[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 15th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
226/16:31:37
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
3
228/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
5
237/06:36:29
751 0
4 1
2 1
2
N/A 1
0 -0
0 221
6
000/00:02:59
502 0
3 0
0 215
2
Coasting Arc #1 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2017/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4206754
66 A = 6777438
05 meter
Y = -384515
03 meter E =
0008196
Z = 5295248
04 I = 51
98027
XDOT = 1627
935043 Wp = 131
92030
YDOT = -7461
254730 meter/sec RA = 106
68499 deg
ZDOT = 745
424627 TA = 310
96075
MA = 311
03164
Ha = 222
657 n
mi
Hp = 213
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13801688
53 X = -4227863
88
Y = -1261532
26 feet Y = -431675
79 meter
Z = 17372861
02 Z = 5274761
74
XDOT = 5340
994235 XDOT = 1707
626883
YDOT = -24479
182186 feet/sec YDOT = -7442
604460 meter/sec
ZDOT = 2445
618856 ZDOT = 753
526253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10228676
17 X = 3117700
50
Y = 9518123
44 feet Y = 2901124
02 meter
Z = 17282183
89 Z = 5267609
65
XDOT = -18506
904144 XDOT = -5640
904383
YDOT = 15344
378668 feet/sec YDOT = 4676
966618 meter/sec
ZDOT = 2482
636172 ZDOT = 756
707505
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 17226
54953842
00016717 00000-0 10270-3 0 9005
2 25544 51
6414 107
3865 0005184 140
1956 219
9578 15
54161609 30829
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
54953842 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 107
3865 deg
Eccentricity:
0005184
Arg of perigee: 140
1956 deg
Mean anomaly: 219
9578 deg
Mean motion: 15
54161609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 318
Coasting Arc #2 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2017/226/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389416
35 A = 6780496
50 meter
Y = 2403548
30 meter E =
0013627
Z = 4569323
30 I = 51
98762
XDOT = -562
513799 Wp = 124
19358
YDOT = -6985
792127 meter/sec RA = 105
76079 deg
ZDOT = 3120
206995 TA = 294
65615
MA = 294
79801
Ha = 222
633 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14400972
27 X = -4438162
68
Y = 7885657
14 feet Y = 2354190
34 meter
Z = 14991218
17 Z = 4547882
53
XDOT = -1845
517714 XDOT = -499
511396
YDOT = -22919
265510 feet/sec YDOT = -6991
730243 meter/sec
ZDOT = 10236
899591 ZDOT = 3117
627573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8532907
80 X = 2600830
30
Y = -14128348
42 feet Y = -4306320
60 meter
Z = 14895887
63 Z = 4540266
55
XDOT = 12192
216870 XDOT = 3716
187702
YDOT = 18194
701325 feet/sec YDOT = 5545
744964 meter/sec
ZDOT = 10226
540094 ZDOT = 3117
049421
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 17226
74244187
00016717 00000-0 10270-3 0 9013
2 25544 51
6369 106
4201 0005318 142
7918 217
3604 15
54156539 30858
Satellite: ISS
Catalog Number: 25544
Epoch time: 17226
74244187 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 106
4201 deg
Eccentricity:
0005318
Arg of perigee: 142
7918 deg
Mean anomaly: 217
3604 deg
Mean motion: 15
54156539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 305
Coasting Arc #3 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2017/227/16:31:37
000
Vector Time (MET): N/A
Weight (LBS) : 902299
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4283452
24 A = 6777815
31 meter
Y = -659807
43 meter E =
0017178
Z = -5225373
04 I = 51
98823
XDOT = -408
113594 Wp = 96
96138
YDOT = 7535
527668 meter/sec RA = 100
78844 deg
ZDOT = -1291
712655 TA = 160
70653
MA = 160
64142
Ha = 222
586 n
mi
Hp = 213
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14053321
00 X = 4315894
21
Y = -2164722
53 feet Y = -611725
51 meter
Z = -17143612
34 Z = -5204486
66
XDOT = -1338
955361 XDOT = -486
073049
YDOT = 24722
859803 feet/sec YDOT = 7530
527978 meter/sec
ZDOT = -4237
902412 ZDOT = -1293
884420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10976605
09 X = -3345669
23
Y = 9212110
57 feet Y = 2807851
30 meter
Z = -17050995
81 Z = -5197143
52
XDOT = -11055
778944 XDOT = -3369
801422
YDOT = -21002
920522 feet/sec YDOT = -6401
690175 meter/sec
ZDOT = -4248
688015 ZDOT = -1295
000107
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 17227
70695817
00016717 00000-0 10270-3 0 9021
2 25544 51
6385 101
6118 0005522 143
9245 216
2281 15
54161515 31000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17227
70695817 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 101
6118 deg
Eccentricity:
0005522
Arg of perigee: 143
9245 deg
Mean anomaly: 216
2281 deg
Mean motion: 15
54161515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 285
Coasting Arc #4 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2017/228/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4140816
63 A = 6779052
56 meter
Y = -2163795
62 meter E =
0014302
Z = -4923998
99 I = 52
00007
XDOT = 973
656904 Wp = 92
61155
YDOT = 7219
947252 meter/sec RA = 96
98295 deg
ZDOT = -2360
464052 TA = 154
39800
MA = 154
32711
Ha = 222
378 n
mi
Hp = 213
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13585356
39 X = 4188623
22
Y = -7099066
99 feet Y = -2117222
79 meter
Z = -16154852
32 Z = -4903768
24
XDOT = 3194
412415 XDOT = 904
315081
YDOT = 23687
490985 feet/sec YDOT = 7230
447678 meter/sec
ZDOT = -7744
304633 ZDOT = -2355
902639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14151766
55 X = -4313458
45
Y = -6130615
34 feet Y = -1868611
55 meter
Z = -16064898
78 Z = -4896581
15
XDOT = 15868
578572 XDOT = 4836
742749
YDOT = -16443
643171 feet/sec YDOT = -5012
022438 meter/sec
ZDOT = -7725
228380 ZDOT = -2354
649610
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 17228
47856808
00016717 00000-0 10270-3 0 9036
2 25544 51
6419 97
7697 0005012 145
9450 214
2025 15
54174382 31122
Satellite: ISS
Catalog Number: 25544
Epoch time: 17228
47856808 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 97
7697 deg
Eccentricity:
0005012
Arg of perigee: 145
9450 deg
Mean anomaly: 214
2025 deg
Mean motion: 15
54174382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 312
Coasting Arc #5 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2017/229/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174083
72 A = 6777290
89 meter
Y = 385402
64 meter E =
0007373
Z = 5321444
76 I = 51
99710
XDOT = -99
509637 Wp = 136
78032
YDOT = -7657
467171 meter/sec RA = 92
00950 deg
ZDOT = 470
917369 TA = 308
71937
MA = 308
78527
Ha = 222
448 n
mi
Hp = 213
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13694500
39 X = -4203931
87
Y = 1264444
36 feet Y = 338558
17 meter
Z = 17458808
27 Z = 5301096
08
XDOT = -326
475187 XDOT = -16
161878
YDOT = -25122
923791 feet/sec YDOT = -7658
113942 meter/sec
ZDOT = 1545
004490 ZDOT = 470
636232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9871402
74 X = 3008803
56
Y = 9738335
27 feet Y = 2968244
59 meter
Z = 17368603
31 Z = 5293950
29
XDOT = -18275
454389 XDOT = -5570
358498
YDOT = 15736
640308 feet/sec YDOT = 4796
527966 meter/sec
ZDOT = 1544
971880 ZDOT = 470
907429
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 17229
50738100
00016717 00000-0 10270-3 0 9046
2 25544 51
6418 92
6414 0005084 150
7294 209
4144 15
54172075 31283
Satellite: ISS
Catalog Number: 25544
Epoch time: 17229
50738100 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 92
6414 deg
Eccentricity:
0005084
Arg of perigee: 150
7294 deg
Mean anomaly: 209
4144 deg
Mean motion: 15
54172075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 293
Coasting Arc #6 (Orbit 3142)
---------------------------------------
Vector Time (GMT): 2017/230/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4132559
00 A = 6777933
71 meter
Y = 1458054
13 meter E =
0017131
Z = -5185691
33 I = 51
99960
XDOT = -772
335188 Wp = 114
55794
YDOT = 7471
120141 meter/sec RA = 87
03352 deg
ZDOT = 1482
078225 TA = 169
68113
MA = 169
64592
Ha = 222
169 n
mi
Hp = 213
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13558264
42 X = 4141136
68
Y = 4783642
16 feet Y = 1504315
28 meter
Z = -17013423
01 Z = -5165596
08
XDOT = -2533
908098 XDOT = -863
020933
YDOT = 24511
549019 feet/sec YDOT = 7461
976280 meter/sec
ZDOT = 4862
461369 ZDOT = 1478
106405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5390796
29 X = -1643114
71
Y = -13441077
85 feet Y = -4096840
53 meter
Z = -16924629
12 Z = -5158626
95
XDOT = 19168
809325 XDOT = 5842
653082
YDOT = -13799
817983 feet/sec YDOT = -4206
184521 meter/sec
ZDOT = 4843
669531 ZDOT = 1476
350473
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 17230
47189103
00016717 00000-0 10270-3 0 9058
2 25544 51
6420 87
8329 0004921 154
7446 205
3948 15
54179902 31439
Satellite: ISS
Catalog Number: 25544
Epoch time: 17230
47189103 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 87
8329 deg
Eccentricity:
0004921
Arg of perigee: 154
7446 deg
Mean anomaly: 205
3948 deg
Mean motion: 15
54179902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3143
Checksum: 311
Coasting Arc #7 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2017/231/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3975537
62 A = 6780639
77 meter
Y = -3162469
99 meter E =
0010321
Z = 4481759
87 I = 52
00624
XDOT = 1650
727701 Wp = 96
24536
YDOT = -6736
760589 meter/sec RA = 82
06272 deg
ZDOT = -3284
025127 TA = 26
66953
MA = 26
61649
Ha = 222
126 n
mi
Hp = 213
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13043102
43 X = -3961648
36
Y = -10375557
71 feet Y = -3206849
52 meter
Z = 14703936
58 Z = 4462482
02
XDOT = 5415
773296 XDOT = 1741
889145
YDOT = -22102
232905 feet/sec YDOT = -6717
791299 meter/sec
ZDOT = -10774
360652 ZDOT = -3275
785171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1117764
88 X = 340694
73
Y = 16703737
68 feet Y = 5091299
24 meter
Z = 14619036
19 Z = 4455882
23
XDOT = -18855
950811 XDOT = -5747
293807
YDOT = 10674
059563 feet/sec YDOT = 3253
453355 meter/sec
ZDOT = -10736
766631 ZDOT = -3272
566469
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 17231
50069767
00016717 00000-0 10270-3 0 9067
2 25544 51
6419 82
7040 0004738 158
7026 201
4324 15
54214693 31594
Satellite: ISS
Catalog Number: 25544
Epoch time: 17231
50069767 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 82
7040 deg
Eccentricity:
0004738
Arg of perigee: 158
7026 deg
Mean anomaly: 201
4324 deg
Mean motion: 15
54214693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 305
Coasting Arc #8 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2017/232/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721477
48 A = 6784574
70 meter
Y = 4599571
27 meter E =
0007446
Z = -3330243
37 I = 52
01184
XDOT = -2533
734082 Wp = 124
35208
YDOT = 5469
284496 meter/sec RA = 77
10072 deg
ZDOT = 4725
949442 TA = 197
15918
MA = 197
18437
Ha = 222
026 n
mi
Hp = 213
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12209571
77 X = 3685943
62
Y = 15090456
91 feet Y = 4640988
62 meter
Z = -10925995
30 Z = -3312252
34
XDOT = -8312
775859 XDOT = -2617
660631
YDOT = 17943
846773 feet/sec YDOT = 5440
481374 meter/sec
ZDOT = 15505
083470 ZDOT = 4713
437669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2624036
91 X = 799806
45
Y = -19277688
61 feet Y = -5875839
49 meter
Z = -10847029
93 Z = -3306174
72
XDOT = 17445
514331 XDOT = 5317
392768
YDOT = -6311
567547 feet/sec YDOT = -1923
765788 meter/sec
ZDOT = 15448
760114 ZDOT = 4708
782083
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 17232
46520514
00016717 00000-0 10270-3 0 9076
2 25544 51
6402 77
8953 0004858 162
2851 197
8472 15
54171107 31744
Satellite: ISS
Catalog Number: 25544
Epoch time: 17232
46520514 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 77
8953 deg
Eccentricity:
0004858
Arg of perigee: 162
2851 deg
Mean anomaly: 197
8472 deg
Mean motion: 15
54171107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 314
Coasting Arc #9 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2017/233/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3292650
39 A = 6787822
75 meter
Y = -5645217
69 meter E =
0017343
Z = 1797538
79 I = 52
01524
XDOT = 3438
460961 Wp = 126
91045
YDOT = -3827
383770 meter/sec RA = 72
14891 deg
ZDOT = -5693
976060 TA = 33
42720
MA = 33
31784
Ha = 221
953 n
mi
Hp = 213
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10802658
76 X = -3238010
74
Y = -18521055
40 feet Y = -5681732
76 meter
Z = 5897436
99 Z = 1781677
39
XDOT = 11281
039899 XDOT = 3508
662205
YDOT = -12557
033365 feet/sec YDOT = -3788
540270 meter/sec
ZDOT = -18681
023818 ZDOT = -5677
102767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5758114
51 X = -1755073
30
Y = 20673274
51 feet Y = 6301214
07 meter
Z = 5828081
22 Z = 1776399
16
XDOT = -15446
852483 XDOT = -4708
200637
YDOT = 968
620216 feet/sec YDOT = 295
235442 meter/sec
ZDOT = -18605
638408 ZDOT = -5670
998587
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 17233
49400988
00016717 00000-0 10270-3 0 9083
2 25544 51
6409 72
7663 0004771 166
0250 194
1036 15
54187999 31902
Satellite: ISS
Catalog Number: 25544
Epoch time: 17233
49400988 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 72
7663 deg
Eccentricity:
0004771
Arg of perigee: 166
0250 deg
Mean anomaly: 194
1036 deg
Mean motion: 15
54187999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 329
Coasting Arc #10 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2017/234/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2707251
08 A = 6789189
03 meter
Y = 6222441
53 meter E =
0009962
Z = -108287
59 I = 52
00766
XDOT = -4291
473258 Wp = 67
57824
YDOT = 1964
476644 meter/sec RA = 67
20134 deg
ZDOT = 6039
677603 TA = 291
26167
MA = 291
36802
Ha = 221
845 n
mi
Hp = 214
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8882057
35 X = 2637994
88
Y = 20414834
41 feet Y = 6252328
61 meter
Z = -355274
24 Z = -95305
44
XDOT = -14079
636674 XDOT = -4342
458860
YDOT = 6445
133347 feet/sec YDOT = 1916
201768 meter/sec
ZDOT = 19815
215234 ZDOT = 6018
707386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8124868
72 X = 2476459
99
Y = -20728720
83 feet Y = -6318114
11 meter
Z = -298776
25 Z = -91067
00
XDOT = 13101
957120 XDOT = 3993
476530
YDOT = 4876
271366 feet/sec YDOT = 1486
287512 meter/sec
ZDOT = 19721
981046 ZDOT = 6011
259823
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 17234
45851155
00016717 00000-0 10270-3 0 9097
2 25544 51
6398 67
9565 0004770 170
1403 189
9844 15
54173751 32058
Satellite: ISS
Catalog Number: 25544
Epoch time: 17234
45851155 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 67
9565 deg
Eccentricity:
0004770
Arg of perigee: 170
1403 deg
Mean anomaly: 189
9844 deg
Mean motion: 15
54173751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 329
Coasting Arc #11 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2017/235/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1878533
68 A = 6788073
15 meter
Y = -6309362
36 meter E =
0012215
Z = -1630876
23 I = 51
98926
XDOT = 5068
555179 Wp = 153
94138
YDOT = -28
185496 meter/sec RA = 62
25514 deg
ZDOT = -5756
157819 TA = 43
82901
MA = 43
73215
Ha = 221
789 n
mi
Hp = 214
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6163168
24 X = -1799919
22
Y = -20700007
75 feet Y = -6329929
97 meter
Z = -5350643
79 Z = -1639809
99
XDOT = 16629
118040 XDOT = 5096
453830
YDOT = -92
472099 feet/sec YDOT = 28
650076 meter/sec
ZDOT = -18885
032214 ZDOT = -5731
468956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9950116
02 X = -3032795
36
Y = 19158712
25 feet Y = 5839575
49 meter
Z = -5389182
59 Z = -1642622
85
XDOT = -10732
011486 XDOT = -3271
117101
YDOT = -10830
421459 feet/sec YDOT = -3301
112461 meter/sec
ZDOT = -18775
643339 ZDOT = -5722
816090
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 17235
48731198
00016717 00000-0 10270-3 0 9107
2 25544 51
6387 62
8275 0004826 174
0882 186
0328 15
54166336 32218
Satellite: ISS
Catalog Number: 25544
Epoch time: 17235
48731198 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 62
8275 deg
Eccentricity:
0004826
Arg of perigee: 174
0882 deg
Mean anomaly: 186
0328 deg
Mean motion: 15
54166336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 319
Coasting Arc #12 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2017/236/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924803
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 874678
65 A = 6784873
75 meter
Y = 5937093
59 meter E =
0013464
Z = 3158942
91 I = 51
96278
XDOT = -5657
444242 Wp = 106
79013
YDOT = -1766
478257 meter/sec RA = 57
30066 deg
ZDOT = 4865
617621 TA = 289
46655
MA = 289
61196
Ha = 221
615 n
mi
Hp = 214
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2869680
61 X = 792879
06
Y = 19478653
50 feet Y = 5946417
75 meter
Z = 10363985
92 Z = 3162992
59
XDOT = -18561
168774 XDOT = -5660
905072
YDOT = -5795
532340 feet/sec YDOT = -1829
762580 meter/sec
ZDOT = 15963
312404 ZDOT = 4838
127560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11221852
74 X = 3420420
72
Y = -16166983
07 feet Y = -4927696
44 meter
Z = 10380938
91 Z = 3164110
18
XDOT = 8535
258227 XDOT = 2601
546708
YDOT = 16140
586794 feet/sec YDOT = 4919
650855 meter/sec
ZDOT = 15841
817053 ZDOT = 4828
585838
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 17236
51610975
00016717 00000-0 10270-3 0 9112
2 25544 51
6386 57
6976 0004897 179
9881 180
1272 15
54202101 32379
Satellite: ISS
Catalog Number: 25544
Epoch time: 17236
51610975 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 57
6976 deg
Eccentricity:
0004897
Arg of perigee: 179
9881 deg
Mean anomaly: 180
1272 deg
Mean motion: 15
54202101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 325
Coasting Arc #13 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2017/237/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4811399
21 A = 6780216
92 meter
Y = 174403
16 meter E =
0012508
Z = -4785761
18 I = 51
93350
XDOT = 2426
516536 Wp = 129
36438
YDOT = 6749
968502 meter/sec RA = 53
19683 deg
ZDOT = 2682
454654 TA = 167
06956
MA = 167
03745
Ha = 221
607 n
mi
Hp = 215
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15785430
49 X = 4832338
10
Y = 572188
86 feet Y = 228324
17 meter
Z = -15701316
20 Z = -4762338
23
XDOT = 7961
012257 XDOT = 2337
826307
YDOT = 22145
565951 feet/sec YDOT = 6776
607796 meter/sec
ZDOT = 8800
704247 ZDOT = 2694
025831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5360164
53 X = 1633778
15
Y = -14967388
20 feet Y = -4562059
92 meter
Z = -15597579
07 Z = -4754142
10
XDOT = 22408
553951 XDOT = 6830
127244
YDOT = -1208
952492 feet/sec YDOT = -368
488719 meter/sec
ZDOT = 8850
834165 ZDOT = 2697
734253
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 17237
28770923
00016717 00000-0 10270-3 0 9128
2 25544 51
6422 53
8527 0004488 191
1550 168
9504 15
53975157 32497
Satellite: ISS
Catalog Number: 25544
Epoch time: 17237
28770923 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 53
8527 deg
Eccentricity:
0004488
Arg of perigee: 191
1550 deg
Mean anomaly: 168
9504 deg
Mean motion: 15
53975157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 329
Coasting Arc #14 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2017/238/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5386665
93 A = 6783717
20 meter
Y = -1551308
85 meter E =
0010873
Z = 3809026
49 I = 51
92470
XDOT = -1181
502740 Wp = 105
31898
YDOT = -6293
511860 meter/sec RA = 48
22868 deg
ZDOT = -4226
814829 TA = 29
12303
MA = 29
06244
Ha = 221
671 n
mi
Hp = 215
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17672788
48 X = -5387420
73
Y = -5089595
97 feet Y = -1611550
14 meter
Z = 12496806
08 Z = 3782858
16
XDOT = -3876
321325 XDOT = -1090
507514
YDOT = -20648
004791 feet/sec YDOT = -6306
215776 meter/sec
ZDOT = -13867
502720 ZDOT = -4232
332667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9965008
83 X = -3037334
69
Y = 15550158
38 feet Y = 4739688
28 meter
Z = 12381145
96 Z = 3773773
29
XDOT = -19733
664153 XDOT = -6014
820834
YDOT = -1566
877745 feet/sec YDOT = -477
584337 meter/sec
ZDOT = -13890
880899 ZDOT = -4233
940498
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 17238
31664474
00016717 00000-0 10270-3 0 9137
2 25544 51
6421 48
7253 0004390 193
1934 166
9104 15
53979246 32650
Satellite: ISS
Catalog Number: 25544
Epoch time: 17238
31664474 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 48
7253 deg
Eccentricity:
0004390
Arg of perigee: 193
1934 deg
Mean anomaly: 166
9104 deg
Mean motion: 15
53979246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 321
Coasting Arc #15 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2017/239/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5710329
09 A = 6787200
16 meter
Y = 2707162
14 meter E =
0002661
Z = -2478872
09 I = 51
91419
XDOT = -282
609692 Wp = 100
99111
YDOT = 5484
598025 meter/sec RA = 43
26802 deg
ZDOT = 5343
041753 TA = 231
36681
MA = 231
39064
Ha = 221
375 n
mi
Hp = 215
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18734675
48 X = 5691673
59
Y = 8881765
57 feet Y = 2770914
46 meter
Z = -8132782
44 Z = -2451178
66
XDOT = -927
197152 XDOT = -369
872717
YDOT = 17994
088007 feet/sec YDOT = 5480
950133 meter/sec
ZDOT = 17529
664544 ZDOT = 5341
456610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13626708
88 X = 4153420
87
Y = -15689471
21 feet Y = -4782150
83 meter
Z = -8010572
59 Z = -2441622
53
XDOT = 15900
704984 XDOT = 4846
534879
YDOT = 4871
534273 feet/sec YDOT = 1484
843646 meter/sec
ZDOT = 17521
705698 ZDOT = 5340
615897
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 17239
28126956
00016717 00000-0 10270-3 0 9143
2 25544 51
6422 43
9177 0004441 198
8916 161
2072 15
53990619 32808
Satellite: ISS
Catalog Number: 25544
Epoch time: 17239
28126956 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 43
9177 deg
Eccentricity:
0004441
Arg of perigee: 198
8916 deg
Mean anomaly: 161
2072 deg
Mean motion: 15
53990619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 325
Coasting Arc #16 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2017/240/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5675788
01 A = 6789558
01 meter
Y = -3603008
98 meter E =
0015167
Z = 882324
04 I = 51
89772
XDOT = 1894
748651 Wp = 142
42107
YDOT = -4453
026487 meter/sec RA = 38
31464 deg
ZDOT = -5953
637028 TA = 28
06050
MA = 27
97882
Ha = 221
418 n
mi
Hp = 215
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18621351
74 X = -5639362
26
Y = -11820895
60 feet Y = -3666275
79 meter
Z = 2894763
91 Z = 854841
56
XDOT = 6216
366965 XDOT = 1973
322534
YDOT = -14609
666952 feet/sec YDOT = -4431
399116 meter/sec
ZDOT = -19532
929881 ZDOT = -5944
241857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16160867
36 X = -4925832
37
Y = 15033335
86 feet Y = 4582160
77 meter
Z = 2773652
92 Z = 845409
41
XDOT = -11428
791555 XDOT = -3483
495666
YDOT = -8663
426565 feet/sec YDOT = -2640
612417 meter/sec
ZDOT = -19490
546608 ZDOT = -5940
718606
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 17240
31020237
00016717 00000-0 10270-3 0 9155
2 25544 51
6427 38
7904 0004544 201
7587 158
3373 15
53947143 32967
Satellite: ISS
Catalog Number: 25544
Epoch time: 17240
31020237 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 38
7904 deg
Eccentricity:
0004544
Arg of perigee: 201
7587 deg
Mean anomaly: 158
3373 deg
Mean motion: 15
53947143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 306
Coasting Arc #17 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2017/241/06:37:59
502
Vector Time (MET): N/A
Weight (LBS) : 924683
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5272850
61 A = 6789420
26 meter
Y = 4200351
57 meter E =
0009594
Z = 775397
77 I = 51
87150
XDOT = -3510
204250 Wp = 64
68436
YDOT = 3295
289315 meter/sec RA = 33
36108 deg
ZDOT = 5965
834022 TA = 303
66813
MA = 303
75959
Ha = 221
101 n
mi
Hp = 215
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17299378
65 X = 5221722
79
Y = 13780681
00 feet Y = 4259030
34 meter
Z = 2543955
95 Z = 800887
20
XDOT = -11516
418143 XDOT = -3575
771181
YDOT = 10811
316649 feet/sec YDOT = 3255
669488 meter/sec
ZDOT = 19572
946268 ZDOT = 5948
623183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17482720
90 X = 5328733
33
Y = -13525784
69 feet Y = -4122659
17 meter
Z = 2656125
15 Z = 809586
95
XDOT = 6760
346466 XDOT = 2060
553603
YDOT = 12599
661105 feet/sec YDOT = 3840
376705 meter/sec
ZDOT = 19496
142291 ZDOT = 5942
424170
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 17241
33912885
00016717 00000-0 10270-3 0 9168
2 25544 51
6426 33
6615 0004379 208
2989 151
7926 15
54001629 33124
Satellite: ISS
Catalog Number: 25544
Epoch time: 17241
33912885 = yrday
fracday
Element set: 916
Inclination: 51
6426 deg
RA of node: 33
6615 deg
Eccentricity:
0004379
Arg of perigee: 208
2989 deg
Mean anomaly: 151
7926 deg
Mean motion: 15
54001629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 316
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