[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 27th 2021
- 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) : 82 0 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
029/19:22:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 223
3
033/03:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 223
3
036/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 223
2
040/05:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 222
9
Coasting Arc #1 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2021/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4971659
15 A = 6803871
88 meter
Y = -4428107
50 meter E =
0008554
Z = -1379880
45 I = 51
45281
XDOT = 4134
442295 Wp = 22
17842
YDOT = 2845
039201 meter/sec RA = 327
81490 deg
ZDOT = 5785
881322 TA = 322
78174
MA = 322
84100
Ha = 228
595 n
mi
Hp = 223
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16311217
69 X = 5027508
63
Y = -14527911
75 feet Y = -4372198
42 meter
Z = -4527166
84 Z = -1355595
38
XDOT = 13564
443224 XDOT = 4074
217010
YDOT = 9334
118112 feet/sec YDOT = 2890
936188 meter/sec
ZDOT = 18982
550269 ZDOT = 5805
818420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21192699
04 X = 6459534
67
Y = 5384705
10 feet Y = 1641258
11 meter
Z = -4414265
55 Z = -1345468
14
XDOT = 195
986699 XDOT = 59
736746
YDOT = 14812
039199 feet/sec YDOT = 4514
709548 meter/sec
ZDOT = 19074
924084 ZDOT = 5814
036861
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 21025
50262281
00016717 00000-0 10270-3 0 9003
2 25544 51
6439 328
4595 0002289 295
7716 64
3197 15
48877081 26472
Satellite: ISS
Catalog Number: 25544
Epoch time: 21025
50262281 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 328
4595 deg
Eccentricity:
0002289
Arg of perigee: 295
7716 deg
Mean anomaly: 64
3197 deg
Mean motion: 15
48877081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 329
Coasting Arc #2 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2021/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4560098
18 A = 6803834
42 meter
Y = 4846443
83 meter E =
0011506
Z = 1391115
46 I = 51
42561
XDOT = -4386
038298 Wp = 119
13676
YDOT = -2459
347725 meter/sec RA = 322
85404 deg
ZDOT = -5778
694751 TA = 45
69014
MA = 45
59585
Ha = 228
630 n
mi
Hp = 223
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14960952
03 X = -4620710
75
Y = 15900406
28 feet Y = 4795110
49 meter
Z = 4564027
09 Z = 1368818
11
XDOT = -14389
889429 XDOT = -4330
142267
YDOT = -8068
726132 feet/sec YDOT = -2508
082457 meter/sec
ZDOT = -18958
972280 ZDOT = -5799
864356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21629112
13 X = -6592553
38
Y = -3125736
87 feet Y = -952724
60 meter
Z = 4460339
25 Z = 1359511
40
XDOT = -1822
661205 XDOT = -555
547135
YDOT = -14729
226367 feet/sec YDOT = -4489
468197 meter/sec
ZDOT = -19057
086439 ZDOT = -5808
599947
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 21026
53493885
00016717 00000-0 10270-3 0 9014
2 25544 51
6449 323
3540 0002266 302
0302 58
0628 15
48885910 26632
Satellite: ISS
Catalog Number: 25544
Epoch time: 21026
53493885 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 323
3540 deg
Eccentricity:
0002266
Arg of perigee: 302
0302 deg
Mean anomaly: 58
0628 deg
Mean motion: 15
48885910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 300
Coasting Arc #3 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2021/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4092928
45 A = 6803792
91 meter
Y = -5237524
99 meter E =
0008813
Z = -1429443
50 I = 51
39824
XDOT = 4612
376367 Wp = 22
10212
YDOT = 2036
065498 meter/sec RA = 317
89189 deg
ZDOT = 5766
044832 TA = 322
29175
MA = 322
35349
Ha = 228
689 n
mi
Hp = 223
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13428242
95 X = 4158135
07
Y = -17183480
92 feet Y = -5191390
19 meter
Z = -4689775
26 Z = -1409404
34
XDOT = 15132
468395 XDOT = 4561
258354
YDOT = 6680
004915 feet/sec YDOT = 2087
358084 meter/sec
ZDOT = 18917
469921 ZDOT = 5788
325313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21814636
07 X = 6649101
08
Y = 759607
31 feet Y = 231528
31 meter
Z = -4596560
34 Z = -1401031
59
XDOT = 3490
216080 XDOT = 1063
817861
YDOT = 14468
433880 feet/sec YDOT = 4409
978647 meter/sec
ZDOT = 19020
761772 ZDOT = 5797
528188
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 21027
50273349
00016717 00000-0 10270-3 0 9024
2 25544 51
6440 318
5686 0002320 306
1407 53
9528 15
48882114 26784
Satellite: ISS
Catalog Number: 25544
Epoch time: 21027
50273349 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 318
5686 deg
Eccentricity:
0002320
Arg of perigee: 306
1407 deg
Mean anomaly: 53
9528 deg
Mean motion: 15
48882114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2678
Checksum: 302
Coasting Arc #4 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2021/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615360
94 A = 6803765
12 meter
Y = 5574728
18 meter E =
0011520
Z = 1438815
49 I = 51
37473
XDOT = -4786
995376 Wp = 117
15173
YDOT = -1610
165569 meter/sec RA = 312
92805 deg
ZDOT = -5759
282546 TA = 47
13044
MA = 47
03374
Ha = 228
692 n
mi
Hp = 223
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11861420
41 X = -3684419
26
Y = 18289790
61 feet Y = 5533912
38 meter
Z = 4720523
25 Z = 1421086
73
XDOT = -15705
365408 XDOT = -4740
659871
YDOT = -5282
695437 feet/sec YDOT = -1663
437717 meter/sec
ZDOT = -18895
283943 ZDOT = -5782
422700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21763108
92 X = -6633395
60
Y = 1532593
50 feet Y = 467134
50 meter
Z = 4638029
96 Z = 1413671
53
XDOT = -5059
175532 XDOT = -1542
036702
YDOT = -14025
832909 feet/sec YDOT = -4275
073871 meter/sec
ZDOT = -19002
586697 ZDOT = -5791
988425
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 21028
53504738
00016717 00000-0 10270-3 0 9038
2 25544 51
6449 313
4638 0002311 308
2628 51
8314 15
48887973 26948
Satellite: ISS
Catalog Number: 25544
Epoch time: 21028
53504738 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 313
4638 deg
Eccentricity:
0002311
Arg of perigee: 308
2628 deg
Mean anomaly: 51
8314 deg
Mean motion: 15
48887973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 320
Coasting Arc #5 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2021/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3087520
20 A = 6803696
17 meter
Y = -5875022
60 meter E =
0008922
Z = -1475260
67 I = 51
35230
XDOT = 4930
146031 Wp = 21
73428
YDOT = 1152
567904 meter/sec RA = 307
96202 deg
ZDOT = 5747
501182 TA = 322
13501
MA = 322
19773
Ha = 228
723 n
mi
Hp = 223
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10129659
44 X = 3160152
74
Y = -19275008
55 feet Y = -5840089
55 meter
Z = -4840094
07 Z = -1460087
10
XDOT = 16175
019788 XDOT = 4888
974156
YDOT = 3781
390761 feet/sec YDOT = 1207
469872 meter/sec
ZDOT = 18856
631174 ZDOT = 5771
349124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21442563
72 X = 6535693
42
Y = -3877001
71 feet Y = -1181710
12 meter
Z = -4769463
72 Z = -1453732
54
XDOT = 6627
892614 XDOT = 2020
181669
YDOT = 13402
681416 feet/sec YDOT = 4085
137296 meter/sec
ZDOT = 18967
238743 ZDOT = 5781
214369
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 21029
50283874
00016717 00000-0 10270-3 0 9042
2 25544 51
6448 308
6779 0002418 312
0134 48
0810 15
48893527 27090
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
50283874 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 308
6779 deg
Eccentricity:
0002418
Arg of perigee: 312
0134 deg
Mean anomaly: 48
0810 deg
Mean motion: 15
48893527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 316
Coasting Arc #6 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2021/029/19:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262168
26 A = 6793201
71 meter
Y = -1192300
10 meter E =
0012665
Z = -5164936
93 I = 51
30932
XDOT = 3533
282953 Wp = 72
35533
YDOT = -6643
551424 meter/sec RA = 306
45874 deg
ZDOT = -1381
126369 TA = 184
26615
MA = 184
27696
Ha = 228
722 n
mi
Hp = 223
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13983491
66 X = -4223431
40
Y = -3911745
75 feet Y = -1239745
94 meter
Z = -16945331
12 Z = -5185546
11
XDOT = 11592
135674 XDOT = 3614
019060
YDOT = -21796
428555 feet/sec YDOT = -6603
588230 meter/sec
ZDOT = -4531
254492 ZDOT = -1363
767841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10521078
02 X = -3206824
58
Y = 9843695
04 feet Y = 3000358
25 meter
Z = -17040910
36 Z = -5194069
48
XDOT = -11924
263864 XDOT = -3634
515626
YDOT = -20454
605728 feet/sec YDOT = -6234
563826 meter/sec
ZDOT = -4450
463670 ZDOT = -1356
501326
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 21029
82543508
00016717 00000-0 10270-3 0 9051
2 25544 51
6430 307
0789 0002019 309
4993 50
5978 15
48910777 27141
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
82543508 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 307
0789 deg
Eccentricity:
0002019
Arg of perigee: 309
4993 deg
Mean anomaly: 50
5978 deg
Mean motion: 15
48910777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 326
Coasting Arc #7 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2021/030/19:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355664
20 A = 6793286
12 meter
Y = 792668
21 meter E =
0002411
Z = 5150882
67 I = 51
28901
XDOT = -2928
160618 Wp = 116
51871
YDOT = 6938
605530 meter/sec RA = 301
49012 deg
ZDOT = 1406
746758 TA = 319
86252
MA = 319
88032
Ha = 228
646 n
mi
Hp = 223
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14290236
86 X = 4321457
42
Y = 2600617
49 feet Y = 841185
05 meter
Z = 16899221
36 Z = 5171957
00
XDOT = -9606
826174 XDOT = -3012
365537
YDOT = 22764
453839 feet/sec YDOT = 6905
389888 meter/sec
ZDOT = 4615
310887 ZDOT = 1392
318973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9370869
64 X = 2856241
07
Y = -10947486
04 feet Y = -3336793
74 meter
Z = 16996973
71 Z = 5180677
59
XDOT = 14041
129979 XDOT = 4279
736418
YDOT = 19088
318786 feet/sec YDOT = 5818
119566 meter/sec
ZDOT = 4548
132021 ZDOT = 1386
270640
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 21030
85774371
00016717 00000-0 10270-3 0 9061
2 25544 51
6418 301
9726 0002080 314
2926 45
8053 15
48887705 27302
Satellite: ISS
Catalog Number: 25544
Epoch time: 21030
85774371 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 301
9726 deg
Eccentricity:
0002080
Arg of perigee: 314
2926 deg
Mean anomaly: 45
8053 deg
Mean motion: 15
48887705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 307
Coasting Arc #8 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2021/031/19:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4423619
23 A = 6793237
71 meter
Y = -389150
10 meter E =
0012859
Z = -5152339
43 I = 51
27262
XDOT = 2293
093740 Wp = 71
51068
YDOT = -7157
579804 meter/sec RA = 296
52256 deg
ZDOT = -1427
113005 TA = 184
64871
MA = 184
66066
Ha = 228
812 n
mi
Hp = 223
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14513186
45 X = -4393912
51
Y = -1276739
18 feet Y = -438452
13 meter
Z = -16904000
75 Z = -5173754
83
XDOT = 7523
273425 XDOT = 2379
893443
YDOT = -23482
873374 feet/sec YDOT = -7131
451458 meter/sec
ZDOT = -4682
129282 ZDOT = -1415
763536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8133940
93 X = -2479225
20
Y = 11947094
65 feet Y = 3641474
45 meter
Z = -17003347
30 Z = -5182620
26
XDOT = -15948
918708 XDOT = -4861
230422
YDOT = -17451
838180 feet/sec YDOT = -5319
320277 meter/sec
ZDOT = -4629
250344 ZDOT = -1410
995505
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 21031
82553139
00016717 00000-0 10270-3 0 9077
2 25544 51
6420 297
1878 0001981 317
4146 42
6850 15
48915752 27457
Satellite: ISS
Catalog Number: 25544
Epoch time: 21031
82553139 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 297
1878 deg
Eccentricity:
0001981
Arg of perigee: 317
4146 deg
Mean anomaly: 42
6850 deg
Mean motion: 15
48915752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 318
Coasting Arc #9 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2021/032/19:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4441123
16 A = 6793254
45 meter
Y = -20914
66 meter E =
0002509
Z = 5138683
29 I = 51
25858
XDOT = -1646
800328 Wp = 114
00440
YDOT = 7340
309780 meter/sec RA = 291
55106 deg
ZDOT = 1451
561585 TA = 321
92865
MA = 321
94638
Ha = 228
629 n
mi
Hp = 223
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14570614
05 X = 4416066
82
Y = -68617
64 feet Y = 28609
18 meter
Z = 16859197
14 Z = 5160195
12
XDOT = -5402
888215 XDOT = -1735
810194
YDOT = 24082
381167 feet/sec YDOT = 7321
396411 meter/sec
ZDOT = 4762
341157 ZDOT = 1443
345965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6768741
60 X = 2063112
44
Y = -12771706
08 feet Y = -3892816
01 meter
Z = 16959000
31 Z = 5169103
29
XDOT = 17726
523193 XDOT = 5403
044269
YDOT = 15674
298077 feet/sec YDOT = 4777
526054 meter/sec
ZDOT = 4724
019395 ZDOT = 1439
881112
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 21032
85783720
00016717 00000-0 10270-3 0 9083
2 25544 51
6419 292
0810 0002148 317
6673 42
4311 15
48915616 27615
Satellite: ISS
Catalog Number: 25544
Epoch time: 21032
85783720 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 292
0810 deg
Eccentricity:
0002148
Arg of perigee: 317
6673 deg
Mean anomaly: 42
4311 deg
Mean motion: 15
48915616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 302
Coasting Arc #10 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2021/033/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3815037
71 A = 6802279
92 meter
Y = 5139894
95 meter E =
0003592
Z = -2300159
13 I = 51
28601
XDOT = -2933
955355 Wp = 128
25800
YDOT = -4583
632558 meter/sec RA = 289
84413 deg
ZDOT = -5384
189068 TA = 77
42548
MA = 77
38531
Ha = 228
900 n
mi
Hp = 223
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12516527
92 X = -3861057
45
Y = 16863172
41 feet Y = 5096975
09 meter
Z = -7546453
85 Z = -2318802
52
XDOT = -9625
837778 XDOT = -2856
329035
YDOT = -15038
164560 feet/sec YDOT = -4616
008228 meter/sec
ZDOT = -17664
662296 ZDOT = -5398
252110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10427966
85 X = 3178444
30
Y = -18192649
94 feet Y = -5545119
70 meter
Z = -7633086
94 Z = -2326564
90
XDOT = 9854
923135 XDOT = 3003
780571
YDOT = 13076
891647 feet/sec YDOT = 3985
836574 meter/sec
ZDOT = -17729
781638 ZDOT = -5404
037443
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 21033
18043158
00016717 00000-0 10270-3 0 9095
2 25544 51
6435 290
4898 0002247 325
4287 34
6717 15
48902714 27662
Satellite: ISS
Catalog Number: 25544
Epoch time: 21033
18043158 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 290
4898 deg
Eccentricity:
0002247
Arg of perigee: 325
4287 deg
Mean anomaly: 34
6717 deg
Mean motion: 15
48902714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 321
Coasting Arc #11 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2021/034/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3335009
85 A = 6802324
99 meter
Y = -5467860
86 meter E =
0013617
Z = 2269613
20 I = 51
27553
XDOT = 3342
060755 Wp = 62
32070
YDOT = 4288
005774 meter/sec RA = 284
87213 deg
ZDOT = 5400
838906 TA = 323
02864
MA = 323
12241
Ha = 228
946 n
mi
Hp = 223
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10941633
35 X = 3384881
00
Y = -17939176
05 feet Y = -5430287
50 meter
Z = 7446237
54 Z = 2285934
26
XDOT = 10964
766256 XDOT = 3267
628900
YDOT = 14068
260413 feet/sec YDOT = 4324
963005 meter/sec
ZDOT = 17719
287749 ZDOT = 5416
892178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8410316
09 X = -2563464
34
Y = 19226663
12 feet Y = 5860286
92 meter
Z = 7522090
12 Z = 2292733
07
XDOT = -11213
682130 XDOT = -3417
930313
YDOT = -11890
499597 feet/sec YDOT = -3624
224277 meter/sec
ZDOT = 17793
657658 ZDOT = 5423
506854
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 21034
21273458
00016717 00000-0 10270-3 0 9100
2 25544 51
6432 285
3840 0002365 333
2574 26
8454 15
48911590 27827
Satellite: ISS
Catalog Number: 25544
Epoch time: 21034
21273458 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 285
3840 deg
Eccentricity:
0002365
Arg of perigee: 333
2574 deg
Mean anomaly: 26
8454 deg
Mean motion: 15
48911590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 301
Coasting Arc #12 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2021/035/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2848626
96 A = 6802373
29 meter
Y = 5745747
78 meter E =
0003841
Z = -2266996
48 I = 51
26689
XDOT = -3705
088888 Wp = 122
89632
YDOT = -3964
095781 meter/sec RA = 279
89990 deg
ZDOT = -5400
141093 TA = 82
39669
MA = 82
35307
Ha = 229
087 n
mi
Hp = 223
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9345888
99 X = -2901654
36
Y = 18850878
53 feet Y = 5713595
89 meter
Z = -7437652
49 Z = -2280962
54
XDOT = -12155
803438 XDOT = -3634
255426
YDOT = -13005
563587 feet/sec YDOT = -4005
132682 meter/sec
ZDOT = -17716
998336 ZDOT = -5417
966644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6364072
26 X = 1939769
23
Y = -20030724
14 feet Y = -6105364
72 meter
Z = -7502573
68 Z = -2286784
46
XDOT = 12386
547333 XDOT = 3775
419627
YDOT = 10591
647910 feet/sec YDOT = 3228
334283 meter/sec
ZDOT = -17799
606874 ZDOT = -5425
320175
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 21035
18051809
00016717 00000-0 10270-3 0 9112
2 25544 51
6420 280
5977 0002305 337
3651 22
7397 15
48897154 27973
Satellite: ISS
Catalog Number: 25544
Epoch time: 21035
18051809 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 280
5977 deg
Eccentricity:
0002305
Arg of perigee: 337
3651 deg
Mean anomaly: 22
7397 deg
Mean motion: 15
48897154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 319
Coasting Arc #13 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2021/036/03:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2316846
33 A = 6802347
80 meter
Y = -5983226
87 meter E =
0013837
Z = 2236650
18 I = 51
26175
XDOT = 4051
519613 Wp = 61
75453
YDOT = 3601
071890 meter/sec RA = 274
92755 deg
ZDOT = 5417
108407 TA = 323
20681
MA = 323
30170
Ha = 228
992 n
mi
Hp = 223
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7601201
86 X = 2372716
21
Y = -19630009
42 feet Y = -5957005
90 meter
Z = 7338091
14 Z = 2248039
87
XDOT = 13292
387182 XDOT = 3984
637421
YDOT = 11814
540320 feet/sec YDOT = 3646
004796 meter/sec
ZDOT = 17772
665378 ZDOT = 5436
626443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4169049
69 X = -1270726
34
Y = 20614423
69 feet Y = 6283276
34 meter
Z = 7391054
17 Z = 2252793
31
XDOT = -13453
599259 XDOT = -4100
657054
YDOT = -9147
971760 feet/sec YDOT = -2788
301793 meter/sec
ZDOT = 17863
143407 ZDOT = 5444
686110
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 21036
21281881
00016717 00000-0 10270-3 0 9123
2 25544 51
6413 275
4926 0002400 337
4692 22
6352 15
48929986 28132
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
21281881 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 275
4926 deg
Eccentricity:
0002400
Arg of perigee: 337
4692 deg
Mean anomaly: 22
6352 deg
Mean motion: 15
48929986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 309
Coasting Arc #14 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2021/036/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4174550
88 A = 6793569
16 meter
Y = -1692090
77 meter E =
0003260
Z = 5082812
26 I = 51
23339
XDOT = 964
303781 Wp = 97
39240
YDOT = 7414
374047 meter/sec RA = 272
95377 deg
ZDOT = 1674
948119 TA = 336
31816
MA = 336
33316
Ha = 228
984 n
mi
Hp = 223
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13696033
06 X = 4168473
11
Y = -5551478
91 feet Y = -1645442
10 meter
Z = 16675893
25 Z = 5103075
44
XDOT = 3163
726314 XDOT = 873
186514
YDOT = 24325
374169 feet/sec YDOT = 7424
648058 meter/sec
ZDOT = 5495
236611 ZDOT = 1679
411212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14609469
43 X = 4452966
28
Y = 1348439
23 feet Y = 411004
28 meter
Z = 16769936
50 Z = 5111476
64
XDOT = -8362
880983 XDOT = -2549
006124
YDOT = 21954
532647 feet/sec YDOT = 6691
741551 meter/sec
ZDOT = 5515
797781 ZDOT = 1681
215164
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 21036
59993312
00016717 00000-0 10270-3 0 9134
2 25544 51
6435 273
5786 0002689 339
0188 21
0851 15
48892824 28199
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
59993312 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 273
5786 deg
Eccentricity:
0002689
Arg of perigee: 339
0188 deg
Mean anomaly: 21
0851 deg
Mean motion: 15
48892824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 337
Coasting Arc #15 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2021/037/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4014022
52 A = 6793508
37 meter
Y = 2071856
12 meter E =
0013247
Z = -5086044
64 I = 51
23232
XDOT = -1615
275658 Wp = 65
17776
YDOT = -7283
800015 meter/sec RA = 267
97984 deg
ZDOT = -1690
353094 TA = 188
34789
MA = 188
36995
Ha = 229
109 n
mi
Hp = 223
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13169365
21 X = -4012187
70
Y = 6797428
23 feet Y = 2026978
97 meter
Z = -16686498
17 Z = -5105538
24
XDOT = -5299
460820 XDOT = -1525
495327
YDOT = -23896
981677 feet/sec YDOT = -7301
361105 meter/sec
ZDOT = -5545
777868 ZDOT = -1697
981658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14715479
42 X = -4485278
13
Y = 253105
05 feet Y = 77146
42 meter
Z = -16776979
31 Z = -5113623
29
XDOT = 5980
494546 XDOT = 1822
854738
YDOT = -22659
012102 feet/sec YDOT = -6906
466889 meter/sec
ZDOT = -5581
045461 ZDOT = -1701
102657
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 21037
56771258
00016717 00000-0 10270-3 0 9146
2 25544 51
6429 268
7911 0002783 339
6457 20
4581 15
48925811 28341
Satellite: ISS
Catalog Number: 25544
Epoch time: 21037
56771258 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 268
7911 deg
Eccentricity:
0002783
Arg of perigee: 339
6457 deg
Mean anomaly: 20
4581 deg
Mean motion: 15
48925811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 331
Coasting Arc #16 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2021/038/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807304
59 A = 6793626
03 meter
Y = -2425700
14 meter E =
0003661
Z = 5073684
85 I = 51
23460
XDOT = 2256
475826 Wp = 94
62220
YDOT = 7120
291828 meter/sec RA = 263
00703 deg
ZDOT = 1709
546124 TA = 338
74322
MA = 338
75842
Ha = 229
137 n
mi
Hp = 223
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12491156
81 X = 3809502
09
Y = -7958333
80 feet Y = -2383112
15 meter
Z = 16645947
67 Z = 5092183
98
XDOT = 7403
135913 XDOT = 2168
383051
YDOT = 23360
537492 feet/sec YDOT = 7145
032699 meter/sec
ZDOT = 5608
747125 ZDOT = 1720
293431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14597614
08 X = 4449352
77
Y = -1845927
84 feet Y = -562638
80 meter
Z = 16731821
86 Z = 5099859
30
XDOT = -3558
528273 XDOT = -1084
639418
YDOT = 23189
127320 feet/sec YDOT = 7068
046007 meter/sec
ZDOT = 5658
509066 ZDOT = 1724
713563
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 21038
60001135
00016717 00000-0 10270-3 0 9153
2 25544 51
6426 263
6854 0002765 346
6896 13
4180 15
48890149 28503
Satellite: ISS
Catalog Number: 25544
Epoch time: 21038
60001135 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 263
6854 deg
Eccentricity:
0002765
Arg of perigee: 346
6896 deg
Mean anomaly: 13
4180 deg
Mean motion: 15
48890149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 310
Coasting Arc #17 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2021/039/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3580843
37 A = 6793574
78 meter
Y = 2769441
91 meter E =
0013606
Z = -5077887
53 I = 51
23778
XDOT = -2872
106602 Wp = 65
46390
YDOT = -6877
183641 meter/sec RA = 258
03428 deg
ZDOT = -1723
523819 TA = 187
73032
MA = 187
75131
Ha = 229
271 n
mi
Hp = 222
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11748173
78 X = -3586881
24
Y = 9086095
52 feet Y = 2729364
89 meter
Z = -16659736
00 Z = -5095295
85
XDOT = -9422
921921 XDOT = -2786
618730
YDOT = -22562
938456 feet/sec YDOT = -6908
823508 meter/sec
ZDOT = -5654
605705 ZDOT = -1737
267770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14356309
95 X = -4375803
27
Y = 3431290
08 feet Y = 1045857
22 meter
Z = -16740553
63 Z = -5102520
75
XDOT = 1088
174206 XDOT = 331
675498
YDOT = -23375
469048 feet/sec YDOT = -7124
842966 meter/sec
ZDOT = -5718
301309 ZDOT = -1742
938239
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 21039
56778870
00016717 00000-0 10270-3 0 9167
2 25544 51
6403 258
8988 0002721 348
7116 11
3972 15
48919824 28656
Satellite: ISS
Catalog Number: 25544
Epoch time: 21039
56778870 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 258
8988 deg
Eccentricity:
0002721
Arg of perigee: 348
7116 deg
Mean anomaly: 11
3972 deg
Mean motion: 15
48919824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 347
Coasting Arc #18 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2021/040/05:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2374706
02 A = 6796284
74 meter
Y = -4620953
24 meter E =
0008510
Z = 4374356
40 I = 51
25320
XDOT = 4278
263337 Wp = 93
54889
YDOT = 5392
745258 meter/sec RA = 254
69245 deg
ZDOT = 3367
999579 TA = 322
12270
MA = 322
18254
Ha = 229
152 n
mi
Hp = 222
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7791030
24 X = 2404955
01
Y = -15160607
74 feet Y = -4594228
67 meter
Z = 14351562
98 Z = 4385964
64
XDOT = 14036
297037 XDOT = 4201
282766
YDOT = 17692
733787 feet/sec YDOT = 5440
157277 meter/sec
ZDOT = 11049
867385 ZDOT = 3388
594353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3524149
99 X = 1074160
92
Y = 16630514
40 feet Y = 5068980
79 meter
Z = 14405481
50 Z = 4390790
76
XDOT = -20759
372686 XDOT = -6327
456795
YDOT = -5272
722207 feet/sec YDOT = -1607
125729 meter/sec
ZDOT = 11145
390123 ZDOT = 3397
114909
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 21040
27749262
00016717 00000-0 10270-3 0 9171
2 25544 51
6411 255
3900 0002640 351
0563 9
0540 15
48952279 28762
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
27749262 = yrday
fracday
Element set: 917
Inclination: 51
6411 deg
RA of node: 255
3900 deg
Eccentricity:
0002640
Arg of perigee: 351
0563 deg
Mean anomaly: 9
0540 deg
Mean motion: 15
48952279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 297
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