[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
117/05:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
2
121/08:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
0
122/14:29:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 213
9
Coasting Arc #1 (Orbit 2953)
---------------------------------------
Vector Time (GMT): 2018/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4988451
47 A = 6780445
28 meter
Y = 711561
32 meter E =
0011025
Z = -4548034
50 I = 51
32277
XDOT = 1831
906029 Wp = 54
82108
YDOT = -6774
068084 meter/sec RA = 305
61976 deg
ZDOT = -3068
190600 TA = 184
30005
MA = 184
30953
Ha = 221
147 n
mi
Hp = 214
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16366310
59 X = -4973945
35
Y = 2334518
77 feet Y = 655858
17 meter
Z = -14921373
04 Z = -4572231
74
XDOT = 6010
190385 XDOT = 1922
423195
YDOT = -22224
632822 feet/sec YDOT = -6753
076313 meter/sec
ZDOT = -10066
242125 ZDOT = -3059
071924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13326368
27 X = -4061877
05
Y = 9616616
70 feet Y = 2931144
77 meter
Z = -15029373
43 Z = -4580953
02
XDOT = -4231
217249 XDOT = -1289
675017
YDOT = -21535
220260 feet/sec YDOT = -6563
935135 meter/sec
ZDOT = -10024
562182 ZDOT = -3055
486553
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 18110
52156150
00016717 00000-0 10270-3 0 9003
2 25544 51
6380 306
1868 0002877 352
5795 7
5315 15
54130468 29545
Satellite: ISS
Catalog Number: 25544
Epoch time: 18110
52156150 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 306
1868 deg
Eccentricity:
0002877
Arg of perigee: 352
5795 deg
Mean anomaly: 7
5315 deg
Mean motion: 15
54130468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2954
Checksum: 302
Coasting Arc #2 (Orbit 2969)
---------------------------------------
Vector Time (GMT): 2018/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4296118
12 A = 6777965
88 meter
Y = 869184
34 meter E =
0003269
Z = 5167080
58 I = 51
29550
XDOT = -2939
320503 Wp = 80
67118
YDOT = 6970
751480 meter/sec RA = 300
60085 deg
ZDOT = 1271
110733 TA = 357
06881
MA = 357
07073
Ha = 221
119 n
mi
Hp = 214
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14094875
73 X = 4260980
22
Y = 2851654
66 feet Y = 917029
96 meter
Z = 16952364
10 Z = 5187864
47
XDOT = -9643
439972 XDOT = -3023
225326
YDOT = 22869
919553 feet/sec YDOT = 6937
412819 meter/sec
ZDOT = 4170
310803 ZDOT = 1256
628714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13639357
83 X = 4157276
27
Y = -4197510
16 feet Y = -1279401
10 meter
Z = 17044909
25 Z = 5195288
34
XDOT = 2167
337062 XDOT = 660
604336
YDOT = 23712
775402 feet/sec YDOT = 7227
653943 meter/sec
ZDOT = 4104
696646 ZDOT = 1251
111538
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 18111
55039424
00016717 00000-0 10270-3 0 9012
2 25544 51
6377 301
0579 0002858 356
4310 3
6821 15
54093393 29701
Satellite: ISS
Catalog Number: 25544
Epoch time: 18111
55039424 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 301
0579 deg
Eccentricity:
0002858
Arg of perigee: 356
4310 deg
Mean anomaly: 3
6821 deg
Mean motion: 15
54093393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2970
Checksum: 297
Coasting Arc #3 (Orbit 2984)
---------------------------------------
Vector Time (GMT): 2018/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3483205
45 A = 6777469
53 meter
Y = -2496772
10 meter E =
0014651
Z = -5263007
04 I = 51
27809
XDOT = 3763
465626 Wp = 84
33013
YDOT = -6636
578241 meter/sec RA = 295
57559 deg
ZDOT = 660
640515 TA = 192
00077
MA = 192
03571
Ha = 221
217 n
mi
Hp = 214
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11427839
39 X = -3429461
96
Y = -8191509
50 feet Y = -2535423
17 meter
Z = -17267083
45 Z = -5279796
79
XDOT = 12347
328169 XDOT = 3834
188889
YDOT = -21773
550661 feet/sec YDOT = -6594
097144 meter/sec
ZDOT = 2167
455757 ZDOT = 679
093945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13884450
78 X = -4231980
60
Y = -1529723
41 feet Y = -466259
69 meter
Z = -17341582
53 Z = -5285714
36
XDOT = -153
417040 XDOT = -46
761514
YDOT = -24011
006998 feet/sec YDOT = -7318
554933 meter/sec
ZDOT = 2250
716516 ZDOT = 686
018394
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 18112
51491989
00016717 00000-0 10270-3 0 9028
2 25544 51
6374 296
2488 0002744
3943 359
7212 15
54143424 29859
Satellite: ISS
Catalog Number: 25544
Epoch time: 18112
51491989 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 296
2488 deg
Eccentricity:
0002744
Arg of perigee:
3943 deg
Mean anomaly: 359
7212 deg
Mean motion: 15
54143424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2985
Checksum: 321
Coasting Arc #4 (Orbit 3000)
---------------------------------------
Vector Time (GMT): 2018/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2584832
00 A = 6779553
96 meter
Y = 4041562
67 meter E =
0009119
Z = 4787184
09 I = 51
27172
XDOT = -4342
904206 Wp = 45
77714
YDOT = 5791
669281 meter/sec RA = 290
55202 deg
ZDOT = -2535
389548 TA = 69
34109
MA = 69
24334
Ha = 221
251 n
mi
Hp = 214
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8480419
96 X = 2516192
38
Y = 13259720
03 feet Y = 4070084
31 meter
Z = 15705984
53 Z = 4799573
56
XDOT = -14248
373379 XDOT = -4395
029850
YDOT = 19001
539637 feet/sec YDOT = 5742
812453 meter/sec
ZDOT = -8318
207180 ZDOT = -2556
612586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13961486
66 X = 4255461
13
Y = 7148047
84 feet Y = 2178724
98 meter
Z = 15760645
63 Z = 4803844
79
XDOT = -2019
290070 XDOT = -615
479613
YDOT = 22562
049723 feet/sec YDOT = 6876
912756 meter/sec
ZDOT = -8413
681142 ZDOT = -2564
490012
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 18113
54374431
00016717 00000-0 10270-3 0 9035
2 25544 51
6376 291
1196 0002775 3
3044 356
8127 15
54121355 30012
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
54374431 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 291
1196 deg
Eccentricity:
0002775
Arg of perigee: 3
3044 deg
Mean anomaly: 356
8127 deg
Mean motion: 15
54121355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3001
Checksum: 281
Coasting Arc #5 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2018/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1706102
45 A = 6783010
25 meter
Y = -5334389
65 meter E =
0006630
Z = -3831353
04 I = 51
27244
XDOT = 4673
687101 Wp = 80
44753
YDOT = -4454
085661 meter/sec RA = 285
53564 deg
ZDOT = 4127
432112 TA = 233
18724
MA = 233
24808
Ha = 221
343 n
mi
Hp = 214
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5597448
98 X = -1627714
32
Y = -17501278
38 feet Y = -5353030
29 meter
Z = -12570055
91 Z = -3839450
15
XDOT = 15333
619097 XDOT = 4703
097618
YDOT = -14613
141932 feet/sec YDOT = -4401
656697 meter/sec
ZDOT = 13541
443938 ZDOT = 4150
206881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13866506
21 X = -4226511
09
Y = -12018997
33 feet Y = -3663390
38 meter
Z = -12605403
38 Z = -3842126
95
XDOT = 4452
407043 XDOT = 1357
093667
YDOT = -19421
390119 feet/sec YDOT = -5919
639708 meter/sec
ZDOT = 13643
633110 ZDOT = 4158
579372
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 18114
50826423
00016717 00000-0 10270-3 0 9046
2 25544 51
6370 286
3110 0002702 10
8796 349
2415 15
54149836 30161
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
50826423 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 286
3110 deg
Eccentricity:
0002702
Arg of perigee: 10
8796 deg
Mean anomaly: 349
2415 deg
Mean motion: 15
54149836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3016
Checksum: 291
Coasting Arc #6 (Orbit 3031)
---------------------------------------
Vector Time (GMT): 2018/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 824021
36 A = 6786696
48 meter
Y = 6273738
50 meter E =
0013733
Z = 2440200
38 I = 51
27649
XDOT = -4830
453121 Wp = 93
85553
YDOT = 2707
866848 meter/sec RA = 280
52944 deg
ZDOT = -5305
742544 TA = 58
68010
MA = 58
54573
Ha = 221
333 n
mi
Hp = 214
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2703482
15 X = 741952
21
Y = 20583131
57 feet Y = 6282494
52 meter
Z = 8005906
76 Z = 2444003
57
XDOT = -15847
943312 XDOT = -4834
601615
YDOT = 8884
077585 feet/sec YDOT = 2653
825943 meter/sec
ZDOT = -17407
291811 ZDOT = -5329
217508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13317442
70 X = 4059156
54
Y = 15917351
41 feet Y = 4851608
71 meter
Z = 8021989
05 Z = 2445102
26
XDOT = -7312
898802 XDOT = -2228
971555
YDOT = 14985
491021 feet/sec YDOT = 4567
577663 meter/sec
ZDOT = -17512
348147 ZDOT = -5337
763715
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 18115
53708136
00016717 00000-0 10270-3 0 9051
2 25544 51
6365 281
1819 0002753 9
6048 350
5157 15
54163083 30322
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
53708136 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 281
1819 deg
Eccentricity:
0002753
Arg of perigee: 9
6048 deg
Mean anomaly: 350
5157 deg
Mean motion: 15
54163083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3032
Checksum: 297
Coasting Arc #7 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2018/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -12669
23 A = 6788935
66 meter
Y = -6732291
25 meter E =
0012793
Z = -825063
50 I = 51
28073
XDOT = 4831
862144 Wp = 34
92549
YDOT = -726
727390 meter/sec RA = 275
53065 deg
ZDOT = 5911
572993 TA = 316
10503
MA = 316
20660
Ha = 221
428 n
mi
Hp = 214
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -41565
72 X = 66621
78
Y = -22087569
73 feet Y = -6731989
63 meter
Z = -2706901
24 Z = -824932
07
XDOT = 15852
566089 XDOT = 4810
913972
YDOT = -2384
276213 feet/sec YDOT = -672
810972 meter/sec
ZDOT = 19394
924518 ZDOT = 5934
993840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12232036
85 X = -3728324
83
Y = -18391517
57 feet Y = -5605734
55 meter
Z = -2705389
91 Z = -824602
84
XDOT = 10443
473835 XDOT = 3183
170825
YDOT = -9787
251047 feet/sec YDOT = -2983
154119 meter/sec
ZDOT = 19499
460685 ZDOT = 5943
435617
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 18116
50159568
00016717 00000-0 10270-3 0 9069
2 25544 51
6382 276
3731 0002726 17
8436 342
2812 15
54164160 30471
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
50159568 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 276
3731 deg
Eccentricity:
0002726
Arg of perigee: 17
8436 deg
Mean anomaly: 342
2812 deg
Mean motion: 15
54164160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 304
Coasting Arc #8 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2018/117/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2664185
95 A = 6785168
54 meter
Y = -5413803
03 meter E =
0014514
Z = 3086220
12 I = 51
26899
XDOT = 3738
163742 Wp = 72
80695
YDOT = 4616
908464 meter/sec RA = 271
98284 deg
ZDOT = 4857
203842 TA = 322
90750
MA = 323
00772
Ha = 221
512 n
mi
Hp = 214
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8740767
57 X = 2709535
18
Y = -17761820
96 feet Y = -5383756
53 meter
Z = 10125394
11 Z = 3099272
41
XDOT = 12264
316739 XDOT = 3662
664401
YDOT = 15147
337481 feet/sec YDOT = 4658
289323 meter/sec
ZDOT = 15935
708142 ZDOT = 4875
179090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19711238
68 X = 6007985
55
Y = 1467433
13 feet Y = 447273
62 meter
Z = 10184331
94 Z = 3104184
37
XDOT = -9451
413543 XDOT = -2880
790848
YDOT = 15472
718635 feet/sec YDOT = 4716
084640 meter/sec
ZDOT = 16015
234009 ZDOT = 4881
443326
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 18117
27320410
00016717 00000-0 10270-3 0 9071
2 25544 51
6409 272
5309 0003248 17
0117 343
1144 15
54153734 30594
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
27320410 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 272
5309 deg
Eccentricity:
0003248
Arg of perigee: 17
0117 deg
Mean anomaly: 343
1144 deg
Mean motion: 15
54153734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 279
Coasting Arc #9 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2018/118/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3249297
68 A = 6781226
55 meter
Y = 4112482
84 meter E =
0010900
Z = -4314492
94 I = 51
25594
XDOT = -3104
207467 Wp = 56
13305
YDOT = -6084
941691 meter/sec RA = 266
97182 deg
ZDOT = -3462
577992 TA = 178
44031
MA = 178
43691
Ha = 221
546 n
mi
Hp = 214
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10660425
47 X = -3274085
26
Y = 13492397
76 feet Y = 4076008
14 meter
Z = -14155160
55 Z = -4330337
54
XDOT = -10184
407700 XDOT = -3019
113657
YDOT = -19963
719459 feet/sec YDOT = -6119
179466 meter/sec
ZDOT = -11360
164017 ZDOT = -3477
450377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16528440
27 X = -5037868
59
Y = -4525396
87 feet Y = -1379340
97 meter
Z = -14226365
82 Z = -4336196
30
XDOT = 14170
090188 XDOT = 4319
043489
YDOT = -15839
586039 feet/sec YDOT = -4827
905825 meter/sec
ZDOT = -11425
665512 ZDOT = -3482
542848
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 18118
23771081
00016717 00000-0 10270-3 0 9083
2 25544 51
6409 267
7232 0003211 17
6066 342
5198 15
54179239 30741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
23771081 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 267
7232 deg
Eccentricity:
0003211
Arg of perigee: 17
6066 deg
Mean anomaly: 342
5198 deg
Mean motion: 15
54179239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 308
Coasting Arc #10 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2018/119/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3749618
59 A = 6778194
27 meter
Y = -2494433
84 meter E =
0005489
Z = 5061021
83 I = 51
24936
XDOT = 2393
589921 Wp = 90
65576
YDOT = 7084
594356 meter/sec RA = 261
94977 deg
ZDOT = 1716
749061 TA = 342
66201
MA = 342
68075
Ha = 221
460 n
mi
Hp = 214
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12301898
26 X = 3752649
14
Y = -8183838
05 feet Y = -2452485
89 meter
Z = 16604402
33 Z = 5079243
95
XDOT = 7852
985305 XDOT = 2305
850948
YDOT = 23243
419804 feet/sec YDOT = 7110
870612 meter/sec
ZDOT = 5632
378809 ZDOT = 1728
163124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12398751
15 X = 3779139
35
Y = 7865544
45 feet Y = 2397417
95 meter
Z = 16685990
03 Z = 5085889
76
XDOT = -17556
321254 XDOT = -5351
166718
YDOT = 15608
528314 feet/sec YDOT = 4757
479430 meter/sec
ZDOT = 5682
336604 ZDOT = 1731
976197
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 18119
26651539
00016717 00000-0 10270-3 0 9093
2 25544 51
6416 262
5939 0003172 22
1046 338
0243 15
54177487 30903
Satellite: ISS
Catalog Number: 25544
Epoch time: 18119
26651539 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 262
5939 deg
Eccentricity:
0003172
Arg of perigee: 22
1046 deg
Mean anomaly: 338
0243 deg
Mean motion: 15
54177487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 310
Coasting Arc #11 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2018/120/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4191648
61 A = 6777160
34 meter
Y = 719799
88 meter E =
0016368
Z = -5290510
49 I = 51
25183
XDOT = -1559
793078 Wp = 80
93306
YDOT = -7493
035188 meter/sec RA = 256
92227 deg
ZDOT = 219
469184 TA = 191
15500
MA = 191
19133
Ha = 221
609 n
mi
Hp = 213
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13752128
00 X = -4173687
07
Y = 2361548
16 feet Y = 673026
32 meter
Z = -17357317
88 Z = -5310828
84
XDOT = -5117
431357 XDOT = -1476
954072
YDOT = -24583
448779 feet/sec YDOT = -7510
014683 meter/sec
ZDOT = 720
043253 ZDOT = 212
093435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7848295
88 X = -2392160
59
Y = -11399353
58 feet Y = -3474522
97 meter
Z = -17448020
17 Z = -5318156
55
XDOT = 19355
331481 XDOT = 5899
505036
YDOT = -14363
581381 feet/sec YDOT = -4378
019605 meter/sec
ZDOT = 688
136592 ZDOT = 209
744033
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 18120
23101464
00016717 00000-0 10270-3 0 9101
2 25544 51
6417 257
7853 0003300 23
4550 336
6752 15
54201317 31058
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
23101464 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 257
7853 deg
Eccentricity:
0003300
Arg of perigee: 23
4550 deg
Mean anomaly: 336
6752 deg
Mean motion: 15
54201317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 263
Coasting Arc #12 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2018/121/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4517028
16 A = 6778576
67 meter
Y = 1080904
81 meter E =
0009212
Z = 4933624
50 I = 51
26489
XDOT = 592
412331 Wp = 46
56231
YDOT = 7342
314550 meter/sec RA = 251
89647 deg
ZDOT = -2142
258050 TA = 64
46248
MA = 64
36726
Ha = 221
471 n
mi
Hp = 213
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14819646
21 X = 4480640
06
Y = 3546275
61 feet Y = 1131213
84 meter
Z = 16186432
10 Z = 4955478
72
XDOT = 1943
610011 XDOT = 520
670702
YDOT = 24088
958496 feet/sec YDOT = 7348
538193 meter/sec
ZDOT = -7028
405677 ZDOT = -2139
554467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3187012
59 X = 971401
44
Y = 14794623
64 feet Y = 4509401
29 meter
Z = 16283753
58 Z = 4963288
09
XDOT = -19760
779396 XDOT = -6023
085560
YDOT = 12011
850315 feet/sec YDOT = 3661
211976 meter/sec
ZDOT = -7017
304939 ZDOT = -2138
874546
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 18121
25980983
00016717 00000-0 10270-3 0 9116
2 25544 51
6412 252
6566 0003287 25
6722 334
4594 15
54228116 31211
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
25980983 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 252
6566 deg
Eccentricity:
0003287
Arg of perigee: 25
6722 deg
Mean anomaly: 334
4594 deg
Mean motion: 15
54228116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 301
Coasting Arc #13 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2018/121/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4481132
36 A = 6782045
03 meter
Y = 3058321
35 meter E =
0012761
Z = 4063183
03 I = 51
27398
XDOT = -1004
781523 Wp = 66
46330
YDOT = 6572
897856 meter/sec RA = 251
22357 deg
ZDOT = -3824
641470 TA = 63
32759
MA = 63
19697
Ha = 221
533 n
mi
Hp = 213
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14701877
82 X = 4426863
14
Y = 10033862
69 feet Y = 3108128
98 meter
Z = 13330652
99 Z = 4084819
46
XDOT = -3296
527307 XDOT = -1059
628327
YDOT = 21564
625512 feet/sec YDOT = 6561
355064 meter/sec
ZDOT = -12548
036318 ZDOT = -3829
655603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11123950
97 X = 3390580
26
Y = 13802539
64 feet Y = 4207014
08 meter
Z = 13426747
01 Z = 4092472
49
XDOT = -8252
999649 XDOT = -2515
514293
YDOT = 18926
576851 feet/sec YDOT = 5768
820624 meter/sec
ZDOT = -12571
252874 ZDOT = -3831
717876
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 18121
38840955
00016717 00000-0 10270-3 0 9125
2 25544 51
6378 252
0118 0003076 27
0474 333
0838 15
54189568 31230
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
38840955 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 252
0118 deg
Eccentricity:
0003076
Arg of perigee: 27
0474 deg
Mean anomaly: 333
0838 deg
Mean motion: 15
54189568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 309
Coasting Arc #14 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2018/122/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4364503
83 A = 6785809
64 meter
Y = -4392629
55 meter E =
0007584
Z = -2773630
35 I = 51
29790
XDOT = 2120
315377 Wp = 50
14050
YDOT = -5316
826947 meter/sec RA = 246
21530 deg
ZDOT = 5097
923164 TA = 278
27139
MA = 278
35738
Ha = 221
644 n
mi
Hp = 213
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14319238
27 X = -4301586
78
Y = -14411514
28 feet Y = -4441084
57 meter
Z = -9099837
10 Z = -2794679
29
XDOT = 6956
415280 XDOT = 2154
848525
YDOT = -17443
657961 feet/sec YDOT = -5292
923182 meter/sec
ZDOT = 16725
469697 ZDOT = 5108
306832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9835885
64 X = -2997977
94
Y = -17727964
05 feet Y = -5403483
44 meter
Z = -9193150
07 Z = -2802072
14
XDOT = 10009
845532 XDOT = 3051
000918
YDOT = -14227
657868 feet/sec YDOT = -4336
590118 meter/sec
ZDOT = 16772
466669 ZDOT = 5112
247841
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 18122
35290320
00016717 00000-0 10270-3 0 9139
2 25544 51
6375 247
2029 0003057 34
1043 326
0305 15
54192571 31389
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
35290320 = yrday
fracday
Element set: 913
Inclination: 51
6375 deg
RA of node: 247
2029 deg
Eccentricity:
0003057
Arg of perigee: 34
1043 deg
Mean anomaly: 326
0305 deg
Mean motion: 15
54192571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 272
Coasting Arc #15 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4605822
03 A = 6784783
25 meter
Y = -3838247
04 meter E =
0006884
Z = -3177737
49 I = 51
30164
XDOT = 1527
098767 Wp = 62
67237
YDOT = -5786
716950 meter/sec RA = 244
93158 deg
ZDOT = 4787
246151 TA = 260
45404
MA = 260
53184
Ha = 221
591 n
mi
Hp = 213
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15110964
68 X = -4547123
34
Y = -12592674
00 feet Y = -3889424
20 meter
Z = -10425647
93 Z = -3199968
93
XDOT = 5010
166559 XDOT = 1568
439587
YDOT = -18985
291832 feet/sec YDOT = -5769
408889 meter/sec
ZDOT = 15706
188160 ZDOT = 4794
764619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15689033
14 X = -4782017
30
Y = 11777264
92 feet Y = 3589710
35 meter
Z = -10524309
81 Z = -3207809
63
XDOT = -16508
362354 XDOT = -5031
748846
YDOT = -7957
938783 feet/sec YDOT = -2425
579741 meter/sec
ZDOT = 15740
465727 ZDOT = 4797
693953
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 18122
61009999
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 245
9224 0002881 33
8095 326
3241 15
54190609 31427
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
61009999 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 245
9224 deg
Eccentricity:
0002881
Arg of perigee: 33
8095 deg
Mean anomaly: 326
3241 deg
Mean motion: 15
54190609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 300
Coasting Arc #16 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4355340
90 A = 6787962
50 meter
Y = 4941830
23 meter E =
0014917
Z = 1615900
12 I = 51
32698
XDOT = -2770
883469 Wp = 105
05291
YDOT = 4318
919283 meter/sec RA = 239
93267 deg
ZDOT = -5699
653378 TA = 57
17923
MA = 57
03567
Ha = 221
717 n
mi
Hp = 213
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14289176
19 X = 4291907
00
Y = 16213353
77 feet Y = 4990179
90 meter
Z = 5301509
60 Z = 1636903
34
XDOT = -9090
825031 XDOT = -2791
286533
YDOT = 14169
682686 feet/sec YDOT = 4287
819534 meter/sec
ZDOT = -18699
650189 ZDOT = -5713
162936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18856603
96 X = 5747492
89
Y = -10511257
50 feet Y = -3203831
29 meter
Z = 5394567
05 Z = 1644264
04
XDOT = 11190
342060 XDOT = 3410
816260
YDOT = 10379
917368 feet/sec YDOT = 3163
798814 meter/sec
ZDOT = -18760
460362 ZDOT = -5718
188318
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 18123
63888538
00016717 00000-0 10270-3 0 9157
2 25544 51
6410 240
7937 0003067 39
3728 320
7647 15
54205295 31583
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
63888538 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 240
7937 deg
Eccentricity:
0003067
Arg of perigee: 39
3728 deg
Mean anomaly: 320
7647 deg
Mean motion: 15
54205295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 324
Coasting Arc #17 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3841938
54 A = 6789189
31 meter
Y = -5587873
11 meter E =
0015406
Z = 81187
13 I = 51
34752
XDOT = 3993
581791 Wp = 45
18637
YDOT = -2648
752060 meter/sec RA = 234
94092 deg
ZDOT = 5989
676980 TA = 315
69198
MA = 315
81520
Ha = 221
805 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12604785
22 X = -3779562
24
Y = -18332917
02 feet Y = -5630487
55 meter
Z = 266361
98 Z = 62675
32
XDOT = 13102
302463 XDOT = 3993
808994
YDOT = -8690
131431 feet/sec YDOT = -2604
092110 meter/sec
ZDOT = 19651
171194 ZDOT = 6009
077077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20431864
79 X = -6227632
39
Y = 8806376
83 feet Y = 2684183
66 meter
Z = 184482
86 Z = 56230
37
XDOT = -5362
047369 XDOT = -1634
352038
YDOT = -12922
440852 feet/sec YDOT = -3938
759972 meter/sec
ZDOT = 19738
049530 ZDOT = 6016
157497
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 18124
66766704
00016717 00000-0 10270-3 0 9162
2 25544 51
6404 235
6650 0003199 40
6934 319
4458 15
54177407 31747
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
66766704 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 235
6650 deg
Eccentricity:
0003199
Arg of perigee: 40
6934 deg
Mean anomaly: 319
4458 deg
Mean motion: 15
54177407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 323
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