[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 17th 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
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 2164)
---------------------------------------
Vector Time (GMT): 2017/167/12:54:23
898
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2877030
12 A = 6777620
83 meter
Y = 3043560
48 meter E =
0002892
Z = 5330788
38 I = 51
87065
XDOT = -5708
941585 Wp = 306
68796
YDOT = -5115
291245 meter/sec RA = 40
92806 deg
ZDOT = -158
970346 TA = 144
83201
MA = 144
81291
Ha = 219
706 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9439075
21 X = -2936744
53
Y = 9985434
64 feet Y = 3011053
20 meter
Z = 17489463
20 Z = 5316667
91
XDOT = -18730
123311 XDOT = -5650
544556
YDOT = -16782
451592 feet/sec YDOT = -5178
805967 meter/sec
ZDOT = -521
556253 ZDOT = -186
561236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11179863
08 X = 3407622
27
Y = 8124868
85 feet Y = 2476460
02 meter
Z = 17426518
20 Z = 5311602
75
XDOT = -13522
135642 XDOT = -4121
546944
YDOT = 19995
932784 feet/sec YDOT = 6094
760312 meter/sec
ZDOT = -642
439070 ZDOT = -195
815429
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
58568477
00016717 00000-0 10270-3 0 9009
2 25544 51
6419 41
3343 0004929 286
0454 74
0156 15
54039366 21658
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
58568477 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 41
3343 deg
Eccentricity:
0004929
Arg of perigee: 286
0454 deg
Mean anomaly: 74
0156 deg
Mean motion: 15
54039366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 321
Coasting Arc #2 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161559
63 A = 6786505
60 meter
Y = -5389202
36 meter E =
0001765
Z = -2646131
84 I = 51
89430
XDOT = 5553
273591 Wp = 194
44427
YDOT = -685
983303 meter/sec RA = 40
20332 deg
ZDOT = -5238
786337 TA = 15
26527
MA = 15
25995
Ha = 219
581 n
mi
Hp = 216
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10372570
97 X = -3088207
58
Y = -17681110
09 feet Y = -5424146
68 meter
Z = -8681534
89 Z = -2661312
04
XDOT = 18219
401545 XDOT = 5585
979152
YDOT = -2250
601388 feet/sec YDOT = -623
699489 meter/sec
ZDOT = -17187
619216 ZDOT = -5211
730885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 724410
80 X = 220800
41
Y = 20458164
84 feet Y = 6235648
64 meter
Z = -8747551
14 Z = -2666253
59
XDOT = -15724
216624 XDOT = -4792
741227
YDOT = -6739
918329 feet/sec YDOT = -2054
327107 meter/sec
ZDOT = -17067
995552 ZDOT = -5202
325044
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
71429694
00016717 00000-0 10270-3 0 9012
2 25544 51
6392 40
6887 0004635 284
4755 75
5883 15
54062677 21679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71429694 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 40
6887 deg
Eccentricity:
0004635
Arg of perigee: 284
4755 deg
Mean anomaly: 75
5883 deg
Mean motion: 15
54062677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 345
Coasting Arc #3 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1920617
60 A = 6782836
98 meter
Y = 5160405
13 meter E =
0006371
Z = 3955930
66 I = 51
85635
XDOT = -6480
675182 Wp = 96
28823
YDOT = -691
444752 meter/sec RA = 35
23752 deg
ZDOT = 4042
101637 TA = 311
60478
MA = 311
65935
Ha = 219
603 n
mi
Hp = 216
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6301238
84 X = 1843553
83
Y = 16930463
02 feet Y = 5181451
55 meter
Z = 12978775
13 Z = 3965073
72
XDOT = -21262
057684 XDOT = -6492
096206
YDOT = -2268
519529 feet/sec YDOT = -763
980261 meter/sec
ZDOT = 13261
488312 ZDOT = 4010
592640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2224823
81 X = 678126
30
Y = -17898948
08 feet Y = -5455599
37 meter
Z = 13018164
60 Z = 3967936
57
XDOT = 16636
480468 XDOT = 5070
799247
YDOT = 11626
949819 feet/sec YDOT = 3543
894305 meter/sec
ZDOT = 13122
465690 ZDOT = 3999
727542
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
74318651
00016717 00000-0 10270-3 0 9027
2 25544 51
6390 35
5595 0004641 285
9157 74
1484 15
54064415 21837
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74318651 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 35
5595 deg
Eccentricity:
0004641
Arg of perigee: 285
9157 deg
Mean anomaly: 74
1484 deg
Mean motion: 15
54064415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 318
Coasting Arc #4 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -433419
65 A = 6779437
47 meter
Y = -4695276
71 meter E =
0008802
Z = -4879182
95 I = 51
81832
XDOT = 7017
514618 Wp = 54
02689
YDOT = 1880
834182 meter/sec RA = 30
26229 deg
ZDOT = -2431
334578 TA = 192
15077
MA = 192
17201
Ha = 219
776 n
mi
Hp = 216
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1421980
49 X = -357182
81
Y = -15404451
15 feet Y = -4699696
81 meter
Z = -16007818
06 Z = -4881103
62
XDOT = 23023
341921 XDOT = 7007
771378
YDOT = 6170
715820 feet/sec YDOT = 1959
254524 meter/sec
ZDOT = -7976
819482 ZDOT = -2397
268962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5634900
72 X = -1717517
74
Y = 14398764
31 feet Y = 4388743
36 meter
Z = -16015394
57 Z = -4881492
26
XDOT = -16913
637005 XDOT = -5155
276559
YDOT = -15331
789712 feet/sec YDOT = -4673
129504 meter/sec
ZDOT = -7826
744579 ZDOT = -2385
591748
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
70776940
00016717 00000-0 10270-3 0 9034
2 25544 51
6395 30
7533 0004513 290
7798 69
2871 15
54060972 21989
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70776940 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 30
7533 deg
Eccentricity:
0004513
Arg of perigee: 290
7798 deg
Mean anomaly: 69
2871 deg
Mean motion: 15
54060972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 337
Coasting Arc #5 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1191638
30 A = 6777705
69 meter
Y = 4053257
77 meter E =
0001826
Z = 5301176
48 I = 51
78396
XDOT = -7096
579978 Wp = 297
43372
YDOT = -2844
919743 meter/sec RA = 25
27524 deg
ZDOT = 580
965749 TA = 147
03797
MA = 147
02658
Ha = 219
975 n
mi
Hp = 216
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3909574
47 X = -1262625
06
Y = 13298089
79 feet Y = 4039534
63 meter
Z = 17392311
29 Z = 5295215
81
XDOT = -23282
742711 XDOT = -7067
061976
YDOT = -9333
726192 feet/sec YDOT = -2924
113523 meter/sec
ZDOT = 1906
055608 ZDOT = 546
563875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9316379
40 X = 2839632
44
Y = -10308794
76 feet Y = -3142120
64 meter
Z = 17365203
21 Z = 5292913
94
XDOT = 16328
014294 XDOT = 4976
778757
YDOT = 17706
530579 feet/sec YDOT = 5396
950520 meter/sec
ZDOT = 1754
693754 ZDOT = 534
830656
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
73665493
00016717 00000-0 10270-3 0 9040
2 25544 51
6399 25
6239 0004625 294
6694 65
3977 15
54038250 22148
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73665493 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 25
6239 deg
Eccentricity:
0004625
Arg of perigee: 294
6694 deg
Mean anomaly: 65
3977 deg
Mean motion: 15
54038250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 332
Coasting Arc #6 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2822058
70 A = 6778142
36 meter
Y = -3324271
14 meter E =
0009662
Z = -5197650
85 I = 51
75668
XDOT = 6646
801247 Wp = 91
62572
YDOT = 3571
532433 meter/sec RA = 20
28638 deg
ZDOT = 1326
483474 TA = 191
09923
MA = 191
12056
Ha = 220
005 n
mi
Hp = 216
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9258722
76 X = 2884269
72
Y = -10906401
36 feet Y = -3292364
51 meter
Z = -17052660
26 Z = -5183791
31
XDOT = 21807
090706 XDOT = 6599
925958
YDOT = 11717
626091 feet/sec YDOT = 3645
599218 meter/sec
ZDOT = 4351
979901 ZDOT = 1358
658470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13027406
63 X = -3970753
54
Y = 6088164
41 feet Y = 1855672
51 meter
Z = -16990811
94 Z = -5178799
48
XDOT = -14586
424146 XDOT = -4445
942080
YDOT = -18688
996067 feet/sec YDOT = -5696
406001 meter/sec
ZDOT = 4493
355527 ZDOT = 1369
574765
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
70123032
00016717 00000-0 10270-3 0 9057
2 25544 51
6408 20
8171 0004566 298
4049 61
6643 15
54070411 22291
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
70123032 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 20
8171 deg
Eccentricity:
0004566
Arg of perigee: 298
4049 deg
Mean anomaly: 61
6643 deg
Mean motion: 15
54070411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 282
Coasting Arc #7 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4330093
46 A = 6780913
30 meter
Y = 2541897
09 meter E =
0007205
Z = 4556727
28 I = 51
73402
XDOT = -5686
052031 Wp = 36
35307
YDOT = -4097
882820 meter/sec RA = 15
29828 deg
ZDOT = -3109
126559 TA = 84
78303
MA = 84
70081
Ha = 220
246 n
mi
Hp = 216
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14206343
36 X = -4380330
35
Y = 8339557
37 feet Y = 2493193
52 meter
Z = 14949892
65 Z = 4535571
16
XDOT = -18655
026350 XDOT = -5624
703075
YDOT = -13444
497442 feet/sec YDOT = -4161
124653 meter/sec
ZDOT = -10200
546453 ZDOT = -3136
599466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16436540
56 X = 5009857
56
Y = -2001936
21 feet Y = -610190
16 meter
Z = 14855978
07 Z = 4528102
12
XDOT = 11606
658953 XDOT = 3537
709649
YDOT = 18503
384051 feet/sec YDOT = 5639
831459 meter/sec
ZDOT = -10321
047036 ZDOT = -3145
855137
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
73010971
00016717 00000-0 10270-3 0 9069
2 25544 51
6402 15
6882 0004508 302
0442 58
0272 15
54032641 22450
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
73010971 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 15
6882 deg
Eccentricity:
0004508
Arg of perigee: 302
0442 deg
Mean anomaly: 58
0272 deg
Mean motion: 15
54032641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 273
Coasting Arc #8 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5554385
50 A = 6784556
49 meter
Y = -1771383
18 meter E =
0002889
Z = -3468253
34 I = 51
71520
XDOT = 4265
357468 Wp = 21
51441
YDOT = 4440
465669 meter/sec RA = 10
31774 deg
ZDOT = 4566
840100 TA = 297
84249
MA = 297
87177
Ha = 220
336 n
mi
Hp = 216
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18223049
53 X = 5590627
93
Y = -5811624
59 feet Y = -1709067
08 meter
Z = -11378783
93 Z = -3441183
93
XDOT = 13993
954949 XDOT = 4193
202397
YDOT = 14568
456918 feet/sec YDOT = 4487
759617 meter/sec
ZDOT = 14983
071194 ZDOT = 4587
385471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19133749
88 X = -5831966
96
Y = -1570914
15 feet Y = -478814
63 meter
Z = -11258911
26 Z = -3431716
15
XDOT = -7436
627028 XDOT = -2266
683918
YDOT = -17359
951105 feet/sec YDOT = -5291
313097 meter/sec
ZDOT = 15072
909663 ZDOT = 4594
222865
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
69467980
00016717 00000-0 10270-3 0 9072
2 25544 51
6406 10
8807 0004719 305
7545 54
3169 15
54051976 22609
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
69467980 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 10
8807 deg
Eccentricity:
0004719
Arg of perigee: 305
7545 deg
Mean anomaly: 54
3169 deg
Mean motion: 15
54051976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 325
Coasting Arc #9 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6403388
58 A = 6787878
91 meter
Y = 994059
81 meter E =
0009589
Z = 2008029
67 I = 51
69472
XDOT = -2475
181225 Wp = 103
51662
YDOT = -4650
916608 meter/sec RA = 5
34424 deg
ZDOT = -5570
516705 TA = 54
32339
MA = 54
23417
Ha = 220
358 n
mi
Hp = 216
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21008492
73 X = -6423782
54
Y = 3261351
09 feet Y = 922338
41 meter
Z = 6588023
85 Z = 1976874
59
XDOT = -8120
673310 XDOT = -2395
930632
YDOT = -15258
912756 feet/sec YDOT = -4678
151695 meter/sec
ZDOT = -18275
973440 ZDOT = -5582
348688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20795451
58 X = 6338453
64
Y = 4619362
20 feet Y = 1407981
60 meter
Z = 6450265
27 Z = 1966040
86
XDOT = 2238
348162 XDOT = 682
248520
YDOT = 15609
153475 feet/sec YDOT = 4757
669979 meter/sec
ZDOT = -18327
294131 ZDOT = -5586
159251
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
72355232
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 5
7518 0004657 309
3300 50
7439 15
54064083 22767
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
72355232 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 5
7518 deg
Eccentricity:
0004657
Arg of perigee: 309
3300 deg
Mean anomaly: 50
7439 deg
Mean motion: 15
54064083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 295
Coasting Arc #10 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2017/175/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6767583
59 A = 6789458
32 meter
Y = -242917
22 meter E =
0012569
Z = -363385
36 I = 51
66813
XDOT = 488
869961 Wp = 20
47159
YDOT = 4750
001590 meter/sec RA =
37591 deg
ZDOT = 6003
485624 TA = 335
61157
MA = 335
67099
Ha = 220
566 n
mi
Hp = 215
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22203358
25 X = 6771562
12
Y = -796972
50 feet Y = -167215
21 meter
Z = -1192209
20 Z = -330501
07
XDOT = 1603
904073 XDOT = 406
556024
YDOT = 15583
994719 feet/sec YDOT = 4755
007202 meter/sec
ZDOT = 19696
475144 ZDOT = 6005
661270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21102032
91 X = -6431899
63
Y = -6975221
64 feet Y = -2126047
56 meter
Z = -1046964
85 Z = -319114
89
XDOT = 3527
387563 XDOT = 1075
147729
YDOT = -13587
433444 feet/sec YDOT = -4141
449714 meter/sec
ZDOT = 19705
139791 ZDOT = 6006
126608
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
68811711
00016717 00000-0 10270-3 0 9090
2 25544 51
6416
9440 0004699 315
4590 44
6184 15
54069562 22911
Satellite: ISS
Catalog Number: 25544
Epoch time: 17175
68811711 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node:
9440 deg
Eccentricity:
0004699
Arg of perigee: 315
4590 deg
Mean anomaly: 44
6184 deg
Mean motion: 15
54069562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2291
Checksum: 315
Coasting Arc #11 (Orbit 2306)
---------------------------------------
Vector Time (GMT): 2017/176/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6631997
47 A = 6788641
52 meter
Y = -531292
89 meter E =
0003994
Z = -1339790
29 I = 51
63274
XDOT = 1552
762743 Wp = 147
24843
YDOT = -4744
135929 meter/sec RA = 355
40699 deg
ZDOT = -5816
332593 TA = 47
33469
MA = 47
30105
Ha = 220
585 n
mi
Hp = 215
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21758521
87 X = -6619055
53
Y = -1743086
90 feet Y = -605383
81 meter
Z = -4395637
44 Z = -1371974
81
XDOT = 5094
365954 XDOT = 1633
950119
YDOT = -15564
750423 feet/sec YDOT = -4726
317028 meter/sec
ZDOT = -19082
456013 ZDOT = -5808
593379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19922520
16 X = 6072384
14
Y = 8848519
08 feet Y = 2697028
62 meter
Z = -4537637
63 Z = -1383071
95
XDOT = -9439
163072 XDOT = -2877
056904
YDOT = 11503
207970 feet/sec YDOT = 3506
177789 meter/sec
ZDOT = -19047
347110 ZDOT = -5805
631399
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
71698414
00016717 00000-0 10270-3 0 9100
2 25544 51
6412 355
8157 0004676 317
9083 42
1710 15
54084816 23078
Satellite: ISS
Catalog Number: 25544
Epoch time: 17176
71698414 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 355
8157 deg
Eccentricity:
0004676
Arg of perigee: 317
9083 deg
Mean anomaly: 42
1710 deg
Mean motion: 15
54084816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2307
Checksum: 312
Coasting Arc #12 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2017/177/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5992047
18 A = 6785767
78 meter
Y = 1310325
17 meter E =
0011648
Z = 2886245
77 I = 51
59231
XDOT = -3449
159788 Wp = 60
96207
YDOT = 4637
890511 meter/sec RA = 350
43041 deg
ZDOT = 5045
282885 TA = 331
95003
MA = 332
01275
Ha = 220
594 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19658947
44 X = 5962929
65
Y = 4298967
09 feet Y = 1377169
11 meter
Z = 9469310
27 Z = 2915282
37
XDOT = -11316
141037 XDOT = -3525
272747
YDOT = 15216
176216 feet/sec YDOT = 4598
893414 meter/sec
ZDOT = 16552
765371 ZDOT = 5028
343907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17241962
00 X = -5255350
02
Y = -10258196
51 feet Y = -3126698
30 meter
Z = 9597255
86 Z = 2925243
58
XDOT = 14890
785576 XDOT = 4538
711444
YDOT = -9583
112517 feet/sec YDOT = -2920
932695 meter/sec
ZDOT = 16477
063876 ZDOT = 5022
209069
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
74584715
00016717 00000-0 10270-3 0 9113
2 25544 51
6426 350
6872 0004693 322
2896 37
7927 15
54105281 23238
Satellite: ISS
Catalog Number: 25544
Epoch time: 17177
74584715 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 350
6872 deg
Eccentricity:
0004693
Arg of perigee: 322
2896 deg
Mean anomaly: 37
7927 deg
Mean motion: 15
54105281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 325
Coasting Arc #13 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2017/178/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4928606
68 A = 6782054
97 meter
Y = -2127581
84 meter E =
0008100
Z = -4153305
69 I = 51
54768
XDOT = 5047
645163 Wp = 34
82862
YDOT = -4381
277924 meter/sec RA = 345
44306 deg
ZDOT = -3742
637648 TA = 196
55876
MA = 196
58522
Ha = 220
861 n
mi
Hp = 215
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16169969
41 X = -4884274
74
Y = -6980255
39 feet Y = -2182448
53 meter
Z = -13626331
02 Z = -4177139
59
XDOT = 16560
515626 XDOT = 5114
442273
YDOT = -14374
271404 feet/sec YDOT = -4324
457831 meter/sec
ZDOT = -12278
994909 ZDOT = -3717
956321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13259022
79 X = 4041350
15
Y = 11468338
41 feet Y = 3495549
55 meter
Z = -13731143
51 Z = -4185252
54
XDOT = -19339
933066 XDOT = -5894
811598
YDOT = 7778
171821 feet/sec YDOT = 2370
786771 meter/sec
ZDOT = -12169
169305 ZDOT = -3709
162804
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 17178
71040443
00016717 00000-0 10270-3 0 9127
2 25544 51
6425 345
8801 0004800 326
0040 34
0804 15
54080395 23386
Satellite: ISS
Catalog Number: 25544
Epoch time: 17178
71040443 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 345
8801 deg
Eccentricity:
0004800
Arg of perigee: 326
0040 deg
Mean anomaly: 34
0804 deg
Mean motion: 15
54080395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 277
Coasting Arc #14 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2017/179/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3524455
76 A = 6778722
82 meter
Y = 2950710
89 meter E =
0002696
Z = 4979741
85 I = 51
50563
XDOT = -6235
572449 Wp = 70
06749
YDOT = 3959
600468 meter/sec RA = 340
44316 deg
ZDOT = 2067
037320 TA = 359
79237
MA = 359
79248
Ha = 220
840 n
mi
Hp = 215
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11563175
07 X = 3467009
33
Y = 9680810
01 feet Y = 2989802
08 meter
Z = 16337735
73 Z = 4996723
11
XDOT = -20457
914860 XDOT = -6289
426841
YDOT = 12990
815183 feet/sec YDOT = 3889
568759 meter/sec
ZDOT = 6781
618503 ZDOT = 2036
616752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8255418
31 X = -2516251
50
Y = -12523445
07 feet Y = -3817146
06 meter
Z = 16412132
73 Z = 5002418
06
XDOT = 22422
936424 XDOT = 6834
511022
YDOT = -6070
704948 feet/sec YDOT = -1850
350868 meter/sec
ZDOT = 6646
548331 ZDOT = 2025
867931
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 17179
73926151
00016717 00000-0 10270-3 0 9130
2 25544 51
6425 340
7519 0004848 330
1342 29
9534 15
54121713 23540
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
73926151 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 340
7519 deg
Eccentricity:
0004848
Arg of perigee: 330
1342 deg
Mean anomaly: 29
9534 deg
Mean motion: 15
54121713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 304
Coasting Arc #15 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2017/180/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1942959
68 A = 6777472
29 meter
Y = -3757654
23 meter E =
0013503
Z = -5306252
10 I = 51
47023
XDOT = 6903
825281 Wp = 69
10862
YDOT = -3311
822058 meter/sec RA = 335
43502 deg
ZDOT = -178
300310 TA = 199
16068
MA = 199
21152
Ha = 221
080 n
mi
Hp = 215
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6374539
64 X = -1875021
27
Y = -12328261
90 feet Y = -3779001
42 meter
Z = -17408963
58 Z = -5315525
60
XDOT = 22650
345409 XDOT = 6941
211929
YDOT = -10865
557933 feet/sec YDOT = -3234
409746 meter/sec
ZDOT = -584
974770 ZDOT = -144
673426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2757181
27 X = 840388
85
Y = 13550533
23 feet Y = 4130202
53 meter
Z = -17449177
93 Z = -5318509
43
XDOT = -23739
049137 XDOT = -7235
662177
YDOT = 4250
659234 feet/sec YDOT = 1295
600934 meter/sec
ZDOT = -435
887927 ZDOT = -132
858640
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 17180
70381412
00016717 00000-0 10270-3 0 9145
2 25544 51
6421 335
9449 0004967 333
5955 26
4944 15
54090470 23691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
70381412 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 335
9449 deg
Eccentricity:
0004967
Arg of perigee: 333
5955 deg
Mean anomaly: 26
4944 deg
Mean motion: 15
54090470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 320
Coasting Arc #16 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2017/181/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 281874
19 A = 6778372
19 meter
Y = 4487990
54 meter E =
0008175
Z = 5071876
63 I = 51
44505
XDOT = -7066
739120 Wp = 17
52495
YDOT = 2417
739720 meter/sec RA = 330
42285 deg
ZDOT = -1738
286150 TA = 89
37184
MA = 89
27818
Ha = 221
185 n
mi
Hp = 215
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 924784
08 X = 207030
81
Y = 14724378
41 feet Y = 4490723
78 meter
Z = 16640015
19 Z = 5073064
44
XDOT = -23184
839632 XDOT = -7084
806018
YDOT = 7932
216928 feet/sec YDOT = 2338
613766 meter/sec
ZDOT = -5703
038551 ZDOT = -1772
657672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2880124
26 X = 877861
87
Y = -14464491
79 feet Y = -4408777
10 meter
Z = 16644398
82 Z = 5073212
76
XDOT = 23338
707081 XDOT = 7113
637918
YDOT = -2122
143221 feet/sec YDOT = -646
829254 meter/sec
ZDOT = -5855
228274 ZDOT = -1784
673578
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 17181
73266457
00016717 00000-0 10270-3 0 9151
2 25544 51
6427 330
8159 0005088 338
1122 21
9812 15
54140816 23853
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
73266457 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 330
8159 deg
Eccentricity:
0005088
Arg of perigee: 338
1122 deg
Mean anomaly: 21
9812 deg
Mean motion: 15
54140816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2385
Checksum: 308
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