[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 26th 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) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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
335/15:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
8
338/19:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
9
340/16:39:40
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
0
341/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 221
8
341/22:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 1701)
---------------------------------------
Vector Time (GMT): 2020/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3771442
71 A = 6794870
85 meter
Y = 3201352
44 meter E =
0009977
Z = 4652111
44 I = 51
23898
XDOT = -2212
492246 Wp = 65
69089
YDOT = 6761
220526 meter/sec RA = 269
35536 deg
ZDOT = -2850
190791 TA = 52
84085
MA = 52
74977
Ha = 229
545 n
mi
Hp = 221
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12373499
70 X = 3712766
27
Y = 10503124
79 feet Y = 3243199
12 meter
Z = 15262832
80 Z = 4670289
55
XDOT = -7258
832827 XDOT = -2274
089014
YDOT = 22182
482042 feet/sec YDOT = 6736
134574 meter/sec
ZDOT = -9351
019655 ZDOT = -2861
087668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14820787
09 X = -4517375
91
Y = 6418254
25 feet Y = 1956283
90 meter
Z = 15346774
01 Z = 4677696
72
XDOT = -16310
670019 XDOT = -4971
492222
YDOT = -15114
307967 feet/sec YDOT = -4606
841068 meter/sec
ZDOT = -9401
606775 ZDOT = -2865
609745
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 20330
54330932
00016717 00000-0 10270-3 0 9004
2 25544 51
6427 270
0720 0001908 72
4801 287
6557 15
49059568 17027
Satellite: ISS
Catalog Number: 25544
Epoch time: 20330
54330932 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 270
0720 deg
Eccentricity:
0001908
Arg of perigee: 72
4801 deg
Mean anomaly: 287
6557 deg
Mean motion: 15
49059568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1702
Checksum: 295
Coasting Arc #2 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2020/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4036191
09 A = 6794905
93 meter
Y = -2891545
39 meter E =
0012120
Z = -4650544
77 I = 51
24068
XDOT = 1637
751540 Wp = 104
85256
YDOT = -6899
019898 meter/sec RA = 264
38142 deg
ZDOT = 2871
432574 TA = 193
90418
MA = 193
93758
Ha = 229
633 n
mi
Hp = 221
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13242096
76 X = -3980966
87
Y = -9486697
48 feet Y = -2936371
94 meter
Z = -15257692
80 Z = -4670017
40
XDOT = 5373
200589 XDOT = 1700
828711
YDOT = -22634
579718 feet/sec YDOT = -6880
352860 meter/sec
ZDOT = 9420
710545 ZDOT = 2879
541093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14154730
50 X = 4314361
86
Y = -7889322
14 feet Y = -2404665
39 meter
Z = -15347636
49 Z = -4677959
60
XDOT = 17687
116707 XDOT = 5391
033172
YDOT = 13354
209282 feet/sec YDOT = 4070
362989 meter/sec
ZDOT = 9458
397765 ZDOT = 2882
919639
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 20331
51099805
00016717 00000-0 10270-3 0 9014
2 25544 51
6426 265
2851 0001846 76
6149 283
5206 15
49059465 17177
Satellite: ISS
Catalog Number: 25544
Epoch time: 20331
51099805 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 265
2851 deg
Eccentricity:
0001846
Arg of perigee: 76
6149 deg
Mean anomaly: 283
5206 deg
Mean motion: 15
49059465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 315
Coasting Arc #3 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2020/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4255553
87 A = 6794964
62 meter
Y = 2579799
51 meter E =
0009990
Z = 4620532
27 I = 51
24644
XDOT = -1071
241264 Wp = 67
47848
YDOT = 7005
874149 meter/sec RA = 259
40802 deg
ZDOT = -2916
160089 TA = 51
77115
MA = 51
68127
Ha = 229
499 n
mi
Hp = 221
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13961790
90 X = 4203945
11
Y = 8463909
16 feet Y = 2627099
27 meter
Z = 15159226
62 Z = 4641079
36
XDOT = -3514
571076 XDOT = -1135
338118
YDOT = 22985
151409 feet/sec YDOT = 6993
536582 meter/sec
ZDOT = -9567
454360 ZDOT = -2921
519047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13376393
78 X = -4077124
83
Y = 9206212
66 feet Y = 2806053
62 meter
Z = 15254155
26 Z = 4649466
52
XDOT = -18913
683853 XDOT = -5764
890838
YDOT = -11539
303716 feet/sec YDOT = -3517
179773 meter/sec
ZDOT = -9592
421108 ZDOT = -2923
769954
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 20332
54319566
00016717 00000-0 10270-3 0 9028
2 25544 51
6436 260
1795 0001803 79
4972 280
6381 15
49065471 17331
Satellite: ISS
Catalog Number: 25544
Epoch time: 20332
54319566 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 260
1795 deg
Eccentricity:
0001803
Arg of perigee: 79
4972 deg
Mean anomaly: 280
6381 deg
Mean motion: 15
49065471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 313
Coasting Arc #4 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2020/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468546
35 A = 6794961
66 meter
Y = -2234937
85 meter E =
0012025
Z = -4616975
85 I = 51
25456
XDOT = 487
778447 Wp = 105
56208
YDOT = -7045
141695 meter/sec RA = 254
43407 deg
ZDOT = 2941
515715 TA = 193
95905
MA = 193
99232
Ha = 229
618 n
mi
Hp = 221
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14660585
13 X = -4420795
36
Y = -7332473
28 feet Y = -2284640
93 meter
Z = -15147558
56 Z = -4638567
01
XDOT = 1600
322989 XDOT = 552
234586
YDOT = -23113
981939 feet/sec YDOT = -7039
326877 meter/sec
ZDOT = 9650
642110 ZDOT = 2944
041117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12448748
88 X = 3794378
66
Y = -10521118
26 feet Y = -3206836
85 meter
Z = -15247333
30 Z = -4647387
19
XDOT = 19898
682403 XDOT = 6065
118396
YDOT = 9556
878596 feet/sec YDOT = 2912
936596 meter/sec
ZDOT = 9662
498389 ZDOT = 2945
129509
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 20333
51087634
00016717 00000-0 10270-3 0 9035
2 25544 51
6441 255
3920 0001881 80
8066 279
3297 15
49081273 17484
Satellite: ISS
Catalog Number: 25544
Epoch time: 20333
51087634 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 255
3920 deg
Eccentricity:
0001881
Arg of perigee: 80
8066 deg
Mean anomaly: 279
3297 deg
Mean motion: 15
49081273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 313
Coasting Arc #5 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2020/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4637157
65 A = 6795066
21 meter
Y = 1894527
03 meter E =
0010244
Z = 4584855
21 I = 51
26480
XDOT = 82
299295 Wp = 69
04791
YDOT = 7056
178720 meter/sec RA = 249
46240 deg
ZDOT = -2989
919266 TA = 51
00658
MA = 50
91539
Ha = 229
523 n
mi
Hp = 221
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15213771
83 X = 4593356
75
Y = 6215639
86 feet Y = 1946137
64 meter
Z = 15042175
88 Z = 4607275
02
XDOT = 270
010809 XDOT = 17
912483
YDOT = 23150
192652 feet/sec YDOT = 7056
739373 meter/sec
ZDOT = -9809
446412 ZDOT = -2989
675081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11439104
77 X = -3486639
13
Y = 11666689
84 feet Y = 3556007
06 meter
Z = 15145801
98 Z = 4616440
44
XDOT = -20728
897549 XDOT = -6318
167973
YDOT = -7552
863407 feet/sec YDOT = -2302
112766 meter/sec
ZDOT = -9808
486315 ZDOT = -2989
626629
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 20334
54306665
00016717 00000-0 10270-3 0 9048
2 25544 51
6438 250
2871 0001918 83
6869 276
4500 15
49074815 17649
Satellite: ISS
Catalog Number: 25544
Epoch time: 20334
54306665 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 250
2871 deg
Eccentricity:
0001918
Arg of perigee: 83
6869 deg
Mean anomaly: 276
4500 deg
Mean motion: 15
49074815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 321
Coasting Arc #6 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2020/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4794648
87 A = 6795066
60 meter
Y = -1521007
99 meter E =
0011866
Z = -4580104
04 I = 51
27847
XDOT = -659
142670 Wp = 106
72224
YDOT = -6998
962390 meter/sec RA = 244
49022 deg
ZDOT = 3017
487093 TA = 193
63010
MA = 193
66217
Ha = 229
598 n
mi
Hp = 221
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15730475
28 X = -4755036
18
Y = -4990183
69 feet Y = -1574403
11 meter
Z = -15026588
07 Z = -4603299
02
XDOT = -2162
541569 XDOT = -595
486679
YDOT = -22962
475033 feet/sec YDOT = -7005
977864 meter/sec
ZDOT = 9899
892038 ZDOT = 3014
438875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10279285
64 X = 3133126
26
Y = -12784830
62 feet Y = -3896816
37 meter
Z = -15133820
65 Z = -4612788
53
XDOT = 21294
423115 XDOT = 6490
540166
YDOT = 5431
128054 feet/sec YDOT = 1655
407831 meter/sec
ZDOT = 9885
952371 ZDOT = 3013
238283
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 20335
51074208
00016717 00000-0 10270-3 0 9052
2 25544 51
6443 245
5000 0001853 87
1212 273
0150 15
49091351 17799
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
51074208 = yrday
fracday
Element set: 905
Inclination: 51
6443 deg
RA of node: 245
5000 deg
Eccentricity:
0001853
Arg of perigee: 87
1212 deg
Mean anomaly: 273
0150 deg
Mean motion: 15
49091351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 275
Coasting Arc #7 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2020/335/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4548800
64 A = 6793105
37 meter
Y = -62513
87 meter E =
0014781
Z = -5058318
70 I = 51
27366
XDOT = -1909
403586 Wp = 101
75723
YDOT = -7182
786940 meter/sec RA = 243
86801 deg
ZDOT = 1807
397305 TA = 185
86529
MA = 185
88262
Ha = 229
532 n
mi
Hp = 221
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14923886
62 X = -4523192
62
Y = -205097
99 feet Y = -113237
97 meter
Z = -16595533
80 Z = -5080353
24
XDOT = -6264
447460 XDOT = -1837
721047
YDOT = -23565
573950 feet/sec YDOT = -7203
738697 meter/sec
ZDOT = 5929
781183 ZDOT = 1798
295147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5992486
78 X = -1826509
97
Y = -13544814
42 feet Y = -4128459
44 meter
Z = -16697434
05 Z = -5089377
90
XDOT = 17797
223733 XDOT = 5424
593794
YDOT = -15125
850157 feet/sec YDOT = -4610
359128 meter/sec
ZDOT = 5887
846818 ZDOT = 1794
615710
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 20335
63976364
00016717 00000-0 10270-3 0 9060
2 25544 51
6441 244
8620 0001686 86
4828 273
6515 15
49099682 17815
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
63976364 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 244
8620 deg
Eccentricity:
0001686
Arg of perigee: 86
4828 deg
Mean anomaly: 273
6515 deg
Mean motion: 15
49099682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 339
Coasting Arc #8 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2020/336/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4546946
99 A = 6793093
67 meter
Y = -274731
33 meter E =
0006853
Z = 5035021
35 I = 51
29034
XDOT = 2487
273517 Wp = 62
80686
YDOT = 7006
580597 meter/sec RA = 238
89723 deg
ZDOT = -1858
825200 TA = 45
33012
MA = 45
27429
Ha = 229
295 n
mi
Hp = 221
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14917805
09 X = 4525223
54
Y = -901349
50 feet Y = -224006
30 meter
Z = 16519098
91 Z = 5057056
19
XDOT = 8160
346185 XDOT = 2417
768204
YDOT = 22987
469151 feet/sec YDOT = 7034
006716 meter/sec
ZDOT = -6098
507875 ZDOT = -1846
910604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7219613
39 X = 2200538
16
Y = 12955803
53 feet Y = 3948928
92 meter
Z = 16621020
01 Z = 5066086
90
XDOT = -16227
444611 XDOT = -4946
125117
YDOT = 16817
066818 feet/sec YDOT = 5125
841966 meter/sec
ZDOT = -6043
544978 ZDOT = -1842
072509
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 20336
67194600
00016717 00000-0 10270-3 0 9071
2 25544 51
6446 239
7561 0001532 88
3425 271
7901 15
49119749 17973
Satellite: ISS
Catalog Number: 25544
Epoch time: 20336
67194600 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 239
7561 deg
Eccentricity:
0001532
Arg of perigee: 88
3425 deg
Mean anomaly: 271
7901 deg
Mean motion: 15
49119749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 328
Coasting Arc #9 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2020/337/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4532020
56 A = 6793181
28 meter
Y = 627423
23 meter E =
0014600
Z = -5034742
43 I = 51
30766
XDOT = -3041
890682 Wp = 102
87887
YDOT = -6756
640818 meter/sec RA = 233
92601 deg
ZDOT = 1897
638904 TA = 185
64625
MA = 185
66272
Ha = 229
501 n
mi
Hp = 221
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14868833
86 X = -4514243
58
Y = 2058475
18 feet Y = 576843
09 meter
Z = -16518183
82 Z = -5056714
20
XDOT = -9979
956306 XDOT = -2975
327549
YDOT = -22167
456751 feet/sec YDOT = -6790
285533 meter/sec
ZDOT = 6225
849424 ZDOT = 1883
023057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8453795
55 X = -2576716
88
Y = -12267209
32 feet Y = -3739045
40 meter
Z = -16619833
13 Z = -5065725
14
XDOT = 14427
709443 XDOT = 4397
565838
YDOT = -18279
573336 feet/sec YDOT = -5571
613953 meter/sec
ZDOT = 6158
366224 ZDOT = 1877
070025
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 20337
63961517
00016717 00000-0 10270-3 0 9088
2 25544 51
6432 234
9678 0001633 91
2090 268
9247 15
49108091 18124
Satellite: ISS
Catalog Number: 25544
Epoch time: 20337
63961517 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 234
9678 deg
Eccentricity:
0001633
Arg of perigee: 91
2090 deg
Mean anomaly: 268
9247 deg
Mean motion: 15
49108091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 316
Coasting Arc #10 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2020/338/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480794
97 A = 6793226
35 meter
Y = -960043
84 meter E =
0007039
Z = 5010218
04 I = 51
32803
XDOT = 3578
701001 Wp = 64
67577
YDOT = 6489
869260 meter/sec RA = 228
95799 deg
ZDOT = -1951
862646 TA = 44
39124
MA = 44
33484
Ha = 229
339 n
mi
Hp = 221
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14700770
89 X = 4466860
50
Y = -3149750
12 feet Y = -910015
04 meter
Z = 16437723
23 Z = 5031950
16
XDOT = 11741
145017 XDOT = 3515
344440
YDOT = 21292
221982 feet/sec YDOT = 6529
534909 meter/sec
ZDOT = -6403
748838 ZDOT = -1934
631490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9552827
16 X = 2911701
72
Y = 11465645
63 feet Y = 3494728
79 meter
Z = 16538282
83 Z = 5040868
61
XDOT = -12566
332178 XDOT = -3830
218048
YDOT = 19615
994170 feet/sec YDOT = 5978
955023 meter/sec
ZDOT = -6324
138159 ZDOT = -1927
597311
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 20338
67179238
00016717 00000-0 10270-3 0 9095
2 25544 51
6424 229
8621 0001607 95
4664 264
6669 15
49111147 18284
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
67179238 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 229
8621 deg
Eccentricity:
0001607
Arg of perigee: 95
4664 deg
Mean anomaly: 264
6669 deg
Mean motion: 15
49111147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 333
Coasting Arc #11 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2020/338/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1901099
17 A = 6792770
90 meter
Y = -4023850
83 meter E =
0006625
Z = 5127767
63 I = 51
32973
XDOT = 5857
718800 Wp = 121
69985
YDOT = 4703
909929 meter/sec RA = 228
05078 deg
ZDOT = 1514
650883 TA = 313
60952
MA = 313
66447
Ha = 229
455 n
mi
Hp = 221
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6237202
00 X = 1921045
88
Y = -13201610
34 feet Y = -4002480
62 meter
Z = 16823384
62 Z = 5137050
33
XDOT = 19218
237534 XDOT = 5797
325543
YDOT = 15432
775356 feet/sec YDOT = 4769
077237 meter/sec
ZDOT = 4969
327043 ZDOT = 1542
959596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4875279
19 X = 1485985
10
Y = -13710132
69 feet Y = -4178848
44 meter
Z = 16866398
22 Z = 5140878
18
XDOT = 19528
382374 XDOT = 5952
250948
YDOT = 13238
184903 feet/sec YDOT = 4034
998758 meter/sec
ZDOT = 5100
223367 ZDOT = 1554
548082
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 20338
86532702
00016717 00000-0 10270-3 0 9107
2 25544 51
6415 228
9005 0001832 111
9417 248
1927 15
49119817 18310
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
86532702 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 228
9005 deg
Eccentricity:
0001832
Arg of perigee: 111
9417 deg
Mean anomaly: 248
1927 deg
Mean motion: 15
49119817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 301
Coasting Arc #12 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2020/339/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1600879
80 A = 6792755
43 meter
Y = 4143816
66 meter E =
0015235
Z = -5152384
02 I = 51
35351
XDOT = -6214
254957 Wp = 83
12488
YDOT = -4213
634026 meter/sec RA = 223
08464 deg
ZDOT = -1459
961978 TA = 172
74006
MA = 172
71797
Ha = 229
548 n
mi
Hp = 221
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5252230
30 X = -1622070
83
Y = 13595199
00 feet Y = 4125796
70 meter
Z = -16904147
06 Z = -5160211
38
XDOT = -20387
975582 XDOT = -6159
583292
YDOT = -13824
258616 feet/sec YDOT = -4282
820393 meter/sec
ZDOT = -4789
901504 ZDOT = -1490
016279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3616029
34 X = -1102165
74
Y = 14075221
54 feet Y = 4290127
53 meter
Z = -16940425
53 Z = -5163441
70
XDOT = -20720
230014 XDOT = -6315
526108
YDOT = -11247
768095 feet/sec YDOT = -3428
319715 meter/sec
ZDOT = -4928
911827 ZDOT = -1502
332325
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 20339
83299186
00016717 00000-0 10270-3 0 9112
2 25544 51
6419 224
1142 0001892 114
4586 245
6762 15
49110511 18462
Satellite: ISS
Catalog Number: 25544
Epoch time: 20339
83299186 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 224
1142 deg
Eccentricity:
0001892
Arg of perigee: 114
4586 deg
Mean anomaly: 245
6762 deg
Mean motion: 15
49110511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 308
Coasting Arc #13 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2020/340/16:39:40
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5287978
43 A = 6796237
81 meter
Y = -124394
86 meter E =
0011222
Z = 4259216
90 I = 51
38547
XDOT = 3024
584636 Wp = 78
85799
YDOT = 6071
446209 meter/sec RA = 218
67885 deg
ZDOT = -3567
668926 TA = 47
75621
MA = 47
66107
Ha = 229
404 n
mi
Hp = 221
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17349010
59 X = 5268287
59
Y = -408119
62 feet Y = -65371
52 meter
Z = 13973808
73 Z = 4284856
00
XDOT = 9923
177941 XDOT = 2973
796791
YDOT = 19919
442944 feet/sec YDOT = 6104
985759 meter/sec
ZDOT = -11704
950544 ZDOT = -3553
099266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14188423
74 X = 4324631
56
Y = 9824109
04 feet Y = 2994388
44 meter
Z = 14092465
15 Z = 4295383
38
XDOT = -2918
707283 XDOT = -889
621980
YDOT = 20956
542781 feet/sec YDOT = 6387
554240 meter/sec
ZDOT = -11637
597847 ZDOT = -3547
139824
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 20340
73614228
00016717 00000-0 10270-3 0 9122
2 25544 51
6398 219
6460 0001734 112
3604 247
7730 15
49087555 18608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20340
73614228 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 219
6460 deg
Eccentricity:
0001734
Arg of perigee: 112
3604 deg
Mean anomaly: 247
7730 deg
Mean motion: 15
49087555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 304
Coasting Arc #14 (Orbit 1874)
---------------------------------------
Vector Time (GMT): 2020/341/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2318844
25 A = 6792002
78 meter
Y = 3555355
65 meter E =
0016677
Z = -5316720
99 I = 51
39902
XDOT = -6376
424834 Wp = 92
34806
YDOT = -4222
663383 meter/sec RA = 213
77396 deg
ZDOT = -43
508037 TA = 177
23947
MA = 177
23026
Ha = 229
587 n
mi
Hp = 221
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7607756
74 X = -2332603
40
Y = 11664552
66 feet Y = 3529348
30 meter
Z = -17443310
34 Z = -5328018
07
XDOT = -20920
028982 XDOT = -6328
520486
YDOT = -13853
882490 feet/sec YDOT = -4293
701289 meter/sec
ZDOT = -142
742902 ZDOT = -74
366303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13040139
41 X = -3974634
49
Y = 4697484
26 feet Y = 1431793
20 meter
Z = -17495634
67 Z = -5332669
45
XDOT = -7823
956446 XDOT = -2384
741925
YDOT = -22773
026023 feet/sec YDOT = -6941
218332 meter/sec
ZDOT = -285
528750 ZDOT = -87
029163
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 20341
70380196
00016717 00000-0 10270-3 0 9135
2 25544 51
6404 214
8589 0001984 111
8831 248
2530 15
49114005 18759
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
70380196 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 214
8589 deg
Eccentricity:
0001984
Arg of perigee: 111
8831 deg
Mean anomaly: 248
2530 deg
Mean motion: 15
49114005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1875
Checksum: 298
Coasting Arc #15 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2020/341/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1614258
28 A = 6792241
92 meter
Y = 3970544
82 meter E =
0015972
Z = -5283041
21 I = 51
40940
XDOT = -6699
736634 Wp = 87
97465
YDOT = -3626
285004 meter/sec RA = 212
50644 deg
ZDOT = -679
484309 TA = 175
50613
MA = 175
49178
Ha = 229
487 n
mi
Hp = 221
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5296122
95 X = -1632876
15
Y = 13026721
86 feet Y = 3952389
46 meter
Z = -17332812
38 Z = -5290927
47
XDOT = -21980
763235 XDOT = -6655
387933
YDOT = -11897
260512 feet/sec YDOT = -3700
958233 meter/sec
ZDOT = -2229
279228 ZDOT = -711
921658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7754558
68 X = 2363589
49
Y = 11676608
49 feet Y = 3559030
27 meter
Z = -17369352
88 Z = -5294178
76
XDOT = -21441
191520 XDOT = -6535
275175
YDOT = 10705
914055 feet/sec YDOT = 3263
162604 meter/sec
ZDOT = -2379
386895 ZDOT = -725
237126
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 20341
96184305
00016717 00000-0 10270-3 0 9148
2 25544 51
6430 213
5844 0001644 116
8669 243
2649 15
49090374 18797
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
96184305 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 213
5844 deg
Eccentricity:
0001644
Arg of perigee: 116
8669 deg
Mean anomaly: 243
2649 deg
Mean motion: 15
49090374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 319
Coasting Arc #16 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2020/342/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1311079
63 A = 6792076
22 meter
Y = -4062820
75 meter E =
0004694
Z = 5279311
27 I = 51
43869
XDOT = 6989
707436 Wp = 118
34877
YDOT = 3078
595409 meter/sec RA = 207
54574 deg
ZDOT = 630
749667 TA = 325
59413
MA = 325
62451
Ha = 229
365 n
mi
Hp = 222
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4301442
34 X = 1330769
95
Y = -13329464
41 feet Y = -4048049
66 meter
Z = 17320575
05 Z = 5285727
49
XDOT = 22932
111011 XDOT = 6951
698333
YDOT = 10100
378639 feet/sec YDOT = 3156
546764 meter/sec
ZDOT = 2069
388670 ZDOT = 664
610937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8758552
30 X = -2669606
74
Y = -10882734
90 feet Y = -3317057
60 meter
Z = 17350308
07 Z = 5288373
90
XDOT = 20336
993511 XDOT = 6198
715622
YDOT = -12804
713491 feet/sec YDOT = -3902
876672 meter/sec
ZDOT = 2226
118179 ZDOT = 678
520821
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 20342
99401032
00016717 00000-0 10270-3 0 9152
2 25544 51
6431 208
4784 0001673 121
1532 238
9782 15
49134944 18953
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
99401032 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 208
4784 deg
Eccentricity:
0001673
Arg of perigee: 121
1532 deg
Mean anomaly: 238
9782 deg
Mean motion: 15
49134944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 309
Coasting Arc #17 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2020/343/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018246
05 A = 6792193
44 meter
Y = 4145226
33 meter E =
0015966
Z = -5297269
88 I = 51
46863
XDOT = -7204
831533 Wp = 89
33363
YDOT = -2501
881223 meter/sec RA = 202
58657 deg
ZDOT = -574
179290 TA = 175
16715
MA = 175
15172
Ha = 229
463 n
mi
Hp = 222
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3340702
26 X = -1038792
30
Y = 13599823
91 feet Y = 4133725
07 meter
Z = -17379494
36 Z = -5302265
75
XDOT = -23637
898731 XDOT = -7173
530211
YDOT = -8208
271728 feet/sec YDOT = -2582
275766 meter/sec
ZDOT = -1883
790321 ZDOT = -609
101893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9691952
01 X = 2954106
97
Y = 10068573
79 feet Y = 3068901
29 meter
Z = -17402649
63 Z = -5304327
61
XDOT = -18953
561781 XDOT = -5777
045631
YDOT = 14716
685223 feet/sec YDOT = 4485
645656 meter/sec
ZDOT = -2045
460646 ZDOT = -623
456405
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 20343
96166743
00016717 00000-0 10270-3 0 9168
2 25544 51
6425 203
6913 0001660 123
5870 236
5439 15
49091454 19103
Satellite: ISS
Catalog Number: 25544
Epoch time: 20343
96166743 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 203
6913 deg
Eccentricity:
0001660
Arg of perigee: 123
5870 deg
Mean anomaly: 236
5439 deg
Mean motion: 15
49091454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 305
Coasting Arc #18 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2020/344/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 709619
86 A = 6792025
05 meter
Y = -4192239
24 meter E =
0004491
Z = 5293227
12 I = 51
50105
XDOT = 7401
820873 Wp = 117
54185
YDOT = 1915
934127 meter/sec RA = 197
62970 deg
ZDOT = 522
744683 TA = 327
44420
MA = 327
47189
Ha = 229
364 n
mi
Hp = 222
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2328149
14 X = 730734
29
Y = -13754065
74 feet Y = -4184186
09 meter
Z = 17366230
72 Z = 5296725
19
XDOT = 24284
189217 XDOT = 7377
306978
YDOT = 6285
873119 feet/sec YDOT = 1998
569501 meter/sec
ZDOT = 1715
041612 ZDOT = 558
640785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10528030
40 X = -3208943
67
Y = -9120941
86 feet Y = -2780063
08 meter
Z = 17382449
99 Z = 5298170
76
XDOT = 17461
210884 XDOT = 5322
177077
YDOT = -16554
894556 feet/sec YDOT = -5045
931861 meter/sec
ZDOT = 1881
244519 ZDOT = 573
403330
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 20344
99382960
00016717 00000-0 10270-3 0 9174
2 25544 51
6432 198
5850 0001644 123
6663 236
4644 15
49137479 19268
Satellite: ISS
Catalog Number: 25544
Epoch time: 20344
99382960 = yrday
fracday
Element set: 917
Inclination: 51
6432 deg
RA of node: 198
5850 deg
Eccentricity:
0001644
Arg of perigee: 123
6663 deg
Mean anomaly: 236
4644 deg
Mean motion: 15
49137479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 336
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