[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 14th 2020
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
316/09:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
5
317/19:38:04
567 1
8 2
1 2
1
N/A -1
1 -0
2 229
1
000/00:06:09
133 0
2 0
1 222
6
320/00:49:49
100 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
6
320/09:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
6
323/04:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 222
7
328/12:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 1453)
---------------------------------------
Vector Time (GMT): 2020/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1523973
77 A = 6792561
41 meter
Y = 4340889
94 meter E =
0007888
Z = 4992222
36 I = 51
55488
XDOT = -7378
804707 Wp = 64
35907
YDOT = -211
428340 meter/sec RA = 348
82406 deg
ZDOT = -2062
793616 TA = 45
77141
MA = 45
70667
Ha = 229
171 n
mi
Hp = 221
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4999913
95 X = -1596651
30
Y = 14241764
90 feet Y = 4323441
26 meter
Z = 16378682
27 Z = 4984643
00
XDOT = -24208
676860 XDOT = -7365
872053
YDOT = -693
662533 feet/sec YDOT = -293
871061 meter/sec
ZDOT = -6767
695591 ZDOT = -2098
605979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7213499
95 X = -2198674
78
Y = -13302162
18 feet Y = -4054499
03 meter
Z = 16343382
14 Z = 4981462
88
XDOT = 15647
553464 XDOT = 4769
374296
YDOT = -17027
581695 feet/sec YDOT = -5190
006900 meter/sec
ZDOT = -6933
304231 ZDOT = -2113
271129
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 20314
54471209
00016717 00000-0 10270-3 0 9009
2 25544 51
6443 349
2217 0001951 90
2203 269
9171 15
49423190 14542
Satellite: ISS
Catalog Number: 25544
Epoch time: 20314
54471209 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 349
2217 deg
Eccentricity:
0001951
Arg of perigee: 90
2203 deg
Mean anomaly: 269
9171 deg
Mean motion: 15
49423190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1454
Checksum: 285
Coasting Arc #2 (Orbit 1468)
---------------------------------------
Vector Time (GMT): 2020/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1310700
45 A = 6792877
28 meter
Y = -4475993
47 meter E =
0014109
Z = -4951756
85 I = 51
52304
XDOT = 7319
161152 Wp = 104
04931
YDOT = -293
243191 meter/sec RA = 343
86772 deg
ZDOT = 2204
354481 TA = 187
53844
MA = 187
55967
Ha = 229
185 n
mi
Hp = 221
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4300198
33 X = 1384708
09
Y = -14685017
95 feet Y = -4460922
42 meter
Z = -16245921
41 Z = -4945210
19
XDOT = 24012
995904 XDOT = 7311
188667
YDOT = -962
083960 feet/sec YDOT = -211
439679 meter/sec
ZDOT = 7232
134123 ZDOT = 2239
889226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8234571
92 X = 2509897
52
Y = 12935383
58 feet Y = 3942704
92 meter
Z = -16215396
92 Z = -4942452
98
XDOT = -13986
582119 XDOT = -4263
110230
YDOT = 18167
722918 feet/sec YDOT = 5537
521945 meter/sec
ZDOT = 7396
474263 ZDOT = 2254
445355
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 20315
51218874
00016717 00000-0 10270-3 0 9015
2 25544 51
6447 344
4334 0001960 92
7037 267
4338 15
49387908 14695
Satellite: ISS
Catalog Number: 25544
Epoch time: 20315
51218874 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 344
4334 deg
Eccentricity:
0001960
Arg of perigee: 92
7037 deg
Mean anomaly: 267
4338 deg
Mean motion: 15
49387908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1469
Checksum: 324
Coasting Arc #3 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2020/316/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4702427
16 A = 6800008
65 meter
Y = -4087370
11 meter E =
0006316
Z = -2725562
86 I = 51
51677
XDOT = 5107
468474 Wp = 67
10199
YDOT = 2450
123271 meter/sec RA = 339
35288 deg
ZDOT = 5149
582490 TA = 262
10136
MA = 262
17305
Ha = 229
110 n
mi
Hp = 221
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15427910
62 X = 4761023
33
Y = -13410006
93 feet Y = -4034456
56 meter
Z = -8942135
36 Z = -2702577
60
XDOT = 16756
786333 XDOT = 5054
676695
YDOT = 8038
462174 feet/sec YDOT = 2506
943465 meter/sec
ZDOT = 16894
955675 ZDOT = 5174
264783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10709912
72 X = -3264381
40
Y = 17465392
79 feet Y = 5323451
72 meter
Z = -8835627
94 Z = -2693099
40
XDOT = -17018
815677 XDOT = -5187
335018
YDOT = -1851
426288 feet/sec YDOT = -564
314733 meter/sec
ZDOT = 17008
950171 ZDOT = 5184
328012
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 20316
41516364
00016717 00000-0 10270-3 0 9021
2 25544 51
6438 339
9641 0001825 101
3494 258
7861 15
49413876 14833
Satellite: ISS
Catalog Number: 25544
Epoch time: 20316
41516364 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 339
9641 deg
Eccentricity:
0001825
Arg of perigee: 101
3494 deg
Mean anomaly: 258
7861 deg
Mean motion: 15
49413876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 318
Coasting Arc #4 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2020/317/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470998
30 A = 6800234
76 meter
Y = 4417472
37 meter E =
0015421
Z = 2577655
17 I = 51
48712
XDOT = -5161
050609 Wp = 102
71872
YDOT = -2151
740929 meter/sec RA = 334
39363 deg
ZDOT = -5241
172284 TA = 48
27327
MA = 48
14149
Ha = 229
064 n
mi
Hp = 221
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14668629
58 X = -4532584
57
Y = 14493019
60 feet Y = 4367130
11 meter
Z = 8456873
92 Z = 2555786
75
XDOT = -16932
580737 XDOT = -5111
146423
YDOT = -7059
517484 feet/sec YDOT = -2209
176464 meter/sec
ZDOT = -17195
447125 ZDOT = -5266
122000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9339959
00 X = 2846819
50
Y = -18430555
80 feet Y = -5617633
41 meter
Z = 8355525
49 Z = 2546764
17
XDOT = 16843
732588 XDOT = 5133
969693
YDOT = 653
023833 feet/sec YDOT = 199
041664 meter/sec
ZDOT = -17310
686063 ZDOT = -5276
297112
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 20317
44713090
00016717 00000-0 10270-3 0 9031
2 25544 51
6443 334
8561 0001802 97
0739 263
0616 15
49448878 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
44713090 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 334
8561 deg
Eccentricity:
0001802
Arg of perigee: 97
0739 deg
Mean anomaly: 263
0616 deg
Mean motion: 15
49448878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 321
Coasting Arc #5 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2020/317/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -645441
73 A = 6792825
84 meter
Y = -4338882
67 meter E =
0014103
Z = -5199048
32 I = 51
44692
XDOT = 7091
625053 Wp = 99
71011
YDOT = -2572
507519 meter/sec RA = 332
36879 deg
ZDOT = 1267
117021 TA = 182
51520
MA = 182
52230
Ha = 229
094 n
mi
Hp = 222
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2117590
98 X = -571620
44
Y = -14235179
38 feet Y = -4345687
68 meter
Z = -17057245
15 Z = -5202004
42
XDOT = 23266
486395 XDOT = 7113
709463
YDOT = -8439
985300 feet/sec YDOT = -2493
080401 meter/sec
ZDOT = 4157
208075 ZDOT = 1301
619827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1309232
31 X = 399054
01
Y = -14316144
12 feet Y = -4363560
73 meter
Z = -17070678
49 Z = -5203142
80
XDOT = 23508
064679 XDOT = 7165
258114
YDOT = -2995
191492 feet/sec YDOT = -912
934367 meter/sec
ZDOT = 4316
865618 ZDOT = 1315
780640
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 20317
83412046
00016717 00000-0 10270-3 0 9042
2 25544 51
6454 332
9419 0000171 109
0196 251
0973 15
49026549 15056
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
83412046 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 332
9419 deg
Eccentricity:
0000171
Arg of perigee: 109
0196 deg
Mean anomaly: 251
0973 deg
Mean motion: 15
49026549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 292
Coasting Arc #6 (Orbit 1520)
---------------------------------------
Vector Time (GMT): 2020/318/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 995202
07 A = 6792733
46 meter
Y = 4272289
60 meter E =
0004367
Z = 5183701
64 I = 51
41671
XDOT = -6858
579461 Wp = 55
61616
YDOT = 3164
738555 meter/sec RA = 327
40916 deg
ZDOT = -1288
353817 TA = 46
82280
MA = 46
78631
Ha = 228
964 n
mi
Hp = 222
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3265098
67 X = 922173
90
Y = 14016698
16 feet Y = 4283010
20 meter
Z = 17006895
14 Z = 5188358
81
XDOT = -22501
901118 XDOT = -6887
200512
YDOT = 10383
000508 feet/sec YDOT = 3087
880998 meter/sec
ZDOT = -4226
882602 ZDOT = -1321
740501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 105268
49 X = 32085
84
Y = 14366370
40 feet Y = 4378869
70 meter
Z = 17028197
18 Z = 5190194
50
XDOT = -23115
151783 XDOT = -7045
498263
YDOT = 5374
978096 feet/sec YDOT = 1638
293324 meter/sec
ZDOT = -4381
398737 ZDOT = -1335
450335
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 20318
86634965
00016717 00000-0 10270-3 0 9053
2 25544 51
6445 327
8362 0000067 107
6085 252
5072 15
49060490 15218
Satellite: ISS
Catalog Number: 25544
Epoch time: 20318
86634965 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 327
8362 deg
Eccentricity:
0000067
Arg of perigee: 107
6085 deg
Mean anomaly: 252
5072 deg
Mean motion: 15
49060490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1521
Checksum: 305
Coasting Arc #7 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2020/319/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1350711
77 A = 6792825
70 meter
Y = -4187371
46 meter E =
0013936
Z = -5187730
85 I = 51
38887
XDOT = 6552
685047 Wp = 100
03001
YDOT = -3726
046430 meter/sec RA = 322
44712 deg
ZDOT = 1302
068361 TA = 182
54816
MA = 182
55527
Ha = 229
033 n
mi
Hp = 222
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4431469
07 X = -1278587
14
Y = -13738095
36 feet Y = -4202072
53 meter
Z = -17020114
35 Z = -5194117
33
XDOT = 21498
310522 XDOT = 6587
538918
YDOT = -12224
561779 feet/sec YDOT = -3652
574796 meter/sec
ZDOT = 4271
877825 ZDOT = 1333
984150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1550567
30 X = -472612
91
Y = -14316796
08 feet Y = -4363759
44 meter
Z = -17049415
40 Z = -5196661
81
XDOT = 22397
423204 XDOT = 6826
734593
YDOT = -7686
483169 feet/sec YDOT = -2342
840070 meter/sec
ZDOT = 4419
614980 ZDOT = 1347
098646
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 20319
83406511
00016717 00000-0 10270-3 0 9066
2 25544 51
6445 323
0493 0000059 139
7076 220
4079 15
49036081 15364
Satellite: ISS
Catalog Number: 25544
Epoch time: 20319
83406511 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 323
0493 deg
Eccentricity:
0000059
Arg of perigee: 139
7076 deg
Mean anomaly: 220
4079 deg
Mean motion: 15
49036081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 294
Coasting Arc #8 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2020/320/00:49:49
100
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5799189
92 A = 6799422
03 meter
Y = -1241975
14 meter E =
0012563
Z = 3314709
00 I = 51
40072
XDOT = -1416
373403 Wp = 90
52671
YDOT = 5903
893298 meter/sec RA = 321
41444 deg
ZDOT = 4674
582846 TA = 308
10123
MA = 308
21444
Ha = 228
947 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19026213
65 X = 5796545
61
Y = -4074721
57 feet Y = -1177139
43 meter
Z = 10875029
54 Z = 3342873
55
XDOT = -4646
894366 XDOT = -1504
994386
YDOT = 19369
728669 feet/sec YDOT = 5887
558586 meter/sec
ZDOT = 15336
557893 ZDOT = 4667
487575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3945192
83 X = 1202494
77
Y = -18978551
48 feet Y = -5784662
49 meter
Z = 11005292
66 Z = 3354413
20
XDOT = 14405
491381 XDOT = 4390
793773
YDOT = 11897
898134 feet/sec YDOT = 3626
479351 meter/sec
ZDOT = 15303
445355 ZDOT = 4664
490144
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 20320
09212107
00016717 00000-0 10270-3 0 9073
2 25544 51
6399 321
7679 0000444 173
5347 186
5809 15
49039489 15401
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
09212107 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 321
7679 deg
Eccentricity:
0000444
Arg of perigee: 173
5347 deg
Mean anomaly: 186
5809 deg
Mean motion: 15
49039489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 318
Coasting Arc #9 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2020/320/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -491289
97 A = 6794207
65 meter
Y = -4709203
55 meter E =
0012062
Z = -4884072
93 I = 51
37689
XDOT = 6571
401297 Wp = 107
52020
YDOT = -3128
682939 meter/sec RA = 319
54606 deg
ZDOT = 2356
922306 TA = 185
69750
MA = 185
71124
Ha = 229
124 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1611843
73 X = -414868
98
Y = -15450142
88 feet Y = -4714269
84 meter
Z = -16023861
32 Z = -4886274
23
XDOT = 21559
715542 XDOT = 6594
449854
YDOT = -10264
707805 feet/sec YDOT = -3055
068119 meter/sec
ZDOT = 7732
684730 ZDOT = 2388
900293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6458462
55 X = 1968539
39
Y = 14116478
90 feet Y = 4302702
77 meter
Z = -16033788
45 Z = -4887098
72
XDOT = -15954
038369 XDOT = -4862
790895
YDOT = 16245
443917 feet/sec YDOT = 4951
611306 meter/sec
ZDOT = 7880
674302 ZDOT = 2402
029527
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 20320
41469259
00016717 00000-0 10270-3 0 9082
2 25544 51
6436 320
1750 0000259 137
7585 222
3585 15
49010999 15456
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
41469259 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 320
1750 deg
Eccentricity:
0000259
Arg of perigee: 137
7585 deg
Mean anomaly: 222
3585 deg
Mean motion: 15
49010999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 312
Coasting Arc #10 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2020/321/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 868643
97 A = 6794123
52 meter
Y = 4659467
49 meter E =
0007104
Z = 4863621
93 I = 51
35191
XDOT = -6291
415813 Wp = 61
19619
YDOT = 3667
840197 meter/sec RA = 314
58118 deg
ZDOT = -2384
218440 TA = 52
31344
MA = 52
24903
Ha = 229
045 n
mi
Hp = 222
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2849881
81 X = 792850
54
Y = 15286966
82 feet Y = 4668756
99 meter
Z = 15956764
85 Z = 4867657
96
XDOT = -20641
127995 XDOT = -6320
381650
YDOT = 12033
596447 feet/sec YDOT = 3597
323360 meter/sec
ZDOT = -7822
238975 ZDOT = -2414
850441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7808114
31 X = -2379913
24
Y = -13426039
66 feet Y = -4092256
89 meter
Z = 15975178
73 Z = 4869234
48
XDOT = 14245
167684 XDOT = 4341
927110
YDOT = -17784
060841 feet/sec YDOT = -5420
581744 meter/sec
ZDOT = -7964
031210 ZDOT = -2427
436713
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 20321
44691585
00016717 00000-0 10270-3 0 9096
2 25544 51
6435 315
0690 0000273 120
8494 239
2683 15
49051579 15612
Satellite: ISS
Catalog Number: 25544
Epoch time: 20321
44691585 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 315
0690 deg
Eccentricity:
0000273
Arg of perigee: 120
8494 deg
Mean anomaly: 239
2683 deg
Mean motion: 15
49051579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 312
Coasting Arc #11 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2020/322/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1258561
92 A = 6794250
13 meter
Y = -4585097
65 meter E =
0011952
Z = -4864611
37 I = 51
33021
XDOT = 5945
928021 Wp = 107
19416
YDOT = -4174
375170 meter/sec RA = 309
61446 deg
ZDOT = 2397
644791 TA = 186
46429
MA = 186
47972
Ha = 229
120 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4129140
16 X = -1183566
46
Y = -15042971
30 feet Y = -4598751
89 meter
Z = -15960011
04 Z = -4870543
49
XDOT = 19507
637865 XDOT = 5980
518612
YDOT = -13695
456593 feet/sec YDOT = -4107
690415 meter/sec
ZDOT = 7866
288686 ZDOT = 2426
611880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9144659
21 X = 2787292
13
Y = 12603468
14 feet Y = 3841537
09 meter
Z = -15987199
11 Z = -4872898
29
XDOT = -12333
105387 XDOT = -3759
130522
YDOT = 19090
832030 feet/sec YDOT = 5818
885603 meter/sec
ZDOT = 8000
407778 ZDOT = 2438
524291
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 20322
41462426
00016717 00000-0 10270-3 0 9106
2 25544 51
6446 310
2820 0000204 109
3445 250
7728 15
49016272 15763
Satellite: ISS
Catalog Number: 25544
Epoch time: 20322
41462426 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 310
2820 deg
Eccentricity:
0000204
Arg of perigee: 109
3445 deg
Mean anomaly: 250
7728 deg
Mean motion: 15
49016272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 273
Coasting Arc #12 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2020/323/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2773159
31 A = 6792434
93 meter
Y = 3323941
21 meter E =
0003349
Z = 5231955
60 I = 51
30814
XDOT = -5028
456628 Wp = 62
62098
YDOT = 5702
305070 meter/sec RA = 305
62983 deg
ZDOT = -955
480661 TA = 36
58336
MA = 36
56049
Ha = 228
838 n
mi
Hp = 222
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9098291
71 X = 2710369
66
Y = 10905318
92 feet Y = 3354600
95 meter
Z = 17165208
65 Z = 5245274
62
XDOT = -16497
561116 XDOT = -5087
206553
YDOT = 18708
349967 feet/sec YDOT = 5645
744885 meter/sec
ZDOT = -3134
779071 ZDOT = -980
049308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2297747
17 X = 700353
34
Y = -13939634
56 feet Y = -4248800
61 meter
Z = 17226613
92 Z = 5250671
92
XDOT = 23912
155989 XDOT = 7288
425146
YDOT = -81
114486 feet/sec YDOT = -24
723695 meter/sec
ZDOT = -3248
637995 ZDOT = -990
184861
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 20323
25330247
00016717 00000-0 10270-3 0 9115
2 25544 51
6448 306
1313 0000379 190
2422 169
8720 15
49071328 15892
Satellite: ISS
Catalog Number: 25544
Epoch time: 20323
25330247 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 306
1313 deg
Eccentricity:
0000379
Arg of perigee: 190
2422 deg
Mean anomaly: 169
8720 deg
Mean motion: 15
49071328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 291
Coasting Arc #13 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2020/324/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3041512
52 A = 6792543
77 meter
Y = -3098831
76 meter E =
0014299
Z = -5236136
87 I = 51
28898
XDOT = 4522
546089 Wp = 98
87719
YDOT = -6091
341704 meter/sec RA = 300
66149 deg
ZDOT = 978
084038 TA = 180
55313
MA = 180
55471
Ha = 228
994 n
mi
Hp = 222
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9978715
61 X = -2981199
98
Y = -10166770
87 feet Y = -3132506
32 meter
Z = -17178926
72 Z = -5250765
35
XDOT = 14837
749635 XDOT = 4585
574169
YDOT = -19984
716875 feet/sec YDOT = -6040
415046 meter/sec
ZDOT = 3208
937134 ZDOT = 1000
205417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -919311
31 X = -280206
09
Y = 14133998
39 feet Y = 4308042
71 meter
Z = -17246404
69 Z = -5256704
15
XDOT = -23727
665197 XDOT = -7232
192352
YDOT = 2496
849773 feet/sec YDOT = 761
039811 meter/sec
ZDOT = 3311
491590 ZDOT = 1009
342637
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 20324
22100823
00016717 00000-0 10270-3 0 9129
2 25544 51
6443 301
3454 0000342 189
3937 170
7207 15
49042540 16043
Satellite: ISS
Catalog Number: 25544
Epoch time: 20324
22100823 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 301
3454 deg
Eccentricity:
0000342
Arg of perigee: 189
3937 deg
Mean anomaly: 170
7207 deg
Mean motion: 15
49042540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 266
Coasting Arc #14 (Orbit 1619)
---------------------------------------
Vector Time (GMT): 2020/325/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275851
15 A = 6792439
88 meter
Y = 2849168
31 meter E =
0003400
Z = 5221517
44 I = 51
27360
XDOT = -4003
116078 Wp = 59
72338
YDOT = 6455
309590 meter/sec RA = 295
69072 deg
ZDOT = -1008
764348 TA = 40
00436
MA = 39
97931
Ha = 228
767 n
mi
Hp = 222
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10747543
14 X = 3218384
11
Y = 9347665
05 feet Y = 2885479
40 meter
Z = 17130962
72 Z = 5237291
04
XDOT = -13133
582932 XDOT = -4070
103750
YDOT = 21178
837238 feet/sec YDOT = 6410
169418 meter/sec
ZDOT = -3309
594317 ZDOT = -1028
372128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -447558
88 X = -136415
95
Y = -14148813
13 feet Y = -4312558
24 meter
Z = 17203755
03 Z = 5243704
53
XDOT = 23386
661168 XDOT = 7128
254324
YDOT = -4883
180320 feet/sec YDOT = -1488
393362 meter/sec
ZDOT = -3400
531280 ZDOT = -1036
481934
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 20325
25322186
00016717 00000-0 10270-3 0 9132
2 25544 51
6451 296
2392 0000320 211
1433 148
9698 15
49080290 16209
Satellite: ISS
Catalog Number: 25544
Epoch time: 20325
25322186 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 296
2392 deg
Eccentricity:
0000320
Arg of perigee: 211
1433 deg
Mean anomaly: 148
9698 deg
Mean motion: 15
49080290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1620
Checksum: 285
Coasting Arc #15 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2020/326/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3503768
29 A = 6792583
77 meter
Y = -2586777
44 meter E =
0014229
Z = -5225202
09 I = 51
25880
XDOT = 3442
118908 Wp = 98
53477
YDOT = -6752
439854 meter/sec RA = 290
71982 deg
ZDOT = 1035
089707 TA = 181
45363
MA = 181
45777
Ha = 228
998 n
mi
Hp = 222
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11495302
77 X = -3449200
58
Y = -8486802
63 feet Y = -2625653
58 meter
Z = -17143051
48 Z = -5242089
78
XDOT = 11293
041036 XDOT = 3512
343009
YDOT = -22153
674062 feet/sec YDOT = -6713
555043 meter/sec
ZDOT = 3395
963607 ZDOT = 1051
980294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1829351
51 X = 557586
34
Y = 14076297
80 feet Y = 4290455
57 meter
Z = -17221014
26 Z = -5248965
15
XDOT = -22721
632441 XDOT = -6925
553568
YDOT = 7201
976923 feet/sec YDOT = 2195
162566 meter/sec
ZDOT = 3474
334548 ZDOT = 1058
977170
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 20326
22092171
00016717 00000-0 10270-3 0 9149
2 25544 51
6438 291
4531 0000145 197
1841 162
9305 15
49040496 16358
Satellite: ISS
Catalog Number: 25544
Epoch time: 20326
22092171 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 291
4531 deg
Eccentricity:
0000145
Arg of perigee: 197
1841 deg
Mean anomaly: 162
9305 deg
Mean motion: 15
49040496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 291
Coasting Arc #16 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2020/327/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3694772
23 A = 6792482
48 meter
Y = 2305760
85 meter E =
0003587
Z = 5210111
00 I = 51
24784
XDOT = -2871
930036 Wp = 58
54043
YDOT = 7023
045196 meter/sec RA = 285
74765 deg
ZDOT = -1069
056358 TA = 41
77901
MA = 41
75162
Ha = 228
772 n
mi
Hp = 222
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12121956
14 X = 3643406
03
Y = 7564832
18 feet Y = 2346790
91 meter
Z = 17093540
02 Z = 5227934
24
XDOT = -9422
342639 XDOT = -2945
057512
YDOT = 23041
486863 feet/sec YDOT = 6990
520397 meter/sec
ZDOT = -3507
402748 ZDOT = -1083
184323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3166069
85 X = -965018
09
Y = -13831988
29 feet Y = -4215990
03 meter
Z = 17175846
96 Z = 5235198
15
XDOT = 21910
388281 XDOT = 6678
286348
YDOT = -9461
607298 feet/sec YDOT = -2883
897904 meter/sec
ZDOT = -3572
993738 ZDOT = -1089
048491
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 20327
25313083
00016717 00000-0 10270-3 0 9152
2 25544 51
6436 286
3474 0000232 209
9649 150
1488 15
49078583 16517
Satellite: ISS
Catalog Number: 25544
Epoch time: 20327
25313083 = yrday
fracday
Element set: 915
Inclination: 51
6436 deg
RA of node: 286
3474 deg
Eccentricity:
0000232
Arg of perigee: 209
9649 deg
Mean anomaly: 150
1488 deg
Mean motion: 15
49078583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 313
Coasting Arc #17 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2020/328/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3878246
17 A = 6792630
24 meter
Y = -2011978
90 meter E =
0014148
Z = -5213594
85 I = 51
23898
XDOT = 2271
385782 Wp = 98
99176
YDOT = -7221
601583 meter/sec RA = 280
77442 deg
ZDOT = 1097
666465 TA = 181
61011
MA = 181
61467
Ha = 228
994 n
mi
Hp = 222
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12723904
75 X = -3830134
51
Y = -6600980
63 feet Y = -2055078
95 meter
Z = -17104969
98 Z = -5232317
25
XDOT = 7452
053090 XDOT = 2346
639226
YDOT = -23692
918580 feet/sec YDOT = -7195
780604 meter/sec
ZDOT = 3601
267931 ZDOT = 1108
882462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4505539
09 X = 1373288
31
Y = 13498326
42 feet Y = 4114289
89 meter
Z = -17191451
26 Z = -5239954
34
XDOT = -20796
222577 XDOT = -6338
688642
YDOT = 11592
761495 feet/sec YDOT = 3533
473704 meter/sec
ZDOT = 3653
384524 ZDOT = 1113
551603
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 20328
22082655
00016717 00000-0 10270-3 0 9169
2 25544 51
6427 281
5606 0000140 205
6833 154
4310 15
49038139 16667
Satellite: ISS
Catalog Number: 25544
Epoch time: 20328
22082655 = yrday
fracday
Element set: 916
Inclination: 51
6427 deg
RA of node: 281
5606 deg
Eccentricity:
0000140
Arg of perigee: 205
6833 deg
Mean anomaly: 154
4310 deg
Mean motion: 15
49038139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 290
Coasting Arc #18 (Orbit 1670)
---------------------------------------
Vector Time (GMT): 2020/328/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1098235
23 A = 6801337
08 meter
Y = -6197509
66 meter E =
0005268
Z = -2575636
45 I = 51
26546
XDOT = 4724
619780 Wp = 50
29750
YDOT = -3003
351610 meter/sec RA = 279
11374 deg
ZDOT = 5222
596544 TA = 280
65586
MA = 280
71518
Ha = 229
006 n
mi
Hp = 222
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3603133
96 X = -1016340
10
Y = -20333036
95 feet Y = -6209332
89 meter
Z = -8450250
81 Z = -2580772
68
XDOT = 15500
721063 XDOT = 4732
484417
YDOT = -9853
515780 feet/sec YDOT = -2950
473799 meter/sec
ZDOT = 17134
503098 ZDOT = 5245
566054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20581823
45 X = 6273339
79
Y = 1550932
05 feet Y = 472724
09 meter
Z = -8473774
71 Z = -2582806
53
XDOT = 5891
359103 XDOT = 1795
686255
YDOT = 15828
945296 feet/sec YDOT = 4824
662526 meter/sec
ZDOT = 17240
799911 ZDOT = 5254
995813
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 20328
54339156
00016717 00000-0 10270-3 0 9176
2 25544 51
6420 279
9658 0000188 7
7488 352
3665 15
49043585 16716
Satellite: ISS
Catalog Number: 25544
Epoch time: 20328
54339156 = yrday
fracday
Element set: 917
Inclination: 51
6420 deg
RA of node: 279
9658 deg
Eccentricity:
0000188
Arg of perigee: 7
7488 deg
Mean anomaly: 352
3665 deg
Mean motion: 15
49043585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1671
Checksum: 336
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