[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 26th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16989 6378 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
175/23:25:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 216
3
176/17:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 216
3
180/21:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 216
3
184/00:03:16
120 0
5 1
6 1
6
N/A -1
5 -0
0 228
4
000/00:00:32
239 0
2 -0
0 217
2
184/09:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 217
3
187/16:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 217
5
Coasting Arc #1 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2019/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -917057
54 A = 6786725
98 meter
Y = -4376134
41 meter E =
0021336
Z = -5124589
35 I = 51
40160
XDOT = 6730
284817 Wp = 94
68105
YDOT = -3265
939002 meter/sec RA = 324
35528 deg
ZDOT = 1588
575206 TA = 190
70975
MA = 190
75525
Ha = 228
556 n
mi
Hp = 216
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3008718
95 X = -843161
96
Y = -14357396
37 feet Y = -4385975
84 meter
Z = -16812957
17 Z = -5128865
05
XDOT = 22080
986931 XDOT = 6758
588914
YDOT = -10715
022974 feet/sec YDOT = -3190
518160 meter/sec
ZDOT = 5211
860911 ZDOT = 1621
336555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14279771
91 X = -4352474
48
Y = 3262027
95 feet Y = 994266
12 meter
Z = -16831816
22 Z = -5130337
58
XDOT = -11037
183616 XDOT = -3364
133566
YDOT = -20722
893475 feet/sec YDOT = -6316
337931 meter/sec
ZDOT = 5360
815011 ZDOT = 1633
976415
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 19175
51330652
00016717 00000-0 10270-3 0 9005
2 25544 51
6405 324
9425 0008162 83
1049 277
1030 15
51220279 16386
Satellite: ISS
Catalog Number: 25544
Epoch time: 19175
51330652 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 324
9425 deg
Eccentricity:
0008162
Arg of perigee: 83
1049 deg
Mean anomaly: 277
1030 deg
Mean motion: 15
51220279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 285
Coasting Arc #2 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:25:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4581800
40 A = 6787772
82 meter
Y = 1308744
12 meter E =
0014212
Z = 4822762
44 I = 51
39169
XDOT = -4289
853877 Wp = 99
11337
YDOT = 5858
601384 meter/sec RA = 322
02116 deg
ZDOT = 2477
215640 TA = 326
43604
MA = 326
52599
Ha = 228
354 n
mi
Hp = 216
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15032153
55 X = 4543398
96
Y = 4293779
91 feet Y = 1359765
78 meter
Z = 15822711
41 Z = 4844925
86
XDOT = -14074
323745 XDOT = -4367
080473
YDOT = 19221
133148 feet/sec YDOT = 5810
197157 meter/sec
ZDOT = 8127
347899 ZDOT = 2456
190329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6004419
49 X = -1830147
06
Y = 14323536
88 feet Y = 4365814
04 meter
Z = 15923053
11 Z = 4853346
59
XDOT = -16400
340341 XDOT = -4998
823736
YDOT = -15833
856375 feet/sec YDOT = -4826
159423 meter/sec
ZDOT = 8031
305414 ZDOT = 2447
941890
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 19176
02868767
00016717 00000-0 10270-3 0 9016
2 25544 51
6395 322
3881 0008040 81
6940 278
5123 15
51233610 16460
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02868767 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 322
3881 deg
Eccentricity:
0008040
Arg of perigee: 81
6940 deg
Mean anomaly: 278
5123 deg
Mean motion: 15
51233610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 310
Coasting Arc #3 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2019/176/17:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711225
32 A = 6787912
32 meter
Y = 918179
72 meter E =
0014573
Z = 4788461
90 I = 51
37428
XDOT = -3807
498535 Wp = 101
38400
YDOT = 6149
986657 meter/sec RA = 318
17167 deg
ZDOT = 2557
387541 TA = 323
30907
MA = 323
40876
Ha = 228
342 n
mi
Hp = 216
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15456776
00 X = 4677348
22
Y = 3012400
67 feet Y = 970674
01 meter
Z = 15710176
83 Z = 4811265
01
XDOT = -12491
793094 XDOT = -3888
408792
YDOT = 20177
121577 feet/sec YDOT = 6106
955864 meter/sec
ZDOT = 8390
379072 ZDOT = 2538
696348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15460356
01 X = -4712316
51
Y = -2389126
80 feet Y = -728205
85 meter
Z = 15813462
73 Z = 4819943
44
XDOT = 11545
954224 XDOT = 3519
206847
YDOT = -19542
055243 feet/sec YDOT = -5956
418438 meter/sec
ZDOT = 8304
897090 ZDOT = 2531
332633
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 19176
80175972
00016717 00000-0 10270-3 0 9022
2 25544 51
6416 318
5503 0007991 85
9770 274
2294 15
51233160 16589
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
80175972 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 318
5503 deg
Eccentricity:
0007991
Arg of perigee: 85
9770 deg
Mean anomaly: 274
2294 deg
Mean motion: 15
51233160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 325
Coasting Arc #4 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2019/177/17:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4325678
72 A = 6786858
05 meter
Y = -1325845
41 meter E =
0021310
Z = -5078048
81 I = 51
34714
XDOT = 3981
306284 Wp = 81
15519
YDOT = -6289
886126 meter/sec RA = 313
18446 deg
ZDOT = -1752
302281 TA = 171
80023
MA = 171
76535
Ha = 228
561 n
mi
Hp = 216
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14191859
32 X = -4285864
91
Y = -4349886
52 feet Y = -1373995
00 meter
Z = -16660265
12 Z = -5098964
78
XDOT = 13062
028492 XDOT = 4059
857401
YDOT = -20636
109336 feet/sec YDOT = -6244
924962 meter/sec
ZDOT = -5749
023232 ZDOT = -1732
772514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14307173
75 X = 4360826
56
Y = 3531498
50 feet Y = 1076400
74 meter
Z = -16754943
00 Z = -5106906
63
XDOT = -11630
463345 XDOT = -3544
965228
YDOT = 20314
608722 feet/sec YDOT = 6191
892738 meter/sec
ZDOT = -5659
736597 ZDOT = -1725
087715
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 19177
76809916
00016717 00000-0 10270-3 0 9031
2 25544 51
6424 313
7540 0008115 88
9246 271
2834 15
51209915 16731
Satellite: ISS
Catalog Number: 25544
Epoch time: 19177
76809916 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 313
7540 deg
Eccentricity:
0008115
Arg of perigee: 88
9246 deg
Mean anomaly: 271
2834 deg
Mean motion: 15
51209915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1673
Checksum: 326
Coasting Arc #5 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2019/178/17:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3942797
85 A = 6786047
21 meter
Y = 1755941
30 meter E =
0011301
Z = 5227142
78 I = 51
32192
XDOT = -4099
487486 Wp = 99
91639
YDOT = 6417
816687 meter/sec RA = 308
19540 deg
ZDOT = 932
656377 TA = 341
10442
MA = 341
14632
Ha = 228
415 n
mi
Hp = 216
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12935688
49 X = 3897478
77
Y = 5760962
28 feet Y = 1799778
38 meter
Z = 17149418
57 Z = 5246185
61
XDOT = -13449
762094 XDOT = -4175
479003
YDOT = 21055
829026 feet/sec YDOT = 6371
548331 meter/sec
ZDOT = 3059
896250 ZDOT = 912
558798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13215534
52 X = -4028094
92
Y = -4786299
79 feet Y = -1458864
18 meter
Z = 17235552
27 Z = 5253396
33
XDOT = 11507
034942 XDOT = 3507
344250
YDOT = -21041
572920 feet/sec YDOT = -6413
471426 meter/sec
ZDOT = 2968
032953 ZDOT = 904
656444
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 19178
79885775
00016717 00000-0 10270-3 0 9043
2 25544 51
6416 308
6386 0008186 91
9662 268
2427 15
51235711 16891
Satellite: ISS
Catalog Number: 25544
Epoch time: 19178
79885775 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 308
6386 deg
Eccentricity:
0008186
Arg of perigee: 91
9662 deg
Mean anomaly: 268
2427 deg
Mean motion: 15
51235711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 358
Coasting Arc #6 (Orbit 1703)
---------------------------------------
Vector Time (GMT): 2019/179/17:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3608580
08 A = 6785877
43 meter
Y = -2250776
80 meter E =
0022931
Z = -5307688
31 I = 51
30192
XDOT = 4132
064202 Wp = 91
44967
YDOT = -6433
543865 meter/sec RA = 303
20343 deg
ZDOT = -81
969345 TA = 177
76846
MA = 177
75822
Ha = 228
560 n
mi
Hp = 216
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11839173
51 X = -3557361
17
Y = -7384438
32 feet Y = -2290843
32 meter
Z = -17413675
55 Z = -5325093
43
XDOT = 13556
641082 XDOT = 4204
096990
YDOT = -21107
427379 feet/sec YDOT = -6386
933454 meter/sec
ZDOT = -268
928297 ZDOT = -61
723236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12351655
45 X = 3764784
58
Y = 6275915
83 feet Y = 1912899
14 meter
Z = -17492328
12 Z = -5331661
61
XDOT = -11101
157989 XDOT = -3383
632955
YDOT = 21364
550427 feet/sec YDOT = 6511
914970 meter/sec
ZDOT = -176
400665 ZDOT = -53
766923
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 19179
76519423
00016717 00000-0 10270-3 0 9056
2 25544 51
6423 303
8423 0008114 95
7017 264
5060 15
51209539 17044
Satellite: ISS
Catalog Number: 25544
Epoch time: 19179
76519423 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 303
8423 deg
Eccentricity:
0008114
Arg of perigee: 95
7017 deg
Mean anomaly: 264
5060 deg
Mean motion: 15
51209539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1704
Checksum: 304
Coasting Arc #7 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2019/180/17:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3292860
42 A = 6785954
39 meter
Y = 2755867
22 meter E =
0010974
Z = 5245164
71 I = 51
28480
XDOT = -4140
006076 Wp = 88
08624
YDOT = 6413
689070 meter/sec RA = 298
21038 deg
ZDOT = -769
012153 TA = 9
30435
MA = 9
28403
Ha = 228
424 n
mi
Hp = 216
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10803347
85 X = 3236320
63
Y = 9041559
12 feet Y = 2792373
29 meter
Z = 17208545
63 Z = 5261023
38
XDOT = -13582
697100 XDOT = -4207
682645
YDOT = 21042
286976 feet/sec YDOT = 6367
014345 meter/sec
ZDOT = -2523
005752 ZDOT = -789
286120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11610339
97 X = -3538831
62
Y = -7822606
42 feet Y = -2384330
44 meter
Z = 17280132
91 Z = 5266984
51
XDOT = 10618
049815 XDOT = 3236
381584
YDOT = -21549
996226 feet/sec YDOT = -6568
438850 meter/sec
ZDOT = -2615
648289 ZDOT = -797
249599
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 19180
79594962
00016717 00000-0 10270-3 0 9063
2 25544 51
6418 298
7265 0008242 98
7842 261
4243 15
51246354 17208
Satellite: ISS
Catalog Number: 25544
Epoch time: 19180
79594962 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 298
7265 deg
Eccentricity:
0008242
Arg of perigee: 98
7842 deg
Mean anomaly: 261
4243 deg
Mean motion: 15
51246354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 335
Coasting Arc #8 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2019/180/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173028
10 A = 6786049
41 meter
Y = 1073535
54 meter E =
0011260
Z = 5233367
66 I = 51
28087
XDOT = -2902
652111 Wp = 104
30270
YDOT = 7048
982013 meter/sec RA = 297
59588 deg
ZDOT = 864
263284 TA = 337
37095
MA = 337
42056
Ha = 228
387 n
mi
Hp = 216
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13691037
08 X = 4135292
51
Y = 3522098
21 feet Y = 1119989
38 meter
Z = 17169841
41 Z = 5253547
26
XDOT = -9523
136848 XDOT = -2985
458236
YDOT = 23126
581408 feet/sec YDOT = 7016
059378 meter/sec
ZDOT = 2835
509463 ZDOT = 849
963318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11169325
28 X = -3404410
35
Y = 8482331
71 feet Y = 2585414
70 meter
Z = 17261209
33 Z = 5261216
60
XDOT = -11641
022542 XDOT = -3548
183671
YDOT = -20993
772266 feet/sec YDOT = -6398
901787 meter/sec
ZDOT = 2769
880775 ZDOT = 844
259660
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 19180
92479475
00016717 00000-0 10270-3 0 9070
2 25544 51
6397 298
0871 0008113 98
5641 261
6429 15
51223354 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 19180
92479475 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 298
0871 deg
Eccentricity:
0008113
Arg of perigee: 98
5641 deg
Mean anomaly: 261
6429 deg
Mean motion: 15
51223354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 331
Coasting Arc #9 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2019/181/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3932522
07 A = 6785847
91 meter
Y = -1626553
16 meter E =
0022880
Z = -5305447
24 I = 51
26610
XDOT = 2931
767005 Wp = 93
88303
YDOT = -7062
372908 meter/sec RA = 292
60138 deg
ZDOT = -9
454387 TA = 176
03524
MA = 176
01708
Ha = 228
536 n
mi
Hp = 216
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12901975
30 X = -3888270
30
Y = -5336460
50 feet Y = -1670280
96 meter
Z = -17406322
96 Z = -5324442
79
XDOT = 9618
658153 XDOT = 3010
568510
YDOT = -23170
514791 feet/sec YDOT = -7029
147226 meter/sec
ZDOT = -31
018330 ZDOT = 4
977118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11987415
46 X = 3653764
23
Y = -6945602
48 feet Y = -2117019
64 meter
Z = -17492264
94 Z = -5331642
36
XDOT = 12114
806496 XDOT = 3692
593020
YDOT = 20807
518714 feet/sec YDOT = 6342
131704 meter/sec
ZDOT = 35
198584 ZDOT = 10
728529
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 19181
89112590
00016717 00000-0 10270-3 0 9080
2 25544 51
6402 293
2910 0008135 101
4325 258
7741 15
51219547 17371
Satellite: ISS
Catalog Number: 25544
Epoch time: 19181
89112590 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 293
2910 deg
Eccentricity:
0008135
Arg of perigee: 101
4325 deg
Mean anomaly: 258
7741 deg
Mean motion: 15
51219547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 305
Coasting Arc #10 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2019/182/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3714875
34 A = 6786038
21 meter
Y = 2180283
15 meter E =
0010676
Z = 5234373
66 I = 51
25456
XDOT = -2941
513138 Wp = 91
95433
YDOT = 7035
760986 meter/sec RA = 287
60647 deg
ZDOT = -841
870337 TA = 6
14002
MA = 6
12694
Ha = 228
340 n
mi
Hp = 216
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12187911
21 X = 3664793
12
Y = 7153159
96 feet Y = 2221544
43 meter
Z = 17173141
93 Z = 5252297
85
XDOT = -9650
633656 XDOT = -3015
881092
YDOT = 23083
205335 feet/sec YDOT = 7002
451274 meter/sec
ZDOT = -2762
041787 ZDOT = -856
338282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12909478
50 X = -3934809
05
Y = 5501687
89 feet Y = 1676914
47 meter
Z = 17254172
72 Z = 5259071
84
XDOT = -12512
823488 XDOT = -3813
908599
YDOT = -20478
857949 feet/sec YDOT = -6241
955903 meter/sec
ZDOT = -2828
410463 ZDOT = -862
099509
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 19182
92187860
00016717 00000-0 10270-3 0 9098
2 25544 51
6396 288
1755 0008048 105
0399 255
1643 15
51230068 17538
Satellite: ISS
Catalog Number: 25544
Epoch time: 19182
92187860 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 288
1755 deg
Eccentricity:
0008048
Arg of perigee: 105
0399 deg
Mean anomaly: 255
1643 deg
Mean motion: 15
51230068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 330
Coasting Arc #11 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2019/183/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916289
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3572322
93 A = 6786793
07 meter
Y = -2751269
06 meter E =
0021317
Z = -5091768
58 I = 51
24822
XDOT = 2911
458237 Wp = 104
76721
YDOT = -6871
254691 meter/sec RA = 282
61128 deg
ZDOT = 1670
717365 TA = 181
49805
MA = 181
50444
Ha = 228
448 n
mi
Hp = 216
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11720219
58 X = -3516559
21
Y = -9026473
29 feet Y = -2790904
47 meter
Z = -16705277
51 Z = -5108986
53
XDOT = 9552
028337 XDOT = 2979
962853
YDOT = -22543
486519 feet/sec YDOT = -6838
314023 meter/sec
ZDOT = 5481
356185 ZDOT = 1685
025021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14073861
09 X = 4289712
86
Y = -4261756
49 feet Y = -1298983
38 meter
Z = -16783054
82 Z = -5115475
11
XDOT = 12596
547203 XDOT = 3839
427587
YDOT = 19761
395653 feet/sec YDOT = 6023
273395 meter/sec
ZDOT = 5546
967893 ZDOT = 1690
715814
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 19183
88820778
00016717 00000-0 10270-3 0 9108
2 25544 51
6400 283
3797 0007983 108
4945 251
7074 15
51219858 17688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19183
88820778 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 283
3797 deg
Eccentricity:
0007983
Arg of perigee: 108
4945 deg
Mean anomaly: 251
7074 deg
Mean motion: 15
51219858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 350
Coasting Arc #12 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2019/184/00:03:32
239
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3908732
89 A = 6786923
15 meter
Y = -1861661
08 meter E =
0020990
Z = -5245161
28 I = 51
24749
XDOT = 2264
814972 Wp = 101
17435
YDOT = -7250
703834 meter/sec RA = 281
98220 deg
ZDOT = 884
770173 TA = 177
36263
MA = 177
35155
Ha = 228
404 n
mi
Hp = 217
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12823926
81 X = -3862146
95
Y = -6107811
94 feet Y = -1905109
75 meter
Z = -17208534
39 Z = -5264035
47
XDOT = 7430
495315 XDOT = 2341
428417
YDOT = -23788
398404 feet/sec YDOT = -7224
948888 meter/sec
ZDOT = 2902
789281 ZDOT = 895
956324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3636149
17 X = 1108298
27
Y = -13623176
27 feet Y = -4152344
13 meter
Z = -17293918
26 Z = -5271186
29
XDOT = 23758
616589 XDOT = 7241
626336
YDOT = 2587
099442 feet/sec YDOT = 788
547910 meter/sec
ZDOT = 2954
285711 ZDOT = 900
466285
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 19184
01705219
00016717 00000-0 10270-3 0 9117
2 25544 51
6425 282
7409 0006697 110
6918 249
4951 15
50942882 17704
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
01705219 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 282
7409 deg
Eccentricity:
0006697
Arg of perigee: 110
6918 deg
Mean anomaly: 249
4951 deg
Mean motion: 15
50942882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 325
Coasting Arc #13 (Orbit 1776)
---------------------------------------
Vector Time (GMT): 2019/184/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3304917
84 A = 6794774
98 meter
Y = -5145269
74 meter E =
0019248
Z = 2946975
26 I = 51
27118
XDOT = 3179
378949 Wp = 94
20754
YDOT = 4901
990542 meter/sec RA = 279
97800 deg
ZDOT = 4963
552762 TA = 299
60581
MA = 299
79744
Ha = 228
327 n
mi
Hp = 217
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10842906
31 X = 3347893
51
Y = -16880806
23 feet Y = -5108072
11 meter
Z = 9668553
99 Z = 2963132
48
XDOT = 10431
033296 XDOT = 3100
217320
YDOT = 16082
646135 feet/sec YDOT = 4937
100999 meter/sec
ZDOT = 16284
621923 ZDOT = 4978
805488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11541520
41 X = -3517855
42
Y = -16367371
49 feet Y = -4988774
83 meter
Z = 9742362
63 Z = 2969472
13
XDOT = 17600
972846 XDOT = 5364
776524
YDOT = -2620
210408 feet/sec YDOT = -798
640132 meter/sec
ZDOT = 16353
267288 ZDOT = 4984
475869
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 19184
46808946
00016717 00000-0 10270-3 0 9128
2 25544 51
6422 280
4988 0006897 117
4097 242
7756 15
50980475 17779
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
46808946 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 280
4988 deg
Eccentricity:
0006897
Arg of perigee: 117
4097 deg
Mean anomaly: 242
7756 deg
Mean motion: 15
50980475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1777
Checksum: 361
Coasting Arc #14 (Orbit 1791)
---------------------------------------
Vector Time (GMT): 2019/185/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3239484
62 A = 6793373
23 meter
Y = 4844882
03 meter E =
0011540
Z = -3497067
50 I = 51
26129
XDOT = -3151
453361 Wp = 105
21301
YDOT = -5338
720030 meter/sec RA = 274
99257 deg
ZDOT = -4492
437812 TA = 116
05860
MA = 115
93976
Ha = 228
386 n
mi
Hp = 217
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10628230
37 X = -3276434
20
Y = 15895282
25 feet Y = 4808449
87 meter
Z = -11473318
58 Z = -3512892
31
XDOT = -10339
413913 XDOT = -3069
698661
YDOT = -17515
485662 feet/sec YDOT = -5373
503868 meter/sec
ZDOT = -14738
969200 ZDOT = -4507
548518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10985098
68 X = 3348258
08
Y = 15597549
39 feet Y = 4754133
05 meter
Z = -11545578
28 Z = -3519092
26
XDOT = -18900
475812 XDOT = -5760
865028
YDOT = 2388
184231 feet/sec YDOT = 727
918554 meter/sec
ZDOT = -14806
945144 ZDOT = -4513
156880
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 19185
43460202
00016717 00000-0 10270-3 0 9136
2 25544 51
6420 275
7043 0006942 119
6033 240
5810 15
50944114 17925
Satellite: ISS
Catalog Number: 25544
Epoch time: 19185
43460202 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 275
7043 deg
Eccentricity:
0006942
Arg of perigee: 119
6033 deg
Mean anomaly: 240
5810 deg
Mean motion: 15
50944114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1792
Checksum: 285
Coasting Arc #15 (Orbit 1807)
---------------------------------------
Vector Time (GMT): 2019/186/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3163034
25 A = 6791851
61 meter
Y = -4529188
44 meter E =
0017561
Z = 3941110
87 I = 51
25432
XDOT = 3196
949582 Wp = 109
19755
YDOT = 5717
547246 meter/sec RA = 270
00565 deg
ZDOT = 3984
634141 TA = 298
93029
MA = 299
10631
Ha = 228
254 n
mi
Hp = 217
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10377408
97 X = 3194302
51
Y = -14859542
12 feet Y = -4493642
95 meter
Z = 12930153
79 Z = 3956550
65
XDOT = 10488
679732 XDOT = 3113
421980
YDOT = 18758
357106 feet/sec YDOT = 5752
830132 meter/sec
ZDOT = 13072
946658 ZDOT = 3999
961428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10370495
05 X = -3160926
89
Y = -14802772
87 feet Y = -4511885
17 meter
Z = 13000624
36 Z = 3962590
30
XDOT = 20121
932108 XDOT = 6133
164907
YDOT = -2496
935427 feet/sec YDOT = -761
065918 meter/sec
ZDOT = 13141
888962 ZDOT = 4005
647756
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 19186
46554488
00016717 00000-0 10270-3 0 9141
2 25544 51
6416 270
5903 0006918 123
6672 236
5140 15
50983114 18087
Satellite: ISS
Catalog Number: 25544
Epoch time: 19186
46554488 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 270
5903 deg
Eccentricity:
0006918
Arg of perigee: 123
6672 deg
Mean anomaly: 236
5140 deg
Mean motion: 15
50983114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1808
Checksum: 322
Coasting Arc #16 (Orbit 1822)
---------------------------------------
Vector Time (GMT): 2019/187/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161714
29 A = 6790480
06 meter
Y = 4134993
93 meter E =
0013854
Z = -4372134
40 I = 51
25050
XDOT = -3250
443018 Wp = 94
35726
YDOT = -6048
381853 meter/sec RA = 265
01678 deg
ZDOT = -3380
102180 TA = 141
19994
MA = 141
10039
Ha = 228
300 n
mi
Hp = 217
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10373078
37 X = -3186481
01
Y = 13566253
04 feet Y = 4099499
49 meter
Z = -14344272
97 Z = -4387552
15
XDOT = -10664
183131 XDOT = -3166
148370
YDOT = -19843
772485 feet/sec YDOT = -6084
258840 meter/sec
ZDOT = -11089
574081 ZDOT = -3395
687334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9407437
60 X = 2867386
98
Y = 14181739
50 feet Y = 4322594
20 meter
Z = -14414594
20 Z = -4393568
31
XDOT = -21194
832813 XDOT = -6460
185042
YDOT = 2750
967194 feet/sec YDOT = 838
494801 meter/sec
ZDOT = -11159
676857 ZDOT = -3401
469506
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 19187
43205565
00016717 00000-0 10270-3 0 9159
2 25544 51
6416 265
7958 0006883 127
3130 232
8650 15
50938916 18236
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
43205565 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 265
7958 deg
Eccentricity:
0006883
Arg of perigee: 127
3130 deg
Mean anomaly: 232
8650 deg
Mean motion: 15
50938916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1823
Checksum: 329
Coasting Arc #17 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2019/187/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193615
06 A = 6786617
26 meter
Y = -683014
03 meter E =
0009051
Z = 5285132
12 I = 51
23594
XDOT = 1007
447638 Wp = 117
65027
YDOT = 7601
264660 meter/sec RA = 263
52180 deg
ZDOT = 178
584131 TA = 330
61311
MA = 330
66397
Ha = 228
155 n
mi
Hp = 217
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13758579
60 X = 4175269
31
Y = -2240859
69 feet Y = -636221
29 meter
Z = 17339672
31 Z = 5305458
10
XDOT = 3305
274404 XDOT = 921
505798
YDOT = 24938
532349 feet/sec YDOT = 7612
050094 meter/sec
ZDOT = 585
905940 ZDOT = 183
270007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13726536
76 X = -4183848
40
Y = 1641476
94 feet Y = 500322
17 meter
Z = 17431923
09 Z = 5313250
16
XDOT = -2088
723216 XDOT = -636
642836
YDOT = -24058
048108 feet/sec YDOT = -7332
893063 meter/sec
ZDOT = 606
435748 ZDOT = 184
841616
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 19187
75422402
00016717 00000-0 10270-3 0 9166
2 25544 51
6389 264
2003 0006769 124
5226 235
6565 15
50952390 18281
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
75422402 = yrday
fracday
Element set: 916
Inclination: 51
6389 deg
RA of node: 264
2003 deg
Eccentricity:
0006769
Arg of perigee: 124
5226 deg
Mean anomaly: 235
6565 deg
Mean motion: 15
50952390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 321
Coasting Arc #18 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2019/188/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283099
78 A = 6786792
44 meter
Y = 202371
57 meter E =
0020713
Z = -5278563
20 I = 51
24152
XDOT = -1064
741005 Wp = 104
64223
YDOT = -7551
965829 meter/sec RA = 258
52786 deg
ZDOT = 571
171336 TA = 170
87239
MA = 170
83468
Ha = 228
306 n
mi
Hp = 217
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14052164
64 X = -4259404
52
Y = 663948
71 feet Y = 154607
94 meter
Z = -17318120
75 Z = -5299310
99
XDOT = -3493
244768 XDOT = -982
988014
YDOT = -24776
790776 feet/sec YDOT = -7563
415455 meter/sec
ZDOT = 1873
921706 ZDOT = 566
197132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13948093
52 X = 4251378
90
Y = -293212
50 feet Y = -89371
17 meter
Z = -17412242
21 Z = -5307251
43
XDOT = 2826
483576 XDOT = 861
512194
YDOT = 23843
767037 feet/sec YDOT = 7267
580193 meter/sec
ZDOT = 1852
055371 ZDOT = 564
506477
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 19188
72073152
00016717 00000-0 10270-3 0 9179
2 25544 51
6393 259
4053 0006780 127
0618 233
1154 15
50932182 18434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19188
72073152 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 259
4053 deg
Eccentricity:
0006780
Arg of perigee: 127
0618 deg
Mean anomaly: 233
1154 deg
Mean motion: 15
50932182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 307
Coasting Arc #19 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2019/189/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4392518
45 A = 6787164
38 meter
Y = 249576
34 meter E =
0008750
Z = 5160282
21 I = 51
24946
XDOT = 1113
488090 Wp = 102
75785
YDOT = 7475
102647 meter/sec RA = 253
53452 deg
ZDOT = -1309
369510 TA = 359
88603
MA = 359
88623
Ha = 228
032 n
mi
Hp = 217
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14411149
76 X = 4364335
67
Y = 818820
01 feet Y = 298538
53 meter
Z = 16930059
75 Z = 5181550
74
XDOT = 3653
176148 XDOT = 1036
176707
YDOT = 24524
614985 feet/sec YDOT = 7487
122292 meter/sec
ZDOT = -4295
831725 ZDOT = -1304
147785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14288758
04 X = -4355213
45
Y = -952945
71 feet Y = -290457
85 meter
Z = 17026506
25 Z = 5189679
11
XDOT = -3523
124055 XDOT = -1073
848212
YDOT = -23515
573090 feet/sec YDOT = -7167
546678 meter/sec
ZDOT = -4272
814652 ZDOT = -1302
353906
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 19189
75167119
00016717 00000-0 10270-3 0 9181
2 25544 51
6380 254
2903 0006639 130
7672 229
4056 15
50953045 18598
Satellite: ISS
Catalog Number: 25544
Epoch time: 19189
75167119 = yrday
fracday
Element set: 918
Inclination: 51
6380 deg
RA of node: 254
2903 deg
Eccentricity:
0006639
Arg of perigee: 130
7672 deg
Mean anomaly: 229
4056 deg
Mean motion: 15
50953045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 333
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