[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 8th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
039/16:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
6
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
5
044/15:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3494)
---------------------------------------
Vector Time (GMT): 2019/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3900795
76 A = 6789494
71 meter
Y = -5006121
34 meter E =
0015833
Z = 2385382
32 I = 51
29550
XDOT = 2805
192869 Wp = 54
04195
YDOT = 4739
144902 meter/sec RA = 290
39803 deg
ZDOT = 5342
790525 TA = 332
75585
MA = 332
83882
Ha = 223
126 n
mi
Hp = 215
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12797886
35 X = 3944899
17
Y = -16424282
60 feet Y = -4962253
24 meter
Z = 7826057
48 Z = 2404437
68
XDOT = 9203
388677 XDOT = 2726
038338
YDOT = 15548
375664 feet/sec YDOT = 4770
072123 meter/sec
ZDOT = 17528
840306 ZDOT = 5356
224319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20604479
14 X = 6280245
24
Y = -2763410
83 feet Y = -842287
62 meter
Z = 7912593
10 Z = 2411758
38
XDOT = -4634
644499 XDOT = -1412
639643
YDOT = 15952
953037 feet/sec YDOT = 4862
460086 meter/sec
ZDOT = 17588
888456 ZDOT = 5361
093201
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 19037
55952712
00016717 00000-0 10270-3 0 9003
2 25544 51
6416 290
8572 0005497 356
1839 3
9271 15
53225255 34956
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
55952712 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 290
8572 deg
Eccentricity:
0005497
Arg of perigee: 356
1839 deg
Mean anomaly: 3
9271 deg
Mean motion: 15
53225255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3495
Checksum: 323
Coasting Arc #2 (Orbit 3509)
---------------------------------------
Vector Time (GMT): 2019/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4090542
21 A = 6786488
88 meter
Y = 4084921
63 meter E =
0007990
Z = -3565229
69 I = 51
27443
XDOT = -2048
315332 Wp = 39
71623
YDOT = -5908
781501 meter/sec RA = 285
39995 deg
ZDOT = -4419
441323 TA = 182
57103
MA = 182
57514
Ha = 223
264 n
mi
Hp = 215
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13420414
09 X = -4118599
48
Y = 13401973
84 feet Y = 4039021
28 meter
Z = -11696947
80 Z = -3585167
84
XDOT = -6720
194658 XDOT = -1960
622790
YDOT = -19385
766081 feet/sec YDOT = -5931
197084 meter/sec
ZDOT = -14499
479405 ZDOT = -4429
177753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18903205
66 X = -5761697
09
Y = 516048
81 feet Y = 157291
68 meter
Z = -11787345
51 Z = -3592782
91
XDOT = 8598
899427 XDOT = 2620
944545
YDOT = -17233
851063 feet/sec YDOT = -5252
877804 meter/sec
ZDOT = -14542
730720 ZDOT = -4432
624323
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 19038
52461150
00016717 00000-0 10270-3 0 9013
2 25544 51
6410 286
0534 0005470 358
4225 1
6909 15
53228406 35102
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
52461150 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 286
0534 deg
Eccentricity:
0005470
Arg of perigee: 358
4225 deg
Mean anomaly: 1
6909 deg
Mean motion: 15
53228406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3510
Checksum: 279
Coasting Arc #3 (Orbit 3525)
---------------------------------------
Vector Time (GMT): 2019/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179233
25 A = 6783388
78 meter
Y = -2918883
98 meter E =
0008950
Z = 4466569
23 I = 51
25553
XDOT = 1355
150563 Wp = 75
79268
YDOT = 6840
427097 meter/sec RA = 280
39318 deg
ZDOT = 3198
978173 TA = 341
87432
MA = 341
90620
Ha = 223
277 n
mi
Hp = 215
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13711395
17 X = 4189866
79
Y = -9576391
01 feet Y = -2872089
16 meter
Z = 14654098
52 Z = 4486895
92
XDOT = 4446
032030 XDOT = 1263
019746
YDOT = 22442
346118 feet/sec YDOT = 6855
066385 meter/sec
ZDOT = 10495
335213 ZDOT = 3205
336682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16502756
83 X = 5030040
28
Y = 2159524
78 feet Y = 658223
15 meter
Z = 14746107
81 Z = 4494613
66
XDOT = -11805
081362 XDOT = -3598
188799
YDOT = 18283
424634 feet/sec YDOT = 5572
787828 meter/sec
ZDOT = 10523
263292 ZDOT = 3207
490651
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 19039
55403589
00016717 00000-0 10270-3 0 9020
2 25544 51
6403 280
9283 0005531 3
9348 356
1847 15
53222757 35263
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
55403589 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 280
9283 deg
Eccentricity:
0005531
Arg of perigee: 3
9348 deg
Mean anomaly: 356
1847 deg
Mean motion: 15
53222757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3526
Checksum: 317
Coasting Arc #4 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2553098
11 A = 6784690
42 meter
Y = -4757012
05 meter E =
0008001
Z = -4113758
76 I = 51
25469
XDOT = 3958
574943 Wp = 70
51185
YDOT = -5372
296470 meter/sec RA = 279
47142 deg
ZDOT = 3764
182575 TA = 238
49369
MA = 238
57188
Ha = 223
254 n
mi
Hp = 215
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8376306
13 X = -2479732
19
Y = -15606994
92 feet Y = -4785152
60 meter
Z = -13496583
87 Z = -4125982
02
XDOT = 12987
450602 XDOT = 4000
071358
YDOT = -17625
644588 feet/sec YDOT = -5327
796680 meter/sec
ZDOT = 12349
680364 ZDOT = 3783
512530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13143720
53 X = -4006206
02
Y = -11811275
08 feet Y = -3600076
64 meter
Z = -13551197
83 Z = -4130405
10
XDOT = 5202
766824 XDOT = 1585
803328
YDOT = -20026
982124 feet/sec YDOT = -6104
224152 meter/sec
ZDOT = 12437
461053 ZDOT = 3790
938129
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 19039
68271314
00016717 00000-0 10270-3 0 9034
2 25544 51
6361 280
2831 0005154 4
6976 355
4224 15
53239909 35284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68271314 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 280
2831 deg
Eccentricity:
0005154
Arg of perigee: 4
6976 deg
Mean anomaly: 355
4224 deg
Mean motion: 15
53239909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 312
Coasting Arc #5 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3835059
43 A = 6780882
86 meter
Y = 2413592
97 meter E =
0009893
Z = 5042607
73 I = 51
24351
XDOT = -2129
766201 Wp = 29
71673
YDOT = 7146
009455 meter/sec RA = 275
48095 deg
ZDOT = -1790
646092 TA = 77
76228
MA = 77
65151
Ha = 223
234 n
mi
Hp = 215
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12582215
98 X = 3783291
20
Y = 7918612
12 feet Y = 2456190
14 meter
Z = 16543988
63 Z = 5061110
78
XDOT = -6987
421920 XDOT = -2200
818807
YDOT = 23444
912909 feet/sec YDOT = 7121
795532 meter/sec
ZDOT = -5874
823135 ZDOT = -1801
164512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1695540
43 X = 516800
72
Y = 14675892
38 feet Y = 4473212
00 meter
Z = 16627190
44 Z = 5067967
65
XDOT = -21520
918370 XDOT = -6559
575919
YDOT = 9233
780160 feet/sec YDOT = 2814
456193 meter/sec
ZDOT = -5923
036988 ZDOT = -1805
341674
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 19040
51911709
00016717 00000-0 10270-3 0 9048
2 25544 51
6409 276
1237 0005523 4
6912 355
4291 15
53287541 35415
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51911709 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 276
1237 deg
Eccentricity:
0005523
Arg of perigee: 4
6912 deg
Mean anomaly: 355
4291 deg
Mean motion: 15
53287541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 297
Coasting Arc #6 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3545016
25 A = 6783389
63 meter
Y = -3697372
53 meter E =
0009935
Z = -4454264
83 I = 51
24923
XDOT = 2646
459116 Wp = 76
98841
YDOT = -6421
065479 meter/sec RA = 270
46683 deg
ZDOT = 3232
035772 TA = 225
72329
MA = 225
80484
Ha = 223
447 n
mi
Hp = 215
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11630630
74 X = -3481771
70
Y = -12130487
30 feet Y = -3736662
01 meter
Z = -14613729
74 Z = -4471331
10
XDOT = 8682
608648 XDOT = 2702
365398
YDOT = -21066
487793 feet/sec YDOT = -6391
158145 meter/sec
ZDOT = 10603
791903 ZDOT = 3245
027241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1882246
57 X = 573708
75
Y = -16632287
45 feet Y = -5069521
22 meter
Z = -14690321
73 Z = -4477610
06
XDOT = 20460
677672 XDOT = 6236
414554
YDOT = -7078
608609 feet/sec YDOT = -2157
559904 meter/sec
ZDOT = 10663
067704 ZDOT = 3250
103036
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 19041
48419931
00016717 00000-0 10270-3 0 9056
2 25544 51
6406 271
3187 0005600 8
8042 351
3208 15
53253664 35567
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48419931 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 271
3187 deg
Eccentricity:
0005600
Arg of perigee: 8
8042 deg
Mean anomaly: 351
3208 deg
Mean motion: 15
53253664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 297
Coasting Arc #7 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3211739
16 A = 6786509
64 meter
Y = 4832602
15 meter E =
0014716
Z = 3513795
78 I = 51
26013
XDOT = -3167
806867 Wp = 65
75650
YDOT = 5367
411480 meter/sec RA = 265
45956 deg
ZDOT = -4465
648628 TA = 72
63061
MA = 72
46971
Ha = 223
562 n
mi
Hp = 215
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10537201
96 X = 3140393
08
Y = 15854993
94 feet Y = 4868119
31 meter
Z = 11528201
38 Z = 3529223
48
XDOT = -10393
067148 XDOT = -3205
899973
YDOT = 17609
617717 feet/sec YDOT = 5331
773640 meter/sec
ZDOT = -14651
078176 ZDOT = -4481
129235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5111043
13 X = -1557845
94
Y = 18294613
44 feet Y = 5576198
18 meter
Z = 11597294
61 Z = 3534855
40
XDOT = -18710
769298 XDOT = -5703
042482
YDOT = 4147
861398 feet/sec YDOT = 1264
268154 meter/sec
ZDOT = -14721
460517 ZDOT = -4487
101165
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 19042
51361789
00016717 00000-0 10270-3 0 9069
2 25544 51
6400 266
1936 0005731 13
0293 347
1006 15
53279079 35721
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51361789 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 266
1936 deg
Eccentricity:
0005731
Arg of perigee: 13
0293 deg
Mean anomaly: 347
1006 deg
Mean motion: 15
53279079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 304
Coasting Arc #8 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2870637
03 A = 6789529
81 meter
Y = -5678862
13 meter E =
0010885
Z = -2356479
50 I = 51
27325
XDOT = 3672
788439 Wp = 30
58665
YDOT = -4071
634250 meter/sec RA = 260
45962 deg
ZDOT = 5358
196080 TA = 302
98017
MA = 303
08476
Ha = 223
627 n
mi
Hp = 215
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9418100
49 X = -2795474
70
Y = -18631437
45 feet Y = -5710543
42 meter
Z = -7731231
96 Z = -2370241
07
XDOT = 12049
830835 XDOT = 3692
018787
YDOT = -13358
380086 feet/sec YDOT = -4030
454855 meter/sec
ZDOT = 17579
383464 ZDOT = 5376
083756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7591172
84 X = 2313789
48
Y = -19422934
55 feet Y = -5920110
45 meter
Z = -7792735
99 Z = -2375225
93
XDOT = 16494
079400 XDOT = 5027
395401
YDOT = -612
837531 feet/sec YDOT = -186
792880 meter/sec
ZDOT = 17660
484954 ZDOT = 5382
915814
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 19043
47869775
00016717 00000-0 10270-3 0 9074
2 25544 51
6397 261
3890 0005660 14
9309 345
2009 15
53236190 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47869775 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 261
3890 deg
Eccentricity:
0005660
Arg of perigee: 14
9309 deg
Mean anomaly: 345
2009 deg
Mean motion: 15
53236190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 334
Coasting Arc #9 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2438667
72 A = 6791494
49 meter
Y = 6257932
99 meter E =
0013313
Z = 985780
78 I = 51
28700
XDOT = -4197
736123 Wp = 100
10738
YDOT = 2571
587356 meter/sec RA = 255
46562 deg
ZDOT = -5874
766896 TA = 69
16686
MA = 69
02433
Ha = 223
770 n
mi
Hp = 215
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8000878
36 X = 2363720
19
Y = 20531276
22 feet Y = 6284784
84 meter
Z = 3234188
92 Z = 997444
63
XDOT = -13772
100141 XDOT = -4197
644332
YDOT = 8436
966391 feet/sec YDOT = 2524
645747 meter/sec
ZDOT = -19274
169605 ZDOT = -5895
157511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9591435
70 X = -2923469
60
Y = 19829590
87 feet Y = 6044059
30 meter
Z = 3286186
67 Z = 1001629
70
XDOT = -14024
169529 XDOT = -4274
566872
YDOT = -3538
842352 feet/sec YDOT = -1078
639149 meter/sec
ZDOT = -19366
410683 ZDOT = -5902
881976
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 19044
50811428
00016717 00000-0 10270-3 0 9082
2 25544 51
6403 256
2635 0005625 19
8814 340
2556 15
53237730 36032
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50811428 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 256
2635 deg
Eccentricity:
0005625
Arg of perigee: 19
8814 deg
Mean anomaly: 340
2556 deg
Mean motion: 15
53237730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 298
Coasting Arc #10 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437735
27 A = 6783126
20 meter
Y = 2386220
08 meter E =
0013024
Z = 4536698
95 I = 51
25733
XDOT = -615
083166 Wp = 51
17706
YDOT = 7002
135860 meter/sec RA = 254
52440 deg
ZDOT = -3067
331327 TA = 69
74242
MA = 69
60246
Ha = 223
671 n
mi
Hp = 215
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14559498
92 X = 4388685
56
Y = 7828806
03 feet Y = 2435571
75 meter
Z = 14884182
89 Z = 4558136
38
XDOT = -2017
989389 XDOT = -678
438095
YDOT = 22972
886681 feet/sec YDOT = 6994
903285 meter/sec
ZDOT = -10063
422988 ZDOT = -3070
473117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16244216
85 X = 4951237
30
Y = 2552144
36 feet Y = 777893
60 meter
Z = 14980657
23 Z = 4566104
32
XDOT = 6018
168919 XDOT = 1834
337886
YDOT = 21120
462098 feet/sec YDOT = 6437
516847 meter/sec
ZDOT = -10078
288006 ZDOT = -3071
862184
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 19044
70113121
00016717 00000-0 10270-3 0 9090
2 25544 51
6372 255
2972 0005241 25
1043 335
0363 15
53222172 36063
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
70113121 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 255
2972 deg
Eccentricity:
0005241
Arg of perigee: 25
1043 deg
Mean anomaly: 335
0363 deg
Mean motion: 15
53222172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 267
Coasting Arc #11 (Orbit 3620)
---------------------------------------
Vector Time (GMT): 2019/045/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468859
33 A = 6786093
60 meter
Y = -3555534
37 meter E =
0008840
Z = -3669640
18 I = 51
27798
XDOT = 1383
854724 Wp = 66
09066
YDOT = -6179
097186 meter/sec RA = 249
51838 deg
ZDOT = 4313
493424 TA = 250
04898
MA = 250
14421
Ha = 223
734 n
mi
Hp = 214
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14661611
99 X = -4410943
39
Y = -11665139
00 feet Y = -3605184
44 meter
Z = -12039501
92 Z = -3691207
26
XDOT = 4540
205789 XDOT = 1431
896024
YDOT = -20272
628564 feet/sec YDOT = -6163
353342 meter/sec
ZDOT = 14151
881311 ZDOT = 4320
332256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17742129
11 X = -5407800
95
Y = -5823325
10 feet Y = -1774949
49 meter
Z = -12136460
76 Z = -3699193
24
XDOT = -3357
169157 XDOT = -1023
265159
YDOT = -19251
344900 feet/sec YDOT = -5867
809926 meter/sec
ZDOT = 14183
333993 ZDOT = 4323
080201
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 19045
66620640
00016717 00000-0 10270-3 0 9107
2 25544 51
6377 250
4935 0005290 28
1224 332
0213 15
53248188 36215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
66620640 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 250
4935 deg
Eccentricity:
0005290
Arg of perigee: 28
1224 deg
Mean anomaly: 332
0213 deg
Mean motion: 15
53248188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 286
Coasting Arc #12 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2019/046/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4379646
87 A = 6789200
59 meter
Y = 4540609
39 meter E =
0015983
Z = 2496705
05 I = 51
30035
XDOT = -2253
791577 Wp = 86
36369
YDOT = 5089
872009 meter/sec RA = 244
51906 deg
ZDOT = -5272
829160 TA = 65
50323
MA = 65
33665
Ha = 223
793 n
mi
Hp = 214
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14368920
17 X = 4316419
60
Y = 14897012
42 feet Y = 4589232
10 meter
Z = 8191289
53 Z = 2517825
83
XDOT = -7394
329321 XDOT = -2284
928444
YDOT = 16699
055148 feet/sec YDOT = 5064
494492 meter/sec
ZDOT = -17299
308269 ZDOT = -5283
852613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18774476
27 X = 5722460
37
Y = 8622220
01 feet Y = 2628052
66 meter
Z = 8286159
12 Z = 2525621
30
XDOT = -30
554523 XDOT = -9
313018
YDOT = 16834
233796 feet/sec YDOT = 5131
074461 meter/sec
ZDOT = -17349
529342 ZDOT = -5288
136543
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 19046
69561992
00016717 00000-0 10270-3 0 9116
2 25544 51
6371 245
3680 0005196 31
3488 328
7973 15
53245071 36372
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
69561992 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 245
3680 deg
Eccentricity:
0005196
Arg of perigee: 31
3488 deg
Mean anomaly: 328
7973 deg
Mean motion: 15
53245071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 332
Coasting Arc #13 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2019/047/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4172053
91 A = 6791241
09 meter
Y = -5217339
45 meter E =
0014457
Z = -1186679
06 I = 51
32395
XDOT = 3159
124588 Wp = 36
88903
YDOT = -3842
561673 meter/sec RA = 239
52714 deg
ZDOT = 5835
897316 TA = 310
16500
MA = 310
29151
Ha = 223
847 n
mi
Hp = 214
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13687840
92 X = -4107637
98
Y = -17117255
40 feet Y = -5263634
08 meter
Z = -3893304
02 Z = -1206788
46
XDOT = 10364
581980 XDOT = 3173
511510
YDOT = -12606
829636 feet/sec YDOT = -3807
153741 meter/sec
ZDOT = 19146
644739 ZDOT = 5851
277719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19165409
51 X = -5841616
82
Y = -10598749
48 feet Y = -3230498
84 meter
Z = -3983569
45 Z = -1214191
97
XDOT = 3870
261567 XDOT = 1179
655726
YDOT = -14162
698982 feet/sec YDOT = -4316
790650 meter/sec
ZDOT = 19216
405581 ZDOT = 5857
160421
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 19047
66069288
00016717 00000-0 10270-3 0 9126
2 25544 51
6385 240
5635 0005328 34
4457 325
7039 15
53255550 36521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
66069288 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 240
5635 deg
Eccentricity:
0005328
Arg of perigee: 34
4457 deg
Mean anomaly: 325
7039 deg
Mean motion: 15
53255550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 321
Coasting Arc #14 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2019/048/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3764969
17 A = 6791794
49 meter
Y = 5643762
31 meter E =
0012078
Z = -259455
17 I = 51
34288
XDOT = -4107
255237 Wp = 110
56753
YDOT = 2475
753753 meter/sec RA = 234
53959 deg
ZDOT = -5977
715210 TA = 72
23751
MA = 72
10574
Ha = 223
952 n
mi
Hp = 214
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12352261
04 X = 3702839
46
Y = 18516280
55 feet Y = 5685517
43 meter
Z = -851230
89 Z = -241317
81
XDOT = -13475
246841 XDOT = -4105
598943
YDOT = 8122
551684 feet/sec YDOT = 2429
832774 meter/sec
ZDOT = -19611
926542 ZDOT = -5997
662159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18705330
45 X = 5701384
72
Y = 12069527
43 feet Y = 3678791
96 meter
Z = -769878
45 Z = -234658
95
XDOT = -8129
963061 XDOT = -2478
012741
YDOT = 11396
413405 feet/sec YDOT = 3473
626806 meter/sec
ZDOT = -19702
172634 ZDOT = -6005
222219
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 19048
69010202
00016717 00000-0 10270-3 0 9133
2 25544 51
6377 235
4382 0005378 38
1607 321
9925 15
53271378 36682
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
69010202 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 235
4382 deg
Eccentricity:
0005378
Arg of perigee: 38
1607 deg
Mean anomaly: 321
9925 deg
Mean motion: 15
53271378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 319
Coasting Arc #15 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2019/049/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3185867
84 A = 6790717
37 meter
Y = -5756965
03 meter E =
0019028
Z = 1639102
35 I = 51
35984
XDOT = 5011
838220 Wp = 57
86657
YDOT = -1140
628920 meter/sec RA = 229
55276 deg
ZDOT = 5696
512690 TA = 320
16117
MA = 320
30070
Ha = 223
993 n
mi
Hp = 214
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10452322
31 X = -3129216
66
Y = -18887680
55 feet Y = -5792274
82 meter
Z = 5377632
40 Z = 1623764
87
XDOT = 16443
038781 XDOT = 4996
550923
YDOT = -3742
220865 feet/sec YDOT = -1084
668323 meter/sec
ZDOT = 18689
346097 ZDOT = 5720
820485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17361510
70 X = -5291788
46
Y = -12857214
28 feet Y = -3918878
91 meter
Z = 5308901
55 Z = 1618153
19
XDOT = 12371
140785 XDOT = 3770
723711
YDOT = -8889
728965 feet/sec YDOT = -2709
589388 meter/sec
ZDOT = 18799
163317 ZDOT = 5729
984979
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 19049
71951040
00016717 00000-0 10270-3 0 9142
2 25544 51
6381 230
3134 0005364 42
7351 317
4217 15
53272095 36847
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
71951040 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 230
3134 deg
Eccentricity:
0005364
Arg of perigee: 42
7351 deg
Mean anomaly: 317
4217 deg
Mean motion: 15
53272095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 293
Coasting Arc #16 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/050/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2372859
64 A = 6788189
05 meter
Y = 5641181
00 meter E =
0008221
Z = -2946386
75 I = 51
37457
XDOT = -5817
995477 Wp = 77
08716
YDOT = -147
478147 meter/sec RA = 224
56294 deg
ZDOT = -4977
830517 TA = 136
64090
MA = 136
57620
Ha = 224
046 n
mi
Hp = 214
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7784972
58 X = 2323913
48
Y = 18507811
67 feet Y = 5667442
10 meter
Z = -9666623
21 Z = -2934979
90
XDOT = -19087
911669 XDOT = -5791
735135
YDOT = -483
852189 feet/sec YDOT = -212
392540 meter/sec
ZDOT = -16331
464952 ZDOT = -5006
027503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15033775
61 X = 4582294
81
Y = 13345946
12 feet Y = 4067844
38 meter
Z = -9615602
34 Z = -2930835
59
XDOT = -16375
821763 XDOT = -4991
350473
YDOT = 6612
191073 feet/sec YDOT = 2015
395839 meter/sec
ZDOT = -16458
738876 ZDOT = -5016
623609
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 19050
68457963
00016717 00000-0 10270-3 0 9156
2 25544 51
6389 225
5085 0005359 45
6795 314
4796 15
53269738 36999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
68457963 = yrday
fracday
Element set: 915
Inclination: 51
6389 deg
RA of node: 225
5085 deg
Eccentricity:
0005359
Arg of perigee: 45
6795 deg
Mean anomaly: 314
4796 deg
Mean motion: 15
53269738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 369
Coasting Arc #17 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2019/051/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1387587
09 A = 6784964
12 meter
Y = -5291021
13 meter E =
0014836
Z = 4000547
33 I = 51
38952
XDOT = 6468
992727 Wp = 84
67483
YDOT = 1279
554356 meter/sec RA = 219
56809 deg
ZDOT = 3924
856058 TA = 324
39196
MA = 324
49085
Ha = 224
049 n
mi
Hp = 214
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4552451
07 X = -1347750
17
Y = -17358993
20 feet Y = -5306314
98 meter
Z = 13125155
30 Z = 3993904
40
XDOT = 21223
729420 XDOT = 6435
139354
YDOT = 4198
012979 feet/sec YDOT = 1351
706238 meter/sec
ZDOT = 12876
824338 ZDOT = 3956
196793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11875629
99 X = -3619692
02
Y = -13483471
16 feet Y = -4109762
01 meter
Z = 13095593
74 Z = 3991536
97
XDOT = 19815
942532 XDOT = 6039
899284
YDOT = -4773
447996 feet/sec YDOT = -1454
946949 meter/sec
ZDOT = 13018
211100 ZDOT = 3967
950743
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 19051
71398267
00016717 00000-0 10270-3 0 9163
2 25544 51
6398 220
3833 0005400 49
1160 311
0460 15
53304400 37151
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
71398267 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 220
3833 deg
Eccentricity:
0005400
Arg of perigee: 49
1160 deg
Mean anomaly: 311
0460 deg
Mean motion: 15
53304400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 278
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