[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 29th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16470 9357 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
212/12:10:46
000 0
0 0
0 0
0
N/A 0
0 0
0 226
3
000/00:00:00
000 0
0 0
0 220
1
212/15:35:09
000 -0
0 -0
0 0
0
N/A -0
0 0
0 226
1
000/00:00:18
000 0
0 -0
0 220
1
213/11:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
3
216/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
8
000/00:00:00
000 0
0 0
0 220
8
224/14:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2019/210/12:39:28
614
Vector Time (MET): N/A
Weight (LBS) : 937191
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4836816
71 A = 6796984
57 meter
Y = -4411721
59 meter E =
0016032
Z = 1790313
05 I = 51
84517
XDOT = 4461
479992 Wp = 136
81044
YDOT = 2578
870440 meter/sec RA = 150
03852 deg
ZDOT = -5679
876597 TA = 23
58914
MA = 23
51570
Ha = 226
508 n
mi
Hp = 219
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15868821
21 X = 4877094
13
Y = -14474152
21 feet Y = -4357407
94 meter
Z = 5873730
47 Z = 1813905
42
XDOT = 14637
401548 XDOT = 4459
900053
YDOT = 8460
861022 feet/sec YDOT = 2628
753759 meter/sec
ZDOT = -18634
765737 ZDOT = -5658
208180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21439194
64 X = -6534666
53
Y = -637137
95 feet Y = -194199
65 meter
Z = 5981326
52 Z = 1823108
32
XDOT = -4748
727228 XDOT = -1447
412059
YDOT = -14788
526929 feet/sec YDOT = -4507
543008 meter/sec
ZDOT = -18536
405264 ZDOT = -5649
896325
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 19210
56324254
00016717 00000-0 10270-3 0 9001
2 25544 51
6412 151
0336 0006154 195
7331 164
3630 15
51018473 21826
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
56324254 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 151
0336 deg
Eccentricity:
0006154
Arg of perigee: 195
7331 deg
Mean anomaly: 164
3630 deg
Mean motion: 15
51018473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 271
Coasting Arc #2 (Orbit 2196)
---------------------------------------
Vector Time (GMT): 2019/211/12:39:28
614
Vector Time (MET): N/A
Weight (LBS) : 937191
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4932228
67 A = 6797792
55 meter
Y = 4535345
75 meter E =
0003985
Z = -1143400
12 I = 51
87588
XDOT = -3983
409539 Wp = 67
70129
YDOT = -2852
706145 meter/sec RA = 145
09655 deg
ZDOT = 5885
523558 TA = 279
95193
MA = 279
99690
Ha = 226
393 n
mi
Hp = 219
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16181852
59 X = -4977023
74
Y = 14879743
27 feet Y = 4479939
79 meter
Z = -3751312
72 Z = -1167466
81
XDOT = -13068
928934 XDOT = -3979
801776
YDOT = -9359
272130 feet/sec YDOT = -2897
232010 meter/sec
ZDOT = 19309
460491 ZDOT = 5866
182400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21963263
02 X = 6694402
57
Y = 196154
36 feet Y = 59787
85 meter
Z = -3861095
85 Z = -1176862
01
XDOT = 3241
829386 XDOT = 988
109597
YDOT = 14252
682987 feet/sec YDOT = 4344
217774 meter/sec
ZDOT = 19221
689900 ZDOT = 5858
771082
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 19211
52970365
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 146
2387 0006075 199
4013 160
6907 15
51018748 21971
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
52970365 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 146
2387 deg
Eccentricity:
0006075
Arg of perigee: 199
4013 deg
Mean anomaly: 160
6907 deg
Mean motion: 15
51018748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2197
Checksum: 314
Coasting Arc #3 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2019/212/12:10:46
000
Vector Time (MET): N/A
Weight (LBS) : 937191
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4722393
99 A = 6788750
86 meter
Y = -956916
04 meter E =
0010225
Z = 4782617
54 I = 51
87254
XDOT = 3938
372314 Wp = 155
45206
YDOT = -6003
022987 meter/sec RA = 140
28123 deg
ZDOT = 2676
566330 TA = 268
12612
MA = 268
24323
Ha = 226
336 n
mi
Hp = 220
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15493418
61 X = -4734573
26
Y = -3139488
32 feet Y = -1009793
80 meter
Z = 15691002
43 Z = 4759648
77
XDOT = 12921
169008 XDOT = 3992
206171
YDOT = -19694
957308 feet/sec YDOT = -5958
680639 meter/sec
ZDOT = 8781
385596 ZDOT = 2695
827093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7776113
89 X = 2370159
51
Y = 13881658
41 feet Y = 4231129
48 meter
Z = 15586583
23 Z = 4750790
57
XDOT = -22309
494310 XDOT = -6799
933866
YDOT = 2497
167577 feet/sec YDOT = 761
136678 meter/sec
ZDOT = 8869
428916 ZDOT = 2703
401934
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 19212
56059380
00016717 00000-0 10270-3 0 9020
2 25544 51
6414 141
1245 0006229 203
8296 156
2567 15
51053037 22130
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
56059380 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 141
1245 deg
Eccentricity:
0006229
Arg of perigee: 203
8296 deg
Mean anomaly: 156
2567 deg
Mean motion: 15
51053037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 284
Coasting Arc #4 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2019/212/15:35:18
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1952241
33 A = 6792681
39 meter
Y = -5397572
92 meter E =
0010427
Z = 3620132
11 I = 51
89119
XDOT = 6213
496393 Wp = 116
86783
YDOT = -729
673118 meter/sec RA = 139
53420 deg
ZDOT = -4433
477681 TA = 20
44565
MA = 20
40394
Ha = 226
140 n
mi
Hp = 220
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6404991
24 X = 1994869
28
Y = -17708572
56 feet Y = -5375503
63 meter
Z = 11877073
85 Z = 3629718
08
XDOT = 20385
486855 XDOT = 6242
728863
YDOT = -2393
940677 feet/sec YDOT = -660
025504 meter/sec
ZDOT = -14545
530451 ZDOT = -4403
224650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5732535
97 X = -1747276
96
Y = 17908338
79 feet Y = 5458461
66 meter
Z = 11921064
17 Z = 3633540
36
XDOT = -19086
046766 XDOT = -5817
427054
YDOT = 3492
745974 feet/sec YDOT = 1064
588973 meter/sec
ZDOT = -14407
852167 ZDOT = -4391
513340
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 19212
68945466
00016717 00000-0 10270-3 0 9033
2 25544 51
6429 140
4861 0006034 205
0167 155
0693 15
51059398 22152
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68945466 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 140
4861 deg
Eccentricity:
0006034
Arg of perigee: 205
0167 deg
Mean anomaly: 155
0693 deg
Mean motion: 15
51059398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 309
Coasting Arc #5 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 447469
67 A = 6790413
58 meter
Y = -5207006
90 meter E =
0006810
Z = 4328483
43 I = 51
90303
XDOT = 6370
156175 Wp = 111
39355
YDOT = -2391
127305 meter/sec RA = 135
40379 deg
ZDOT = -3532
929630 TA = 14
45869
MA = 14
43921
Ha = 226
155 n
mi
Hp = 220
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1468076
34 X = 484637
85
Y = -17083355
96 feet Y = -5201795
53 meter
Z = 14201061
13 Z = 4330746
83
XDOT = 20899
462515 XDOT = 6413
581559
YDOT = -7844
905857 feet/sec YDOT = -2319
648630 meter/sec
ZDOT = -11590
976476 ZDOT = -3501
881361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14998078
84 X = -4571414
43
Y = 8291612
30 feet Y = 2527283
43 meter
Z = 14211728
70 Z = 4331734
91
XDOT = -17522
447183 XDOT = -5340
841901
YDOT = -12059
179718 feet/sec YDOT = -3675
637978 meter/sec
ZDOT = -11449
545983 ZDOT = -3489
821616
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 19213
52705359
00016717 00000-0 10270-3 0 9043
2 25544 51
6419 136
3296 0006143 207
7637 152
3187 15
51029968 22281
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52705359 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 136
3296 deg
Eccentricity:
0006143
Arg of perigee: 207
7637 deg
Mean anomaly: 152
3187 deg
Mean motion: 15
51029968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 318
Coasting Arc #6 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -700062
99 A = 6791906
15 meter
Y = 5524311
13 meter E =
0007573
Z = -3896939
02 I = 51
93156
XDOT = -6079
346310 Wp = 156
42987
YDOT = 2144
917835 meter/sec RA = 130
45945 deg
ZDOT = 4128
779607 TA = 156
82703
MA = 156
79286
Ha = 225
965 n
mi
Hp = 220
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2296794
58 X = -742856
74
Y = 18124380
36 feet Y = 5516243
48 meter
Z = -12785233
02 Z = -3900443
20
XDOT = -19945
361908 XDOT = -6122
934346
YDOT = 7037
132005 feet/sec YDOT = 2076
690363 meter/sec
ZDOT = 13545
864852 ZDOT = 4099
143476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16186049
58 X = 4933507
91
Y = -8447613
25 feet Y = -2574832
52 meter
Z = -12801571
84 Z = -3901919
10
XDOT = 16536
004957 XDOT = 5040
174311
YDOT = 11341
130689 feet/sec YDOT = 3456
776634 meter/sec
ZDOT = 13410
860365 ZDOT = 4087
630239
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 19214
49350928
00016717 00000-0 10270-3 0 9059
2 25544 51
6424 131
5339 0006058 211
2824 148
7968 15
51038506 22436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49350928 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 131
5339 deg
Eccentricity:
0006058
Arg of perigee: 211
2824 deg
Mean anomaly: 148
7968 deg
Mean motion: 15
51038506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 309
Coasting Arc #7 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892206
39 A = 6793468
30 meter
Y = -5812817
79 meter E =
0010306
Z = 3387878
52 I = 51
95730
XDOT = 5798
351229 Wp = 119
37775
YDOT = -1834
627573 meter/sec RA = 125
51972 deg
ZDOT = -4669
066122 TA = 21
28881
MA = 21
24596
Ha = 225
863 n
mi
Hp = 220
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2927186
31 X = 940684
65
Y = -19070924
50 feet Y = -5802569
55 meter
Z = 11115087
01 Z = 3392329
99
XDOT = 19023
462038 XDOT = 5841
114793
YDOT = -6019
119334 feet/sec YDOT = -1769
547090 meter/sec
ZDOT = -15318
458406 ZDOT = -4640
796788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17181619
64 X = -5236957
67
Y = 8752170
77 feet Y = 2667661
65 meter
Z = 11135761
92 Z = 3394180
23
XDOT = -15369
544039 XDOT = -4684
637023
YDOT = -10821
952870 feet/sec YDOT = -3298
531235 meter/sec
ZDOT = -15189
682683 ZDOT = -4629
815282
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 19215
52439350
00016717 00000-0 10270-3 0 9062
2 25544 51
6422 126
4200 0006011 214
9367 145
1390 15
51034111 22590
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52439350 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 126
4200 deg
Eccentricity:
0006011
Arg of perigee: 214
9367 deg
Mean anomaly: 145
1390 deg
Mean motion: 15
51034111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 266
Coasting Arc #8 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1026390
18 A = 6794880
34 meter
Y = 6091585
70 meter E =
0002531
Z = -2833830
97 I = 51
98078
XDOT = -5507
061514 Wp = 173
56737
YDOT = 1453
925281 meter/sec RA = 120
58162 deg
ZDOT = 5117
957824 TA = 154
47670
MA = 154
46420
Ha = 225
672 n
mi
Hp = 220
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3367421
85 X = -1080666
86
Y = 19985517
39 feet Y = 6079804
44 meter
Z = -9297345
71 Z = -2838948
44
XDOT = -18067
787120 XDOT = -5547
770127
YDOT = 4770
096067 feet/sec YDOT = 1392
113769 meter/sec
ZDOT = 16791
200210 ZDOT = 5091
108269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18033002
59 X = 5496459
19
Y = -9226558
06 feet Y = -2812254
90 meter
Z = -9321079
15 Z = -2841064
93
XDOT = 13973
780841 XDOT = 4259
208400
YDOT = 10465
002983 feet/sec YDOT = 3189
732909 meter/sec
ZDOT = 16668
902828 ZDOT = 5080
681582
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 19216
49084559
00016717 00000-0 10270-3 0 9077
2 25544 51
6423 121
6244 0006073 218
9426 141
1288 15
51051282 22741
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
49084559 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 121
6244 deg
Eccentricity:
0006073
Arg of perigee: 218
9426 deg
Mean anomaly: 141
1288 deg
Mean motion: 15
51051282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 302
Coasting Arc #9 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3815739
00 A = 6798079
02 meter
Y = 5569980
43 meter E =
0007294
Z = 770107
79 I = 51
99216
XDOT = -3528
978101 Wp = 65
75205
YDOT = -3249
042987 meter/sec RA = 119
29910 deg
ZDOT = 5972
468386 TA = 302
51749
MA = 302
58795
Ha = 225
753 n
mi
Hp = 220
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12518828
75 X = -3881481
22
Y = 18274214
01 feet Y = 5526942
56 meter
Z = 2526600
36 Z = 751413
09
XDOT = -11578
012141 XDOT = -3521
394475
YDOT = -10659
589851 feet/sec YDOT = -3288
464156 meter/sec
ZDOT = 19594
712551 ZDOT = 5955
344644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2959071
15 X = -901924
89
Y = -21962161
77 feet Y = -6694066
91 meter
Z = 2441112
17 Z = 744050
99
XDOT = 14232
421293 XDOT = 4338
042010
YDOT = 267
412390 feet/sec YDOT = 81
507296 meter/sec
ZDOT = 19517
019685 ZDOT = 5948
787600
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 19216
81299487
00016717 00000-0 10270-3 0 9082
2 25544 51
6387 120
0219 0006330 218
7639 141
3059 15
51042597 22797
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
81299487 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 120
0219 deg
Eccentricity:
0006330
Arg of perigee: 218
7639 deg
Mean anomaly: 141
3059 deg
Mean motion: 15
51042597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 323
Coasting Arc #10 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 953594
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3733140
38 A = 6797328
21 meter
Y = -5481181
73 meter E =
0011195
Z = -1458527
65 I = 52
00645
XDOT = 3275
427252 Wp = 175
02094
YDOT = 3773
930739 meter/sec RA = 114
36621 deg
ZDOT = -5813
148805 TA = 20
79568
MA = 20
75017
Ha = 225
539 n
mi
Hp = 220
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12247835
91 X = 3801239
70
Y = -17982879
69 feet Y = -5439054
35 meter
Z = -4785195
71 Z = -1440228
36
XDOT = 10746
152401 XDOT = 3261
219286
YDOT = 12381
662528 feet/sec YDOT = 3810
479477 meter/sec
ZDOT = -19072
010515 ZDOT = -5797
272708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3324159
78 X = 1013203
90
Y = 21520627
46 feet Y = 6559487
25 meter
Z = -4701499
76 Z = -1433017
13
XDOT = -14830
138851 XDOT = -4520
226322
YDOT = -1849
781075 feet/sec YDOT = -563
813272 meter/sec
ZDOT = -19000
036497 ZDOT = -5791
211124
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 19217
77944285
00016717 00000-0 10270-3 0 9092
2 25544 51
6398 115
2262 0006089 223
3037 136
7636 15
51083345 22940
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
77944285 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 115
2262 deg
Eccentricity:
0006089
Arg of perigee: 223
3037 deg
Mean anomaly: 136
7636 deg
Mean motion: 15
51083345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 326
Coasting Arc #11 (Orbit 2309)
---------------------------------------
Vector Time (GMT): 2019/218/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3627329
95 A = 6796447
82 meter
Y = 5345679
41 meter E =
0008616
Z = 2103049
37 I = 52
01552
XDOT = -3084
924652 Wp = 87
01797
YDOT = -4284
761840 meter/sec RA = 109
43290 deg
ZDOT = 5551
305561 TA = 296
10731
MA = 296
19595
Ha = 225
475 n
mi
Hp = 221
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11900688
80 X = -3697052
62
Y = 17538318
27 feet Y = 5304726
17 meter
Z = 6899768
28 Z = 2085260
10
XDOT = -10121
143873 XDOT = -3063
746813
YDOT = -14057
617584 feet/sec YDOT = -4319
141322 meter/sec
ZDOT = 18212
944754 ZDOT = 5536
371670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3623700
30 X = -1104503
85
Y = -20909428
13 feet Y = -6373193
69 meter
Z = 6818388
04 Z = 2078244
68
XDOT = 15613
124282 XDOT = 4758
880281
YDOT = 3231
925850 feet/sec YDOT = 985
090999 meter/sec
ZDOT = 18145
302733 ZDOT = 5530
688273
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 19218
81031934
00016717 00000-0 10270-3 0 9108
2 25544 51
6393 110
1104 0006246 225
0266 135
0379 15
51057715 23109
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
81031934 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 110
1104 deg
Eccentricity:
0006246
Arg of perigee: 225
0266 deg
Mean anomaly: 135
0379 deg
Mean motion: 15
51057715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2310
Checksum: 271
Coasting Arc #12 (Orbit 2324)
---------------------------------------
Vector Time (GMT): 2019/219/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3527547
30 A = 6795137
73 meter
Y = -5119173
78 meter E =
0006773
Z = -2732750
11 I = 52
02151
XDOT = 2947
470964 Wp = 185
19253
YDOT = 4801
431705 meter/sec RA = 104
50040 deg
ZDOT = -5195
202180 TA = 25
50555
MA = 25
47215
Ha = 225
369 n
mi
Hp = 221
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11573317
93 X = 3597803
27
Y = -16795189
56 feet Y = -5079333
35 meter
Z = -8965715
60 Z = -2715444
29
XDOT = 9670
180329 XDOT = 2918
796104
YDOT = 15752
728690 feet/sec YDOT = 4834
232236 meter/sec
ZDOT = -17044
626575 ZDOT = -5180
954081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3678072
43 X = 1121076
48
Y = 20097397
60 feet Y = 6125686
79 meter
Z = -8886536
40 Z = -2708616
30
XDOT = -16597
197986 XDOT = -5058
825946
YDOT = -4462
556682 feet/sec YDOT = -1360
187277 meter/sec
ZDOT = -16980
153666 ZDOT = -5175
550837
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 19219
77676384
00016717 00000-0 10270-3 0 9119
2 25544 51
6395 105
3155 0006163 229
0763 130
9855 15
51068347 23259
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
77676384 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 105
3155 deg
Eccentricity:
0006163
Arg of perigee: 229
0763 deg
Mean anomaly: 130
9855 deg
Mean motion: 15
51068347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2325
Checksum: 322
Coasting Arc #13 (Orbit 2340)
---------------------------------------
Vector Time (GMT): 2019/220/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3428151
55 A = 6793688
53 meter
Y = 4847884
23 meter E =
0008326
Z = 3298622
69 I = 52
02505
XDOT = -2874
134972 Wp = 113
69476
YDOT = -5275
864994 meter/sec RA = 99
56599 deg
ZDOT = 4754
057959 TA = 284
33560
MA = 284
42803
Ha = 225
159 n
mi
Hp = 221
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11247216
37 X = -3498129
94
Y = 15905131
99 feet Y = 4809156
80 meter
Z = 10822252
91 Z = 3281800
43
XDOT = -9429
576680 XDOT = -2838
017497
YDOT = -17309
268352 feet/sec YDOT = -5307
803876 meter/sec
ZDOT = 15597
303014 ZDOT = 4740
184073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3599950
98 X = -1097265
06
Y = -19187849
80 feet Y = -5848456
62 meter
Z = 10745279
46 Z = 3275161
18
XDOT = 17680
270935 XDOT = 5388
946581
YDOT = 5405
871529 feet/sec YDOT = 1647
709642 meter/sec
ZDOT = 15534
580526 ZDOT = 4734
940144
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 19220
80763548
00016717 00000-0 10270-3 0 9125
2 25544 51
6405 100
1999 0006353 232
6473 127
4100 15
51076433 23416
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
80763548 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 100
1999 deg
Eccentricity:
0006353
Arg of perigee: 232
6473 deg
Mean anomaly: 127
4100 deg
Mean motion: 15
51076433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2341
Checksum: 285
Coasting Arc #14 (Orbit 2355)
---------------------------------------
Vector Time (GMT): 2019/221/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3360482
27 A = 6792135
99 meter
Y = -4493527
37 meter E =
0002107
Z = -3826279
79 I = 52
02515
XDOT = 2845
057432 Wp = 160
11613
YDOT = 5722
951660 meter/sec RA = 94
63098 deg
ZDOT = -4224
848242 TA = 65
50296
MA = 65
48099
Ha = 225
061 n
mi
Hp = 221
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11025204
30 X = 3429066
18
Y = -14742543
85 feet Y = -4455564
38 meter
Z = -12553411
40 Z = -3809789
70
XDOT = 9334
177926 XDOT = 2801
372043
YDOT = 18776
088122 feet/sec YDOT = 5754
523091 meter/sec
ZDOT = -13861
050664 ZDOT = -4211
133913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3221920
43 X = 982041
35
Y = 18177060
53 feet Y = 5540368
05 meter
Z = -12477963
21 Z = -3803283
19
XDOT = -18840
391829 XDOT = -5742
551429
YDOT = -6127
230801 feet/sec YDOT = -1867
579948 meter/sec
ZDOT = -13799
101122 ZDOT = -4205
966022
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 19221
77407595
00016717 00000-0 10270-3 0 9130
2 25544 51
6415 95
4048 0006190 236
7553 123
3005 15
51065700 23561
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
77407595 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 95
4048 deg
Eccentricity:
0006190
Arg of perigee: 236
7553 deg
Mean anomaly: 123
3005 deg
Mean motion: 15
51065700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2356
Checksum: 295
Coasting Arc #15 (Orbit 2371)
---------------------------------------
Vector Time (GMT): 2019/222/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3315220
58 A = 6790550
74 meter
Y = 4104971
02 meter E =
0007238
Z = 4274596
18 I = 52
02177
XDOT = -2867
487708 Wp = 144
81145
YDOT = -6106
362722 meter/sec RA = 89
69443 deg
ZDOT = 3631
325660 TA = 268
18343
MA = 268
26632
Ha = 224
800 n
mi
Hp = 221
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10876707
95 X = -3381640
49
Y = 13467752
70 feet Y = 4067526
22 meter
Z = 14024265
67 Z = 4258331
26
XDOT = -9407
768071 XDOT = -2816
630212
YDOT = -20033
998433 feet/sec YDOT = -6138
144874 meter/sec
ZDOT = 11913
798097 ZDOT = 3617
519766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2678962
00 X = -816547
62
Y = -17163557
18 feet Y = -5231452
23 meter
Z = 13949861
42 Z = 4251917
76
XDOT = 19988
542536 XDOT = 6092
507765
YDOT = 6536
115575 feet/sec YDOT = 1992
208027 meter/sec
ZDOT = 11851
473877 ZDOT = 3612
329238
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 19222
80494269
00016717 00000-0 10270-3 0 9140
2 25544 51
6416 90
2899 0006266 240
3748 119
6779 15
51087314 23729
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
80494269 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 90
2899 deg
Eccentricity:
0006266
Arg of perigee: 240
3748 deg
Mean anomaly: 119
6779 deg
Mean motion: 15
51087314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2372
Checksum: 333
Coasting Arc #16 (Orbit 2386)
---------------------------------------
Vector Time (GMT): 2019/223/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3320855
84 A = 6789162
19 meter
Y = -3655023
75 meter E =
0004205
Z = -4662849
72 I = 52
01565
XDOT = 2916
000857 Wp = 79
28296
YDOT = 6431
459870 meter/sec RA = 84
75685 deg
ZDOT = -2966
112788 TA = 161
29661
MA = 161
28116
Ha = 224
728 n
mi
Hp = 221
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10895196
32 X = 3384129
70
Y = -11991547
74 feet Y = -3617533
50 meter
Z = -15298063
39 Z = -4646565
10
XDOT = 9566
931946 XDOT = 2858
273184
YDOT = 21100
590124 feet/sec YDOT = 6463
746070 meter/sec
ZDOT = -9731
341167 ZDOT = -2952
087952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1841640
93 X = 561332
16
Y = 16167365
86 feet Y = 4927813
11 meter
Z = -15223596
93 Z = -4640152
35
XDOT = -21067
189433 XDOT = -6421
279339
YDOT = -6699
227983 feet/sec YDOT = -2041
924689 meter/sec
ZDOT = -9668
057480 ZDOT = -2946
823920
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 19223
77138070
00016717 00000-0 10270-3 0 9153
2 25544 51
6416 85
4954 0006242 244
1627 115
8881 15
51063905 23877
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
77138070 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 85
4954 deg
Eccentricity:
0006242
Arg of perigee: 244
1627 deg
Mean anomaly: 115
8881 deg
Mean motion: 15
51063905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2387
Checksum: 314
Coasting Arc #17 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2019/224/14:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 938318
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4265428
19 A = 6787486
90 meter
Y = 1486373
51 meter E =
0008604
Z = -5073623
84 I = 52
00478
XDOT = -289
575701 Wp = 127
85824
YDOT = 7405
917437 meter/sec RA = 80
54387 deg
ZDOT = 1923
284921 TA = 160
74410
MA = 160
71157
Ha = 224
336 n
mi
Hp = 221
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13994186
99 X = 4273134
48
Y = 4876553
52 feet Y = 1534115
93 meter
Z = -16645747
52 Z = -5052885
59
XDOT = -950
051514 XDOT = -381
711345
YDOT = 24297
629385 feet/sec YDOT = 7402
163914 meter/sec
ZDOT = 6309
989897 ZDOT = 1921
654986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13571598
99 X = -4136623
37
Y = -6209660
39 feet Y = -1892704
49 meter
Z = -16551458
33 Z = -5044884
50
XDOT = 2872
180678 XDOT = 875
440671
YDOT = -23100
254215 feet/sec YDOT = -7040
957485 meter/sec
ZDOT = 6301
901274 ZDOT = 1920
819508
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 19224
60895712
00016717 00000-0 10270-3 0 9160
2 25544 51
6396 81
3401 0006113 250
0119 110
0374 15
51073872 24009
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
60895712 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 81
3401 deg
Eccentricity:
0006113
Arg of perigee: 250
0119 deg
Mean anomaly: 110
0374 deg
Mean motion: 15
51073872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 273
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