[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 1st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
152/21:55:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
1
153/10:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 216
2
153/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
155/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 216
3
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
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
Coasting Arc #1 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2017/151/09:37:14
177
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1689602
17 A = 6780056
85 meter
Y = -4481618
17 meter E =
0003616
Z = 4795702
03 I = 51
94452
XDOT = 5324
227794 Wp = 93
73863
YDOT = -4843
874125 meter/sec RA = 120
95802 deg
ZDOT = -2649
339065 TA = 22
28820
MA = 22
27249
Ha = 221
001 n
mi
Hp = 215
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5543314
22 X = -1662657
14
Y = -14703471
68 feet Y = -4500362
19 meter
Z = 15733930
55 Z = 4787559
54
XDOT = 17467
938958 XDOT = 5390
866749
YDOT = -15891
975476 feet/sec YDOT = -4783
962182 meter/sec
ZDOT = -8692
057300 ZDOT = -2623
314157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12665306
86 X = -3860385
53
Y = -9360423
26 feet Y = -2853057
01 meter
Z = 15698708
90 Z = 4784966
47
XDOT = 5548
004972 XDOT = 1691
031916
YDOT = -21898
812078 feet/sec YDOT = -6674
757921 meter/sec
ZDOT = -8576
390211 ZDOT = -2614
083736
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 17151
44449976
00016717 00000-0 10270-3 0 9009
2 25544 51
6390 121
7795 0004790 217
7560 142
3257 15
53974660 19141
Satellite: ISS
Catalog Number: 25544
Epoch time: 17151
44449976 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 121
7795 deg
Eccentricity:
0004790
Arg of perigee: 217
7560 deg
Mean anomaly: 142
3257 deg
Mean motion: 15
53974660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 324
Coasting Arc #2 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2017/152/09:37:14
177
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 640456
32 A = 6783599
31 meter
Y = 5554192
07 meter E =
0005874
Z = -3848381
77 I = 51
97158
XDOT = -5361
498453 Wp = 149
66125
YDOT = 3521
870942 meter/sec RA = 115
99178 deg
ZDOT = 4188
532654 TA = 164
30121
MA = 164
28299
Ha = 220
825 n
mi
Hp = 216
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2101234
65 X = 596993
87
Y = 18222414
94 feet Y = 5561111
34 meter
Z = -12625924
44 Z = -3845375
80
XDOT = -17590
218021 XDOT = -5420
828331
YDOT = 11554
694690 feet/sec YDOT = 3461
583010 meter/sec
ZDOT = 13741
905034 ZDOT = 4162
344250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11880603
82 X = 3621208
04
Y = 13986958
09 feet Y = 4263224
83 meter
Z = -12613556
89 Z = -3844612
14
XDOT = -7340
938040 XDOT = -2237
517914
YDOT = 18529
585077 feet/sec YDOT = 5647
817532 meter/sec
ZDOT = 13625
715888 ZDOT = 4153
118203
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 17152
40913465
00016717 00000-0 10270-3 0 9016
2 25544 51
6386 116
9727 0004631 221
2162 138
8642 15
53946686 19290
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
40913465 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 116
9727 deg
Eccentricity:
0004631
Arg of perigee: 221
2162 deg
Mean anomaly: 138
8642 deg
Mean motion: 15
53946686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 320
Coasting Arc #3 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2017/152/21:55:41
000
Vector Time (MET): N/A
Weight (LBS) : 915838
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1619993
65 A = 6781656
92 meter
Y = 4909217
61 meter E =
0008502
Z = -4397750
37 I = 51
97088
XDOT = -4968
637422 Wp = 143
26305
YDOT = 4714
948153 meter/sec RA = 113
44539 deg
ZDOT = 3429
805726 TA = 161
39166
MA = 161
36055
Ha = 220
814 n
mi
Hp = 216
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5314939
78 X = 1586339
26
Y = 16106357
00 feet Y = 4927145
59 meter
Z = -14428314
86 Z = -4389962
34
XDOT = -16301
303877 XDOT = -5037
652292
YDOT = 15468
990002 feet/sec YDOT = 4658
999375 meter/sec
ZDOT = 11252
643458 ZDOT = 3405
502229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14279445
44 X = -4352374
97
Y = -9204818
43 feet Y = -2805628
66 meter
Z = -14394733
27 Z = -4387514
70
XDOT = 2463
337535 XDOT = 750
825281
YDOT = -21266
059560 feet/sec YDOT = -6481
894954 meter/sec
ZDOT = 11144
574617 ZDOT = 3396
866343
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 17152
92360645
00016717 00000-0 10270-3 0 9020
2 25544 51
6370 114
4045 0004895 221
4830 138
5951 15
53965115 19372
Satellite: ISS
Catalog Number: 25544
Epoch time: 17152
92360645 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 114
4045 deg
Eccentricity:
0004895
Arg of perigee: 221
4830 deg
Mean anomaly: 138
5951 deg
Mean motion: 15
53965115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 306
Coasting Arc #4 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2017/153/10:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4572891
53 A = 6780262
81 meter
Y = 1548498
58 meter E =
0007601
Z = 4760663
05 I = 51
97341
XDOT = 433
661418 Wp = 154
01451
YDOT = -7150
122128 meter/sec RA = 110
83686 deg
ZDOT = 2733
974713 TA = 269
02697
MA = 269
11406
Ha = 220
671 n
mi
Hp = 216
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15002924
97 X = -4612992
45
Y = 5080375
92 feet Y = 1497136
90 meter
Z = 15618973
25 Z = 4738351
95
XDOT = 1422
773680 XDOT = 500
303360
YDOT = -23458
405931 feet/sec YDOT = -7144
900183 meter/sec
ZDOT = 8969
733310 ZDOT = 2736
242737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5298692
28 X = -1615041
41
Y = 15029874
49 feet Y = 4581105
74 meter
Z = 15520213
77 Z = 4730561
16
XDOT = -16545
009652 XDOT = -5042
918942
YDOT = -15135
056208 feet/sec YDOT = -4613
165132 meter/sec
ZDOT = 8980
921246 ZDOT = 2737
384796
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 17153
50238469
00016717 00000-0 10270-3 0 9034
2 25544 51
6373 111
5240 0004816 227
7520 132
3224 15
53983236 19467
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
50238469 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 111
5240 deg
Eccentricity:
0004816
Arg of perigee: 227
7520 deg
Mean anomaly: 132
3224 deg
Mean motion: 15
53983236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 295
Coasting Arc #5 (Orbit 1946)
---------------------------------------
Vector Time (GMT): 2017/153/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4295980
14 A = 6778264
60 meter
Y = 218460
37 meter E =
0010562
Z = -5247370
56 I = 51
96941
XDOT = -1772
041526 Wp = 95
34691
YDOT = 7364
144040 meter/sec RA = 110
33275 deg
ZDOT = -1147
106965 TA = 163
71142
MA = 163
67745
Ha = 220
631 n
mi
Hp = 216
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14094423
04 X = 4318707
25
Y = 716733
50 feet Y = 266628
33 meter
Z = -17215782
69 Z = -5226446
71
XDOT = -5813
784535 XDOT = -1848
685504
YDOT = 24160
577560 feet/sec YDOT = 7343
899400 meter/sec
ZDOT = -3763
474294 ZDOT = -1155
900740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1251830
14 X = 381557
83
Y = -14169348
68 feet Y = -4318817
48 meter
Z = -17123437
76 Z = -5219223
83
XDOT = 22890
840990 XDOT = 6977
128334
YDOT = 6607
128620 feet/sec YDOT = 2013
852803 meter/sec
ZDOT = -3803
510584 ZDOT = -1159
310026
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 17153
56669459
00016717 00000-0 10270-3 0 9048
2 25544 51
6390 111
2030 0004696 228
0644 132
0108 15
53968252 19477
Satellite: ISS
Catalog Number: 25544
Epoch time: 17153
56669459 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 111
2030 deg
Eccentricity:
0004696
Arg of perigee: 228
0644 deg
Mean anomaly: 132
0108 deg
Mean motion: 15
53968252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1947
Checksum: 309
Coasting Arc #6 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2017/154/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778988
58 A = 6777930
02 meter
Y = -1889389
40 meter E =
0001791
Z = 5300766
51 I = 51
97962
XDOT = 2568
249651 Wp = 217
40930
YDOT = -7187
860545 meter/sec RA = 105
35840 deg
ZDOT = -732
593304 TA = 239
54753
MA = 239
56522
Ha = 220
509 n
mi
Hp = 216
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12398256
48 X = -3783328
79
Y = -6198784
12 feet Y = -1931673
21 meter
Z = 17390966
25 Z = 5282398
55
XDOT = 8426
015915 XDOT = 2651
993922
YDOT = -23582
219636 feet/sec YDOT = -7158
672349 meter/sec
ZDOT = -2403
521339 ZDOT = -719
914488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6453841
50 X = -1967130
89
Y = 12381154
30 feet Y = 3773775
83 meter
Z = 17310180
34 Z = 5276142
97
XDOT = -22500
554458 XDOT = -6858
168999
YDOT = -8455
248761 feet/sec YDOT = -2577
159822 meter/sec
ZDOT = -2346
344639 ZDOT = -715
165846
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 17154
59563174
00016717 00000-0 10270-3 0 9050
2 25544 51
6397 106
0758 0004758 233
6745 126
3969 15
53986584 19633
Satellite: ISS
Catalog Number: 25544
Epoch time: 17154
59563174 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 106
0758 deg
Eccentricity:
0004758
Arg of perigee: 233
6745 deg
Mean anomaly: 126
3969 deg
Mean motion: 15
53986584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 357
Coasting Arc #7 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2017/155/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900606
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3209078
43 A = 6779900
50 meter
Y = 3501322
35 meter E =
0009401
Z = -4846943
50 I = 51
99399
XDOT = -3210
027104 Wp = 130
62732
YDOT = 6472
354669 meter/sec RA = 100
38504 deg
ZDOT = 2547
456205 TA = 164
35019
MA = 164
32111
Ha = 220
284 n
mi
Hp = 216
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10528472
54 X = 3193231
54
Y = 11487278
04 feet Y = 3537120
17 meter
Z = -15902045
59 Z = -4831392
86
XDOT = -10531
584987 XDOT = -3294
538520
YDOT = 21234
759414 feet/sec YDOT = 6435
985261 meter/sec
ZDOT = 8357
795949 ZDOT = 2531
657907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11522092
22 X = 3511933
71
Y = -10592830
75 feet Y = -3228694
81 meter
Z = -15833972
09 Z = -4826194
69
XDOT = 20426
798445 XDOT = 6226
088166
YDOT = 9818
162081 feet/sec YDOT = 2992
575802 meter/sec
ZDOT = 8286
947550 ZDOT = 2525
861613
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 17155
56025774
00016717 00000-0 10270-3 0 9068
2 25544 51
6398 101
2673 0004613 236
5576 123
5136 15
53980716 19783
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
56025774 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 101
2673 deg
Eccentricity:
0004613
Arg of perigee: 236
5576 deg
Mean anomaly: 123
5136 deg
Mean motion: 15
53980716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1978
Checksum: 325
Coasting Arc #8 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2017/155/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2413533
51 A = 6782612
32 meter
Y = -4803339
86 meter E =
0006377
Z = 4130431
07 I = 52
00360
XDOT = 3997
093302 Wp = 91
22155
YDOT = -5307
478574 meter/sec RA = 100
20855 deg
ZDOT = -3831
570011 TA = 38
14098
MA = 38
09587
Ha = 220
422 n
mi
Hp = 216
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7918417
03 X = -2379705
75
Y = -15758989
04 feet Y = -4830140
78 meter
Z = 13551283
04 Z = 4118788
57
XDOT = 13113
823170 XDOT = 4074
757935
YDOT = -17412
987449 feet/sec YDOT = -5262
345849 meter/sec
ZDOT = -12570
767753 ZDOT = -3811
964896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13682850
57 X = -4170532
85
Y = 11189076
04 feet Y = 3410430
38 meter
Z = 13500685
67 Z = 4115008
99
XDOT = -19015
710608 XDOT = -5795
988593
YDOT = -8171
864053 feet/sec YDOT = -2490
784163 meter/sec
ZDOT = -12483
306164 ZDOT = -3804
911719
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 17155
62456657
00016717 00000-0 10270-3 0 9074
2 25544 51
6402 100
9479 0004610 236
2036 123
8678 15
53967433 19790
Satellite: ISS
Catalog Number: 25544
Epoch time: 17155
62456657 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 100
9479 deg
Eccentricity:
0004610
Arg of perigee: 236
2036 deg
Mean anomaly: 123
8678 deg
Mean motion: 15
53967433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 328
Coasting Arc #9 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2017/156/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1722944
58 A = 6786220
04 meter
Y = 5894239
06 meter E =
0000269
Z = -2888697
93 I = 52
02124
XDOT = -4331
404149 Wp = 162
82391
YDOT = 3757
949930 meter/sec RA = 95
25125 deg
ZDOT = 5084
336456 TA = 164
49149
MA = 164
49067
Ha = 220
141 n
mi
Hp = 216
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5652705
32 X = 1670937
66
Y = 19338054
67 feet Y = 5913215
65 meter
Z = -9477355
41 Z = -2880454
11
XDOT = -14210
643533 XDOT = -4397
802136
YDOT = 12329
232053 feet/sec YDOT = 3709
141553 meter/sec
ZDOT = 16680
893883 ZDOT = 5063
134610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17499711
94 X = 5333912
20
Y = -10017142
31 feet Y = -3053224
98 meter
Z = -9441961
84 Z = -2877909
97
XDOT = 14568
371727 XDOT = 4440
439702
YDOT = 9815
968576 feet/sec YDOT = 2991
907222 meter/sec
ZDOT = 16586
630380 ZDOT = 5055
604940
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 17156
58918968
00016717 00000-0 10270-3 0 9089
2 25544 51
6408 96
1400 0004672 240
2878 119
7810 15
53990005 19943
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
58918968 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 96
1400 deg
Eccentricity:
0004672
Arg of perigee: 240
2878 deg
Mean anomaly: 119
7810 deg
Mean motion: 15
53990005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1994
Checksum: 336
Coasting Arc #10 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1544021
97 A = 6788979
33 meter
Y = 6466515
33 meter E =
0008909
Z = 1353474
75 I = 52
02828
XDOT = -4405
049084 Wp = 59
22985
YDOT = -2280
542008 meter/sec RA = 94
28647 deg
ZDOT = 5846
553484 TA = 315
42876
MA = 315
50037
Ha = 220
112 n
mi
Hp = 216
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5065688
89 X = -1622792
09
Y = 21215601
47 feet Y = 6448808
48 meter
Z = 4440533
95 Z = 1345783
51
XDOT = -14452
260775 XDOT = -4407
620128
YDOT = -7482
093202 feet/sec YDOT = -2329
817137 meter/sec
ZDOT = 19181
605919 ZDOT = 5825
148397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6553860
92 X = 1997616
81
Y = -20811537
73 feet Y = -6343356
70 meter
Z = 4405462
05 Z = 1342784
83
XDOT = 12505
675043 XDOT = 3811
729753
YDOT = 7995
540627 feet/sec YDOT = 2437
040783 meter/sec
ZDOT = 19087
478484 ZDOT = 5817
863442
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 17156
84642015
00016717 00000-0 10270-3 0 9096
2 25544 51
6380 94
8561 0004899 241
3140 118
7521 15
53986388 19981
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84642015 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 94
8561 deg
Eccentricity:
0004899
Arg of perigee: 241
3140 deg
Mean anomaly: 118
7521 deg
Mean motion: 15
53986388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 341
Coasting Arc #11 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2193952
56 A = 6786197
29 meter
Y = -5729468
19 meter E =
0004025
Z = -2894809
02 I = 52
02083
XDOT = 4014
903782 Wp = 183
45099
YDOT = 4103
116147 meter/sec RA = 89
33825 deg
ZDOT = -5081
652933 TA = 29
32564
MA = 29
30306
Ha = 220
005 n
mi
Hp = 216
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7198007
07 X = 2271919
66
Y = -18797467
81 feet Y = -5704497
68 meter
Z = -9497404
91 Z = -2883962
55
XDOT = 13172
256501 XDOT = 3993
407774
YDOT = 13461
667149 feet/sec YDOT = 4147
893857 meter/sec
ZDOT = -16672
089675 ZDOT = -5062
201292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8231075
78 X = -2508831
90
Y = 18393799
17 feet Y = 5606429
99 meter
Z = -9448510
22 Z = -2879905
91
XDOT = -11218
977112 XDOT = -3419
544224
YDOT = -13534
751104 feet/sec YDOT = -4125
392137 meter/sec
ZDOT = -16586
908002 ZDOT = -5055
689559
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 17157
81104048
00016717 00000-0 10270-3 0 9105
2 25544 51
6383 90
0481 0004803 245
8931 114
1720 15
53995686 20136
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81104048 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 90
0481 deg
Eccentricity:
0004803
Arg of perigee: 245
8931 deg
Mean anomaly: 114
1720 deg
Mean motion: 15
53995686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 295
Coasting Arc #12 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2795003
70 A = 6782510
20 meter
Y = 4589563
99 meter E =
0007022
Z = 4136514
16 I = 52
00723
XDOT = -3553
029345 Wp = 126
82348
YDOT = -5616
980761 meter/sec RA = 84
38090 deg
ZDOT = 3822
862654 TA = 283
89124
MA = 283
96934
Ha = 219
862 n
mi
Hp = 216
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9169959
66 X = -2866211
10
Y = 15057624
64 feet Y = 4557909
73 meter
Z = 13571240
70 Z = 4122764
32
XDOT = -11656
920423 XDOT = -3508
524555
YDOT = -18428
414571 feet/sec YDOT = -5656
464759 meter/sec
ZDOT = 12542
200308 ZDOT = 3805
710334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9779857
88 X = 2980900
68
Y = -14725519
75 feet Y = -4488338
42 meter
Z = 13509709
18 Z = 4117759
36
XDOT = 10012
554833 XDOT = 3051
826713
YDOT = 18113
750444 feet/sec YDOT = 5521
071135 meter/sec
ZDOT = 12467
447251 ZDOT = 3800
077922
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 17158
83996426
00016717 00000-0 10270-3 0 9118
2 25544 51
6383 84
9193 0004904 249
1860 110
8767 15
54001547 20294
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
83996426 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 84
9193 deg
Eccentricity:
0004904
Arg of perigee: 249
1860 deg
Mean anomaly: 110
8767 deg
Mean motion: 15
54001547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 326
Coasting Arc #13 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3380261
86 A = 6779268
47 meter
Y = -3122143
12 meter E =
0007803
Z = -4985545
80 I = 51
99188
XDOT = 2986
514278 Wp = 76
33815
YDOT = 6711
117112 meter/sec RA = 79
41470 deg
ZDOT = -2178
930659 TA = 172
51063
MA = 172
49897
Ha = 219
860 n
mi
Hp = 216
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11090097
97 X = 3439140
87
Y = -10243251
70 feet Y = -3084012
86 meter
Z = -16356777
55 Z = -4968982
75
XDOT = 9798
275190 XDOT = 2921
831137
YDOT = 22018
100761 feet/sec YDOT = 6744
152962 meter/sec
ZDOT = -7148
722635 ZDOT = -2164
579143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11377368
83 X = -3467822
02
Y = 10043690
57 feet Y = 3061316
88 meter
Z = -16283071
23 Z = -4963080
11
XDOT = -8718
701043 XDOT = -2657
460078
YDOT = -21359
643919 feet/sec YDOT = -6510
419467 meter/sec
ZDOT = -7086
545568 ZDOT = -2159
979089
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 17159
80457915
00016717 00000-0 10270-3 0 9122
2 25544 51
6380 80
1120 0004664 250
4267 109
6382 15
54001105 20444
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
80457915 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 80
1120 deg
Eccentricity:
0004664
Arg of perigee: 250
4267 deg
Mean anomaly: 109
6382 deg
Mean motion: 15
54001105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 280
Coasting Arc #14 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3526092
96 A = 6778593
39 meter
Y = 2687402
37 meter E =
0004570
Z = 5129344
05 I = 51
99184
XDOT = -2821
991161 Wp = 186
64896
YDOT = -6926
723136 meter/sec RA = 77
97348 deg
ZDOT = 1684
893514 TA = 247
13166
MA = 247
17992
Ha = 219
806 n
mi
Hp = 216
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11568546
47 X = -3580798
24
Y = 8816936
93 feet Y = 2647664
64 meter
Z = 16828556
61 Z = 5112082
70
XDOT = -9258
501185 XDOT = -2752
509463
YDOT = -22725
469607 feet/sec YDOT = -6957
892287 meter/sec
ZDOT = 5527
865860 ZDOT = 1671
352822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11344002
98 X = -3457652
11
Y = -9244423
45 feet Y = -2817700
27 meter
Z = 16751841
48 Z = 5105961
28
XDOT = 19186
511437 XDOT = 5848
048686
YDOT = -13607
680718 feet/sec YDOT = -4147
621083 meter/sec
ZDOT = 5469
312309 ZDOT = 1667
046392
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 17160
12611507
00016717 00000-0 10270-3 0 9139
2 25544 51
6417 78
5112 0004983 251
2876 108
7736 15
54018122 20491
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12611507 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 78
5112 deg
Eccentricity:
0004983
Arg of perigee: 251
2876 deg
Mean anomaly: 108
7736 deg
Mean motion: 15
54018122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 294
Coasting Arc #15 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060076
65 A = 6777780
60 meter
Y = -1005043
70 meter E =
0010169
Z = -5341976
76 I = 51
98066
XDOT = 2088
997059 Wp = 99
08023
YDOT = 7367
995025 meter/sec RA = 72
99936 deg
ZDOT = 200
249131 TA = 172
82843
MA = 172
81387
Ha = 219
633 n
mi
Hp = 216
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13320461
44 X = 4096962
46
Y = -3297387
46 feet Y = -959434
16 meter
Z = -17526170
46 Z = -5322164
55
XDOT = 6853
664892 XDOT = 2005
478228
YDOT = 24173
212023 feet/sec YDOT = 7390
888593 meter/sec
ZDOT = 656
985339 ZDOT = 210
195124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6611008
09 X = 2015035
27
Y = 12151866
31 feet Y = 3703888
85 meter
Z = -17438486
89 Z = -5315250
80
XDOT = -20746
422418 XDOT = -6323
509553
YDOT = 12296
489316 feet/sec YDOT = 3747
969943 meter/sec
ZDOT = 699
569414 ZDOT = 213
228757
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 17161
09072529
00016717 00000-0 10270-3 0 9142
2 25544 51
6413 73
7040 0004957 256
0683 103
9919 15
53987054 20649
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09072529 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 73
7040 deg
Eccentricity:
0004957
Arg of perigee: 256
0683 deg
Mean anomaly: 103
9919 deg
Mean motion: 15
53987054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 315
Coasting Arc #16 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507175
93 A = 6779027
80 meter
Y = -683785
26 meter E =
0002553
Z = 5017888
11 I = 51
97553
XDOT = -1197
760940 Wp = 4
73380
YDOT = -7286
113773 meter/sec RA = 68
02532 deg
ZDOT = -2066
178655 TA = 105
28382
MA = 105
25560
Ha = 219
581 n
mi
Hp = 216
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14787322
59 X = -4523569
23
Y = -2243389
95 feet Y = -734279
95 meter
Z = 16462887
50 Z = 4995953
62
XDOT = -3929
661878 XDOT = -1106
160155
YDOT = -23904
572746 feet/sec YDOT = -7298
995471 meter/sec
ZDOT = -6778
801362 ZDOT = -2071
775625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1881824
96 X = -573580
25
Y = -14944319
65 feet Y = -4555028
63 meter
Z = 16366136
32 Z = 4988398
35
XDOT = 20865
622304 XDOT = 6359
841678
YDOT = -10086
016543 feet/sec YDOT = -3074
217842 meter/sec
ZDOT = -6802
179349 ZDOT = -2073
304265
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 17162
11963589
00016717 00000-0 10270-3 0 9152
2 25544 51
6420 68
5763 0004936 260
9389 99
1206 15
54040961 20806
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
11963589 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 68
5763 deg
Eccentricity:
0004936
Arg of perigee: 260
9389 deg
Mean anomaly: 99
1206 deg
Mean motion: 15
54040961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 322
Coasting Arc #17 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829232
77 A = 6782217
42 meter
Y = 2243379
47 meter E =
0004107
Z = -4204927
91 I = 51
97195
XDOT = 134
549192 Wp = 138
40240
YDOT = 6695
207982 meter/sec RA = 63
05690 deg
ZDOT = 3725
592137 TA = 169
71332
MA = 169
70491
Ha = 219
485 n
mi
Hp = 216
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15843939
54 X = 4824213
31
Y = 7360168
86 feet Y = 2297355
76 meter
Z = -13795695
23 Z = -4181480
81
XDOT = 441
434356 XDOT = 41
574489
YDOT = 21965
905454 feet/sec YDOT = 6696
192211 meter/sec
ZDOT = 12223
071316 ZDOT = 3726
020883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2462999
82 X = -750722
35
Y = 17377323
74 feet Y = 5296608
27 meter
Z = -13692551
42 Z = -4173489
67
XDOT = -19666
795567 XDOT = -5994
439289
YDOT = 6846
605148 feet/sec YDOT = 2086
845249 meter/sec
ZDOT = 12223
720560 ZDOT = 3725
790027
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
08423919
00016717 00000-0 10270-3 0 9168
2 25544 51
6408 63
7693 0004634 264
1474 95
9151 15
54036439 20951
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
08423919 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 63
7693 deg
Eccentricity:
0004634
Arg of perigee: 264
1474 deg
Mean anomaly: 95
9151 deg
Mean motion: 15
54036439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 323
Coasting Arc #18 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4949391
92 A = 6785898
43 meter
Y = -3566819
07 meter E =
0008485
Z = 2961953
70 I = 51
96898
XDOT = 1087
370267 Wp = 102
68611
YDOT = -5690
240482 meter/sec RA = 58
09661 deg
ZDOT = -5024
994379 TA = 43
63867
MA = 43
57160
Ha = 219
414 n
mi
Hp = 216
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16238162
47 X = -4923526
67
Y = -11702162
30 feet Y = -3622022
30 meter
Z = 9717695
85 Z = 2937973
43
XDOT = 3567
487751 XDOT = 1175
328150
YDOT = -18668
767987 feet/sec YDOT = -5677
588284 meter/sec
ZDOT = -16486
202032 ZDOT = -5019
499415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6188529
67 X = 1886263
84
Y = -19088088
24 feet Y = -5818049
30 meter
Z = 9612446
27 Z = 2929873
62
XDOT = 17511
548891 XDOT = 5337
520102
YDOT = -2629
182038 feet/sec YDOT = -801
374685 meter/sec
ZDOT = -16460
865859 ZDOT = -5017
271914
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
11314276
00016717 00000-0 10270-3 0 9179
2 25544 51
6410 58
6411 0004841 269
6193 90
4405 15
54056797 21113
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
11314276 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 58
6411 deg
Eccentricity:
0004841
Arg of perigee: 269
6193 deg
Mean anomaly: 90
4405 deg
Mean motion: 15
54056797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 296
Coasting Arc #19 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2017/165/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4818227
81 A = 6788784
93 meter
Y = 4555213
13 meter E =
0007144
Z = -1435389
55 I = 51
96076
XDOT = -2407
389272 Wp = 4
13107
YDOT = 4376
755162 meter/sec RA = 53
14394 deg
ZDOT = 5817
396252 TA = 340
28559
MA = 340
31319
Ha = 219
496 n
mi
Hp = 216
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15807834
02 X = 4773904
52
Y = 14944924
98 feet Y = 4608846
17 meter
Z = -4709283
30 Z = -1412091
23
XDOT = -7898
258765 XDOT = -2484
410361
YDOT = 14359
432947 feet/sec YDOT = 4349
402732 meter/sec
ZDOT = 19085
945709 ZDOT = 5805
515399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9079800
13 X = -2767523
08
Y = 19792583
36 feet Y = 6032779
41 meter
Z = -4607235
78 Z = -1404285
47
XDOT = -14731
606386 XDOT = -4490
193626
YDOT = -2334
561395 feet/sec YDOT = -711
574313 meter/sec
ZDOT = 19032
644652 ZDOT = 5801
150090
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
07773751
00016717 00000-0 10270-3 0 9183
2 25544 51
6414 53
8333 0004696 274
0527 86
0089 15
54027280 21266
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
07773751 = yrday
fracday
Element set: 918
Inclination: 51
6414 deg
RA of node: 53
8333 deg
Eccentricity:
0004696
Arg of perigee: 274
0527 deg
Mean anomaly: 86
0089 deg
Mean motion: 15
54027280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 313
Coasting Arc #20 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5029216
24 A = 6781124
06 meter
Y = 661338
31 meter E =
0004910
Z = -4505377
37 I = 51
92862
XDOT = 2029
149151 Wp = 122
86693
YDOT = 6641
433813 meter/sec RA = 51
57577 deg
ZDOT = 3239
926982 TA = 179
61687
MA = 179
61649
Ha = 219
500 n
mi
Hp = 216
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16500053
29 X = 5043332
06
Y = 2169745
11 feet Y = 717657
88 meter
Z = -14781421
80 Z = -4480912
69
XDOT = 6657
313486 XDOT = 1938
994152
YDOT = 21789
481015 feet/sec YDOT = 6663
620659 meter/sec
ZDOT = 10629
681698 ZDOT = 3249
565758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13774880
58 X = 4198583
60
Y = -9507436
92 feet Y = -2897866
77 meter
Z = -14673489
41 Z = -4472479
57
XDOT = 18794
788118 XDOT = 5728
651418
YDOT = 10761
396531 feet/sec YDOT = 3280
073663 meter/sec
ZDOT = 10671
001325 ZDOT = 3252
521204
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
39926870
00016717 00000-0 10270-3 0 9191
2 25544 51
6409 52
2314 0004744 277
4199 82
6415 15
54035870 21313
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39926870 = yrday
fracday
Element set: 919
Inclination: 51
6409 deg
RA of node: 52
2314 deg
Eccentricity:
0004744
Arg of perigee: 277
4199 deg
Mean anomaly: 82
6415 deg
Mean motion: 15
54035870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 318
Coasting Arc #21 (Orbit 2145)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 923344
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5531094
34 A = 6784868
81 meter
Y = -1999625
64 meter E =
0007897
Z = 3376710
25 I = 51
92008
XDOT = -674
170545 Wp = 84
83734
YDOT = -6042
617474 meter/sec RA = 46
61018 deg
ZDOT = -4672
557506 TA = 55
92505
MA = 55
85012
Ha = 219
591 n
mi
Hp = 216
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18146634
98 X = -5524725
28
Y = -6560451
58 feet Y = -2061442
83 meter
Z = 11078445
70 Z = 3349857
23
XDOT = -2211
845619 XDOT = -583
853372
YDOT = -19824
860480 feet/sec YDOT = -6049
651018 meter/sec
ZDOT = -15329
913078 ZDOT = -4675
613683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17792079
96 X = -5423025
97
Y = 7641157
89 feet Y = 2329024
93 meter
Z = 10960220
89 Z = 3340675
33
XDOT = -14518
412327 XDOT = -4425
212077
YDOT = -11751
118742 feet/sec YDOT = -3581
740992 meter/sec
ZDOT = -15342
265305 ZDOT = -4676
322465
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
42816407
00016717 00000-0 10270-3 0 9202
2 25544 51
6408 47
1039 0004782 281
4276 78
6339 15
54035347 21467
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42816407 = yrday
fracday
Element set: 920
Inclination: 51
6408 deg
RA of node: 47
1039 deg
Eccentricity:
0004782
Arg of perigee: 281
4276 deg
Mean anomaly: 78
6339 deg
Mean motion: 15
54035347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2146
Checksum: 313
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