[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 7th 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
200/11:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5196181
27 A = 6782187
53 meter
Y = -1595240
42 meter E =
0010474
Z = 4045513
55 I = 51
33838
XDOT = -996
401731 Wp = 75
58466
YDOT = 6556
971496 meter/sec RA = 306
38829 deg
ZDOT = 3859
541088 TA = 334
28874
MA = 334
34078
Ha = 221
503 n
mi
Hp = 214
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17047838
80 X = 5193982
38
Y = -5233728
42 feet Y = -1537146
00 meter
Z = 13272682
24 Z = 4070749
42
XDOT = -3269
034549 XDOT = -1088
397190
YDOT = 21512
373674 feet/sec YDOT = 6545
314193 meter/sec
ZDOT = 12662
536378 ZDOT = 3854
478264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8862931
67 X = -2701421
57
Y = -15378301
16 feet Y = -4687306
19 meter
Z = 13384360
66 Z = 4079553
13
XDOT = 20599
778982 XDOT = 6278
812634
YDOT = -855
480648 feet/sec YDOT = -260
750501 meter/sec
ZDOT = 12638
969085 ZDOT = 3852
357777
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 17186
55535622
00016717 00000-0 10270-3 0 9003
2 25544 51
6411 306
7722 0004911 358
0515 2
0617 15
54153357 24606
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
55535622 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 306
7722 deg
Eccentricity:
0004911
Arg of perigee: 358
0515 deg
Mean anomaly: 2
0617 deg
Mean motion: 15
54153357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 283
Coasting Arc #2 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2017/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4667056
43 A = 6778947
30 meter
Y = 70651
48 meter E =
0014700
Z = -4929411
72 I = 51
30959
XDOT = 2211
486357 Wp = 54
84038
YDOT = -6995
965587 meter/sec RA = 301
37495 deg
ZDOT = -2190
395331 TA = 193
64040
MA = 193
68017
Ha = 221
798 n
mi
Hp = 214
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15311864
94 X = -4643555
03
Y = 231796
20 feet Y = 18593
36 meter
Z = -16172610
63 Z = -4952025
67
XDOT = 7255
532667 XDOT = 2300
192554
YDOT = -22952
643002 feet/sec YDOT = -6970
738965 meter/sec
ZDOT = -7186
336389 ZDOT = -2179
438142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3849779
37 X = 1173412
75
Y = 14712150
73 feet Y = 4484263
54 meter
Z = -16272433
49 Z = -4959837
73
XDOT = -22959
641368 XDOT = -6998
098689
YDOT = -1898
830095 feet/sec YDOT = -578
763413 meter/sec
ZDOT = -7136
681612 ZDOT = -2175
260555
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 17187
51989028
00016717 00000-0 10270-3 0 9014
2 25544 51
6421 301
9649 0005000 1
5161 358
6006 15
54122145 24758
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
51989028 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 301
9649 deg
Eccentricity:
0005000
Arg of perigee: 1
5161 deg
Mean anomaly: 358
6006 deg
Mean motion: 15
54122145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 286
Coasting Arc #3 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2017/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939995
46 A = 6777241
33 meter
Y = 1580280
39 meter E =
0005418
Z = 5280271
21 I = 51
28854
XDOT = -3187
968122 Wp = 32
63914
YDOT = 6971
399374 meter/sec RA = 296
35202 deg
ZDOT = 296
717155 TA = 54
54496
MA = 54
49439
Ha = 221
728 n
mi
Hp = 214
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12926494
28 X = 3896382
71
Y = 5184646
93 feet Y = 1624095
49 meter
Z = 17323724
46 Z = 5299304
67
XDOT = -10459
212998 XDOT = -3267
128506
YDOT = 22872
045189 feet/sec YDOT = 6935
306698 meter/sec
ZDOT = 973
481481 ZDOT = 281
039794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1745511
25 X = 532031
83
Y = -13712051
35 feet Y = -4179433
25 meter
Z = 17407443
40 Z = 5305788
75
XDOT = 23785
373102 XDOT = 7249
781721
YDOT = 4156
187877 feet/sec YDOT = 1266
806065 meter/sec
ZDOT = 903
008656 ZDOT = 275
237038
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 17188
54872024
00016717 00000-0 10270-3 0 9026
2 25544 51
6424 296
8358 0005125 5
6292 354
4917 15
54172114 24912
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
54872024 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 296
8358 deg
Eccentricity:
0005125
Arg of perigee: 5
6292 deg
Mean anomaly: 354
4917 deg
Mean motion: 15
54172114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 312
Coasting Arc #4 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2017/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3139600
60 A = 6778151
97 meter
Y = -3196723
10 meter E =
0014264
Z = -5097683
28 I = 51
27755
XDOT = 3891
046003 Wp = 81
03619
YDOT = -6394
605189 meter/sec RA = 291
32942 deg
ZDOT = 1619
642251 TA = 204
65722
MA = 204
72548
Ha = 221
951 n
mi
Hp = 213
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10300526
91 X = -3078858
85
Y = -10487936
67 feet Y = -3231491
90 meter
Z = -16724682
69 Z = -5112787
27
XDOT = 12765
898961 XDOT = 3954
395618
YDOT = -20979
675816 feet/sec YDOT = -6350
738890 meter/sec
ZDOT = 5313
786914 ZDOT = 1638
696551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7325557
12 X = -2232829
81
Y = 12657761
64 feet Y = 3858085
75 meter
Z = -16790770
22 Z = -5117826
76
XDOT = -22726
172279 XDOT = -6926
937311
YDOT = -6016
945575 feet/sec YDOT = -1833
965011 meter/sec
ZDOT = 5399
048623 ZDOT = 1645
630020
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 17189
51324823
00016717 00000-0 10270-3 0 9034
2 25544 51
6421 292
0296 0005160 10
5101 349
6159 15
54161428 25068
Satellite: ISS
Catalog Number: 25544
Epoch time: 17189
51324823 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 292
0296 deg
Eccentricity:
0005160
Arg of perigee: 10
5101 deg
Mean anomaly: 349
6159 deg
Mean motion: 15
54161428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2506
Checksum: 286
Coasting Arc #5 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2017/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2272214
43 A = 6781188
81 meter
Y = 4670667
90 meter E =
0013104
Z = 4355593
42 I = 51
27662
XDOT = -4382
417468 Wp = 51
48267
YDOT = 5305
059008 meter/sec RA = 286
30928 deg
ZDOT = -3387
650237 TA = 73
07063
MA = 72
92702
Ha = 222
065 n
mi
Hp = 213
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7454771
75 X = 2198659
84
Y = 15323713
59 feet Y = 4695665
50 meter
Z = 14290004
67 Z = 4366452
97
XDOT = -14378
010067 XDOT = -4424
958985
YDOT = 17405
049239 feet/sec YDOT = 5255
814429 meter/sec
ZDOT = -11114
338049 ZDOT = -3409
041031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12552731
44 X = 3826072
54
Y = -11466056
84 feet Y = -3494854
12 meter
Z = 14337103
18 Z = 4369949
05
XDOT = 19952
595870 XDOT = 6081
551221
YDOT = 7765
842865 feet/sec YDOT = 2367
028905 meter/sec
ZDOT = -11209
706456 ZDOT = -3416
718528
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 17190
54207451
00016717 00000-0 10270-3 0 9047
2 25544 51
6421 286
9008 0005194 14
3452 345
7848 15
54141841 25226
Satellite: ISS
Catalog Number: 25544
Epoch time: 17190
54207451 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 286
9008 deg
Eccentricity:
0005194
Arg of perigee: 14
3452 deg
Mean anomaly: 345
7848 deg
Mean motion: 15
54141841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 297
Coasting Arc #6 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2017/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1443073
55 A = 6784974
59 meter
Y = -5813143
69 meter E =
0008394
Z = -3185862
87 I = 51
28102
XDOT = 4660
224778 Wp = 44
81696
YDOT = -3768
671383 meter/sec RA = 281
29924 deg
ZDOT = 4779
234756 TA = 278
17816
MA = 278
27337
Ha = 222
142 n
mi
Hp = 213
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4734493
27 X = -1362487
06
Y = -19071993
72 feet Y = -5828830
14 meter
Z = -10452305
99 Z = -3192677
74
XDOT = 15289
451372 XDOT = 4678
805857
YDOT = -12364
407424 feet/sec YDOT = -3716
454272 meter/sec
ZDOT = 15679
904054 ZDOT = 4801
917035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16744521
59 X = -5103730
18
Y = 10255198
83 feet Y = 3125784
60 meter
Z = -10481362
76 Z = -3194719
37
XDOT = -15654
352889 XDOT = -4771
446760
YDOT = -9476
807679 feet/sec YDOT = -2888
530981 meter/sec
ZDOT = 15780
692427 ZDOT = 4809
955052
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 17191
50659455
00016717 00000-0 10270-3 0 9050
2 25544 51
6421 282
0935 0005309 15
7892 344
3426 15
54136367 25373
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
50659455 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 282
0935 deg
Eccentricity:
0005309
Arg of perigee: 15
7892 deg
Mean anomaly: 344
3426 deg
Mean motion: 15
54136367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 317
Coasting Arc #7 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 599634
24 A = 6788133
87 meter
Y = 6555533
83 meter E =
0014464
Z = 1640799
36 I = 51
28513
XDOT = -4791
559636 Wp = 94
81397
YDOT = 1871
859214 meter/sec RA = 276
29864 deg
ZDOT = -5685
382279 TA = 67
12919
MA = 66
97655
Ha = 222
275 n
mi
Hp = 213
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1967303
95 X = 518313
90
Y = 21507656
91 feet Y = 6561784
48 meter
Z = 5383200
00 Z = 1643515
33
XDOT = -15720
340013 XDOT = -4784
518781
YDOT = 6141
270387 feet/sec YDOT = 1818
316708 meter/sec
ZDOT = -18652
829000 ZDOT = -5708
640530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19749606
07 X = 6019679
93
Y = -8734169
05 feet Y = -2662174
73 meter
Z = 5394050
78 Z = 1644106
68
XDOT = 10184
906930 XDOT = 3104
359632
YDOT = 11361
388976 feet/sec YDOT = 3462
951360 meter/sec
ZDOT = -18755
824028 ZDOT = -5716
775164
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 17192
53541491
00016717 00000-0 10270-3 0 9065
2 25544 51
6410 276
9653 0005325 21
4009 338
7366 15
54146136 25535
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53541491 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 276
9653 deg
Eccentricity:
0005325
Arg of perigee: 21
4009 deg
Mean anomaly: 338
7366 deg
Mean motion: 15
54146136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 304
Coasting Arc #8 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 182642
30 A = 6789342
54 meter
Y = -6777577
01 meter E =
0017368
Z = 35485
83 I = 51
28611
XDOT = 4795
962362 Wp = 39
07307
YDOT = 168
908014 meter/sec RA = 271
30327 deg
ZDOT = 5986
610792 TA = 321
31125
MA = 321
43553
Ha = 222
369 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 599220
16 X = 258245
01
Y = -22236145
06 feet Y = -6775111
87 meter
Z = 116423
34 Z = 36556
07
XDOT = 15734
784651 XDOT = 4764
637587
YDOT = 554
160152 feet/sec YDOT = 222
364047 meter/sec
ZDOT = 19641
111522 ZDOT = 6009
831658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21135215
06 X = -6442013
55
Y = 6935884
37 feet Y = 2114057
56 meter
Z = 122305
95 Z = 37278
85
XDOT = -4234
088067 XDOT = -1290
550043
YDOT = -13337
912982 feet/sec YDOT = -4065
395877 meter/sec
ZDOT = 19743
591233 ZDOT = 6017
846608
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 17193
56423347
00016717 00000-0 10270-3 0 9079
2 25544 51
6408 271
8367 0005465 23
9850 336
1557 15
54125624 25694
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56423347 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 271
8367 deg
Eccentricity:
0005465
Arg of perigee: 23
9850 deg
Mean anomaly: 336
1557 deg
Mean motion: 15
54125624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 327
Coasting Arc #9 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2017/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -989572
59 A = 6787926
79 meter
Y = 6483634
39 meter E =
0007261
Z = -1752616
25 I = 51
28134
XDOT = -4677
268634 Wp = 98
53031
YDOT = -2233
470093 meter/sec RA = 266
30774 deg
ZDOT = -5642
771015 TA = 100
79187
MA = 100
71013
Ha = 222
409 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3246629
23 X = -1053487
52
Y = 21271766
38 feet Y = 6472211
08 meter
Z = -5750053
33 Z = -1757577
99
XDOT = -15345
369533 XDOT = -4624
536345
YDOT = -7327
657787 feet/sec YDOT = -2285
479237 meter/sec
ZDOT = -18513
028265 ZDOT = -5665
363494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21032712
75 X = 6410770
85
Y = -4515381
98 feet Y = -1376288
43 meter
Z = -5773047
67 Z = -1759624
93
XDOT = -1805
499267 XDOT = -550
316177
YDOT = 15297
990484 feet/sec YDOT = 4662
827499 meter/sec
ZDOT = -18612
390660 ZDOT = -5673
056673
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 17194
52874646
00016717 00000-0 10270-3 0 9089
2 25544 51
6401 267
0286 0005431 27
9709 332
1734 15
54157392 25841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17194
52874646 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 267
0286 deg
Eccentricity:
0005431
Arg of perigee: 27
9709 deg
Mean anomaly: 332
1734 deg
Mean motion: 15
54157392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 324
Coasting Arc #10 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2017/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764214
96 A = 6784703
43 meter
Y = -5679823
56 meter E =
0016444
Z = 3245470
05 I = 51
27368
XDOT = 4457
075819 Wp = 71
35180
YDOT = 4091
414517 meter/sec RA = 261
30525 deg
ZDOT = 4722
943494 TA = 326
52755
MA = 326
63138
Ha = 222
411 n
mi
Hp = 213
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5788106
84 X = 1811832
41
Y = -18634591
72 feet Y = -5659828
86 meter
Z = 10647867
62 Z = 3254155
27
XDOT = 14622
952162 XDOT = 4388
051815
YDOT = 13423
275976 feet/sec YDOT = 4140
870344 meter/sec
ZDOT = 15495
221438 ZDOT = 4744
426933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19427981
81 X = -5921648
86
Y = 1570221
24 feet Y = 478603
43 meter
Z = 10687151
26 Z = 3257443
70
XDOT = 7224
712024 XDOT = 2202
092225
YDOT = -17036
820550 feet/sec YDOT = -5192
822904 meter/sec
ZDOT = 15589
389150 ZDOT = 4751
645813
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 17195
55755820
00016717 00000-0 10270-3 0 9096
2 25544 51
6401 261
8995 0005507 31
6682 328
4801 15
54170531 26008
Satellite: ISS
Catalog Number: 25544
Epoch time: 17195
55755820 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 261
8995 deg
Eccentricity:
0005507
Arg of perigee: 31
6682 deg
Mean anomaly: 328
4801 deg
Mean motion: 15
54170531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 308
Coasting Arc #11 (Orbit 2614)
---------------------------------------
Vector Time (GMT): 2017/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2567843
11 A = 6780908
69 meter
Y = 4461913
18 meter E =
0014156
Z = -4428148
85 I = 51
26576
XDOT = -4070
591877 Wp = 57
05885
YDOT = -5595
135254 meter/sec RA = 256
29346 deg
ZDOT = -3277
397817 TA = 179
65875
MA = 179
65779
Ha = 222
577 n
mi
Hp = 213
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8424682
13 X = -2596036
96
Y = 14638822
78 feet Y = 4433040
42 meter
Z = -14528047
41 Z = -4440690
76
XDOT = -13354
960225 XDOT = -3991
803208
YDOT = -18356
742960 feet/sec YDOT = -5640
214660 meter/sec
ZDOT = -10752
617510 ZDOT = -3296
980274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16716882
24 X = 5095305
71
Y = 2045250
70 feet Y = 623392
41 meter
Z = -14584147
58 Z = -4445248
18
XDOT = -11671
298975 XDOT = -3557
411928
YDOT = 18113
735650 feet/sec YDOT = 5521
066626 meter/sec
ZDOT = -10838
159975 ZDOT = -3303
471160
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 17196
52207011
00016717 00000-0 10270-3 0 9100
2 25544 51
6391 257
0916 0005519 35
8216 324
3306 15
54151467 26156
Satellite: ISS
Catalog Number: 25544
Epoch time: 17196
52207011 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 257
0916 deg
Eccentricity:
0005519
Arg of perigee: 35
8216 deg
Mean anomaly: 324
3306 deg
Mean motion: 15
54151467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2615
Checksum: 290
Coasting Arc #12 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2017/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3338791
52 A = 6777968
87 meter
Y = -2927837
69 meter E =
0007520
Z = 5113910
40 I = 51
26546
XDOT = 3527
058850 Wp = 77
54932
YDOT = 6648
090743 meter/sec RA = 251
27176 deg
ZDOT = 1503
153060 TA = 357
90695
MA = 357
91009
Ha = 222
462 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10954040
41 X = 3346442
48
Y = -9605766
71 feet Y = -2890458
58 meter
Z = 16777921
25 Z = 5130147
54
XDOT = 11571
715387 XDOT = 3445
154466
YDOT = 21811
321336 feet/sec YDOT = 6687
074665 meter/sec
ZDOT = 4931
604526 ZDOT = 1520
087796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147951
62 X = -4007495
66
Y = -6080006
55 feet Y = -1853186
00 meter
Z = 16850082
65 Z = 5135905
19
XDOT = 14906
811383 XDOT = 4543
596109
YDOT = -18361
645481 feet/sec YDOT = -5596
629542 meter/sec
ZDOT = 5005
302224 ZDOT = 1525
616118
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 17197
55087810
00016717 00000-0 10270-3 0 9118
2 25544 51
6397 251
9623 0005574 38
4254 321
7294 15
54177609 26313
Satellite: ISS
Catalog Number: 25544
Epoch time: 17197
55087810 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 251
9623 deg
Eccentricity:
0005574
Arg of perigee: 38
4254 deg
Mean anomaly: 321
7294 deg
Mean motion: 15
54177609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 325
Coasting Arc #13 (Orbit 2645)
---------------------------------------
Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075537
78 A = 6777365
67 meter
Y = 1256554
92 meter E =
0018900
Z = -5283176
91 I = 51
27489
XDOT = -2755
901304 Wp = 79
62855
YDOT = -7128
416872 meter/sec RA = 246
24601 deg
ZDOT = 435
194984 TA = 194
52318
MA = 194
57757
Ha = 222
733 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13371186
95 X = -4063623
00
Y = 4122555
51 feet Y = 1211046
49 meter
Z = -17333257
58 Z = -5302945
53
XDOT = -9041
670945 XDOT = -2678
098601
YDOT = -23387
194461 feet/sec YDOT = -7158
800241 meter/sec
ZDOT = 1427
805065 ZDOT = 421
996166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9272644
60 X = 2826302
08
Y = 10332552
57 feet Y = 3149362
02 meter
Z = -17420744
59 Z = -5309842
95
XDOT = -16731
359014 XDOT = -5099
718227
YDOT = 17300
302505 feet/sec YDOT = 5273
132203 meter/sec
ZDOT = 1370
663979 ZDOT = 417
778381
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 17198
51538528
00016717 00000-0 10270-3 0 9123
2 25544 51
6400 247
1541 0005747 41
6899 318
4691 15
54146220 26462
Satellite: ISS
Catalog Number: 25544
Epoch time: 17198
51538528 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 247
1541 deg
Eccentricity:
0005747
Arg of perigee: 41
6899 deg
Mean anomaly: 318
4691 deg
Mean motion: 15
54146220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2646
Checksum: 319
Coasting Arc #14 (Orbit 2661)
---------------------------------------
Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4694633
03 A = 6778965
15 meter
Y = 452025
41 meter E =
0012406
Z = 4863513
39 I = 51
29398
XDOT = 1754
839771 Wp = 52
85255
YDOT = 7092
921381 meter/sec RA = 241
22318 deg
ZDOT = -2341
633855 TA = 60
23085
MA = 60
10751
Ha = 222
594 n
mi
Hp = 212
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15402339
34 X = 4665604
94
Y = 1483022
98 feet Y = 504361
24 meter
Z = 15956408
75 Z = 4886247
95
XDOT = 5757
348330 XDOT = 1686
768915
YDOT = 23270
739439 feet/sec YDOT = 7112
164790 meter/sec
ZDOT = -7682
525772 ZDOT = -2333
274110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5277069
43 X = -1608450
76
Y = -14435111
01 feet Y = -4399821
84 meter
Z = 16056727
65 Z = 4894090
59
XDOT = 17417
479745 XDOT = 5308
847826
YDOT = -14914
807469 feet/sec YDOT = -4546
033316 meter/sec
ZDOT = -7646
732361 ZDOT = -2330
724024
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 17199
54418997
00016717 00000-0 10270-3 0 9135
2 25544 51
6392 242
0259 0005752 45
6459 314
5164 15
54192937 26620
Satellite: ISS
Catalog Number: 25544
Epoch time: 17199
54418997 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 242
0259 deg
Eccentricity:
0005752
Arg of perigee: 45
6459 deg
Mean anomaly: 314
5164 deg
Mean motion: 15
54192937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2662
Checksum: 339
Coasting Arc #15 (Orbit 2676)
---------------------------------------
Vector Time (GMT): 2017/200/11:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 901991
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5067797
16 A = 6781253
77 meter
Y = -1387204
07 meter E =
0012575
Z = -4297421
18 I = 51
31876
XDOT = -1122
155829 Wp = 86
38684
YDOT = -6718
900580 meter/sec RA = 236
21455 deg
ZDOT = 3501
843724 TA = 219
41803
MA = 219
50959
Ha = 222
810 n
mi
Hp = 212
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16626631
11 X = -5031033
74
Y = -4551194
46 feet Y = -1443669
61 meter
Z = -14099150
84 Z = -4321949
74
XDOT = -3681
613613 XDOT = -1063
950088
YDOT = -22043
637073 feet/sec YDOT = -6731
124211 meter/sec
ZDOT = 11488
988596 ZDOT = 3496
533317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3224854
55 X = 982935
67
Y = 16843350
60 feet Y = 5133853
26 meter
Z = -14207256
64 Z = -4330371
82
XDOT = -16883
522543 XDOT = -5146
097671
YDOT = 12877
984990 feet/sec YDOT = 3925
209825 meter/sec
ZDOT = 11466
589835 ZDOT = 3495
016582
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 17200
50869442
00016717 00000-0 10270-3 0 9140
2 25544 51
6399 237
2173 0005916 49
4019 310
7648 15
54175321 26773
Satellite: ISS
Catalog Number: 25544
Epoch time: 17200
50869442 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 237
2173 deg
Eccentricity:
0005916
Arg of perigee: 49
4019 deg
Mean anomaly: 310
7648 deg
Mean motion: 15
54175321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2677
Checksum: 317
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