[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 15th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 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
166/13:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
2
170/05:52:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
171/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2016/165/12:39:27
081
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4375114
52 A = 6777329
79 meter
Y = 1074160
29 meter E =
0012606
Z = -5074648
40 I = 51
98716
XDOT = 383
112343 Wp = 102
64716
YDOT = 7410
083293 meter/sec RA = 75
49392 deg
ZDOT = 1900
090533 TA = 185
69827
MA = 185
71263
Ha = 220
237 n
mi
Hp = 214
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14354050
28 X = 4387428
35
Y = 3524147
94 feet Y = 1123154
97 meter
Z = -16649108
92 Z = -5053365
14
XDOT = 1256
930260 XDOT = 290
992613
YDOT = 24311
296894 feet/sec YDOT = 7413
852296 meter/sec
ZDOT = 6233
892825 ZDOT = 1901
728409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3201624
93 X = 975855
28
Y = -14535517
95 feet Y = -4430425
87 meter
Z = -16556555
25 Z = -5046438
04
XDOT = 23219
046781 XDOT = 7077
165459
YDOT = -1988
040888 feet/sec YDOT = -605
954863 meter/sec
ZDOT = 6239
582754 ZDOT = 1901
824823
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 16165
54018716
00016717 00000-0 10270-3 0 9008
2 25544 51
6441 76
2279 0000507 322
3584 37
7533 15
54548251 4412
Satellite: ISS
Catalog Number: 25544
Epoch time: 16165
54018716 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 76
2279 deg
Eccentricity:
0000507
Arg of perigee: 322
3584 deg
Mean anomaly: 37
7533 deg
Mean motion: 15
54548251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 294
Coasting Arc #2 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2016/166/12:39:27
081
Vector Time (MET): N/A
Weight (LBS) : 923955
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4485806
13 A = 6780743
77 meter
Y = -2888142
73 meter E =
0010287
Z = 4178681
80 I = 51
98925
XDOT = 766
248429 Wp = 72
74358
YDOT = -6643
616625 meter/sec RA = 70
52147 deg
ZDOT = -3758
670701 TA = 55
75627
MA = 55
65887
Ha = 220
349 n
mi
Hp = 214
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14717211
73 X = -4473475
14
Y = -9475533
91 feet Y = -2938237
40 meter
Z = 13709585
95 Z = 4156920
47
XDOT = 2513
938414 XDOT = 858
740164
YDOT = -21796
642471 feet/sec YDOT = -6634
530467 meter/sec
ZDOT = -12331
596787 ZDOT = -3754
724327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8884640
21 X = -2708038
34
Y = 15166454
16 feet Y = 4622735
23 meter
Z = 13615309
30 Z = 4149946
28
XDOT = -20776
976194 XDOT = -6332
822344
YDOT = -1086
208710 feet/sec YDOT = -331
076415 meter/sec
ZDOT = -12313
084117 ZDOT = -3753
028039
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 16166
56874177
00016717 00000-0 10270-3 0 9013
2 25544 51
6436 71
0983 0000518 335
5469 24
5659 15
54566340 4570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
56874177 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 71
0983 deg
Eccentricity:
0000518
Arg of perigee: 335
5469 deg
Mean anomaly: 24
5659 deg
Mean motion: 15
54566340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 327
Coasting Arc #3 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2016/166/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4127381
47 A = 6784146
88 meter
Y = 4423020
40 meter E =
0004370
Z = -3071238
68 I = 52
00054
XDOT = -2158
765911 Wp = 63
89449
YDOT = 5443
334693 meter/sec RA = 70
34785 deg
ZDOT = 4945
359812 TA = 261
04427
MA = 261
09374
Ha = 220
233 n
mi
Hp = 214
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13541277
78 X = 4092534
22
Y = 14511221
77 feet Y = 4468980
93 meter
Z = -10076242
39 Z = -3051273
06
XDOT = -7082
565326 XDOT = -2243
496754
YDOT = 17858
709624 feet/sec YDOT = 5418
719772 meter/sec
ZDOT = 16224
933767 ZDOT = 4934
667654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10516264
30 X = 3205357
36
Y = -16884270
54 feet Y = -5146325
66 meter
Z = -9990095
86 Z = -3044981
22
XDOT = 17877
553382 XDOT = 5449
078271
YDOT = 1577
467662 feet/sec YDOT = 480
812143 meter/sec
ZDOT = 16177
256138 ZDOT = 4930
827671
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 16166
56874098
00016717 00000-0 10270-3 0 9026
2 25544 51
6439 71
0981 0000614 324
1422 35
9690 15
54557629 4572
Satellite: ISS
Catalog Number: 25544
Epoch time: 16166
56874098 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 71
0981 deg
Eccentricity:
0000614
Arg of perigee: 324
1422 deg
Mean anomaly: 35
9690 deg
Mean motion: 15
54557629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 322
Coasting Arc #4 (Orbit 472)
---------------------------------------
Vector Time (GMT): 2016/167/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3698807
97 A = 6787365
82 meter
Y = -5517258
92 meter E =
0013401
Z = 1364211
29 I = 51
99972
XDOT = 3332
023445 Wp = 119
28366
YDOT = -3687
540673 meter/sec RA = 65
39553 deg
ZDOT = -5842
620983 TA = 45
92482
MA = 45
81457
Ha = 220
271 n
mi
Hp = 214
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12135196
75 X = -3643464
49
Y = -18101243
18 feet Y = -5558312
14 meter
Z = 4475758
82 Z = 1346377
19
XDOT = 10931
835450 XDOT = 3401
391940
YDOT = -12098
230555 feet/sec YDOT = -3649
891365 meter/sec
ZDOT = -19168
704011 ZDOT = -5826
266582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14072625
62 X = -4289336
29
Y = 16660110
38 feet Y = 5078001
65 meter
Z = 4399130
81 Z = 1340855
07
XDOT = -13452
345431 XDOT = -4100
274887
YDOT = -6288
220907 feet/sec YDOT = -1916
649733 meter/sec
ZDOT = -19096
686799 ZDOT = -5820
670136
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 16167
59728769
00016717 00000-0 10270-3 0 9034
2 25544 51
6442 65
9684 0000440 321
4350 38
6771 15
54542539 4737
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
59728769 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 65
9684 deg
Eccentricity:
0000440
Arg of perigee: 321
4350 deg
Mean anomaly: 38
6771 deg
Mean motion: 15
54542539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 473
Checksum: 325
Coasting Arc #5 (Orbit 488)
---------------------------------------
Vector Time (GMT): 2016/168/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3003506
95 A = 6787835
55 meter
Y = 6060739
66 meter E =
0012964
Z = 481838
10 I = 51
98821
XDOT = -4436
490772 Wp = 47
09009
YDOT = 1712
687719 meter/sec RA = 60
44671 deg
ZDOT = 6018
350225 TA = 318
08407
MA = 318
18324
Ha = 220
105 n
mi
Hp = 214
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9854025
44 X = 2933170
43
Y = 19884316
49 feet Y = 6093933
55 meter
Z = 1580833
68 Z = 496258
31
XDOT = -14555
415918 XDOT = -4484
547526
YDOT = 5619
054197 feet/sec YDOT = 1662
806585 meter/sec
ZDOT = 19745
243520 ZDOT = 5996
682147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16164969
94 X = 4927082
84
Y = -15198123
74 feet Y = -4632388
12 meter
Z = 1642460
38 Z = 500621
92
XDOT = 8537
451555 XDOT = 2602
215234
YDOT = 11236
070300 feet/sec YDOT = 3424
754228 meter/sec
ZDOT = 19650
457679 ZDOT = 5989
459501
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 16168
62582068
00016717 00000-0 10270-3 0 9040
2 25544 51
6446 60
8374 0000698 319
3939 40
7162 15
54606914 4898
Satellite: ISS
Catalog Number: 25544
Epoch time: 16168
62582068 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 60
8374 deg
Eccentricity:
0000698
Arg of perigee: 319
3939 deg
Mean anomaly: 40
7162 deg
Mean motion: 15
54606914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 489
Checksum: 332
Coasting Arc #6 (Orbit 503)
---------------------------------------
Vector Time (GMT): 2016/169/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 912263
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1981417
16 A = 6785759
56 meter
Y = -6065688
10 meter E =
0005102
Z = -2304932
67 I = 51
96333
XDOT = 5383
533832 Wp = 134
44436
YDOT = 307
576966 meter/sec RA = 55
49549 deg
ZDOT = -5448
224577 TA = 71
10809
MA = 71
05278
Ha = 220
133 n
mi
Hp = 214
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6500712
47 X = -1902245
40
Y = -19900551
52 feet Y = -6087402
67 meter
Z = -7562115
06 Z = -2314366
41
XDOT = 17662
512573 XDOT = 5406
159637
YDOT = 1009
110781 feet/sec YDOT = 367
906396 meter/sec
ZDOT = -17874
752548 ZDOT = -5422
017522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16958650
89 X = -5168996
79
Y = 12251148
39 feet Y = 3734150
03 meter
Z = -7601994
50 Z = -2317087
92
XDOT = -3606
729210 XDOT = -1099
331063
YDOT = -15991
237807 feet/sec YDOT = -4874
129284 meter/sec
ZDOT = -17760
592233 ZDOT = -5413
428513
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 16169
59006505
00016717 00000-0 10270-3 0 9055
2 25544 51
6436 56
0278 0000702 318
3518 41
7581 15
54572044 5045
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
59006505 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 56
0278 deg
Eccentricity:
0000702
Arg of perigee: 318
3518 deg
Mean anomaly: 41
7581 deg
Mean motion: 15
54572044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 504
Checksum: 294
Coasting Arc #7 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1358920
22 A = 6777789
86 meter
Y = 4489804
71 meter E =
0006305
Z = 4888505
68 I = 51
92148
XDOT = -5811
116285 Wp = 118
11364
YDOT = -4390
020713 meter/sec RA = 52
10431 deg
ZDOT = 2411
328367 TA = 308
32385
MA = 308
38052
Ha = 220
182 n
mi
Hp = 214
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4458399
68 X = -1432771
76
Y = 14730330
43 feet Y = 4474194
79 meter
Z = 16038404
47 Z = 4881725
56
XDOT = -19065
342143 XDOT = -5773
307347
YDOT = -14402
955096 feet/sec YDOT = -4454
793399 meter/sec
ZDOT = 7911
182306 ZDOT = 2383
190484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6032054
39 X = -1838570
18
Y = 14193337
60 feet Y = 4326129
30 meter
Z = 16007931
40 Z = 4879217
49
XDOT = -16522
008791 XDOT = -5035
908279
YDOT = -15826
523417 feet/sec YDOT = -4823
924338 meter/sec
ZDOT = 7789
445146 ZDOT = 2374
222881
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 16170
29717233
00016717 00000-0 10270-3 0 9062
2 25544 51
6407 52
5000 0000612 328
4979 31
6137 15
54618336 5152
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29717233 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 52
5000 deg
Eccentricity:
0000612
Arg of perigee: 328
4979 deg
Mean anomaly: 31
6137 deg
Mean motion: 15
54618336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 288
Coasting Arc #8 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2803270
66 A = 6775985
73 meter
Y = -3125414
11 meter E =
0014661
Z = -5331239
13 I = 51
89536
XDOT = 5398
308274 Wp = 85
11271
YDOT = 5421
833789 meter/sec RA = 47
11924 deg
ZDOT = -339
574591 TA = 181
65466
MA = 181
65951
Ha = 220
175 n
mi
Hp = 214
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9197082
21 X = 2863908
45
Y = -10253983
29 feet Y = -3093726
26 meter
Z = -17490942
04 Z = -5317474
65
XDOT = 17710
985152 XDOT = 5338
928268
YDOT = 17788
168598 feet/sec YDOT = 5481
869301 meter/sec
ZDOT = -1114
089866 ZDOT = -313
494296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10140851
99 X = 3090931
69
Y = -9434576
93 feet Y = -2875659
05 meter
Z = -17430301
98 Z = -5312756
04
XDOT = 15467
704506 XDOT = 4714
556334
YDOT = 18478
475105 feet/sec YDOT = 5632
239212 meter/sec
ZDOT = -1001
541861 ZDOT = -305
269959
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 16171
26140275
00016717 00000-0 10270-3 0 9077
2 25544 51
6412 47
6897 0000591 339
6293 20
4836 15
54610225 5304
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
26140275 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 47
6897 deg
Eccentricity:
0000591
Arg of perigee: 339
6293 deg
Mean anomaly: 20
4836 deg
Mean motion: 15
54610225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 295
Coasting Arc #9 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5685731
00 A = 6784420
35 meter
Y = -2312886
85 meter E =
0012984
Z = 2876404
77 I = 51
91141
XDOT = -244
437107 Wp = 97
86839
YDOT = -5741
507606 meter/sec RA = 43
68428 deg
ZDOT = -5082
023312 TA = 49
50685
MA = 49
39378
Ha = 220
150 n
mi
Hp = 214
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18653973
09 X = -5673417
50
Y = -7588211
44 feet Y = -2376400
05 meter
Z = 9437023
52 Z = 2848814
41
XDOT = -801
959013 XDOT = -155
529633
YDOT = -18836
967212 feet/sec YDOT = -5743
743201 meter/sec
ZDOT = -16673
304831 ZDOT = -5082
995634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15321797
74 X = 4670083
95
Y = -13154482
51 feet Y = -4009486
27 meter
Z = 9317251
83 Z = 2839898
36
XDOT = 16101
832363 XDOT = 4907
838504
YDOT = 6900
997560 feet/sec YDOT = 2103
424056 meter/sec
ZDOT = -16676
347026 ZDOT = -5082
950573
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 16171
96849798
00016717 00000-0 10270-3 0 9081
2 25544 51
6442 44
1615 0000475 316
1340 43
9776 15
54640578 5410
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
96849798 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 44
1615 deg
Eccentricity:
0000475
Arg of perigee: 316
1340 deg
Mean anomaly: 43
9776 deg
Mean motion: 15
54640578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 325
Coasting Arc #10 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5731244
82 A = 6787432
92 meter
Y = 3441100
23 meter E =
0009660
Z = -1148731
97 I = 51
89646
XDOT = -1607
928858 Wp = 34
04617
YDOT = 4634
959339 meter/sec RA = 38
72557 deg
ZDOT = 5893
745688 TA = 313
52534
MA = 313
60556
Ha = 220
171 n
mi
Hp = 214
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18803296
67 X = 5697919
66
Y = 11289698
91 feet Y = 3505004
66 meter
Z = -3768805
67 Z = -1120971
48
XDOT = -5275
357145 XDOT = -1688
267866
YDOT = 15206
559511 feet/sec YDOT = 4616
528323 meter/sec
ZDOT = 19336
435984 ZDOT = 5885
740342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18462094
05 X = -5627246
27
Y = 11877056
33 feet Y = 3620126
77 meter
Z = -3648531
11 Z = -1112072
28
XDOT = -10375
902662 XDOT = -3162
575131
YDOT = -10232
674044 feet/sec YDOT = -3118
919049 meter/sec
ZDOT = 19300
573119 ZDOT = 5882
814687
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 16172
93271384
00016717 00000-0 10270-3 0 9090
2 25544 51
6433 39
3519 0000672 326
0739 34
0371 15
54599335 5562
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
93271384 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 39
3519 deg
Eccentricity:
0000672
Arg of perigee: 326
0739 deg
Mean anomaly: 34
0371 deg
Mean motion: 15
54599335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 316
Coasting Arc #11 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5250832
33 A = 6787535
59 meter
Y = -4226736
02 meter E =
0009829
Z = -757769
39 I = 51
87095
XDOT = 3506
052745 Wp = 139
53529
YDOT = -3294
036554 meter/sec RA = 33
77055 deg
ZDOT = -5971
491783 TA = 48
62931
MA = 48
54482
Ha = 220
069 n
mi
Hp = 213
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17227140
18 X = -5199496
75
Y = -13867244
16 feet Y = -4285167
18 meter
Z = -2486120
03 Z = -783152
42
XDOT = 11502
797719 XDOT = 3571
633703
YDOT = -10807
206542 feet/sec YDOT = -3254
461987 meter/sec
ZDOT = -19591
508476 ZDOT = -5954
301525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19894554
90 X = 6063860
33
Y = -9629319
18 feet Y = -2935016
49 meter
Z = -2595864
02 Z = -791219
35
XDOT = 4097
163744 XDOT = 1248
815509
YDOT = 13683
121349 feet/sec YDOT = 4170
615387 meter/sec
ZDOT = -19515
890689 ZDOT = -5948
443482
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 16173
96120498
00016717 00000-0 10270-3 0 9105
2 25544 51
6425 34
2215 0000485 328
7539 31
3585 15
54653568 5723
Satellite: ISS
Catalog Number: 25544
Epoch time: 16173
96120498 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 34
2215 deg
Eccentricity:
0000485
Arg of perigee: 328
7539 deg
Mean anomaly: 31
3585 deg
Mean motion: 15
54653568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 312
Coasting Arc #12 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4261036
73 A = 6785002
64 meter
Y = 4620293
02 meter E =
0013600
Z = 2538561
02 I = 51
83571
XDOT = -5215
391540 Wp = 73
54889
YDOT = 1886
419540 meter/sec RA = 28
80898 deg
ZDOT = 5301
077812 TA = 314
89644
MA = 315
00676
Ha = 220
076 n
mi
Hp = 213
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13979779
28 X = 4196723
62
Y = 15158441
67 feet Y = 4667582
83 meter
Z = 8328612
28 Z = 2559104
33
XDOT = -17110
864632 XDOT = -5261
848490
YDOT = 6189
040485 feet/sec YDOT = 1827
837088 meter/sec
ZDOT = 17391
987572 ZDOT = 5275
630352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19549825
09 X = -5958786
69
Y = 6444676
18 feet Y = 1964337
30 meter
Z = 8417176
08 Z = 2565555
27
XDOT = 1923
602819 XDOT = 586
314139
YDOT = -16818
095347 feet/sec YDOT = -5126
155462 meter/sec
ZDOT = 17280
676491 ZDOT = 5267
150195
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
98968740
00016717 00000-0 10270-3 0 9119
2 25544 51
6429 29
0901 0000571 340
1614 19
9517 15
54657206 5886
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
98968740 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 29
0901 deg
Eccentricity:
0000571
Arg of perigee: 340
1614 deg
Mean anomaly: 19
9517 deg
Mean motion: 15
54657206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 319
Coasting Arc #13 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2783487
14 A = 6780826
77 meter
Y = -4696918
49 meter E =
0007266
Z = -4029207
28 I = 51
79307
XDOT = 6549
497300 Wp = 66
58620
YDOT = -500
390160 meter/sec RA = 23
83565 deg
ZDOT = -3944
080616 TA = 162
49803
MA = 162
47298
Ha = 220
121 n
mi
Hp = 213
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9132175
66 X = -2711186
18
Y = -15409837
58 feet Y = -4727640
56 meter
Z = -13219183
98 Z = -4042553
59
XDOT = 21487
852034 XDOT = 6573
764478
YDOT = -1641
700001 feet/sec YDOT = -427
013160 meter/sec
ZDOT = -12939
897034 ZDOT = -3912
206212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17734226
32 X = 5405392
18
Y = -2200455
13 feet Y = -670698
72 meter
Z = -13276361
15 Z = -4046634
88
XDOT = -7198
430737 XDOT = -2194
081689
YDOT = 19163
305102 feet/sec YDOT = 5840
975395 meter/sec
ZDOT = -12800
869261 ZDOT = -3901
704951
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
95388352
00016717 00000-0 10270-3 0 9123
2 25544 51
6427 24
2800 0000608 350
7928 9
3213 15
54666477 6039
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
95388352 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 24
2800 deg
Eccentricity:
0000608
Arg of perigee: 350
7928 deg
Mean anomaly: 9
3213 deg
Mean motion: 15
54666477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 306
Coasting Arc #14 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 971162
19 A = 6777111
79 meter
Y = 4483766
55 meter E =
0005611
Z = 4984756
36 I = 51
75048
XDOT = -7339
486129 Wp = 118
09214
YDOT = -753
442840 meter/sec RA = 18
84805 deg
ZDOT = 2103
261029 TA = 311
45211
MA = 311
50029
Ha = 220
073 n
mi
Hp = 213
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3186227
66 X = 896737
85
Y = 14710520
18 feet Y = 4494210
09 meter
Z = 16354187
53 Z = 4989293
67
XDOT = -24079
678901 XDOT = -7340
732094
YDOT = -2471
925329 feet/sec YDOT = -835
525047 meter/sec
ZDOT = 6900
462694 ZDOT = 2067
604879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14778073
06 X = -4504356
67
Y = -2746600
90 feet Y = -837163
95 meter
Z = 16373015
63 Z = 4990495
16
XDOT = 11260
715208 XDOT = 3432
265995
YDOT = -20293
027376 feet/sec YDOT = -6185
314744 meter/sec
ZDOT = 6745
222863 ZDOT = 2055
943929
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
98235215
00016717 00000-0 10270-3 0 9137
2 25544 51
6421 19
1493 0000654 349
7804 10
3336 15
54690309 6192
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
98235215 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 19
1493 deg
Eccentricity:
0000654
Arg of perigee: 349
7804 deg
Mean anomaly: 10
3336 deg
Mean motion: 15
54690309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 619
Checksum: 303
Coasting Arc #15 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2016/177/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1023758
74 A = 6775772
12 meter
Y = -4077663
65 meter E =
0014811
Z = -5326497
86 I = 51
71615
XDOT = 7432
797981 Wp = 87
19462
YDOT = 1845
757371 meter/sec RA = 13
84950 deg
ZDOT = 16
331598 TA = 182
95665
MA = 182
96542
Ha = 220
129 n
mi
Hp = 213
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3358788
52 X = 1095153
73
Y = -13378161
57 feet Y = -4065815
64 meter
Z = -17475386
67 Z = -5321351
68
XDOT = 24385
820146 XDOT = 7411
526507
YDOT = 6055
634418 feet/sec YDOT = 1928
756934 meter/sec
ZDOT = 53
581359 ZDOT = 52
386479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11194972
77 X = 3412227
70
Y = 8108183
61 feet Y = 2471374
36 meter
Z = -17452098
72 Z = -5319399
69
XDOT = -13933
581085 XDOT = -4246
955515
YDOT = 19685
518286 feet/sec YDOT = 6000
145974 meter/sec
ZDOT = 210
320484 ZDOT = 64
105683
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
94653578
00016717 00000-0 10270-3 0 9141
2 25544 51
6433 14
3388 0000740 353
6343 6
4801 15
54673234 6341
Satellite: ISS
Catalog Number: 25544
Epoch time: 16177
94653578 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 14
3388 deg
Eccentricity:
0000740
Arg of perigee: 353
6343 deg
Mean anomaly: 6
4801 deg
Mean motion: 15
54673234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 306
Coasting Arc #16 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2016/178/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2985741
38 A = 6777183
67 meter
Y = 3507422
51 meter E =
0006888
Z = 4968063
36 I = 51
68956
XDOT = -6826
004619 Wp = 51
09201
YDOT = -2772
743296 meter/sec RA = 8
84988 deg
ZDOT = -2138
577244 TA = 59
75145
MA = 59
68328
Ha = 220
185 n
mi
Hp = 213
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9795739
42 X = -3048872
94
Y = 11507291
70 feet Y = 3473680
59 meter
Z = 16299420
48 Z = 4953406
38
XDOT = -22395
028278 XDOT = -6784
103550
YDOT = -9096
926825 feet/sec YDOT = -2848
841782 meter/sec
ZDOT = -7016
329542 ZDOT = -2171
634546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7339582
99 X = -2237104
90
Y = -13289352
84 feet Y = -4050594
75 meter
Z = 16234808
40 Z = 4948369
60
XDOT = 15343
360678 XDOT = 4676
656335
YDOT = -17245
732601 feet/sec YDOT = -5256
499297 meter/sec
ZDOT = -7159
800616 ZDOT = -2182
307228
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
97498918
00016717 00000-0 10270-3 0 9151
2 25544 51
6430 9
2085 0000867 2
1733 357
9424 15
54727131 6503
Satellite: ISS
Catalog Number: 25544
Epoch time: 16178
97498918 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 9
2085 deg
Eccentricity:
0000867
Arg of perigee: 2
1733 deg
Mean anomaly: 357
9424 deg
Mean motion: 15
54727131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 318
Coasting Arc #17 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2016/179/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 897031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4688255
24 A = 6780951
10 meter
Y = -2847888
81 meter E =
0006726
Z = -3992891
98 I = 51
67064
XDOT = 5522
314327 Wp = 98
76979
YDOT = 3522
815870 meter/sec RA = 3
85596 deg
ZDOT = 3976
138612 TA = 212
62192
MA = 212
66348
Ha = 220
185 n
mi
Hp = 213
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15381414
84 X = 4739148
33
Y = -9343467
22 feet Y = -2795176
75 meter
Z = -13100039
30 Z = -3969994
24
XDOT = 18117
829157 XDOT = 5463
196545
YDOT = 11557
794849 feet/sec YDOT = 3584
239217 meter/sec
ZDOT = 13045
074185 ZDOT = 4002
821278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3677502
17 X = 1120902
66
Y = 17691357
07 feet Y = 5392325
63 meter
Z = -12999661
33 Z = -3962296
77
XDOT = -15602
286422 XDOT = -4755
576901
YDOT = 12902
219082 feet/sec YDOT = 3932
596376 meter/sec
ZDOT = 13160
599639 ZDOT = 4011
350770
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
93916024
00016717 00000-0 10270-3 0 9162
2 25544 51
6435 4
3984 0000910 11
1896 348
9277 15
54721023 6657
Satellite: ISS
Catalog Number: 25544
Epoch time: 16179
93916024 = yrday
fracday
Element set: 916
Inclination: 51
6435 deg
RA of node: 4
3984 deg
Eccentricity:
0000910
Arg of perigee: 11
1896 deg
Mean anomaly: 348
9277 deg
Mean motion: 15
54721023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 313
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