
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
54439090 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 130
1560 deg
Eccentricity:
0002087
Arg of perigee: 336
7240 deg
Mean anomaly: 23
3818 deg
Mean motion: 15
54283162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 278
Coasting Arc #6 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2016/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 110176
82 A = 6781937
38 meter
Y = 5448506
55 meter E =
0006320
Z = -4042486
16 I = 51
93924
XDOT = -5821
492410 Wp = 92
15277
YDOT = 3041
870448 meter/sec RA = 124
34975 deg
ZDOT = 3946
284595 TA = 218
67539
MA = 218
72066
Ha = 220
737 n
mi
Hp = 214
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 361472
52 X = 68878
71
Y = 17875677
66 feet Y = 5449507
05 meter
Z = -13262749
88 Z = -4042052
15
XDOT = -19099
384547 XDOT = -5874
244025
YDOT = 9979
889921 feet/sec YDOT = 2976
476338 meter/sec
ZDOT = 12947
127935 ZDOT = 3917
876662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 620877
71 X = 189243
53
Y = 17869294
85 feet Y = 5446561
07 meter
Z = -13261744
28 Z = -4042179
66
XDOT = -17780
994426 XDOT = -5419
647101
YDOT = 10122
205499 feet/sec YDOT = 3085
248236 meter/sec
ZDOT = 12823
198426 ZDOT = 3908
510880
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 16083
50883798
00016717 00000-0 10270-3 0 9058
2 25544 51
6415 125
3465 0002066 347
3510 12
7591 15
54289208 31651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
50883798 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 125
3465 deg
Eccentricity:
0002066
Arg of perigee: 347
3510 deg
Mean anomaly: 12
7591 deg
Mean motion: 15
54289208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 313
Coasting Arc #7 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2016/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1070501
08 A = 6785771
71 meter
Y = -6144002
47 meter E =
0012926
Z = 2662065
88 I = 51
96888
XDOT = 5446
465049 Wp = 93
36123
YDOT = -1328
030195 meter/sec RA = 119
38718 deg
ZDOT = -5234
164344 TA = 56
74440
MA = 56
62060
Ha = 220
744 n
mi
Hp = 214
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3512142
65 X = 1126194
08
Y = -20157488
40 feet Y = -6131719
59 meter
Z = 8733811
93 Z = 2667402
35
XDOT = 17868
979820 XDOT = 5486
335999
YDOT = -4357
054445 feet/sec YDOT = -1266
902092 meter/sec
ZDOT = -17172
455198 ZDOT = -5207
609674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2911578
19 X = 887449
03
Y = -20242505
58 feet Y = -6169915
70 meter
Z = 8758004
11 Z = 2669439
65
XDOT = 16378
927455 XDOT = 4992
297088
YDOT = -5053
727323 feet/sec YDOT = -1540
376088 meter/sec
ZDOT = -17056
848033 ZDOT = -5198
927281
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 16084
53756698
00016717 00000-0 10270-3 0 9061
2 25544 51
6408 120
2163 0002164 350
9916 9
1197 15
54313483 31814
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
53756698 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 120
2163 deg
Eccentricity:
0002164
Arg of perigee: 350
9916 deg
Mean anomaly: 9
1197 deg
Mean motion: 15
54313483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 309
Coasting Arc #8 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2016/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2034401
20 A = 6788313
72 meter
Y = 6390586
58 meter E =
0011339
Z = -1012634
55 I = 51
99277
XDOT = -4820
923827 Wp = 31
31827
YDOT = -600
583410 meter/sec RA = 114
43509 deg
ZDOT = 5934
255104 TA = 317
75921
MA = 317
84650
Ha = 220
792 n
mi
Hp = 214
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6674544
61 X = -2100792
16
Y = 20966491
40 feet Y = 6367465
19 meter
Z = -3322291
82 Z = -1022679
41
XDOT = -15816
679221 XDOT = -4842
675865
YDOT = -1970
418011 feet/sec YDOT = -654
614935 meter/sec
ZDOT = 19469
340891 ZDOT = 5910
783397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5721230
18 X = -1743830
96
Y = 21239392
10 feet Y = 6473766
71 meter
Z = -3366998
42 Z = -1026261
12
XDOT = -14464
057542 XDOT = -4408
644739
YDOT = -845
999186 feet/sec YDOT = -257
860552 meter/sec
ZDOT = 19367
442220 ZDOT = 5903
196389
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 16085
50198961
00016717 00000-0 10270-3 0 9073
2 25544 51
6412 115
4069 0002147 355
5934 4
5200 15
54323449 31965
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
50198961 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 115
4069 deg
Eccentricity:
0002147
Arg of perigee: 355
5934 deg
Mean anomaly: 4
5200 deg
Mean motion: 15
54323449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 302
Coasting Arc #9 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2016/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2821158
99 A = 6788487
91 meter
Y = -6120037
12 meter E =
0008834
Z = -791006
13 I = 52
00537
XDOT = 4024
063919 Wp = 131
25366
YDOT = 2621
030525 meter/sec RA = 109
48761 deg
ZDOT = -5975
823480 TA = 57
25321
MA = 57
16810
Ha = 220
862 n
mi
Hp = 214
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9255770
96 X = 2893227
49
Y = -20078861
93 feet Y = -6088086
19 meter
Z = -2595164
47 Z = -777125
68
XDOT = 13202
309446 XDOT = 4023
484021
YDOT = 8599
181513 feet/sec YDOT = 2666
026239 meter/sec
ZDOT = -19605
720078 ZDOT = -5956
277204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8023712
39 X = 2445627
54
Y = -20609819
80 feet Y = -6281873
08 meter
Z = -2533818
91 Z = -772308
00
XDOT = 12327
232367 XDOT = 3757
340425
YDOT = 7178
983207 feet/sec YDOT = 2188
154082 meter/sec
ZDOT = -19521
215653 ZDOT = -5950
066531
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 16086
53069368
00016717 00000-0 10270-3 0 9086
2 25544 51
6408 110
2761 0002153
9780 359
1376 15
54329769 32122
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
53069368 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 110
2761 deg
Eccentricity:
0002153
Arg of perigee:
9780 deg
Mean anomaly: 359
1376 deg
Mean motion: 15
54329769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 312
Coasting Arc #10 (Orbit 3227)
---------------------------------------
Vector Time (GMT): 2016/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380939
84 A = 6786155
08 meter
Y = 5326821
89 meter E =
0014713
Z = 2477996
16 I = 52
00698
XDOT = -3153
273914 Wp = 66
42442
YDOT = -4501
162242 meter/sec RA = 104
53800 deg
ZDOT = 5354
317721 TA = 321
21310
MA = 321
31863
Ha = 220
979 n
mi
Hp = 214
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11092322
30 X = -3452291
54
Y = 17476449
78 feet Y = 5288615
32 meter
Z = 8129908
67 Z = 2461398
33
XDOT = -10345
386858 XDOT = -3128
715628
YDOT = -14767
592657 feet/sec YDOT = -4536
286292 meter/sec
ZDOT = 17566
659190 ZDOT = 5339
059970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9738508
30 X = -2968297
33
Y = 18297803
27 feet Y = 5577170
44 meter
Z = 8056871
45 Z = 2455734
42
XDOT = -10250
280563 XDOT = -3124
285516
YDOT = -13189
673894 feet/sec YDOT = -4020
212603 meter/sec
ZDOT = 17501
113859 ZDOT = 5334
339504
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 16087
55938505
00016717 00000-0 10270-3 0 9098
2 25544 51
6404 105
1459 0002306 5
7082 354
4097 15
54341501 32286
Satellite: ISS
Catalog Number: 25544
Epoch time: 16087
55938505 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 105
1459 deg
Eccentricity:
0002306
Arg of perigee: 5
7082 deg
Mean anomaly: 354
4097 deg
Mean motion: 15
54341501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3228
Checksum: 298
Coasting Arc #11 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2016/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3788671
78 A = 6782200
60 meter
Y = -4042297
55 meter E =
0007644
Z = -3920840
36 I = 52
00138
XDOT = 2229
111487 Wp = 58
58924
YDOT = 6070
479929 meter/sec RA = 99
57943 deg
ZDOT = -4106
570350 TA = 168
55479
MA = 168
53740
Ha = 220
898 n
mi
Hp = 214
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12430025
51 X = 3852638
08
Y = -13262131
06 feet Y = -3999572
86 meter
Z = -12863649
46 Z = -3902279
99
XDOT = 7313
357898 XDOT = 2181
012310
YDOT = 19916
272734 feet/sec YDOT = 6095
137961 meter/sec
ZDOT = -13472
999837 ZDOT = -4095
859272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11187049
15 X = 3409812
58
Y = -14398825
41 feet Y = -4388761
99 meter
Z = -12782288
14 Z = -3896041
42
XDOT = 8220
007313 XDOT = 2505
458229
YDOT = 18300
572602 feet/sec YDOT = 5578
014529 meter/sec
ZDOT = -13427
492423 ZDOT = -4092
699691
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 16088
52377002
00016717 00000-0 10270-3 0 9107
2 25544 51
6405 100
3360 0002264 7
8195 352
2993 15
54369310 32432
Satellite: ISS
Catalog Number: 25544
Epoch time: 16088
52377002 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 100
3360 deg
Eccentricity:
0002264
Arg of perigee: 7
8195 deg
Mean anomaly: 352
2993 deg
Mean motion: 15
54369310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 283
Coasting Arc #12 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2016/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4030978
11 A = 6778511
92 meter
Y = 2382233
04 meter E =
0006528
Z = 4896416
26 I = 51
99287
XDOT = -1308
404333 Wp = 100
90593
YDOT = -7167
055999 meter/sec RA = 94
60976 deg
ZDOT = 2405
901972 TA = 325
62152
MA = 325
66374
Ha = 221
087 n
mi
Hp = 214
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13224993
80 X = -4081102
08
Y = 7815725
21 feet Y = 2336876
17 meter
Z = 16064357
81 Z = 4876712
68
XDOT = -4292
665134 XDOT = -1239
850200
YDOT = -23513
963250 feet/sec YDOT = -7181
303909 meter/sec
ZDOT = 7893
379172 ZDOT = 2399
713219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12361923
05 X = -3767914
15
Y = 9269642
44 feet Y = 2825387
01 meter
Z = 15978304
07 Z = 4870187
08
XDOT = -6290
049513 XDOT = -1917
207091
YDOT = -21972
393307 feet/sec YDOT = -6697
185480 meter/sec
ZDOT = 7867
730053 ZDOT = 2398
084120
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 16089
55243544
00016717 00000-0 10270-3 0 9115
2 25544 51
6398 95
2052 0002348 12
0489 348
0720 15
54382370 32599
Satellite: ISS
Catalog Number: 25544
Epoch time: 16089
55243544 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 95
2052 deg
Eccentricity:
0002348
Arg of perigee: 12
0489 deg
Mean anomaly: 348
0720 deg
Mean motion: 15
54382370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3259
Checksum: 308
Coasting Arc #13 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2016/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166664
72 A = 6776640
22 meter
Y = -493775
86 meter E =
0015641
Z = -5334838
04 I = 51
98858
XDOT = 372
518028 Wp = 78
60325
YDOT = 7637
245020 meter/sec RA = 89
63268 deg
ZDOT = -413
952852 TA = 187
45086
MA = 187
47413
Ha = 220
950 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13670159
84 X = 4197791
03
Y = -1619999
55 feet Y = -447007
88 meter
Z = -17502749
48 Z = -5314521
70
XDOT = 1222
172008 XDOT = 289
099581
YDOT = 25056
578149 feet/sec YDOT = 7640
944308 meter/sec
ZDOT = -1358
113032 ZDOT = -412
346524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13455352
07 X = 4101191
31
Y = -3396703
67 feet Y = -1035315
28 meter
Z = -17414356
51 Z = -5307895
86
XDOT = 4224
921746 XDOT = 1287
756148
YDOT = 23703
568888 feet/sec YDOT = 7224
847797 meter/sec
ZDOT = -1352
478533 ZDOT = -412
235457
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 16090
51679621
00016717 00000-0 10270-3 0 9123
2 25544 51
6401 90
3959 0002334 14
1190 346
0027 15
54394617 32745
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
51679621 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 90
3959 deg
Eccentricity:
0002334
Arg of perigee: 14
1190 deg
Mean anomaly: 346
0027 deg
Mean motion: 15
54394617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 292
Coasting Arc #14 (Orbit 3289)
---------------------------------------
Vector Time (GMT): 2016/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4169641
91 A = 6777341
98 meter
Y = -1454385
38 meter E =
0007044
Z = 5138279
68 I = 51
98961
XDOT = 583
951199 Wp = 42
61470
YDOT = -7472
450221 meter/sec RA = 84
65290 deg
ZDOT = -1634
848681 TA = 63
11389
MA = 63
04191
Ha = 221
061 n
mi
Hp = 213
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13679927
53 X = -4178028
31
Y = -4771605
57 feet Y = -1501059
54 meter
Z = 16857872
98 Z = 5118004
33
XDOT = 1915
850392 XDOT = 675
408001
YDOT = -24515
912799 feet/sec YDOT = -7465
408863 meter/sec
ZDOT = -5363
676776 ZDOT = -1631
789220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14338982
78 X = -4370521
95
Y = -2693911
57 feet Y = -821104
25 meter
Z = 16770000
94 Z = 5111496
29
XDOT = -1867
012619 XDOT = -569
065446
YDOT = -23491
426296 feet/sec YDOT = -7160
186735 meter/sec
ZDOT = -5349
045432 ZDOT = -1630
389048
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 16091
54543437
00016717 00000-0 10270-3 0 9133
2 25544 51
6395 85
2648 0002399 16
3902 343
7328 15
54433462 32909
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
54543437 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 85
2648 deg
Eccentricity:
0002399
Arg of perigee: 16
3902 deg
Mean anomaly: 343
7328 deg
Mean motion: 15
54433462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3290
Checksum: 316
Coasting Arc #15 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2016/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4058080
45 A = 6780479
96 meter
Y = 3243111
86 meter E =
0009006
Z = -4365799
65 I = 51
99608
XDOT = -1560
785980 Wp = 94
39253
YDOT = 6640
505424 meter/sec RA = 79
67964 deg
ZDOT = 3487
597137 TA = 210
87101
MA = 210
92400
Ha = 221
042 n
mi
Hp = 213
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13313912
24 X = 4042720
73
Y = 10640130
77 feet Y = 3288405
75 meter
Z = -14323489
65 Z = -4346124
11
XDOT = -5120
688911 XDOT = -1651
867000
YDOT = 21786
435119 feet/sec YDOT = 6622
542719 meter/sec
ZDOT = 11442
247826 ZDOT = 3479
793428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14967501
25 X = 4562094
38
Y = 8298957
80 feet Y = 2529522
34 meter
Z = -14238546
40 Z = -4339908
94
XDOT = -949
530602 XDOT = -289
416927
YDOT = 21252
579132 feet/sec YDOT = 6477
786120 meter/sec
ZDOT = 11407
130666 ZDOT = 3476
893427
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 16092
50977026
00016717 00000-0 10270-3 0 9146
2 25544 51
6395 80
4552 0002482 20
4776 339
6476 15
54427783 33052
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
50977026 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 80
4552 deg
Eccentricity:
0002482
Arg of perigee: 20
4776 deg
Mean anomaly: 339
6476 deg
Mean motion: 15
54427783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 322
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