[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 14th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
257/18:31:19
752 -1
3 2
0 2
0
N/A -0
3 -0
2 229
7
000/00:00:39
505 -1
4 -0
0 218
9
259/19:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
7
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
268/17:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
Coasting Arc #1 (Orbit 2894)
---------------------------------------
Vector Time (GMT): 2019/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3770083
74 A = 6788673
14 meter
Y = -2254977
14 meter E =
0019274
Z = -5191136
55 I = 51
24755
XDOT = 2570
140902 Wp = 76
19860
YDOT = -7099
560688 meter/sec RA = 282
41372 deg
ZDOT = 1225
765111 TA = 205
61119
MA = 205
70678
Ha = 229
412 n
mi
Hp = 218
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12369041
16 X = -3719372
28
Y = -7398218
97 feet Y = -2296853
81 meter
Z = -17031287
88 Z = -5209326
67
XDOT = 8432
220808 XDOT = 2643
385186
YDOT = -23292
521943 feet/sec YDOT = -7070
409913 meter/sec
ZDOT = 4021
539079 ZDOT = 1238
428343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10993816
44 X = 3350915
25
Y = 9167591
57 feet Y = 2794281
91 meter
Z = -17113820
58 Z = -5216292
51
XDOT = -11162
792413 XDOT = -3402
419127
YDOT = 20951
323262 feet/sec YDOT = 6385
963330 meter/sec
ZDOT = 4079
672442 ZDOT = 1243
484160
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 19256
51399165
00016717 00000-0 10270-3 0 9009
2 25544 51
6423 283
1789 0008430 35
3638 324
8070 15
50424556 28959
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
51399165 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 283
1789 deg
Eccentricity:
0008430
Arg of perigee: 35
3638 deg
Mean anomaly: 324
8070 deg
Mean motion: 15
50424556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2895
Checksum: 322
Coasting Arc #2 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2019/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3757618
36 A = 6789108
30 meter
Y = 2533497
93 meter E =
0013789
Z = 5049069
60 I = 51
24154
XDOT = -2362
333939 Wp = 45
78448
YDOT = 7074
136710 meter/sec RA = 277
42565 deg
ZDOT = -1779
042489 TA = 61
59545
MA = 61
45653
Ha = 229
376 n
mi
Hp = 218
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12328144
21 X = 3704483
30
Y = 8312001
07 feet Y = 2575221
68 meter
Z = 16565188
97 Z = 5067193
31
XDOT = -7750
439434 XDOT = -2432
621843
YDOT = 23209
109940 feet/sec YDOT = 7047
326239 meter/sec
ZDOT = -5836
753572 ZDOT = -1790
689212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10989818
82 X = -3349696
78
Y = -9877541
55 feet Y = -3010674
66 meter
Z = 16647403
48 Z = 5074128
58
XDOT = 10036
160748 XDOT = 3059
021796
YDOT = -21162
302004 feet/sec YDOT = -6450
269651 meter/sec
ZDOT = -5890
242487 ZDOT = -1795
345910
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 19257
54527116
00016717 00000-0 10270-3 0 9013
2 25544 51
6405 278
0662 0008505 39
9102 320
2672 15
50464971 29113
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
54527116 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 278
0662 deg
Eccentricity:
0008505
Arg of perigee: 39
9102 deg
Mean anomaly: 320
2672 deg
Mean motion: 15
50464971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 300
Coasting Arc #3 (Orbit 2914)
---------------------------------------
Vector Time (GMT): 2019/257/18:31:39
505
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1197340
69 A = 6800968
55 meter
Y = 6666417
91 meter E =
0012610
Z = -602663
78 I = 51
27674
XDOT = -4641
381884 Wp = 103
94752
YDOT = -1360
489855 meter/sec RA = 276
09096 deg
ZDOT = -5935
934785 TA = 82
57543
MA = 82
43215
Ha = 229
743 n
mi
Hp = 218
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3928283
09 X = -1268870
11
Y = 21871449
84 feet Y = 6652628
40 meter
Z = -1977243
38 Z = -608654
42
XDOT = -15227
630854 XDOT = -4596
990147
YDOT = -4463
549394 feet/sec YDOT = -1412
145469 meter/sec
ZDOT = -19474
851656 ZDOT = -5958
372846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21902617
32 X = -6675917
76
Y = -3735857
27 feet Y = -1138689
30 meter
Z = -2004979
45 Z = -611117
74
XDOT = 4068
679423 XDOT = 1240
133488
YDOT = -13534
878239 feet/sec YDOT = -4125
430887 meter/sec
ZDOT = -19576
771610 ZDOT = -5966
999987
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 19257
80309974
00016717 00000-0 10270-3 0 9023
2 25544 51
6410 276
7887 0007271 45
8840 314
2908 15
50076828 29156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
80309974 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 276
7887 deg
Eccentricity:
0007271
Arg of perigee: 45
8840 deg
Mean anomaly: 314
2908 deg
Mean motion: 15
50076828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 333
Coasting Arc #4 (Orbit 2930)
---------------------------------------
Vector Time (GMT): 2019/258/18:31:39
505
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 886664
39 A = 6800765
54 meter
Y = -6665701
37 meter E =
0020792
Z = 944068
90 I = 51
27361
XDOT = 4691
184561 Wp = 52
97609
YDOT = 1468
440511 meter/sec RA = 271
11270 deg
ZDOT = 5884
489048 TA = 317
28954
MA = 317
45097
Ha = 229
787 n
mi
Hp = 218
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2909003
90 X = 956550
52
Y = -21869098
98 feet Y = -6655395
20 meter
Z = 3097338
90 Z = 948546
44
XDOT = 15391
025463 XDOT = 4645
831756
YDOT = 4817
718211 feet/sec YDOT = 1520
647691 meter/sec
ZDOT = 19306
066429 ZDOT = 5907
166780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21935163
58 X = 6685837
86
Y = 2332137
33 feet Y = 710835
46 meter
Z = 3118178
33 Z = 950420
76
XDOT = -4259
974725 XDOT = -1298
440296
YDOT = 13778
402168 feet/sec YDOT = 4199
656981 meter/sec
ZDOT = 19409
070637 ZDOT = 5915
884730
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 19258
83461897
00016717 00000-0 10270-3 0 9031
2 25544 51
6410 271
6776 0007352 49
0023 311
1762 15
50074573 29313
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
83461897 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 271
6776 deg
Eccentricity:
0007352
Arg of perigee: 49
0023 deg
Mean anomaly: 311
1762 deg
Mean motion: 15
50074573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 308
Coasting Arc #5 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2019/259/18:31:39
505
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -627559
95 A = 6800368
24 meter
Y = 6637947
48 meter E =
0011475
Z = -1338851
37 I = 51
27379
XDOT = -4754
906600 Wp = 102
55708
YDOT = -1606
544383 meter/sec RA = 266
13448 deg
ZDOT = -5780
983035 TA = 92
05968
MA = 91
92827
Ha = 229
856 n
mi
Hp = 218
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2058923
72 X = -695237
32
Y = 21778042
92 feet Y = 6630551
12 meter
Z = -4392556
99 Z = -1342064
90
XDOT = -15600
087270 XDOT = -4708
507399
YDOT = -5270
814904 feet/sec YDOT = -1659
458264 meter/sec
ZDOT = -18966
479774 ZDOT = -5803
967851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21844424
73 X = -6658180
66
Y = -1100346
12 feet Y = -335385
50 meter
Z = -4407632
41 Z = -1343446
36
XDOT = 4528
290686 XDOT = 1380
223001
YDOT = -14089
387832 feet/sec YDOT = -4294
445411 meter/sec
ZDOT = -19070
873824 ZDOT = -5812
802341
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 19259
80166580
00016717 00000-0 10270-3 0 9041
2 25544 51
6419 266
8859 0007331 52
9933 307
1888 15
50075335 29467
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
80166580 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 266
8859 deg
Eccentricity:
0007331
Arg of perigee: 52
9933 deg
Mean anomaly: 307
1888 deg
Mean motion: 15
50075335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 342
Coasting Arc #6 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2019/259/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1152619
05 A = 6800771
94 meter
Y = -6640866
39 meter E =
0017340
Z = -852521
73 I = 51
27562
XDOT = 4635
340306 Wp = 44
89670
YDOT = -1551
237153 meter/sec RA = 265
97459 deg
ZDOT = 5902
352240 TA = 305
84744
MA = 306
00838
Ha = 229
800 n
mi
Hp = 218
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3781558
56 X = -1074132
19
Y = -21787619
40 feet Y = -6653317
03 meter
Z = -2796987
30 Z = -857929
44
XDOT = 15207
809404 XDOT = 4623
671668
YDOT = -5089
360739 feet/sec YDOT = -1499
466144 meter/sec
ZDOT = 19364
672703 ZDOT = 5924
840927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20449203
59 X = 6232917
25
Y = -8408037
15 feet Y = -2562769
72 meter
Z = -2821110
81 Z = -859874
57
XDOT = 7630
271960 XDOT = 2325
706893
YDOT = 12119
504216 feet/sec YDOT = 3694
024885 meter/sec
ZDOT = 19467
031751 ZDOT = 5933
551278
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 19259
80166541
00016717 00000-0 10270-3 0 9059
2 25544 51
6422 266
8862 0007345 52
4216 307
7600 15
50092891 29463
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
80166541 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 266
8862 deg
Eccentricity:
0007345
Arg of perigee: 52
4216 deg
Mean anomaly: 307
7600 deg
Mean motion: 15
50092891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 316
Coasting Arc #7 (Orbit 2961)
---------------------------------------
Vector Time (GMT): 2019/260/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1415424
85 A = 6801084
96 meter
Y = 6633010
57 meter E =
0016549
Z = 449132
77 I = 51
27956
XDOT = -4611
462386 Wp = 105
22591
YDOT = 1399
400961 meter/sec RA = 260
99762 deg
ZDOT = -5954
109078 TA = 69
91587
MA = 69
73784
Ha = 229
904 n
mi
Hp = 218
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4643782
31 X = 1338965
75
Y = 21761845
69 feet Y = 6648411
38 meter
Z = 1473532
73 Z = 455822
12
XDOT = -15129
469769 XDOT = -4597
846138
YDOT = 4591
210501 feet/sec YDOT = 1347
907919 meter/sec
ZDOT = -19534
478603 ZDOT = -5976
477092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20072486
50 X = -6118093
89
Y = 9599412
55 feet Y = 2925900
94 meter
Z = 1503497
69 Z = 458266
10
XDOT = -7273
371647 XDOT = -2216
923678
YDOT = -12042
507745 feet/sec YDOT = -3670
556361 meter/sec
ZDOT = -19636
277108 ZDOT = -5985
137263
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 19260
83318290
00016717 00000-0 10270-3 0 9065
2 25544 51
6419 261
7758 0007278 57
3517 302
8335 15
50062366 29623
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
83318290 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 261
7758 deg
Eccentricity:
0007278
Arg of perigee: 57
3517 deg
Mean anomaly: 302
8335 deg
Mean motion: 15
50062366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 322
Coasting Arc #8 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2019/261/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1722905
65 A = 6801065
39 meter
Y = -6570019
44 meter E =
0018946
Z = -105610
68 I = 51
28691
XDOT = 4616
731550 Wp = 50
13363
YDOT = -1295
101756 meter/sec RA = 256
01985 deg
ZDOT = 5979
666035 TA = 308
72469
MA = 308
89392
Ha = 229
821 n
mi
Hp = 218
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5652577
60 X = -1648796
74
Y = -21555181
88 feet Y = -6588871
82 meter
Z = -346491
72 Z = -113799
50
XDOT = 15146
757054 XDOT = 4601
824400
YDOT = -4249
021510 feet/sec YDOT = -1243
557104 meter/sec
ZDOT = 19618
326887 ZDOT = 6002
056529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19449378
37 X = 5928170
53
Y = -10875308
02 feet Y = -3314793
88 meter
Z = -383291
81 Z = -116827
34
XDOT = 7084
409773 XDOT = 2159
328099
YDOT = 12050
798251 feet/sec YDOT = 3673
083307 meter/sec
ZDOT = 19720
221601 ZDOT = 6010
723544
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 19261
80022781
00016717 00000-0 10270-3 0 9071
2 25544 51
6426 256
9843 0007233 58
9047 301
2813 15
50098249 29777
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
80022781 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 256
9843 deg
Eccentricity:
0007233
Arg of perigee: 58
9047 deg
Mean anomaly: 301
2813 deg
Mean motion: 15
50098249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 322
Coasting Arc #9 (Orbit 2992)
---------------------------------------
Vector Time (GMT): 2019/262/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1975418
91 A = 6801140
23 meter
Y = 6497752
33 meter E =
0015234
Z = -302661
38 I = 51
29655
XDOT = -4660
651088 Wp = 110
03512
YDOT = 1150
620223 meter/sec RA = 251
04355 deg
ZDOT = -5967
754841 TA = 73
23536
MA = 73
06826
Ha = 229
945 n
mi
Hp = 218
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6481033
18 X = 1904082
53
Y = 21318085
08 feet Y = 6519443
97 meter
Z = -992983
54 Z = -293239
06
XDOT = -15290
850027 XDOT = -4644
182882
YDOT = 3775
000733 feet/sec YDOT = 1098
593274 meter/sec
ZDOT = -19579
248165 ZDOT = -5990
354871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18806951
93 X = -5732358
95
Y = 11951801
53 feet Y = 3642909
10 meter
Z = -950556
81 Z = -289729
72
XDOT = -6818
270632 XDOT = -2078
208889
YDOT = -12225
996271 feet/sec YDOT = -3726
483664 meter/sec
ZDOT = -19682
089715 ZDOT = -5999
100945
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 19262
83174193
00016717 00000-0 10270-3 0 9081
2 25544 51
6432 251
8735 0007211 63
8268 296
3623 15
50060685 29938
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
83174193 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 251
8735 deg
Eccentricity:
0007211
Arg of perigee: 63
8268 deg
Mean anomaly: 296
3623 deg
Mean motion: 15
50060685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 323
Coasting Arc #10 (Orbit 3008)
---------------------------------------
Vector Time (GMT): 2019/263/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 916777
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2261103
67 A = 6800877
89 meter
Y = -6371810
61 meter E =
0020262
Z = 646928
56 I = 51
30741
XDOT = 4730
848266 Wp = 56
91304
YDOT = -1063
325166 meter/sec RA = 246
06696 deg
ZDOT = 5937
343415 TA = 310
09645
MA = 310
27389
Ha = 229
890 n
mi
Hp = 218
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7418319
14 X = -2192826
65
Y = -20904890
45 feet Y = -6396714
08 meter
Z = 2122469
01 Z = 636110
93
XDOT = 15521
155729 XDOT = 4713
546445
YDOT = -3488
599627 feet/sec YDOT = -1010
517990 meter/sec
ZDOT = 19479
473145 ZDOT = 5960
282363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17934043
49 X = 5466296
45
Y = -13062187
19 feet Y = -3981354
65 meter
Z = 2073675
11 Z = 632056
17
XDOT = 6761
026089 XDOT = 2060
760752
YDOT = 12458
143833 feet/sec YDOT = 3797
242240 meter/sec
ZDOT = 19583
856304 ZDOT = 5969
159401
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 19263
86325220
00016717 00000-0 10270-3 0 9095
2 25544 51
6426 246
7623 0007291 65
7909 294
4003 15
50108310 30099
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
86325220 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 246
7623 deg
Eccentricity:
0007291
Arg of perigee: 65
7909 deg
Mean anomaly: 294
4003 deg
Mean motion: 15
50108310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3009
Checksum: 298
Coasting Arc #11 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2019/264/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2484638
74 A = 6800718
40 meter
Y = 6240768
46 meter E =
0013776
Z = -1051410
85 I = 51
32034
XDOT = -4836
012535 Wp = 112
06108
YDOT = 949
193715 meter/sec RA = 241
09238 deg
ZDOT = -5861
193618 TA = 79
36444
MA = 79
20931
Ha = 229
989 n
mi
Hp = 218
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8151701
89 X = 2419775
21
Y = 20474962
15 feet Y = 6268190
74 meter
Z = -3449510
67 Z = -1039499
03
XDOT = -15866
182858 XDOT = -4817
796625
YDOT = 3114
152609 feet/sec YDOT = 895
215706 meter/sec
ZDOT = -19229
637855 ZDOT = -5884
641119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17073572
65 X = -5204024
94
Y = 13947604
44 feet Y = 4251229
83 meter
Z = -3395716
44 Z = -1035014
37
XDOT = -6679
113834 XDOT = -2035
793897
YDOT = -12829
331494 feet/sec YDOT = -3910
380239 meter/sec
ZDOT = -19336
334963 ZDOT = -5893
714897
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 19264
83029507
00016717 00000-0 10270-3 0 9104
2 25544 51
6419 241
9713 0007196 70
5854 289
6074 15
50061820 30240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
83029507 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 241
9713 deg
Eccentricity:
0007196
Arg of perigee: 70
5854 deg
Mean anomaly: 289
6074 deg
Mean motion: 15
50061820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3024
Checksum: 308
Coasting Arc #12 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2019/265/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2731679
07 A = 6800219
20 meter
Y = -6060388
77 meter E =
0020838
Z = 1388321
70 I = 51
33625
XDOT = 4961
448790 Wp = 64
73676
YDOT = -899
817663 meter/sec RA = 236
11758 deg
ZDOT = 5774
874751 TA = 310
44128
MA = 310
62283
Ha = 229
880 n
mi
Hp = 218
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8962201
69 X = -2670450
75
Y = -19883165
25 feet Y = -6090593
95 meter
Z = 4554861
21 Z = 1375201
02
XDOT = 16277
719127 XDOT = 4943
090816
YDOT = -2952
157686 feet/sec YDOT = -844
437760 meter/sec
ZDOT = 18946
439473 ZDOT = 5798
931141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16010661
01 X = 4880049
48
Y = -14827573
54 feet Y = -4519444
42 meter
Z = 4495539
69 Z = 1370240
50
XDOT = 6833
220737 XDOT = 2082
765681
YDOT = 13215
820805 feet/sec YDOT = 4028
182181 meter/sec
ZDOT = 19055
913068 ZDOT = 5808
242303
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 19265
86180302
00016717 00000-0 10270-3 0 9110
2 25544 51
6418 236
8602 0007158 72
9071 287
2863 15
50120680 30402
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
86180302 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 236
8602 deg
Eccentricity:
0007158
Arg of perigee: 72
9071 deg
Mean anomaly: 287
2863 deg
Mean motion: 15
50120680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 296
Coasting Arc #13 (Orbit 3054)
---------------------------------------
Vector Time (GMT): 2019/266/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2909221
91 A = 6799801
50 meter
Y = 5881996
23 meter E =
0012292
Z = -1781754
85 I = 51
35387
XDOT = -5115
179150 Wp = 110
13678
YDOT = 833
694436 meter/sec RA = 231
14372 deg
ZDOT = -5635
678094 TA = 89
46635
MA = 89
32550
Ha = 229
965 n
mi
Hp = 218
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9544691
30 X = 2851886
28
Y = 19297887
88 feet Y = 5914208
56 meter
Z = -5845652
38 Z = -1767762
36
XDOT = -16782
083827 XDOT = -5096
746588
YDOT = 2735
217965 feet/sec YDOT = 776
595801 meter/sec
ZDOT = -18489
757525 ZDOT = -5660
480979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15004421
85 X = -4573347
78
Y = 15463285
38 feet Y = 4713209
38 meter
Z = -5782334
37 Z = -1762455
52
XDOT = -6997
558290 XDOT = -2132
855767
YDOT = -13701
625959 feet/sec YDOT = -4176
255592 meter/sec
ZDOT = -18602
634213 ZDOT = -5670
082908
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 19266
82884166
00016717 00000-0 10270-3 0 9127
2 25544 51
6416 232
0680 0007122 76
4255 283
7688 15
50081692 30559
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
82884166 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 232
0680 deg
Eccentricity:
0007122
Arg of perigee: 76
4255 deg
Mean anomaly: 283
7688 deg
Mean motion: 15
50081692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3055
Checksum: 320
Coasting Arc #14 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2019/267/19:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3102275
05 A = 6799159
32 meter
Y = -5660999
14 meter E =
0020981
Z = 2105331
34 I = 51
37258
XDOT = 5282
143532 Wp = 73
27662
YDOT = -836
738706 meter/sec RA = 226
17066 deg
ZDOT = 5493
889206 TA = 310
10781
MA = 310
29152
Ha = 229
919 n
mi
Hp = 218
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10178067
75 X = -3048968
06
Y = -18572831
82 feet Y = -5695392
82 meter
Z = 6907255
05 Z = 2090391
41
XDOT = 17329
867230 XDOT = 5264
421415
YDOT = -2745
205727 feet/sec YDOT = -777
768901 meter/sec
ZDOT = 18024
570886 ZDOT = 5519
504802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13833076
09 X = 4216321
59
Y = -16066091
46 feet Y = -4896944
68 meter
Z = 6839592
69 Z = 2084707
85
XDOT = 7408
662669 XDOT = 2258
160381
YDOT = 14157
813555 feet/sec YDOT = 4315
301572 meter/sec
ZDOT = 18141
156717 ZDOT = 5529
424567
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 19267
86034611
00016717 00000-0 10270-3 0 9135
2 25544 51
6402 226
9564 0007167 79
9532 280
2427 15
50126730 30716
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
86034611 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 226
9564 deg
Eccentricity:
0007167
Arg of perigee: 79
9532 deg
Mean anomaly: 280
2427 deg
Mean motion: 15
50126730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 305
Coasting Arc #15 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 845780
76 A = 6790595
15 meter
Y = -4569620
67 meter E =
0012848
Z = 4941264
19 I = 51
36275
XDOT = 6454
183582 Wp = 101
88567
YDOT = 3536
819822 meter/sec RA = 222
28206 deg
ZDOT = 2158
696567 TA = 326
95411
MA = 327
03433
Ha = 229
889 n
mi
Hp = 218
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2774871
26 X = 872814
90
Y = -14992193
80 feet Y = -4560011
09 meter
Z = 16211496
68 Z = 4945438
60
XDOT = 21175
142986 XDOT = 6403
668444
YDOT = 11603
739575 feet/sec YDOT = 3608
712741 meter/sec
ZDOT = 7082
337818 ZDOT = 2189
925535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5840448
90 X = 1780168
83
Y = 14061684
51 feet Y = 4286001
44 meter
Z = 16230729
98 Z = 4947126
50
XDOT = -23023
958944 XDOT = -7017
702686
YDOT = 1196
413135 feet/sec YDOT = 364
666724 meter/sec
ZDOT = 7224
243827 ZDOT = 2201
949519
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 19268
63397622
00016717 00000-0 10270-3 0 9146
2 25544 51
6403 223
1239 0007227 83
4453 276
7520 15
50138102 30837
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63397622 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 223
1239 deg
Eccentricity:
0007227
Arg of perigee: 83
4453 deg
Mean anomaly: 276
7520 deg
Mean motion: 15
50138102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 297
Coasting Arc #16 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 950049
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1033001
85 A = 6790379
34 meter
Y = -4446846
61 meter E =
0012367
Z = 5016895
34 I = 51
36647
XDOT = 6450
292468 Wp = 101
50550
YDOT = 3676
599974 meter/sec RA = 221
63771 deg
ZDOT = 1924
239840 TA = 329
72507
MA = 329
79646
Ha = 229
987 n
mi
Hp = 218
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3389113
69 X = 1058281
81
Y = -14589391
76 feet Y = -4435153
18 meter
Z = 16459630
37 Z = 5021974
94
XDOT = 21162
376865 XDOT = 6399
353414
YDOT = 12062
335872 feet/sec YDOT = 3748
447001 meter/sec
ZDOT = 6313
122836 ZDOT = 1955
448854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13729826
51 X = 4184851
12
Y = 5921088
07 feet Y = 1804747
64 meter
Z = 16482974
72 Z = 5024010
69
XDOT = -15330
813910 XDOT = -4672
832080
YDOT = 17521
125748 feet/sec YDOT = 5340
439128 meter/sec
ZDOT = 6454
933928 ZDOT = 1967
463861
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 19268
76291502
00016717 00000-0 10270-3 0 9151
2 25544 51
6419 222
4856 0007348 83
5848 276
6140 15
50100596 30859
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76291502 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 222
4856 deg
Eccentricity:
0007348
Arg of perigee: 83
5848 deg
Mean anomaly: 276
6140 deg
Mean motion: 15
50100596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 324
Coasting Arc #17 (Orbit 3099)
---------------------------------------
Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 965158
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1081122
61 A = 6789826
13 meter
Y = 4317847
34 meter E =
0020724
Z = -5145811
07 I = 51
39097
XDOT = -6653
087020 Wp = 81
33796
YDOT = -3455
327169 meter/sec RA = 216
66237 deg
ZDOT = -1503
724500 TA = 174
09769
MA = 174
07323
Ha = 229
923 n
mi
Hp = 218
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3546990
20 X = -1104330
26
Y = 14166165
81 feet Y = 4305627
23 meter
Z = -16882582
25 Z = -5151119
50
XDOT = -21827
713319 XDOT = -6606
649844
YDOT = -11336
375226 feet/sec YDOT = -3529
467172 meter/sec
ZDOT = -4933
479331 ZDOT = -1535
929498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13386361
27 X = -4080162
92
Y = -5765695
84 feet Y = -1757384
09 meter
Z = -16906953
01 Z = -5153239
28
XDOT = 14418
913759 XDOT = 4394
884914
YDOT = -18601
651990 feet/sec YDOT = -5669
783526 meter/sec
ZDOT = -5079
857135 ZDOT = -1548
340455
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 19269
72994825
00016717 00000-0 10270-3 0 9167
2 25544 51
6423 217
6936 0007175 86
1098 274
0873 15
50128994 31008
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
72994825 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 217
6936 deg
Eccentricity:
0007175
Arg of perigee: 86
1098 deg
Mean anomaly: 274
0873 deg
Mean motion: 15
50128994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 339
Coasting Arc #18 (Orbit 3115)
---------------------------------------
Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 965158
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1131599
89 A = 6789497
83 meter
Y = -4189068
80 meter E =
0010693
Z = 5213183
00 I = 51
41786
XDOT = 6874
657526 Wp = 101
76905
YDOT = 3220
585013 meter/sec RA = 211
68894 deg
ZDOT = 1091
620915 TA = 337
71727
MA = 337
76369
Ha = 229
940 n
mi
Hp = 218
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3712598
08 X = 1153036
41
Y = -13743664
03 feet Y = -4176294
00 meter
Z = 17103618
78 Z = 5218732
43
XDOT = 22554
650675 XDOT = 6832
830581
YDOT = 10566
223796 feet/sec YDOT = 3297
228538 meter/sec
ZDOT = 3581
433449 ZDOT = 1124
913490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13041096
56 X = 3974926
23
Y = 5632948
39 feet Y = 1716922
67 meter
Z = 17129073
35 Z = 5220941
56
XDOT = -13439
495063 XDOT = -4096
358095
YDOT = 19723
183184 feet/sec YDOT = 6011
626235 meter/sec
ZDOT = 3732
792419 ZDOT = 1137
755129
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 19270
76144891
00016717 00000-0 10270-3 0 9174
2 25544 51
6429 212
5823 0007238 89
8331 270
3649 15
50109312 31163
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
76144891 = yrday
fracday
Element set: 917
Inclination: 51
6429 deg
RA of node: 212
5823 deg
Eccentricity:
0007238
Arg of perigee: 89
8331 deg
Mean anomaly: 270
3649 deg
Mean motion: 15
50109312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3116
Checksum: 311
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