[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 12th 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 2875)
---------------------------------------
Vector Time (GMT): 2019/255/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3617952
07 A = 6798018
84 meter
Y = -5329881
97 meter E =
0020708
Z = 2134218
05 I = 51
29088
XDOT = 3157
238656 Wp = 56
51149
YDOT = 4346
525565 meter/sec RA = 288
77145 deg
ZDOT = 5475
320698 TA = 327
25612
MA = 327
38430
Ha = 229
077 n
mi
Hp = 218
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11869921
48 X = 3666916
72
Y = -17486489
41 feet Y = -5289149
55 meter
Z = 7002027
74 Z = 2151911
83
XDOT = 10358
394541 XDOT = 3081
804132
YDOT = 14260
254477 feet/sec YDOT = 4381
410654 meter/sec
ZDOT = 17963
650585 ZDOT = 5490
473671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13135453
84 X = -4003686
33
Y = -16522495
80 feet Y = -5036056
72 meter
Z = 7082917
84 Z = 2158873
36
XDOT = 15470
223669 XDOT = 4715
324174
YDOT = -4530
875421 feet/sec YDOT = -1381
010828 meter/sec
ZDOT = 18032
195520 ZDOT = 5496
213195
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 19255
28934544
00016717 00000-0 10270-3 0 9008
2 25544 51
6422 289
2458 0007959 32
3376 327
8261 15
50471300 28762
Satellite: ISS
Catalog Number: 25544
Epoch time: 19255
28934544 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 289
2458 deg
Eccentricity:
0007959
Arg of perigee: 32
3376 deg
Mean anomaly: 327
8261 deg
Mean motion: 15
50471300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 324
Coasting Arc #2 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2019/256/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3436485
16 A = 6797137
89 meter
Y = 5264477
54 meter E =
0009453
Z = -2597146
56 I = 51
27731
XDOT = -3163
611877 Wp = 67
92070
YDOT = -4628
575385 meter/sec RA = 283
79168 deg
ZDOT = -5208
046880 TA = 141
37968
MA = 141
31203
Ha = 229
290 n
mi
Hp = 218
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11274557
60 X = -3482483
27
Y = 17271907
93 feet Y = 5225790
92 meter
Z = -8520822
03 Z = -2613951
75
XDOT = -10379
304060 XDOT = -3086
321107
YDOT = -15185
614780 feet/sec YDOT = -4663
521427 meter/sec
ZDOT = -17086
767978 ZDOT = -5223
226248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13383510
87 X = 4079294
11
Y = 15652505
18 feet Y = 4770883
58 meter
Z = -8597649
63 Z = -2620563
61
XDOT = -16331
738102 XDOT = -4977
913774
YDOT = 4562
241949 feet/sec YDOT = 1390
571346 meter/sec
ZDOT = -17155
422133 ZDOT = -5228
972666
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
25617209
00016717 00000-0 10270-3 0 9013
2 25544 51
6413 284
4531 0008102 35
8608 324
3085 15
50451933 28911
Satellite: ISS
Catalog Number: 25544
Epoch time: 19256
25617209 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 284
4531 deg
Eccentricity:
0008102
Arg of perigee: 35
8608 deg
Mean anomaly: 324
3085 deg
Mean motion: 15
50451933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 298
Coasting Arc #3 (Orbit 2906)
---------------------------------------
Vector Time (GMT): 2019/257/05:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3230093
42 A = 6796129
33 meter
Y = -5161039
46 meter E =
0019666
Z = 2994044
03 I = 51
26744
XDOT = 3242
693813 Wp = 66
91883
YDOT = 4900
680441 meter/sec RA = 278
81053 deg
ZDOT = 4930
971004 TA = 327
53170
MA = 327
65252
Ha = 229
199 n
mi
Hp = 218
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10597419
37 X = 3273022
26
Y = -16932544
16 feet Y = -5124677
95 meter
Z = 9822979
11 Z = 3009839
31
XDOT = 10638
759229 XDOT = 3163
700190
YDOT = 16078
347904 feet/sec YDOT = 4936
501343 meter/sec
ZDOT = 16177
726392 ZDOT = 4946
530359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13506729
37 X = -4116851
11
Y = -14668358
10 feet Y = -4470915
55 meter
Z = 9895190
74 Z = 3016054
14
XDOT = 17236
829838 XDOT = 5253
785735
YDOT = -4870
666418 feet/sec YDOT = -1484
579124 meter/sec
ZDOT = 16248
099354 ZDOT = 4952
420683
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
28745133
00016717 00000-0 10270-3 0 9026
2 25544 51
6415 279
3409 0007995 39
8181 320
3555 15
50474694 29074
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
28745133 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 279
3409 deg
Eccentricity:
0007995
Arg of perigee: 39
8181 deg
Mean anomaly: 320
3555 deg
Mean motion: 15
50474694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2907
Checksum: 334
Coasting Arc #4 (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 = -1197216
02 A = 6800970
79 meter
Y = 6666443
37 meter E =
0012600
Z = -602494
48 I = 51
27686
XDOT = -4641
417633 Wp = 104
04771
YDOT = -1360
267347 meter/sec RA = 276
09105 deg
ZDOT = -5935
976871 TA = 82
47340
MA = 82
33028
Ha = 229
736 n
mi
Hp = 218
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3927874
09 X = -1268746
56
Y = 21871533
36 feet Y = 6652655
24 meter
Z = -1976687
93 Z = -608484
52
XDOT = -15227
748139 XDOT = -4597
028176
YDOT = -4462
819380 feet/sec YDOT = -1411
923373 meter/sec
ZDOT = -19474
989734 ZDOT = -5958
415112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21902697
56 X = -6675942
22
Y = -3735451
35 feet Y = -1138565
57 meter
Z = -2004421
25 Z = -610947
60
XDOT = 4067
978091 XDOT = 1239
919722
YDOT = -13534
982765 feet/sec YDOT = -4125
462747 meter/sec
ZDOT = -19576
910519 ZDOT = -5967
042326
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
80310003
00016717 00000-0 10270-3 0 9039
2 25544 51
6411 276
7887 0007247 45
9053 314
2693 15
50076097 29156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19257
80310003 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 276
7887 deg
Eccentricity:
0007247
Arg of perigee: 45
9053 deg
Mean anomaly: 314
2693 deg
Mean motion: 15
50076097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 309
Coasting Arc #5 (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 = 886319
56 A = 6800769
19 meter
Y = -6665828
43 meter E =
0020768
Z = 943623
69 I = 51
27373
XDOT = 4691
246439 Wp = 52
98312
YDOT = 1467
787443 meter/sec RA = 271
11281 deg
ZDOT = 5884
579135 TA = 317
27757
MA = 317
43885
Ha = 229
781 n
mi
Hp = 218
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2907872
56 X = 956209
30
Y = -21869515
84 feet Y = -6655526
10 meter
Z = 3095878
24 Z = 948099
56
XDOT = 15391
228474 XDOT = 4645
900494
YDOT = 4815
575601 feet/sec YDOT = 1519
995353 meter/sec
ZDOT = 19306
361990 ZDOT = 5907
257184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21935551
94 X = 6685956
23
Y = 2331005
64 feet Y = 710490
52 meter
Z = 3116710
11 Z = 949973
24
XDOT = -4257
910245 XDOT = -1297
811043
YDOT = 13778
520423 feet/sec YDOT = 4199
693025 meter/sec
ZDOT = 19409
367687 ZDOT = 5915
975271
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
83461990
00016717 00000-0 10270-3 0 9046
2 25544 51
6411 271
6777 0007328 49
0178 311
1606 15
50073440 29318
Satellite: ISS
Catalog Number: 25544
Epoch time: 19258
83461990 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 271
6777 deg
Eccentricity:
0007328
Arg of perigee: 49
0178 deg
Mean anomaly: 311
1606 deg
Mean motion: 15
50073440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2931
Checksum: 308
Coasting Arc #6 (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 = -626824
68 A = 6800373
87 meter
Y = 6638189
44 meter E =
0011463
Z = -1337943
87 I = 51
27391
XDOT = -4755
022749 Wp = 102
66164
YDOT = -1605
245911 meter/sec RA = 266
13462 deg
ZDOT = -5781
267657 TA = 91
94500
MA = 91
81371
Ha = 229
850 n
mi
Hp = 218
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2056511
40 X = -694509
22
Y = 21778836
74 feet Y = 6630801
26 meter
Z = -4389579
61 Z = -1341153
84
XDOT = -15600
468335 XDOT = -4708
636677
YDOT = -5266
554826 feet/sec YDOT = -1658
161165 meter/sec
ZDOT = -18967
413574 ZDOT = -5804
253070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21845116
18 X = -6658391
41
Y = -1097922
29 feet Y = -334646
71 meter
Z = -4404638
89 Z = -1342533
94
XDOT = 4524
195320 XDOT = 1378
974734
YDOT = -14089
530484 feet/sec YDOT = -4294
488891 meter/sec
ZDOT = -19071
810425 ZDOT = -5813
087817
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
80166759
00016717 00000-0 10270-3 0 9050
2 25544 51
6420 266
8860 0007307 53
0070 307
1748 15
50073767 29460
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
80166759 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 266
8860 deg
Eccentricity:
0007307
Arg of perigee: 53
0070 deg
Mean anomaly: 307
1748 deg
Mean motion: 15
50073767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 324
Coasting Arc #7 (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 = -1153315
94 A = 6800775
82 meter
Y = -6640643
84 meter E =
0017314
Z = -853430
99 I = 51
27574
XDOT = 4635
096150 Wp = 44
88937
YDOT = -1552
536090 meter/sec RA = 265
97472 deg
ZDOT = 5902
183507 TA = 305
84485
MA = 306
00556
Ha = 229
794 n
mi
Hp = 218
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3783844
96 X = -1074827
11
Y = -21786889
23 feet Y = -6653102
26 meter
Z = -2799970
44 Z = -858842
08
XDOT = 15207
008366 XDOT = 4623
442874
YDOT = -5093
622343 feet/sec YDOT = -1500
767726 meter/sec
ZDOT = 19364
119118 ZDOT = 5924
671046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20447998
50 X = 6232549
94
Y = -8410090
56 feet Y = -2563395
60 meter
Z = -2824109
33 Z = -860788
52
XDOT = 7634
108707 XDOT = 2326
876334
YDOT = 12117
887638 feet/sec YDOT = 3693
532152 meter/sec
ZDOT = 19466
473034 ZDOT = 5933
380981
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
80166719
00016717 00000-0 10270-3 0 9067
2 25544 51
6423 266
8863 0007321 52
4335 307
7479 15
50091330 29462
Satellite: ISS
Catalog Number: 25544
Epoch time: 19259
80166719 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 266
8863 deg
Eccentricity:
0007321
Arg of perigee: 52
4335 deg
Mean anomaly: 307
7479 deg
Mean motion: 15
50091330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 323
Coasting Arc #8 (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 = 1416611
24 A = 6801090
25 meter
Y = 6632645
98 meter E =
0016538
Z = 450689
89 I = 51
27968
XDOT = -4610
990229 Wp = 105
28215
YDOT = 1401
576683 meter/sec RA = 260
99778 deg
ZDOT = -5953
974860 TA = 69
84274
MA = 69
66492
Ha = 229
899 n
mi
Hp = 218
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4647674
66 X = 1340148
56
Y = 21760649
53 feet Y = 6648060
04 meter
Z = 1478641
36 Z = 457384
99
XDOT = -15127
920700 XDOT = -4597
398998
YDOT = 4598
348696 feet/sec YDOT = 1350
088781 meter/sec
ZDOT = -19534
038253 ZDOT = -5976
340640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20070420
76 X = -6117464
25
Y = 9602883
24 feet Y = 2926958
81 meter
Z = 1508632
52 Z = 459831
19
XDOT = -7279
696502 XDOT = -2218
851494
YDOT = -12039
484232 feet/sec YDOT = -3669
634794 meter/sec
ZDOT = -19635
826754 ZDOT = -5984
999995
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
83318589
00016717 00000-0 10270-3 0 9077
2 25544 51
6420 261
7759 0007255 57
3635 302
8215 15
50060351 29621
Satellite: ISS
Catalog Number: 25544
Epoch time: 19260
83318589 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 261
7759 deg
Eccentricity:
0007255
Arg of perigee: 57
3635 deg
Mean anomaly: 302
8215 deg
Mean motion: 15
50060351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2962
Checksum: 312
Coasting Arc #9 (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 = -1724641
54 A = 6801072
24 meter
Y = -6569547
28 meter E =
0018917
Z = -107880
92 I = 51
28703
XDOT = 4615
878271 Wp = 50
11234
YDOT = -1298
273221 meter/sec RA = 256
02003 deg
ZDOT = 5979
613764 TA = 308
72145
MA = 308
89042
Ha = 229
817 n
mi
Hp = 218
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5658272
75 X = -1650526
75
Y = -21553632
82 feet Y = -6588419
05 meter
Z = -353940
02 Z = -116078
16
XDOT = 15143
957582 XDOT = 4601
006902
YDOT = -4259
426579 feet/sec YDOT = -1246
737911 meter/sec
ZDOT = 19618
155394 ZDOT = 6002
000200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19446463
60 X = 5927282
10
Y = -10880384
07 feet Y = -3316341
07 meter
Z = -390778
42 Z = -119109
26
XDOT = 7093
410415 XDOT = 2162
071495
YDOT = 12045
692517 feet/sec YDOT = 3671
527079 meter/sec
ZDOT = 19720
031866 ZDOT = 6010
665713
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
80023220
00016717 00000-0 10270-3 0 9081
2 25544 51
6427 256
9844 0007210 58
9060 301
2797 15
50095818 29779
Satellite: ISS
Catalog Number: 25544
Epoch time: 19261
80023220 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 256
9844 deg
Eccentricity:
0007210
Arg of perigee: 58
9060 deg
Mean anomaly: 301
2797 deg
Mean motion: 15
50095818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 314
Coasting Arc #10 (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 = 1977902
11 A = 6801149
57 meter
Y = 6497140
14 meter E =
0015227
Z = -299453
79 I = 51
29668
XDOT = -4659
300129 Wp = 110
09262
YDOT = 1155
023484 meter/sec RA = 251
04375 deg
ZDOT = -5967
973318 TA = 73
14316
MA = 72
97622
Ha = 229
941 n
mi
Hp = 218
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6489180
15 X = 1906556
81
Y = 21316076
56 feet Y = 6518859
50 meter
Z = -982459
94 Z = -290019
43
XDOT = -15286
417745 XDOT = -4642
880200
YDOT = 3789
447127 feet/sec YDOT = 1103
011372 meter/sec
ZDOT = -19579
964953 ZDOT = -5990
566903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18802857
67 X = -5731111
02
Y = 11959046
39 feet Y = 3645117
34 meter
Z = -939978
42 Z = -286505
42
XDOT = -6830
476158 XDOT = -2081
929133
YDOT = -12218
156417 feet/sec YDOT = -3724
094076 meter/sec
ZDOT = -19682
777479 ZDOT = -5999
310576
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
83174813
00016717 00000-0 10270-3 0 9091
2 25544 51
6433 251
8736 0007188 63
8273 296
3616 15
50057762 29933
Satellite: ISS
Catalog Number: 25544
Epoch time: 19262
83174813 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 251
8736 deg
Eccentricity:
0007188
Arg of perigee: 63
8273 deg
Mean anomaly: 296
3616 deg
Mean motion: 15
50057762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 338
Coasting Arc #11 (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 = -2264429
81 A = 6800889
89 meter
Y = -6371081
29 meter E =
0020233
Z = 642732
91 I = 51
30754
XDOT = 4728
789078 Wp = 56
87189
YDOT = -1069
053282 meter/sec RA = 246
06719 deg
ZDOT = 5937
926602 TA = 310
09188
MA = 310
26908
Ha = 229
887 n
mi
Hp = 218
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7429231
65 X = -2196140
31
Y = -20902497
66 feet Y = -6396021
88 meter
Z = 2108703
76 Z = 631899
16
XDOT = 15514
399863 XDOT = 4711
548631
YDOT = -3507
392659 feet/sec YDOT = -1016
268790 meter/sec
ZDOT = 19481
386490 ZDOT = 5960
855697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17928677
93 X = 5464661
03
Y = -13071882
20 feet Y = -3984309
69 meter
Z = 2059836
47 Z = 627838
16
XDOT = 6776
416722 XDOT = 2065
451817
YDOT = 12446
709064 feet/sec YDOT = 3793
756923 meter/sec
ZDOT = 19585
725198 ZDOT = 5969
729040
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
86326051
00016717 00000-0 10270-3 0 9100
2 25544 51
6427 246
7625 0007268 65
7804 294
4105 15
50104961 30091
Satellite: ISS
Catalog Number: 25544
Epoch time: 19263
86326051 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 246
7625 deg
Eccentricity:
0007268
Arg of perigee: 65
7804 deg
Mean anomaly: 294
4105 deg
Mean motion: 15
50104961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3009
Checksum: 305
Coasting Arc #12 (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 = 2489051
73 A = 6800734
54 meter
Y = 6239908
08 meter E =
0013773
Z = -1046033
19 I = 51
32048
XDOT = -4833
114118 Wp = 112
13613
YDOT = 956
425505 meter/sec RA = 241
09264 deg
ZDOT = -5862
427906 TA = 79
23015
MA = 79
07513
Ha = 229
987 n
mi
Hp = 218
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8166180
22 X = 2424171
37
Y = 20472139
37 feet Y = 6267379
61 meter
Z = -3431867
41 Z = -1034099
96
XDOT = -15856
673616 XDOT = -4814
973296
YDOT = 3137
878955 feet/sec YDOT = 902
479489 meter/sec
ZDOT = -19233
687356 ZDOT = -5885
861510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17066567
95 X = -5201889
91
Y = 13960452
76 feet Y = 4255146
00 meter
Z = -3377975
82 Z = -1029607
03
XDOT = -6697
942690 XDOT = -2041
532932
YDOT = -12813
619341 feet/sec YDOT = -3905
591175 meter/sec
ZDOT = -19340
321701 ZDOT = -5894
930055
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
83030568
00016717 00000-0 10270-3 0 9114
2 25544 51
6420 241
9715 0007174 70
5747 289
6179 15
50057914 30246
Satellite: ISS
Catalog Number: 25544
Epoch time: 19264
83030568 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 241
9715 deg
Eccentricity:
0007174
Arg of perigee: 70
5747 deg
Mean anomaly: 289
6179 deg
Mean motion: 15
50057914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3024
Checksum: 314
Coasting Arc #13 (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 = -2737318
59 A = 6800239
37 meter
Y = -6059386
16 meter E =
0020811
Z = 1381736
57 I = 51
33639
XDOT = 4957
451412 Wp = 64
66849
YDOT = -908
609829 meter/sec RA = 236
11787 deg
ZDOT = 5776
896162 TA = 310
43572
MA = 310
61705
Ha = 229
878 n
mi
Hp = 218
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8980704
05 X = -2676069
08
Y = -19879875
84 feet Y = -6089654
28 meter
Z = 4533256
46 Z = 1368588
55
XDOT = 16264
604370 XDOT = 4939
182232
YDOT = -2981
003377 feet/sec YDOT = -853
274132 meter/sec
ZDOT = 18953
071398 ZDOT = 5800
933349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16001727
85 X = 4877326
65
Y = -14843943
15 feet Y = -4524433
87 meter
Z = 4473810
51 Z = 1363617
44
XDOT = 6855
218897 XDOT = 2089
470720
YDOT = 13194
853877 feet/sec YDOT = 4021
791462 meter/sec
ZDOT = 19062
458171 ZDOT = 5810
237250
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
86181639
00016717 00000-0 10270-3 0 9125
2 25544 51
6419 236
8604 0007136 72
8866 287
3066 15
50116384 30404
Satellite: ISS
Catalog Number: 25544
Epoch time: 19265
86181639 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 236
8604 deg
Eccentricity:
0007136
Arg of perigee: 72
8866 deg
Mean anomaly: 287
3066 deg
Mean motion: 15
50116384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 323
Coasting Arc #14 (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 = 2916389
43 A = 6799827
76 meter
Y = 5880836
81 meter E =
0012291
Z = -1773827
74 I = 51
35403
XDOT = -5109
979123 Wp = 110
26053
YDOT = 844
147180 meter/sec RA = 231
14406 deg
ZDOT = -5638
866339 TA = 89
25180
MA = 89
11097
Ha = 229
964 n
mi
Hp = 218
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9568206
78 X = 2859027
73
Y = 19294084
02 feet Y = 5913129
15 meter
Z = -5819644
80 Z = -1759800
49
XDOT = -16765
023369 XDOT = -5091
648346
YDOT = 2769
511744 feet/sec YDOT = 787
106126 meter/sec
ZDOT = -18500
217646 ZDOT = -5663
644211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14993064
05 X = -4569885
92
Y = 15484026
55 feet Y = 4719531
29 meter
Z = -5756168
63 Z = -1754480
20
XDOT = -7022
676713 XDOT = -2140
511862
YDOT = -13674
881132 feet/sec YDOT = -4168
103769 meter/sec
ZDOT = -18612
981145 ZDOT = -5673
236653
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
82885795
00016717 00000-0 10270-3 0 9137
2 25544 51
6417 232
0683 0007099 76
3987 283
7954 15
50076757 30559
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
82885795 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 232
0683 deg
Eccentricity:
0007099
Arg of perigee: 76
3987 deg
Mean anomaly: 283
7954 deg
Mean motion: 15
50076757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3055
Checksum: 360
Coasting Arc #15 (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 = -3111157
01 A = 6799191
07 meter
Y = -5659611
44 meter E =
0020961
Z = 2096070
81 I = 51
37275
XDOT = 5275
445178 Wp = 73
17380
YDOT = -848
875677 meter/sec RA = 226
17105 deg
ZDOT = 5498
420308 TA = 310
10149
MA = 310
28502
Ha = 229
919 n
mi
Hp = 218
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10207208
04 X = -3057819
89
Y = -18568279
01 feet Y = -5694104
28 meter
Z = 6876872
73 Z = 2081087
81
XDOT = 17307
891004 XDOT = 5257
837269
YDOT = -2785
025186 feet/sec YDOT = -789
980139 meter/sec
ZDOT = 18039
436706 ZDOT = 5524
003644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13818707
86 X = 4211942
16
Y = -16091615
73 feet Y = -4904724
47 meter
Z = 6809014
34 Z = 2075387
57
XDOT = 7436
404809 XDOT = 2266
616186
YDOT = 14124
270765 feet/sec YDOT = 4305
077729 meter/sec
ZDOT = 18155
876426 ZDOT = 5533
911135
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
86036584
00016717 00000-0 10270-3 0 9147
2 25544 51
6403 226
9567 0007145 79
9210 280
2746 15
50121469 30717
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
86036584 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 226
9567 deg
Eccentricity:
0007145
Arg of perigee: 79
9210 deg
Mean anomaly: 280
2746 deg
Mean motion: 15
50121469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 318
Coasting Arc #16 (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 = 833328
38 A = 6790630
33 meter
Y = -4576454
70 meter E =
0012859
Z = 4937109
28 I = 51
36293
XDOT = 6456
205483 Wp = 101
90066
YDOT = 3525
586067 meter/sec RA = 222
28263 deg
ZDOT = 2170
899350 TA = 326
81375
MA = 326
89434
Ha = 229
891 n
mi
Hp = 218
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2734017
00 X = 860460
04
Y = -15014615
16 feet Y = -4566983
83 meter
Z = 16197865
09 Z = 4941223
44
XDOT = 21181
776519 XDOT = 6405
756540
YDOT = 11566
883421 feet/sec YDOT = 3597
501967 meter/sec
ZDOT = 7122
373197 ZDOT = 2202
138301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5886866
87 X = 1794317
02
Y = 14058582
76 feet Y = 4285056
03 meter
Z = 16216824
60 Z = 4942888
14
XDOT = -23009
667810 XDOT = -7013
346749
YDOT = 1227
494806 feet/sec YDOT = 374
140417 meter/sec
ZDOT = 7264
325217 ZDOT = 2214
166326
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
63399877
00016717 00000-0 10270-3 0 9151
2 25544 51
6404 223
1242 0007206 83
4082 276
7889 15
50132191 30837
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63399877 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 223
1242 deg
Eccentricity:
0007206
Arg of perigee: 83
4082 deg
Mean anomaly: 276
7889 deg
Mean motion: 15
50132191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 322
Coasting Arc #17 (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 = 1020283
94 A = 6790413
62 meter
Y = -4454104
55 meter E =
0012377
Z = 5013112
27 I = 51
36664
XDOT = 6452
829493 Wp = 101
53448
YDOT = 3665
428360 meter/sec RA = 221
63831 deg
ZDOT = 1936
901155 TA = 329
56798
MA = 329
63976
Ha = 229
989 n
mi
Hp = 218
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3347388
27 X = 1045664
38
Y = -14613203
90 feet Y = -4442552
78 meter
Z = 16447218
74 Z = 5018130
34
XDOT = 21170
700435 XDOT = 6401
953673
YDOT = 12025
683596 feet/sec YDOT = 3737
304113 meter/sec
ZDOT = 6354
662582 ZDOT = 1968
122647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13760933
91 X = 4194332
66
Y = 5884573
13 feet Y = 1793617
89 meter
Z = 16470283
48 Z = 5020142
40
XDOT = -15298
948270 XDOT = -4663
119433
YDOT = 17533
543942 feet/sec YDOT = 5344
224193 meter/sec
ZDOT = 6496
531031 ZDOT = 1980
142658
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
76293807
00016717 00000-0 10270-3 0 9162
2 25544 51
6420 222
4859 0007327 83
5388 276
6596 15
50094554 30851
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76293807 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 222
4859 deg
Eccentricity:
0007327
Arg of perigee: 83
5388 deg
Mean anomaly: 276
6596 deg
Mean motion: 15
50094554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 347
Coasting Arc #18 (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 = -1065679
22 A = 6789860
71 meter
Y = 4325852
49 meter E =
0020678
Z = -5142310
48 I = 51
39114
XDOT = -6656
211641 Wp = 81
24633
YDOT = -3442
705481 meter/sec RA = 216
66305 deg
ZDOT = -1518
858802 TA = 174
03948
MA = 174
01483
Ha = 229
926 n
mi
Hp = 218
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3496322
89 X = -1088994
53
Y = 14192429
44 feet Y = 4313804
48 meter
Z = -16871097
39 Z = -5147544
16
XDOT = -21837
964701 XDOT = -6609
841859
YDOT = -11294
965489 feet/sec YDOT = -3516
880804 meter/sec
ZDOT = -4983
132554 ZDOT = -1551
079143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13420756
83 X = -4090646
68
Y = -5720242
79 feet Y = -1743530
00 meter
Z = -16895128
37 Z = -5149635
13
XDOT = 14383
077999 XDOT = 4383
962174
YDOT = -18615
880454 feet/sec YDOT = -5674
120362 meter/sec
ZDOT = -5129
580802 ZDOT = -1563
496228
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
72997516
00016717 00000-0 10270-3 0 9178
2 25544 51
6424 217
6940 0007153 86
0555 274
1413 15
50122480 31002
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
72997516 = yrday
fracday
Element set: 917
Inclination: 51
6424 deg
RA of node: 217
6940 deg
Eccentricity:
0007153
Arg of perigee: 86
0555 deg
Mean anomaly: 274
1413 deg
Mean motion: 15
50122480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3100
Checksum: 304
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