[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 12th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
165/09:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
7
167/11:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
167/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2017/163/12:53:26
982
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2250601
09 A = 6788840
51 meter
Y = 6247052
36 meter E =
0009980
Z = 1385281
35 I = 51
98885
XDOT = -4952
805126 Wp = 46
45748
YDOT = 486
080271 meter/sec RA = 60
80307 deg
ZDOT = 5835
036828 TA = 328
56552
MA = 328
62512
Ha = 219
435 n
mi
Hp = 216
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7383861
85 X = 2173848
62
Y = 20495578
62 feet Y = 6271790
76 meter
Z = 4544886
32 Z = 1396028
54
XDOT = -16249
360651 XDOT = -4986
216261
YDOT = 1594
751544 feet/sec YDOT = 430
507011 meter/sec
ZDOT = 19143
821613 ZDOT = 5810
896535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20002744
26 X = 6096836
45
Y = -8605658
10 feet Y = -2623004
59 meter
Z = 4591189
50 Z = 1399394
56
XDOT = 1977
023872 XDOT = 602
596876
YDOT = 14785
627579 feet/sec YDOT = 4506
659286 meter/sec
ZDOT = 19037
107295 ZDOT = 5802
510303
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 17163
59870279
00016717 00000-0 10270-3 0 9002
2 25544 51
6425 61
2068 0004789 270
7591 89
3013 15
54011823 21037
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
59870279 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 61
2068 deg
Eccentricity:
0004789
Arg of perigee: 270
7591 deg
Mean anomaly: 89
3013 deg
Mean motion: 15
54011823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 303
Coasting Arc #2 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2017/164/12:53:26
982
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1289123
20 A = 6786034
67 meter
Y = -5982751
79 meter E =
0001734
Z = -2929039
40 I = 51
96319
XDOT = 5627
798936 Wp = 205
82448
YDOT = 1259
439335 meter/sec RA = 55
85199 deg
ZDOT = -5049
779323 TA = 7
41315
MA = 7
41059
Ha = 219
387 n
mi
Hp = 216
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4229406
83 X = -1207898
88
Y = -19628450
76 feet Y = -5996713
10 meter
Z = -9609709
33 Z = -2935105
06
XDOT = 18463
907269 XDOT = 5637
826593
YDOT = 4132
018814 feet/sec YDOT = 1322
429924 meter/sec
ZDOT = -16567
517464 ZDOT = -5022
416740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19239313
52 X = -5864142
76
Y = 5702525
93 feet Y = 1738129
90 meter
Z = -9635376
90 Z = -2936862
88
XDOT = 3067
961717 XDOT = 935
114731
YDOT = -17436
842679 feet/sec YDOT = -5314
749649 meter/sec
ZDOT = -16446
896709 ZDOT = -5013
014117
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 17164
56330185
00016717 00000-0 10270-3 0 9018
2 25544 51
6429 56
3997 0004952 273
2695 86
7891 15
54003745 21187
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
56330185 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 56
3997 deg
Eccentricity:
0004952
Arg of perigee: 273
2695 deg
Mean anomaly: 86
7891 deg
Mean motion: 15
54003745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 329
Coasting Arc #3 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5026295
23 A = 6781121
91 meter
Y = 651743
13 meter E =
0004963
Z = -4510084
02 I = 51
92886
XDOT = 2038
407548 Wp = 122
13725
YDOT = 6642
585632 meter/sec RA = 51
57548 deg
ZDOT = 3231
649712 TA = 180
25316
MA = 180
25341
Ha = 219
532 n
mi
Hp = 216
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16490469
90 X = 5040541
41
Y = 2138264
85 feet Y = 708030
76 meter
Z = -14796863
59 Z = -4485633
22
XDOT = 6687
688806 XDOT = 1948
279188
YDOT = 21793
259948 feet/sec YDOT = 6664
876161 meter/sec
ZDOT = 10602
525301 ZDOT = 3241
333527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13746751
45 X = 4190009
84
Y = -9524459
25 feet Y = -2903055
18 meter
Z = -14688990
66 Z = -4477204
35
XDOT = 18818
760763 XDOT = 5735
958281
YDOT = 10745
785600 feet/sec YDOT = 3275
315451 meter/sec
ZDOT = 10644
043642 ZDOT = 3244
304502
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 17165
39928538
00016717 00000-0 10270-3 0 9026
2 25544 51
6410 52
2313 0004696 277
8922 82
1698 15
54030515 21317
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39928538 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 52
2313 deg
Eccentricity:
0004696
Arg of perigee: 277
8922 deg
Mean anomaly: 82
1698 deg
Mean motion: 15
54030515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 307
Coasting Arc #4 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5529926
90 A = 6784861
73 meter
Y = -1989182
23 meter E =
0007941
Z = 3384778
72 I = 51
92030
XDOT = -686
445705 Wp = 84
43246
YDOT = -6047
004401 meter/sec RA = 46
60991 deg
ZDOT = -4665
084502 TA = 56
21816
MA = 56
14255
Ha = 219
623 n
mi
Hp = 216
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18142804
79 X = -5523713
90
Y = -6526188
43 feet Y = -2050987
24 meter
Z = 11104917
06 Z = 3357930
99
XDOT = -2252
118456 XDOT = -596
114865
YDOT = -19839
253283 feet/sec YDOT = -6054
175138 meter/sec
ZDOT = -15305
395347 ZDOT = -4668
200274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17766019
32 X = -5415082
69
Y = 7663704
36 feet Y = 2335897
09 meter
Z = 10986713
64 Z = 3348750
32
XDOT = -14556
140005 XDOT = -4436
711473
YDOT = -11735
939486 feet/sec YDOT = -3577
114355 meter/sec
ZDOT = -15318
009964 ZDOT = -4668
929437
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 17166
42818437
00016717 00000-0 10270-3 0 9038
2 25544 51
6410 47
1038 0004734 281
8972 78
1649 15
54029940 21475
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42818437 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 47
1038 deg
Eccentricity:
0004734
Arg of perigee: 281
8972 deg
Mean anomaly: 78
1649 deg
Mean motion: 15
54029940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2147
Checksum: 317
Coasting Arc #5 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5732081
62 A = 6788067
66 meter
Y = 3069617
02 meter E =
0006743
Z = -1933873
21 I = 51
90852
XDOT = -856
470274 Wp = 357
91154
YDOT = 5139
666759 meter/sec RA = 41
65129 deg
ZDOT = 5625
471476 TA = 340
85203
MA = 340
87736
Ha = 219
679 n
mi
Hp = 216
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18806042
06 X = 5706724
13
Y = 10070921
98 feet Y = 3133575
44 meter
Z = -6344728
39 Z = -1906089
86
XDOT = -2809
941845 XDOT = -941
205475
YDOT = 16862
423751 feet/sec YDOT = 5129
614817 meter/sec
ZDOT = 18456
271246 ZDOT = 5621
105686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20550005
21 X = 6263641
59
Y = -5858561
89 feet Y = -1785689
67 meter
Z = -6222604
29 Z = -1896649
79
XDOT = 9186
626488 XDOT = 2800
083754
YDOT = 12663
344678 feet/sec YDOT = 3859
787458 meter/sec
ZDOT = 18436
009585 ZDOT = 5619
295721
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 17167
39277370
00016717 00000-0 10270-3 0 9041
2 25544 51
6414 42
2958 0004833 285
2180 74
8438 15
54036957 21627
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
39277370 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 42
2958 deg
Eccentricity:
0004833
Arg of perigee: 285
2180 deg
Mean anomaly: 74
8438 deg
Mean motion: 15
54036957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2162
Checksum: 322
Coasting Arc #6 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5440320
12 A = 6789473
78 meter
Y = -3984780
81 meter E =
0009034
Z = 742569
04 I = 51
91196
XDOT = 2278
018987 Wp = 139
18014
YDOT = -4230
169911 meter/sec RA = 41
17207 deg
ZDOT = -5976
131321 TA = 32
82606
MA = 32
76997
Ha = 219
631 n
mi
Hp = 216
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17848819
30 X = -5398963
95
Y = -13073427
84 feet Y = -4045386
99 meter
Z = 2436250
14 Z = 716241
75
XDOT = 7473
815574 XDOT = 2354
181641
YDOT = -13878
510207 feet/sec YDOT = -4204
269152 meter/sec
ZDOT = -19606
730056 ZDOT = -5964
880824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16057562
04 X = -4894344
91
Y = 15238080
07 feet Y = 4644566
81 meter
Z = 2320732
13 Z = 707359
15
XDOT = -11185
642008 XDOT = -3409
383684
YDOT = -8790
827947 feet/sec YDOT = -2679
444358 meter/sec
ZDOT = -19556
234256 ZDOT = -5960
740201
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 17167
52138541
00016717 00000-0 10270-3 0 9053
2 25544 51
6428 41
6561 0004788 284
2332 75
8289 15
54005823 21647
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52138541 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 41
6561 deg
Eccentricity:
0004788
Arg of perigee: 284
2332 deg
Mean anomaly: 75
8289 deg
Mean motion: 15
54005823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 314
Coasting Arc #7 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3163762
92 A = 6786510
41 meter
Y = -5388936
20 meter E =
0001781
Z = -2644015
89 I = 51
89442
XDOT = 5551
655926 Wp = 195
04340
YDOT = -688
705615 meter/sec RA = 40
20373 deg
ZDOT = -5240
162804 TA = 14
63999
MA = 14
63483
Ha = 219
574 n
mi
Hp = 216
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10379799
59 X = -3090423
95
Y = -17680236
88 feet Y = -5423905
24 meter
Z = -8674592
81 Z = -2659206
83
XDOT = 18214
094244 XDOT = 5584
398734
YDOT = -2259
532858 feet/sec YDOT = -626
439682 meter/sec
ZDOT = -17192
135184 ZDOT = -5213
115120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 731232
72 X = 222879
73
Y = 20460835
72 feet Y = 6236462
73 meter
Z = -8740656
52 Z = -2664152
11
XDOT = -15723
597059 XDOT = -4792
552384
YDOT = -6730
049894 feet/sec YDOT = -2051
319208 meter/sec
ZDOT = -17072
545307 ZDOT = -5203
711809
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 17167
71430155
00016717 00000-0 10270-3 0 9061
2 25544 51
6394 40
6890 0004656 284
3718 75
6917 15
54062657 21673
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71430155 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 40
6890 deg
Eccentricity:
0004656
Arg of perigee: 284
3718 deg
Mean anomaly: 75
6917 deg
Mean motion: 15
54062657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 328
Coasting Arc #8 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1923185
94 A = 6782842
49 meter
Y = 5160699
12 meter E =
0006355
Z = 3954322
05 I = 51
85646
XDOT = -6479
667336 Wp = 96
27505
YDOT = -688
844924 meter/sec RA = 35
23796 deg
ZDOT = 4044
137866 TA = 311
59197
MA = 311
64641
Ha = 219
596 n
mi
Hp = 216
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6309665
15 X = 1846126
50
Y = 16931427
57 feet Y = 5181774
29 meter
Z = 12973497
55 Z = 3963477
60
XDOT = -21258
751104 XDOT = -6491
127398
YDOT = -2259
989907 feet/sec YDOT = -761
369381 meter/sec
ZDOT = 13268
168852 ZDOT = 4012
633669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2217743
25 X = 675968
14
Y = -17903678
54 feet Y = -5457041
22 meter
Z = 13012942
11 Z = 3966344
75
XDOT = 16637
139873 XDOT = 5071
000233
YDOT = 11618
388579 feet/sec YDOT = 3541
284839 meter/sec
ZDOT = 13129
166934 ZDOT = 4001
770081
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 17168
74319115
00016717 00000-0 10270-3 0 9078
2 25544 51
6391 35
5599 0004661 285
8219 74
2419 15
54064372 21833
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74319115 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 35
5599 deg
Eccentricity:
0004661
Arg of perigee: 285
8219 deg
Mean anomaly: 74
2419 deg
Mean motion: 15
54064372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 325
Coasting Arc #9 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -436244
30 A = 6779441
53 meter
Y = -4696028
08 meter E =
0008779
Z = -4878189
86 I = 51
81843
XDOT = 7017
287758 Wp = 53
91404
YDOT = 1878
465205 meter/sec RA = 30
26275 deg
ZDOT = -2433
873160 TA = 192
23727
MA = 192
25861
Ha = 219
770 n
mi
Hp = 216
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1431247
69 X = -360003
66
Y = -15406916
28 feet Y = -4700479
74 meter
Z = -16004559
91 Z = -4880124
25
XDOT = 23022
597631 XDOT = 7007
583357
YDOT = 6162
943586 feet/sec YDOT = 1956
883227 meter/sec
ZDOT = -7985
148162 ZDOT = -2399
808552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5627661
59 X = -1715311
25
Y = 14405084
34 feet Y = 4390669
71 meter
Z = -16012196
83 Z = -4880517
59
XDOT = -16915
996620 XDOT = -5155
995770
YDOT = -15325
041612 feet/sec YDOT = -4671
072683 meter/sec
ZDOT = -7835
077252 ZDOT = -2388
131546
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 17169
70777407
00016717 00000-0 10270-3 0 9088
2 25544 51
6397 30
7536 0004533 290
6780 69
3886 15
54060942 21980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70777407 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 30
7536 deg
Eccentricity:
0004533
Arg of perigee: 290
6780 deg
Mean anomaly: 69
3886 deg
Mean motion: 15
54060942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 342
Coasting Arc #10 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1188778
85 A = 6777706
56 meter
Y = 4054406
76 meter E =
0001842
Z = 5300958
35 I = 51
78406
XDOT = -7097
160890 Wp = 297
02216
YDOT = -2842
861577 meter/sec RA = 25
27572 deg
ZDOT = 583
728192 TA = 147
42312
MA = 147
41175
Ha = 219
969 n
mi
Hp = 216
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3900193
08 X = -1259777
62
Y = 13301859
46 feet Y = 4040715
53 meter
Z = 17391595
64 Z = 5295011
53
XDOT = -23284
648589 XDOT = -7067
679278
YDOT = -9326
973677 feet/sec YDOT = -2922
062056 meter/sec
ZDOT = 1915
118739 ZDOT = 549
323407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9309501
47 X = 2837536
05
Y = -10316210
85 feet Y = -3144381
07 meter
Z = 17364548
53 Z = 5292714
39
XDOT = 16332
133827 XDOT = 4978
034390
YDOT = 17701
764275 feet/sec YDOT = 5395
497751 meter/sec
ZDOT = 1763
743634 ZDOT = 537
589060
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 17170
73665962
00016717 00000-0 10270-3 0 9096
2 25544 51
6400 25
6242 0004645 294
5687 65
4982 15
54038277 22144
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73665962 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 25
6242 deg
Eccentricity:
0004645
Arg of perigee: 294
5687 deg
Mean anomaly: 65
4982 deg
Mean motion: 15
54038277 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 324
Coasting Arc #11 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2819356
14 A = 6778139
88 meter
Y = -3325693
95 meter E =
0009644
Z = -5198188
87 I = 51
75677
XDOT = 6648
257998 Wp = 91
59086
YDOT = 3569
857658 meter/sec RA = 20
28687 deg
ZDOT = 1323
772559 TA = 191
10759
MA = 191
12890
Ha = 220
000 n
mi
Hp = 216
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9249856
10 X = 2881585
89
Y = -10911069
39 feet Y = -3293817
44 meter
Z = -17054425
44 Z = -5184342
41
XDOT = 21811
870071 XDOT = 6601
414496
YDOT = 11712
131423 feet/sec YDOT = 3643
940912 meter/sec
ZDOT = 4343
085825 ZDOT = 1355
954709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13021255
71 X = -3968878
74
Y = 6096061
76 feet Y = 1858079
62 meter
Z = -16992634
61 Z = -5179355
03
XDOT = -14592
517950 XDOT = -4447
799471
YDOT = -18686
425380 feet/sec YDOT = -5695
622456 meter/sec
ZDOT = 4484
493367 ZDOT = 1366
873578
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 17171
70123503
00016717 00000-0 10270-3 0 9106
2 25544 51
6409 20
8175 0004587 298
3033 61
7657 15
54070396 22299
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
70123503 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 20
8175 deg
Eccentricity:
0004587
Arg of perigee: 298
3033 deg
Mean anomaly: 61
7657 deg
Mean motion: 15
54070396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 299
Coasting Arc #12 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4327773
78 A = 6780908
37 meter
Y = 2543550
60 meter E =
0007192
Z = 4558025
43 I = 51
73410
XDOT = -5688
285245 Wp = 36
14029
YDOT = -4096
577597 meter/sec RA = 15
29877 deg
ZDOT = -3106
721401 TA = 84
96905
MA = 84
88695
Ha = 220
242 n
mi
Hp = 216
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14198732
87 X = -4378035
64
Y = 8344982
27 feet Y = 2494872
83 meter
Z = 14954151
67 Z = 4536880
51
XDOT = -18662
353166 XDOT = -5626
962401
YDOT = -13440
215213 feet/sec YDOT = -4159
844549 meter/sec
ZDOT = -10192
655516 ZDOT = -3134
205220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16431722
86 X = 5008389
13
Y = -2009918
54 feet Y = -612623
17 meter
Z = 14860286
26 Z = 4529415
25
XDOT = 11614
547535 XDOT = 3540
114089
YDOT = 18502
720632 feet/sec YDOT = 5639
629249 meter/sec
ZDOT = -10313
204537 ZDOT = -3143
464743
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 17172
73011445
00016717 00000-0 10270-3 0 9112
2 25544 51
6403 15
6886 0004528 301
9429 58
1283 15
54032602 22450
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
73011445 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 15
6886 deg
Eccentricity:
0004528
Arg of perigee: 301
9429 deg
Mean anomaly: 58
1283 deg
Mean motion: 15
54032602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 286
Coasting Arc #13 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5552637
54 A = 6784551
06 meter
Y = -1773151
27 meter E =
0002881
Z = -3470126
43 I = 51
71528
XDOT = 4268
248032 Wp = 21
21069
YDOT = 4439
569341 meter/sec RA = 10
31823 deg
ZDOT = 4565
026537 TA = 298
11963
MA = 298
14875
Ha = 220
333 n
mi
Hp = 216
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18217314
75 X = 5588908
97
Y = -5817425
42 feet Y = -1710854
56 meter
Z = -11384929
23 Z = -3443065
44
XDOT = 14003
438424 XDOT = 4196
111578
YDOT = 14565
516211 feet/sec YDOT = 4486
895718 meter/sec
ZDOT = 14977
121184 ZDOT = 4585
585995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19130684
97 X = -5831032
78
Y = -1563384
90 feet Y = -476519
72 meter
Z = -11265093
39 Z = -3433600
47
XDOT = -7446
003779 XDOT = -2269
541952
YDOT = -17361
069645 feet/sec YDOT = -5291
654028 meter/sec
ZDOT = 15067
022029 ZDOT = 4592
428314
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 17173
69468456
00016717 00000-0 10270-3 0 9127
2 25544 51
6408 10
8811 0004740 305
6554 54
4157 15
54051946 22604
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
69468456 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 10
8811 deg
Eccentricity:
0004740
Arg of perigee: 305
6554 deg
Mean anomaly: 54
4157 deg
Mean motion: 15
54051946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 305
Coasting Arc #14 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6402372
23 A = 6787875
10 meter
Y = 995944
19 meter E =
0009568
Z = 2010358
98 I = 51
69481
XDOT = -2478
540407 Wp = 103
46296
YDOT = -4650
392619 meter/sec RA = 5
34473 deg
ZDOT = -5569
446617 TA = 54
35003
MA = 54
26097
Ha = 220
355 n
mi
Hp = 216
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21005158
24 X = -6422798
65
Y = 3267533
43 feet Y = 924233
97 meter
Z = 6595665
95 Z = 1979208
76
XDOT = -8131
694248 XDOT = -2399
300621
YDOT = -15257
193631 feet/sec YDOT = -4677
665331 meter/sec
ZDOT = -18272
462654 ZDOT = -5581
294945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20794641
37 X = 6338206
69
Y = 4612407
99 feet Y = 1405861
96 meter
Z = 6457928
45 Z = 1968376
59
XDOT = 2248
753563 XDOT = 685
420086
YDOT = 15611
628300 feet/sec YDOT = 4758
424306 meter/sec
ZDOT = -18323
855614 ZDOT = -5585
111191
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 17174
72355710
00016717 00000-0 10270-3 0 9131
2 25544 51
6413 5
7522 0004678 309
2307 50
8430 15
54064046 22764
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
72355710 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 5
7522 deg
Eccentricity:
0004678
Arg of perigee: 309
2307 deg
Mean anomaly: 50
8430 deg
Mean motion: 15
54064046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 289
Coasting Arc #15 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2017/175/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6767377
43 A = 6789457
70 meter
Y = -244814
69 meter E =
0012565
Z = -365858
09 I = 51
66823
XDOT = 492
412168 Wp = 20
34568
YDOT = 4749
870405 meter/sec RA =
37640 deg
ZDOT = 6003
306047 TA = 335
71079
MA = 335
76997
Ha = 220
564 n
mi
Hp = 215
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22202681
86 X = 6771389
20
Y = -803197
81 feet Y = -169114
80 meter
Z = -1200321
82 Z = -332974
72
XDOT = 1615
525487 XDOT = 410
100307
YDOT = 15583
564322 feet/sec YDOT = 4754
915640 meter/sec
ZDOT = 19695
885982 ZDOT = 6005
498906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21103613
23 X = -6432381
31
Y = -6969167
32 feet Y = -2124202
20 meter
Z = -1055081
16 Z = -321588
74
XDOT = 3516
779685 XDOT = 1071
914448
YDOT = -13590
956587 feet/sec YDOT = -4142
523568 meter/sec
ZDOT = 19704
626652 ZDOT = 6005
970204
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 17175
68812190
00016717 00000-0 10270-3 0 9148
2 25544 51
6417
9444 0004719 315
3504 44
7268 15
54069545 22918
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
68812190 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node:
9444 deg
Eccentricity:
0004719
Arg of perigee: 315
3504 deg
Mean anomaly: 44
7268 deg
Mean motion: 15
54069545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2291
Checksum: 310
Coasting Arc #16 (Orbit 2306)
---------------------------------------
Vector Time (GMT): 2017/176/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6632647
00 A = 6788644
39 meter
Y = -529355
13 meter E =
0003983
Z = -1337348
31 I = 51
63285
XDOT = 1549
262781 Wp = 147
40447
YDOT = -4744
393468 meter/sec RA = 355
40750 deg
ZDOT = -5817
055405 TA = 47
15146
MA = 47
11801
Ha = 220
584 n
mi
Hp = 215
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21760652
89 X = -6619738
55
Y = -1736729
44 feet Y = -603453
50 meter
Z = -4387625
69 Z = -1369536
07
XDOT = 5082
883141 XDOT = 1630
456808
YDOT = -15565
595366 feet/sec YDOT = -4726
613668 meter/sec
ZDOT = -19084
827444 ZDOT = -5809
333176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19926687
88 X = 6073654
47
Y = 8843244
27 feet Y = 2695420
85 meter
Z = -4529640
56 Z = -1380634
44
XDOT = -9429
009306 XDOT = -2873
962036
YDOT = 11507
502940 feet/sec YDOT = 3507
486896 meter/sec
ZDOT = -19049
793485 ZDOT = -5806
377054
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 17176
71698894
00016717 00000-0 10270-3 0 9157
2 25544 51
6414 355
8162 0004697 317
8052 42
2739 15
54084815 23075
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
71698894 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 355
8162 deg
Eccentricity:
0004697
Arg of perigee: 317
8052 deg
Mean anomaly: 42
2739 deg
Mean motion: 15
54084815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2307
Checksum: 336
Coasting Arc #17 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2017/177/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5993461
04 A = 6785773
04 meter
Y = 1308456
40 meter E =
0011642
Z = 2884164
14 I = 51
59243
XDOT = -3446
016676 Wp = 60
84058
YDOT = 4638
546053 meter/sec RA = 350
43094 deg
ZDOT = 5046
827210 TA = 332
04471
MA = 332
10719
Ha = 220
593 n
mi
Hp = 215
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19663586
07 X = 5964374
41
Y = 4292835
97 feet Y = 1375316
33 meter
Z = 9462480
78 Z = 2913207
68
XDOT = -11305
828990 XDOT = -3522
144700
YDOT = 15218
326947 feet/sec YDOT = 4599
584021 meter/sec
ZDOT = 16557
832054 ZDOT = 5029
903464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17248339
36 X = -5257293
84
Y = -10253853
76 feet Y = -3125374
62 meter
Z = 9590457
38 Z = 2923171
41
XDOT = 14882
025779 XDOT = 4536
041457
YDOT = -9587
929221 feet/sec YDOT = -2922
400827 meter/sec
ZDOT = 16482
197679 ZDOT = 5023
773853
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 17177
74585196
00016717 00000-0 10270-3 0 9162
2 25544 51
6427 350
6877 0004713 322
1857 37
8964 15
54105249 23239
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
74585196 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 350
6877 deg
Eccentricity:
0004713
Arg of perigee: 322
1857 deg
Mean anomaly: 37
8964 deg
Mean motion: 15
54105249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 335
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