[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 24th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
183/05:31:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
6
183/06:09:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
6
185/03:48:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 213
6
187/04:14:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
5
189/01:37:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
4
Coasting Arc #1 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2016/174/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1702754
95 A = 6779971
85 meter
Y = 4947681
05 meter E =
0009143
Z = 4305072
06 I = 51
82772
XDOT = -6758
387943 Wp = 102
66842
YDOT = -769
230144 meter/sec RA = 30
70803 deg
ZDOT = 3548
853247 TA = 311
24967
MA = 311
32841
Ha = 220
094 n
mi
Hp = 214
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5586466
36 X = 1626390
14
Y = 16232549
38 feet Y = 4966294
81 meter
Z = 14124252
15 Z = 4313158
77
XDOT = -22173
188790 XDOT = -6766
522605
YDOT = -2523
720945 feet/sec YDOT = -844
852916 meter/sec
ZDOT = 11643
219314 ZDOT = 3516
003037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13724223
98 X = 4183143
47
Y = -10265601
56 feet Y = -3128955
36 meter
Z = 14158455
61 Z = 4315497
27
XDOT = 3763
562179 XDOT = 1147
133752
YDOT = 20930
240699 feet/sec YDOT = 6379
537365 meter/sec
ZDOT = 11500
202631 ZDOT = 3505
261762
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 16174
60402830
00016717 00000-0 10270-3 0 9009
2 25544 51
6414 31
0142 0000986 338
6514 21
4598 15
54626203 5825
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
60402830 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 31
0142 deg
Eccentricity:
0000986
Arg of perigee: 338
6514 deg
Mean anomaly: 21
4598 deg
Mean motion: 15
54626203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 278
Coasting Arc #2 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2016/175/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 113617
49 A = 6776638
40 meter
Y = -4433468
66 meter E =
0013642
Z = -5136112
21 I = 51
78740
XDOT = 7198
828054 Wp = 74
03198
YDOT = 2055
974923 meter/sec RA = 25
71939 deg
ZDOT = -1615
365065 TA = 180
39655
MA = 180
39763
Ha = 220
133 n
mi
Hp = 213
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 372760
80 X = 188134
00
Y = -14545500
85 feet Y = -4431780
82 meter
Z = -16850761
83 Z = -5135379
85
XDOT = 23618
202276 XDOT = 7183
149272
YDOT = 6745
324551 feet/sec YDOT = 2136
389551 meter/sec
ZDOT = -5299
754150 ZDOT = -1580
433090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13905253
75 X = -4238321
34
Y = 4300413
62 feet Y = 1310766
07 meter
Z = -16846634
11 Z = -5134854
08
XDOT = -1043
876971 XDOT = -318
173701
YDOT = -23543
339427 feet/sec YDOT = -7176
009857 meter/sec
ZDOT = -5147
938384 ZDOT = -1569
091619
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 16175
56823380
00016717 00000-0 10270-3 0 9013
2 25544 51
6402 26
2030 0000870 349
1227 10
9907 15
54655578 5974
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
56823380 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 26
2030 deg
Eccentricity:
0000870
Arg of perigee: 349
1227 deg
Mean anomaly: 10
9907 deg
Mean motion: 15
54655578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 301
Coasting Arc #3 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2016/176/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2020584
94 A = 6775989
65 meter
Y = 3702714
14 meter E =
0003127
Z = 5300970
09 I = 51
75534
XDOT = -7005
570518 Wp = 51
59061
YDOT = -3083
797539 meter/sec RA = 20
72353 deg
ZDOT = -514
204310 TA = 43
31754
MA = 43
29295
Ha = 220
257 n
mi
Hp = 213
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6629215
69 X = -2087589
02
Y = 12148012
27 feet Y = 3679743
39 meter
Z = 17391634
16 Z = 5290992
35
XDOT = -22984
155244 XDOT = -6968
068294
YDOT = -10117
445995 feet/sec YDOT = -3161
928752 meter/sec
ZDOT = -1687
022013 ZDOT = -548
144539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13725088
93 X = 4183407
11
Y = 2163438
54 feet Y = 659416
07 meter
Z = 17347366
05 Z = 5287477
17
XDOT = -1463
598606 XDOT = -446
104855
YDOT = 24048
835559 feet/sec YDOT = 7330
085078 meter/sec
ZDOT = -1834
293571 ZDOT = -559
092680
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 16176
59671687
00016717 00000-0 10270-3 0 9029
2 25544 51
6400 21
0721 0000825 350
0305 10
0832 15
54629943 6134
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
59671687 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 21
0721 deg
Eccentricity:
0000825
Arg of perigee: 350
0305 deg
Mean anomaly: 10
0832 deg
Mean motion: 15
54629943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 277
Coasting Arc #4 (Orbit 627)
---------------------------------------
Vector Time (GMT): 2016/177/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824867
05 A = 6778038
50 meter
Y = -2868789
89 meter E =
0011060
Z = -4814778
64 I = 51
73204
XDOT = 6112
793916 Wp = 104
46041
YDOT = 3831
721163 meter/sec RA = 15
72647 deg
ZDOT = 2575
213779 TA = 190
87998
MA = 190
90393
Ha = 220
152 n
mi
Hp = 213
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12548776
41 X = 3880050
22
Y = -9412040
33 feet Y = -2825708
69 meter
Z = -15796517
85 Z = -4796064
79
XDOT = 20055
098149 XDOT = 6056
983166
YDOT = 12571
263658 feet/sec YDOT = 3899
766203 meter/sec
ZDOT = 8448
864105 ZDOT = 2604
772741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13329400
75 X = -4062801
35
Y = -8424630
41 feet Y = -2567827
35 meter
Z = -15714354
81 Z = -4789735
35
XDOT = 3934
327661 XDOT = 1199
183071
YDOT = -22209
329036 feet/sec YDOT = -6769
403490 meter/sec
ZDOT = 8576
877058 ZDOT = 2614
232127
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 16177
56091427
00016717 00000-0 10270-3 0 9036
2 25544 51
6400 16
2606 0000736 355
0962 5
0183 15
54670599 6289
Satellite: ISS
Catalog Number: 25544
Epoch time: 16177
56091427 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 16
2606 deg
Eccentricity:
0000736
Arg of perigee: 355
0962 deg
Mean anomaly: 5
0183 deg
Mean motion: 15
54670599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 628
Checksum: 299
Coasting Arc #5 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2016/178/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5333672
07 A = 6782049
07 meter
Y = 1957298
28 meter E =
0011791
Z = 3695247
06 I = 51
71479
XDOT = -4604
183624 Wp = 80
99415
YDOT = -4350
134868 meter/sec RA = 10
73795 deg
ZDOT = -4327
857797 TA = 55
00955
MA = 54
89891
Ha = 220
199 n
mi
Hp = 213
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17498924
10 X = -5373112
46
Y = 6421582
29 feet Y = 1897432
79 meter
Z = 12123513
98 Z = 3669241
94
XDOT = -15105
589317 XDOT = -4534
174396
YDOT = -14272
096024 feet/sec YDOT = -4401
230127 meter/sec
ZDOT = -14199
008520 ZDOT = -4350
053936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12548472
93 X = 3824774
55
Y = 13882716
55 feet Y = 4231452
01 meter
Z = 12009773
66 Z = 3660579
01
XDOT = -6584
954314 XDOT = -2007
094075
YDOT = 18357
278849 feet/sec YDOT = 5595
298593 meter/sec
ZDOT = -14294
818479 ZDOT = -4357
060672
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 16178
58938568
00016717 00000-0 10270-3 0 9046
2 25544 51
6405 11
1293 0000824 349
8597 10
2539 15
54676338 6441
Satellite: ISS
Catalog Number: 25544
Epoch time: 16178
58938568 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 11
1293 deg
Eccentricity:
0000824
Arg of perigee: 349
8597 deg
Mean anomaly: 10
2539 deg
Mean motion: 15
54676338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 331
Coasting Arc #6 (Orbit 658)
---------------------------------------
Vector Time (GMT): 2016/179/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353077
71 A = 6785862
40 meter
Y = -1052216
14 meter E =
0007092
Z = -2132609
35 I = 51
69557
XDOT = 2614
508259 Wp = 37
92860
YDOT = 4641
165848 meter/sec RA = 5
75992 deg
ZDOT = 5513
941213 TA = 298
45439
MA = 298
52583
Ha = 220
246 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20843430
81 X = 6374730
95
Y = -3452152
69 feet Y = -981050
56 meter
Z = -6996749
83 Z = -2101695
25
XDOT = 8577
783001 XDOT = 2535
630986
YDOT = 15226
922074 feet/sec YDOT = 4669
961576 meter/sec
ZDOT = 18090
358309 ZDOT = 5526
450574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11347142
47 X = -3458609
02
Y = -17873956
09 feet Y = -5447981
81 meter
Z = -6861816
51 Z = -2091481
67
XDOT = 9403
175494 XDOT = 2866
087891
YDOT = -12915
454450 feet/sec YDOT = -3936
630516 meter/sec
ZDOT = 18143
889215 ZDOT = 5530
257433
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 16179
55357519
00016717 00000-0 10270-3 0 9056
2 25544 51
6402 6
3190 0000707 12
4741 347
6430 15
54681302 6594
Satellite: ISS
Catalog Number: 25544
Epoch time: 16179
55357519 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 6
3190 deg
Eccentricity:
0000707
Arg of perigee: 12
4741 deg
Mean anomaly: 347
6430 deg
Mean motion: 15
54681302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 659
Checksum: 294
Coasting Arc #7 (Orbit 674)
---------------------------------------
Vector Time (GMT): 2016/180/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6776093
48 A = 6787559
80 meter
Y = 115145
02 meter E =
0011948
Z = 263692
04 I = 51
66964
XDOT = -321
509480 Wp = 128
47706
YDOT = -4755
274369 meter/sec RA =
78930 deg
ZDOT = -6008
493450 TA = 48
68199
MA = 48
57922
Ha = 220
089 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22231277
81 X = -6778158
35
Y = 377772
39 feet Y = 39358
66 meter
Z = 865131
37 Z = 230770
45
XDOT = -1054
821129 XDOT = -239
124225
YDOT = -15601
293862 feet/sec YDOT = -4758
408568 meter/sec
ZDOT = -19712
905020 ZDOT = -6009
855549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9392568
61 X = 2862854
91
Y = 20158862
64 feet Y = 6144421
33 meter
Z = 721657
28 Z = 219961
14
XDOT = -12405
791408 XDOT = -3781
285221
YDOT = 6510
972354 feet/sec YDOT = 1984
544373 meter/sec
ZDOT = -19717
835201 ZDOT = -6009
996169
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 16180
58203705
00016717 00000-0 10270-3 0 9069
2 25544 51
6401 1
1881 0000930 3
0991 357
0168 15
54730342 6754
Satellite: ISS
Catalog Number: 25544
Epoch time: 16180
58203705 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 1
1881 deg
Eccentricity:
0000930
Arg of perigee: 3
0991 deg
Mean anomaly: 357
0168 deg
Mean motion: 15
54730342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 675
Checksum: 277
Coasting Arc #8 (Orbit 690)
---------------------------------------
Vector Time (GMT): 2016/181/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6538428
79 A = 6786482
04 meter
Y = 795676
55 meter E =
0014430
Z = 1604974
05 I = 51
63492
XDOT = -1986
510055 Wp = 61
20718
YDOT = 4695
429421 meter/sec RA = 355
81691 deg
ZDOT = 5732
726474 TA = 316
36702
MA = 316
48104
Ha = 220
142 n
mi
Hp = 213
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21451538
04 X = 6521249
10
Y = 2610487
36 feet Y = 868697
40 meter
Z = 5265662
91 Z = 1636694
54
XDOT = -6517
421439 XDOT = -2066
715073
YDOT = 15404
952169 feet/sec YDOT = 4672
765935 meter/sec
ZDOT = 18808
157724 ZDOT = 5722
882123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6682840
15 X = -2036929
68
Y = -20514628
39 feet Y = -6252858
73 meter
Z = 5403702
79 Z = 1647048
61
XDOT = 15272
930341 XDOT = 4655
189168
YDOT = -5
515255 feet/sec YDOT = -1
681050 meter/sec
ZDOT = 18764
271496 ZDOT = 5719
349952
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 16181
61049562
00016717 00000-0 10270-3 0 9074
2 25544 51
6413 356
0568 0000696 18
0547 342
0631 15
54713658 6911
Satellite: ISS
Catalog Number: 25544
Epoch time: 16181
61049562 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 356
0568 deg
Eccentricity:
0000696
Arg of perigee: 18
0547 deg
Mean anomaly: 342
0631 deg
Mean motion: 15
54713658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 691
Checksum: 309
Coasting Arc #9 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2016/182/13:11:11
324
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5667364
29 A = 6782899
93 meter
Y = -1737491
29 meter E =
0005089
Z = -3301907
11 I = 51
59066
XDOT = 4101
562533 Wp = 83
99617
YDOT = -4442
614497 meter/sec RA = 350
83566 deg
ZDOT = -4707
872970 TA = 134
39441
MA = 134
35273
Ha = 220
199 n
mi
Hp = 213
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18593714
87 X = -5631474
73
Y = -5700430
74 feet Y = -1800666
48 meter
Z = -10833028
58 Z = -3329350
86
XDOT = 13456
569989 XDOT = 4173
805010
YDOT = -14575
506880 feet/sec YDOT = -4396
343616 meter/sec
ZDOT = -15445
777461 ZDOT = -4687
773589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2988968
04 X = 911037
46
Y = 19149161
66 feet Y = 5836664
47 meter
Z = -10952229
41 Z = -3338239
53
XDOT = -17645
795001 XDOT = -5378
438316
YDOT = -6018
539430 feet/sec YDOT = -1834
450818 meter/sec
ZDOT = -15357
265286 ZDOT = -4680
894459
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 16182
57467022
00016717 00000-0 10270-3 0 9086
2 25544 51
6409 351
2468 0000847 23
9139 336
2053 15
54714414 7063
Satellite: ISS
Catalog Number: 25544
Epoch time: 16182
57467022 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 351
2468 deg
Eccentricity:
0000847
Arg of perigee: 23
9139 deg
Mean anomaly: 336
2053 deg
Mean motion: 15
54714414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 303
Coasting Arc #10 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2016/183/05:31:00
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3211773
78 A = 6777074
23 meter
Y = 3316522
86 meter E =
0005868
Z = 4957243
83 I = 51
55211
XDOT = -6629
052578 Wp = 111
77352
YDOT = 3217
056171 meter/sec RA = 347
43474 deg
ZDOT = 2138
471631 TA = 317
35601
MA = 317
40155
Ha = 220
126 n
mi
Hp = 213
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10537315
55 X = 3150368
68
Y = 10880980
51 feet Y = 3352095
08 meter
Z = 16263923
31 Z = 4972697
13
XDOT = -21748
860164 XDOT = -6674
921615
YDOT = 10554
646231 feet/sec YDOT = 3142
668946 meter/sec
ZDOT = 7015
983040 ZDOT = 2106
158289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10732562
47 X = 3271285
04
Y = 10586373
37 feet Y = 3226726
60 meter
Z = 16330546
80 Z = 4977550
66
XDOT = -20717
841811 XDOT = -6314
798184
YDOT = 10378
303625 feet/sec YDOT = 3163
306945 meter/sec
ZDOT = 6874
518254 ZDOT = 2095
353164
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 16183
28172888
00016717 00000-0 10270-3 0 9099
2 25544 51
6433 347
7240 0001171 14
4948 345
6239 15
54721448 7179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
28172888 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 347
7240 deg
Eccentricity:
0001171
Arg of perigee: 14
4948 deg
Mean anomaly: 345
6239 deg
Mean motion: 15
54721448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 717
Checksum: 322
Coasting Arc #11 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2016/183/06:09:00
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5843170
69 A = 6783225
76 meter
Y = -1287091
55 meter E =
0004689
Z = -3200397
36 I = 51
57219
XDOT = 3663
559749 Wp = 83
62152
YDOT = -4723
961143 meter/sec RA = 347
31129 deg
ZDOT = -4794
515912 TA = 133
39695
MA = 133
35790
Ha = 220
169 n
mi
Hp = 213
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19170507
50 X = -5812797
65
Y = -4222741
31 feet Y = -1352263
54 meter
Z = -10499991
34 Z = -3228708
47
XDOT = 12019
552981 XDOT = 3739
401717
YDOT = -15498
560182 feet/sec YDOT = -4682
568105 meter/sec
ZDOT = -15730
039081 ZDOT = -4776
535615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19558407
33 X = -5961402
56
Y = -457095
15 feet Y = -139322
60 meter
Z = -10623063
91 Z = -3237909
88
XDOT = 8867
638938 XDOT = 2702
856348
YDOT = -16121
924586 feet/sec YDOT = -4913
962614 meter/sec
ZDOT = -15650
700787 ZDOT = -4770
333600
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 16183
28172880
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 347
7246 0001159 5
8217 354
2950 15
54698485 7179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
28172880 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 347
7246 deg
Eccentricity:
0001159
Arg of perigee: 5
8217 deg
Mean anomaly: 354
2950 deg
Mean motion: 15
54698485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 717
Checksum: 326
Coasting Arc #12 (Orbit 732)
---------------------------------------
Vector Time (GMT): 2016/184/06:09:00
000
Vector Time (MET): N/A
Weight (LBS) : 891816
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4539276
97 A = 6779010
76 meter
Y = 2288072
40 meter E =
0008812
Z = 4478649
99 I = 51
52748
XDOT = -5398
811569 Wp = 103
51829
YDOT = 4403
144699 meter/sec RA = 342
31383 deg
ZDOT = 3215
054679 TA = 314
08716
MA = 314
15966
Ha = 220
139 n
mi
Hp = 213
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14892640
97 X = 4491598
48
Y = 7506799
22 feet Y = 2338566
40 meter
Z = 14693733
57 Z = 4500585
15
XDOT = -17712
636382 XDOT = -5463
264714
YDOT = 14446
012792 feet/sec YDOT = 4342
410757 meter/sec
ZDOT = 10548
079654 ZDOT = 3188
672713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16043728
08 X = 4890128
32
Y = 4235371
14 feet Y = 1290941
12 meter
Z = 14788813
90 Z = 4507630
48
XDOT = -14043
448109 XDOT = -4280
442984
YDOT = 16686
931635 feet/sec YDOT = 5086
176762 meter/sec
ZDOT = 10432
207110 ZDOT = 3179
736727
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 16184
31017392
00016717 00000-0 10270-3 0 9115
2 25544 51
6443 342
5930 0001276 14
2556 345
8633 15
54707937 7333
Satellite: ISS
Catalog Number: 25544
Epoch time: 16184
31017392 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 342
5930 deg
Eccentricity:
0001276
Arg of perigee: 14
2556 deg
Mean anomaly: 345
8633 deg
Mean motion: 15
54707937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 733
Checksum: 302
Coasting Arc #13 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2016/185/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463122
20 A = 6776627
94 meter
Y = 2916563
44 meter E =
0005192
Z = 5038463
35 I = 51
49111
XDOT = -6192
636600 Wp = 110
98677
YDOT = 4128
903118 meter/sec RA = 337
79504 deg
ZDOT = 1862
997631 TA = 320
91707
MA = 320
95456
Ha = 220
083 n
mi
Hp = 213
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11361949
49 X = 3405776
53
Y = 9568777
68 feet Y = 2954968
99 meter
Z = 16530391
58 Z = 5055147
39
XDOT = -20317
049211 XDOT = -6247
396371
YDOT = 13546
270072 feet/sec YDOT = 4059
346475 meter/sec
ZDOT = 6112
196951 ZDOT = 1832
783118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6822808
20 X = 2079591
94
Y = 13104075
48 feet Y = 3994122
21 meter
Z = 16602461
94 Z = 5060430
40
XDOT = -23003
322727 XDOT = -7011
412767
YDOT = 4386
932640 feet/sec YDOT = 1337
137069 meter/sec
ZDOT = 5979
687329 ZDOT = 1822
608698
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 16185
21005718
00016717 00000-0 10270-3 0 9125
2 25544 51
6430 338
1025 0001251 15
4861 344
6330 15
54752969 7471
Satellite: ISS
Catalog Number: 25544
Epoch time: 16185
21005718 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 338
1025 deg
Eccentricity:
0001251
Arg of perigee: 15
4861 deg
Mean anomaly: 344
6330 deg
Mean motion: 15
54752969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 747
Checksum: 290
Coasting Arc #14 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2016/186/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1651200
83 A = 6775603
66 meter
Y = -3900282
31 meter E =
0015343
Z = -5301930
94 I = 51
45854
XDOT = 6904
545440 Wp = 87
16071
YDOT = -3301
276071 meter/sec RA = 332
77795 deg
ZDOT = 279
668158 TA = 185
50691
MA = 185
52381
Ha = 220
272 n
mi
Hp = 213
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5417325
55 X = -1581709
94
Y = -12796201
81 feet Y = -3918357
82 meter
Z = -17394786
56 Z = -5309783
77
XDOT = 22652
708136 XDOT = 6939
589487
YDOT = -10830
958238 feet/sec YDOT = -3223
868941 meter/sec
ZDOT = 917
546451 ZDOT = 313
293007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -333631
89 X = -101691
00
Y = -13849769
68 feet Y = -4221409
80 meter
Z = -17428177
36 Z = -5312108
46
XDOT = 24018
281038 XDOT = 7320
772060
YDOT = -1912
463619 feet/sec YDOT = -582
918911 meter/sec
ZDOT = 1064
736002 ZDOT = 324
531534
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 16186
17421620
00016717 00000-0 10270-3 0 9136
2 25544 51
6435 333
2921 0001396 21
6890 338
4322 15
54742676 7621
Satellite: ISS
Catalog Number: 25544
Epoch time: 16186
17421620 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 333
2921 deg
Eccentricity:
0001396
Arg of perigee: 21
6890 deg
Mean anomaly: 338
4322 deg
Mean motion: 15
54742676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 301
Coasting Arc #15 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/03:48:30
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -222655
10 A = 6777464
38 meter
Y = 4718127
29 meter E =
0008095
Z = 4856694
26 I = 51
43672
XDOT = -6968
301154 Wp = 52
66947
YDOT = 2140
687864 meter/sec RA = 327
76090 deg
ZDOT = -2391
509472 TA = 60
86548
MA = 60
78448
Ha = 220
218 n
mi
Hp = 213
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -730495
75 X = -298989
23
Y = 15479420
25 feet Y = 4715209
94 meter
Z = 15934036
29 Z = 4855427
91
XDOT = -22861
880428 XDOT = -6980
104213
YDOT = 7023
254148 feet/sec YDOT = 2062
698008 meter/sec
ZDOT = -7846
159684 ZDOT = -2425
387633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6115016
60 X = -1863857
06
Y = 14246399
44 feet Y = 4342302
55 meter
Z = 15927531
59 Z = 4854711
63
XDOT = -22794
864475 XDOT = -6947
874692
YDOT = -818
985898 feet/sec YDOT = -249
626902 meter/sec
ZDOT = -7994
205370 ZDOT = -2436
633797
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 16187
20264652
00016717 00000-0 10270-3 0 9142
2 25544 51
6435 328
1617 0001390 18
2593 341
8610 15
54764797 7785
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20264652 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 328
1617 deg
Eccentricity:
0001390
Arg of perigee: 18
2593 deg
Mean anomaly: 341
8610 deg
Mean motion: 15
54764797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 321
Coasting Arc #16 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2016/187/04:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6046601
57 A = 6783998
98 meter
Y = 1117090
21 meter E =
0004559
Z = -2868838
34 I = 51
45885
XDOT = 1353
602012 Wp = 98
99483
YDOT = -5608
557031 meter/sec RA = 327
71444 deg
ZDOT = -5044
434006 TA = 113
72700
MA = 113
67916
Ha = 220
204 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19837931
65 X = -6044708
38
Y = 3664994
14 feet Y = 1049484
06 meter
Z = -9412199
27 Z = -2898206
05
XDOT = 4440
951483 XDOT = 1440
721037
YDOT = -18400
777660 feet/sec YDOT = -5592
932354 meter/sec
ZDOT = -16549
980336 ZDOT = -5037
647804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20080777
23 X = -6120620
90
Y = -1144004
23 feet Y = -348692
49 meter
Z = -9540379
95 Z = -2907907
81
XDOT = 8709
932429 XDOT = 2654
787404
YDOT = -15328
664779 feet/sec YDOT = -4672
177025 meter/sec
ZDOT = -16519
240832 ZDOT = -5035
064606
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 16187
20264675
00016717 00000-0 10270-3 0 9158
2 25544 51
6444 328
1617 0001246 15
8757 344
2435 15
54727783 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 16187
20264675 = yrday
fracday
Element set: 915
Inclination: 51
6444 deg
RA of node: 328
1617 deg
Eccentricity:
0001246
Arg of perigee: 15
8757 deg
Mean anomaly: 344
2435 deg
Mean motion: 15
54727783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 328
Coasting Arc #17 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2016/188/04:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5267762
58 A = 6779740
07 meter
Y = 253048
13 meter E =
0010130
Z = 4252754
07 I = 51
41855
XDOT = -3178
627860 Wp = 98
65274
YDOT = 6001
537552 meter/sec RA = 322
71165 deg
ZDOT = 3571
383685 TA = 314
76468
MA = 314
84705
Ha = 220
178 n
mi
Hp = 213
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17282685
64 X = 5243883
73
Y = 830210
41 feet Y = 311821
75 meter
Z = 13952605
23 Z = 4278285
15
XDOT = -10428
569096 XDOT = -3262
850271
YDOT = 19690
083832 feet/sec YDOT = 5965
520676 meter/sec
ZDOT = 11717
138075 ZDOT = 3555
739116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16583117
18 X = 5054534
12
Y = 4611494
04 feet Y = 1405583
38 meter
Z = 14063783
71 Z = 4286641
28
XDOT = -14260
777818 XDOT = -4346
685079
YDOT = 15672
745513 feet/sec YDOT = 4777
052832 meter/sec
ZDOT = 11647
733898 ZDOT = 3550
229292
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 16188
23107130
00016717 00000-0 10270-3 0 9165
2 25544 51
6449 323
0301 0001456 24
3756 335
7466 15
54741369 7945
Satellite: ISS
Catalog Number: 25544
Epoch time: 16188
23107130 = yrday
fracday
Element set: 916
Inclination: 51
6449 deg
RA of node: 323
0301 deg
Eccentricity:
0001456
Arg of perigee: 24
3756 deg
Mean anomaly: 335
7466 deg
Mean motion: 15
54741369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 304
Coasting Arc #18 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2016/189/01:37:00
000
Vector Time (MET): N/A
Weight (LBS) : 877382
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5222998
24 A = 6787474
17 meter
Y = -4310984
22 meter E =
0014177
Z = 330872
85 I = 51
41938
XDOT = 2817
689919 Wp = 46
28096
YDOT = 3884
719337 meter/sec RA = 318
23060 deg
ZDOT = 5984
822656 TA = 317
29797
MA = 317
40806
Ha = 220
326 n
mi
Hp = 213
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17135821
01 X = 5269209
36
Y = -14143649
03 feet Y = -4252318
83 meter
Z = 1085540
86 Z = 356356
24
XDOT = 9244
389499 XDOT = 2744
969418
YDOT = 12745
142182 feet/sec YDOT = 3915
821418 meter/sec
ZDOT = 19635
244933 ZDOT = 5998
333814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21759790
30 X = 6632384
08
Y = 4464886
18 feet Y = 1360897
31 meter
Z = 1197449
69 Z = 364982
67
XDOT = -3880
623913 XDOT = -1182
814169
YDOT = 13510
324914 feet/sec YDOT = 4117
947034 meter/sec
ZDOT = 19693
308506 ZDOT = 6002
520433
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 16189
13093784
00016717 00000-0 10270-3 0 9175
2 25544 51
6423 318
5400 0001526 26
5089 333
6142 15
54748627 8085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16189
13093784 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 318
5400 deg
Eccentricity:
0001526
Arg of perigee: 26
5089 deg
Mean anomaly: 333
6142 deg
Mean motion: 15
54748627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 314
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