[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 29th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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
213/16:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
8
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 212
8
220/05:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
7
223/08:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
9
Coasting Arc #1 (Orbit 1156)
---------------------------------------
Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5607679
79 A = 6786537
52 meter
Y = -3657218
31 meter E =
0015300
Z = 1069016
01 I = 51
49057
XDOT = 3436
107671 Wp = 60
38795
YDOT = -3533
996104 meter/sec RA = 205
81212 deg
ZDOT = 5878
503749 TA = 311
23707
MA = 311
36882
Ha = 220
446 n
mi
Hp = 212
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18397899
57 X = -5571559
84
Y = -11998747
74 feet Y = -3719725
25 meter
Z = 3507270
37 Z = 1041863
04
XDOT = 11273
319130 XDOT = 3446
815377
YDOT = -11594
475408 feet/sec YDOT = -3495
511806 meter/sec
ZDOT = 19286
429623 ZDOT = 5895
221089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1394702
55 X = 425105
34
Y = 21939007
02 feet Y = 6687009
34 meter
Z = 3389450
84 Z = 1033104
62
XDOT = -14358
118931 XDOT = -4376
354650
YDOT = -2107
556622 feet/sec YDOT = -642
383258 meter/sec
ZDOT = 19359
926763 ZDOT = 5900
905677
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 16211
56227129
00016717 00000-0 10270-3 0 9002
2 25544 51
6387 206
6068 0001954 87
3196 272
8181 15
54934887 11570
Satellite: ISS
Catalog Number: 25544
Epoch time: 16211
56227129 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 206
6068 deg
Eccentricity:
0001954
Arg of perigee: 87
3196 deg
Mean anomaly: 272
8181 deg
Mean motion: 15
54934887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1157
Checksum: 326
Coasting Arc #2 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4486421
30 A = 6783621
40 meter
Y = 4178645
00 meter E =
0006442
Z = -2905988
27 I = 51
50879
XDOT = -5336
138426 Wp = 107
18574
YDOT = 2243
751828 meter/sec RA = 200
82367 deg
ZDOT = -5022
914314 TA = 105
99042
MA = 105
91945
Ha = 220
579 n
mi
Hp = 212
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14719229
99 X = 4453477
04
Y = 13709465
21 feet Y = 4228631
17 meter
Z = -9534082
23 Z = -2884274
36
XDOT = -17507
015834 XDOT = -5336
433222
YDOT = 7361
390513 feet/sec YDOT = 2184
078296 meter/sec
ZDOT = -16479
377671 ZDOT = -5048
836127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1807062
44 X = 550792
63
Y = -20077943
12 feet Y = -6119757
06 meter
Z = -9440053
89 Z = -2877328
43
XDOT = 15000
242721 XDOT = 4572
073981
YDOT = 9134
243427 feet/sec YDOT = 2784
117397 meter/sec
ZDOT = -16592
820660 ZDOT = -5057
491737
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 16212
52633186
00016717 00000-0 10270-3 0 9014
2 25544 51
6378 201
7947 0002043 84
3398 275
7988 15
54883111 11720
Satellite: ISS
Catalog Number: 25544
Epoch time: 16212
52633186 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 201
7947 deg
Eccentricity:
0002043
Arg of perigee: 84
3398 deg
Mean anomaly: 275
7988 deg
Mean motion: 15
54883111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 318
Coasting Arc #3 (Orbit 1187)
---------------------------------------
Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2864896
56 A = 6779221
09 meter
Y = -4371728
43 meter E =
0011572
Z = 4309329
12 I = 51
52516
XDOT = 6760
726830 Wp = 104
72447
YDOT = -972
475898 meter/sec RA = 195
82605 deg
ZDOT = 3497
315074 TA = 309
62222
MA = 309
72431
Ha = 220
493 n
mi
Hp = 212
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9399266
93 X = -2836730
35
Y = -14342941
05 feet Y = -4403608
43 meter
Z = 14138218
88 Z = 4295480
52
XDOT = 22180
862303 XDOT = 6754
110690
YDOT = -3190
537723 feet/sec YDOT = -896
910174 meter/sec
ZDOT = 11474
130821 ZDOT = 3530
140265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5262287
89 X = -1603945
35
Y = 16372509
42 feet Y = 4990340
87 meter
Z = 14078518
09 Z = 4291132
31
XDOT = -15113
817806 XDOT = -4606
691667
YDOT = -14877
914678 feet/sec YDOT = -4534
788394 meter/sec
ZDOT = 11617
498283 ZDOT = 3541
013477
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 16213
55465791
00016717 00000-0 10270-3 0 9024
2 25544 51
6382 196
6630 0001832 87
8120 272
3243 15
54913888 11881
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
55465791 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 196
6630 deg
Eccentricity:
0001832
Arg of perigee: 87
8120 deg
Mean anomaly: 272
3243 deg
Mean motion: 15
54913888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1188
Checksum: 319
Coasting Arc #4 (Orbit 1190)
---------------------------------------
Vector Time (GMT): 2016/213/16:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2795145
73 A = 6779013
46 meter
Y = -4343962
44 meter E =
0011303
Z = 4382344
09 I = 51
53290
XDOT = 6820
711651 Wp = 105
41773
YDOT = -968
536905 meter/sec RA = 194
86112 deg
ZDOT = 3380
112432 TA = 310
29844
MA = 310
39717
Ha = 220
556 n
mi
Hp = 212
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9170425
63 X = -2767649
85
Y = -14251845
28 feet Y = -4375066
19 meter
Z = 14377769
31 Z = 4368832
71
XDOT = 22377
662898 XDOT = 6814
616329
YDOT = -3177
614518 feet/sec YDOT = -892
297464 meter/sec
ZDOT = 11089
607716 ZDOT = 3413
230251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13283695
33 X = 4048870
34
Y = 10603135
23 feet Y = 3231835
62 meter
Z = 14319532
55 Z = 4364593
52
XDOT = -19393
142030 XDOT = -5911
029691
YDOT = 9078
569928 feet/sec YDOT = 2767
148114 meter/sec
ZDOT = 11234
255283 ZDOT = 3424
201010
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 16213
74747083
00016717 00000-0 10270-3 0 9033
2 25544 51
6408 195
7011 0001914 84
8224 275
3148 15
54892111 11912
Satellite: ISS
Catalog Number: 25544
Epoch time: 16213
74747083 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 195
7011 deg
Eccentricity:
0001914
Arg of perigee: 84
8224 deg
Mean anomaly: 275
3148 deg
Mean motion: 15
54892111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1191
Checksum: 299
Coasting Arc #5 (Orbit 1205)
---------------------------------------
Vector Time (GMT): 2016/214/16:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 781065
47 A = 6775705
55 meter
Y = 4311446
20 meter E =
0015855
Z = -5182372
35 I = 51
55437
XDOT = -7537
296976 Wp = 80
61176
YDOT = -235
188542 meter/sec RA = 189
85203 deg
ZDOT = -1332
610302 TA = 176
55594
MA = 176
54501
Ha = 220
484 n
mi
Hp = 212
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2562550
75 X = 757968
92
Y = 14145164
69 feet Y = 4320051
74 meter
Z = -17002533
97 Z = -5178634
08
XDOT = -24728
664619 XDOT = -7527
633750
YDOT = -771
615951 feet/sec YDOT = -319
421527 meter/sec
ZDOT = -4372
081044 ZDOT = -1369
200347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7210719
91 X = -2197827
43
Y = -12457466
02 feet Y = -3797035
64 meter
Z = -16986923
52 Z = -5177614
29
XDOT = 22650
246318 XDOT = 6903
795078
YDOT = -6935
457583 feet/sec YDOT = -2113
927471 meter/sec
ZDOT = -4531
704557 ZDOT = -1381
263549
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 16214
71152506
00016717 00000-0 10270-3 0 9042
2 25544 51
6417 190
8898 0001972 85
0276 275
1102 15
54913270 12060
Satellite: ISS
Catalog Number: 25544
Epoch time: 16214
71152506 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 190
8898 deg
Eccentricity:
0001972
Arg of perigee: 85
0276 deg
Mean anomaly: 275
1102 deg
Mean motion: 15
54913270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1206
Checksum: 296
Coasting Arc #6 (Orbit 1221)
---------------------------------------
Vector Time (GMT): 2016/215/16:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1350450
59 A = 6775223
84 meter
Y = -4062138
86 meter E =
0004910
Z = 5247776
14 I = 51
58486
XDOT = 7502
645610 Wp = 70
56735
YDOT = 1342
805697 meter/sec RA = 184
83991 deg
ZDOT = -889
011934 TA = 27
94888
MA = 27
92252
Ha = 220
325 n
mi
Hp = 212
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4430612
16 X = 1370283
25
Y = -13327227
24 feet Y = -4046926
52 meter
Z = 17217113
34 Z = 5254384
16
XDOT = 24614
979035 XDOT = 7491
390744
YDOT = 4405
530502 feet/sec YDOT = 1426
642394 meter/sec
ZDOT = -2916
705819 ZDOT = -852
594104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 584225
49 X = 178071
93
Y = 13995981
21 feet Y = 4265975
07 meter
Z = 17246608
14 Z = 5256766
16
XDOT = -23607
238168 XDOT = -7195
486194
YDOT = 4393
160376 feet/sec YDOT = 1339
035283 meter/sec
ZDOT = -2757
990132 ZDOT = -840
635392
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 16215
73984838
00016717 00000-0 10270-3 0 9057
2 25544 51
6415 185
7583 0001753 89
1275 271
0079 15
54937360 12225
Satellite: ISS
Catalog Number: 25544
Epoch time: 16215
73984838 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 185
7583 deg
Eccentricity:
0001753
Arg of perigee: 89
1275 deg
Mean anomaly: 271
0079 deg
Mean motion: 15
54937360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1222
Checksum: 326
Coasting Arc #7 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2016/216/16:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3362217
85 A = 6777968
28 meter
Y = 3665150
63 meter E =
0012045
Z = -4616410
79 I = 51
62726
XDOT = -6652
369511 Wp = 107
61437
YDOT = -2345
064758 meter/sec RA = 179
83321 deg
ZDOT = 2986
071991 TA = 192
18985
MA = 192
21902
Ha = 220
406 n
mi
Hp = 212
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11030898
45 X = -3380528
60
Y = 12024772
42 feet Y = 3627449
76 meter
Z = -15145704
70 Z = -4632787
64
XDOT = -21825
359287 XDOT = -6640
156698
YDOT = -7693
782015 feet/sec YDOT = -2419
387760 meter/sec
ZDOT = 9796
824119 ZDOT = 2953
786834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5809199
87 X = 1770644
12
Y = -15176983
18 feet Y = -4625944
47 meter
Z = -15217773
22 Z = -4638377
28
XDOT = 22080
303087 XDOT = 6730
076381
YDOT = -1221
310432 feet/sec YDOT = -372
255420 meter/sec
ZDOT = 9656
285482 ZDOT = 2943
235815
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 16216
70390204
00016717 00000-0 10270-3 0 9064
2 25544 51
6428 180
9470 0001733 91
0098 269
1253 15
54902760 12378
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
70390204 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 180
9470 deg
Eccentricity:
0001733
Arg of perigee: 91
0098 deg
Mean anomaly: 269
1253 deg
Mean motion: 15
54902760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 296
Coasting Arc #8 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3202206
54 A = 6777536
74 meter
Y = -3631200
70 meter E =
0009677
Z = 4737270
04 I = 51
63901
XDOT = 6760
738435 Wp = 116
12450
YDOT = -2406
957548 meter/sec RA = 177
83715 deg
ZDOT = 2716
540315 TA = 306
99183
MA = 307
08036
Ha = 220
476 n
mi
Hp = 212
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10505926
97 X = -3184374
63
Y = -11913388
12 feet Y = -3666910
24 meter
Z = 15542224
55 Z = 4721758
17
XDOT = 22180
900378 XDOT = 6773
955697
YDOT = -7896
842348 feet/sec YDOT = -2331
280571 meter/sec
ZDOT = 8912
533842 ZDOT = 2749
413613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8015185
98 X = -2443028
69
Y = -13789205
55 feet Y = -4202949
85 meter
Z = 15475098
26 Z = 4716809
95
XDOT = 22248
171774 XDOT = 6781
242757
YDOT = -2737
086947 feet/sec YDOT = -834
264101 meter/sec
ZDOT = 9056
408445 ZDOT = 2760
393294
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 16217
15379138
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 178
6973 0001863 109
5095 250
6259 15
54931644 12448
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15379138 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 178
6973 deg
Eccentricity:
0001863
Arg of perigee: 109
5095 deg
Mean anomaly: 250
6259 deg
Mean motion: 15
54931644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 330
Coasting Arc #9 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1160210
26 A = 6775239
30 meter
Y = 4077633
75 meter E =
0016363
Z = -5299123
31 I = 51
66326
XDOT = -7507
504919 Wp = 88
31227
YDOT = 1397
655112 meter/sec RA = 172
83378 deg
ZDOT = -569
286853 TA = 176
25532
MA = 176
24305
Ha = 220
423 n
mi
Hp = 212
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3806464
09 X = 1140267
21
Y = 13378063
50 feet Y = 4090496
43 meter
Z = -17385575
18 Z = -5293535
91
XDOT = -24630
921651 XDOT = -7519
810590
YDOT = 4585
482650 feet/sec YDOT = 1313
632363 meter/sec
ZDOT = -1867
739019 ZDOT = -605
785562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1408775
11 X = 429394
65
Y = 13867301
06 feet Y = 4226753
36 meter
Z = -17361834
30 Z = -5291887
09
XDOT = -24030
493265 XDOT = -7324
494347
YDOT = -92
598495 feet/sec YDOT = -28
224021 meter/sec
ZDOT = -2027
293192 ZDOT = -617
918965
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 16218
11784273
00016717 00000-0 10270-3 0 9086
2 25544 51
6428 173
8873 0001822 109
6175 250
5175 15
54899782 12597
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11784273 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 173
8873 deg
Eccentricity:
0001822
Arg of perigee: 109
6175 deg
Mean anomaly: 250
5175 deg
Mean motion: 15
54899782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 337
Coasting Arc #10 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 967326
73 A = 6775849
77 meter
Y = -4337669
24 meter E =
0006103
Z = 5110358
70 I = 51
69789
XDOT = 7488
483690 Wp = 69
83376
YDOT = -280
456304 meter/sec RA = 167
82882 deg
ZDOT = -1651
871185 TA = 36
10773
MA = 36
06653
Ha = 220
335 n
mi
Hp = 212
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3173644
11 X = 990936
28
Y = -14231198
31 feet Y = -4326719
82 meter
Z = 16766268
71 Z = 5115115
10
XDOT = 24568
516044 XDOT = 7499
087198
YDOT = -920
132232 feet/sec YDOT = -196
655826 meter/sec
ZDOT = -5419
524886 ZDOT = -1615
468915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5381666
48 X = 1640331
94
Y = -13524672
10 feet Y = -4122320
06 meter
Z = 16787724
66 Z = 5116898
48
XDOT = 23429
005761 XDOT = 7141
160956
YDOT = 2778
127635 feet/sec YDOT = 846
773303 meter/sec
ZDOT = -5260
553855 ZDOT = -1603
416815
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 16219
14616206
00016717 00000-0 10270-3 0 9091
2 25544 51
6430 168
7552 0001808 112
7154 247
4190 15
54934624 12758
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14616206 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 168
7552 deg
Eccentricity:
0001808
Arg of perigee: 112
7154 deg
Mean anomaly: 247
4190 deg
Mean motion: 15
54934624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 303
Coasting Arc #11 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935307
86 A = 6779303
16 meter
Y = 4408322
10 meter E =
0010079
Z = -4242513
20 I = 51
74078
XDOT = -6673
753820 Wp = 111
70280
YDOT = -943
296951 meter/sec RA = 162
83423 deg
ZDOT = 3640
579220 TA = 195
52766
MA = 195
55860
Ha = 220
356 n
mi
Hp = 212
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9630275
13 X = -2963776
69
Y = 14462999
01 feet Y = 4375338
22 meter
Z = -13919006
57 Z = -4256841
25
XDOT = -21895
517781 XDOT = -6680
393726
YDOT = -3094
806271 feet/sec YDOT = -1017
964346 meter/sec
ZDOT = 11944
157547 ZDOT = 3608
144190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11585583
92 X = -3531285
98
Y = 12881370
42 feet Y = 3926241
71 meter
Z = -13982268
21 Z = -4261795
35
XDOT = -20328
084210 XDOT = -6196
000067
YDOT = -5483
539474 feet/sec YDOT = -1671
382832 meter/sec
ZDOT = 11802
688019 ZDOT = 3597
459308
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 16220
11021068
00016717 00000-0 10270-3 0 9108
2 25544 51
6430 163
9451 0001851 116
0302 244
1042 15
54930656 12901
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
11021068 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 163
9451 deg
Eccentricity:
0001851
Arg of perigee: 116
0302 deg
Mean anomaly: 244
1042 deg
Mean motion: 15
54930656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 253
Coasting Arc #12 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4693076
37 A = 6778945
76 meter
Y = -2130398
36 meter E =
0011560
Z = 4396214
02 I = 51
74247
XDOT = 5221
121727 Wp = 108
83940
YDOT = -4488
271784 meter/sec RA = 162
14644 deg
ZDOT = 3387
754275 TA = 306
89677
MA = 307
00266
Ha = 220
604 n
mi
Hp = 212
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15397232
18 X = -4690259
52
Y = -6989495
95 feet Y = -2182863
60 meter
Z = 14423274
34 Z = 4373423
47
XDOT = 17129
664458 XDOT = 5254
466665
YDOT = -14725
301130 feet/sec YDOT = -4429
699167 meter/sec
ZDOT = 11114
679380 ZDOT = 3413
197926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15911353
24 X = -4849780
47
Y = 5967207
99 feet Y = 1818804
99 meter
Z = 14324102
83 Z = 4365986
54
XDOT = 2147
923825 XDOT = 654
687182
YDOT = -21308
110224 feet/sec YDOT = -6494
711996 meter/sec
ZDOT = 11226
488929 ZDOT = 3421
833826
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 16220
30302032
00016717 00000-0 10270-3 0 9113
2 25544 51
6418 162
9838 0002037 105
7521 254
3857 15
54913869 12937
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30302032 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 162
9838 deg
Eccentricity:
0002037
Arg of perigee: 105
7521 deg
Mean anomaly: 254
3857 deg
Mean motion: 15
54913869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 294
Coasting Arc #13 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2973076
00 A = 6775731
90 meter
Y = 3192244
85 meter E =
0015602
Z = -5198407
60 I = 51
76303
XDOT = -6475
118958 Wp = 83
50973
YDOT = 3866
168594 meter/sec RA = 157
15224 deg
ZDOT = -1330
821079 TA = 173
71771
MA = 173
69813
Ha = 220
461 n
mi
Hp = 212
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9754186
36 X = 2962409
87
Y = 10473244
26 feet Y = 3225431
99 meter
Z = -17055143
03 Z = -5183991
31
XDOT = -21243
828601 XDOT = -6511
405711
YDOT = 12684
280164 feet/sec YDOT = 3793
556556 meter/sec
ZDOT = -4366
210890 ZDOT = -1362
363455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14384350
22 X = 4384349
95
Y = 222460
10 feet Y = 67805
84 meter
Z = -16992700
81 Z = -5179375
21
XDOT = -5670
532483 XDOT = -1728
378301
YDOT = 23005
696341 feet/sec YDOT = 7012
136245 meter/sec
ZDOT = -4504
565169 ZDOT = -1372
991464
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 16221
26706662
00016717 00000-0 10270-3 0 9127
2 25544 51
6428 158
1731 0001927 109
6277 250
5084 15
54901214 13083
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26706662 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 158
1731 deg
Eccentricity:
0001927
Arg of perigee: 109
6277 deg
Mean anomaly: 250
5084 deg
Mean motion: 15
54901214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 294
Coasting Arc #14 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1040299
44 A = 6775281
47 meter
Y = -4134829
14 meter E =
0004875
Z = 5261480
03 I = 51
78934
XDOT = 7039
993320 Wp = 79
28777
YDOT = -2918
028326 meter/sec RA = 152
15396 deg
ZDOT = -899
647492 TA = 19
30239
MA = 19
28393
Ha = 220
512 n
mi
Hp = 212
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3413055
91 X = -1019543
18
Y = -13565712
41 feet Y = -4146346
29 meter
Z = 17262073
59 Z = 5256477
07
XDOT = 23097
090944 XDOT = 7076
470282
YDOT = -9573
583747 feet/sec YDOT = -2839
098480 meter/sec
ZDOT = -2951
599382 ZDOT = -865
360635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12301804
04 X = -3749589
87
Y = -6713722
39 feet Y = -2046342
58 meter
Z = 17240888
54 Z = 5255022
83
XDOT = 8350
816737 XDOT = 2545
328941
YDOT = -22508
936643 feet/sec YDOT = -6860
723889 meter/sec
ZDOT = -2801
395382 ZDOT = -853
865313
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 16222
29538133
00016717 00000-0 10270-3 0 9138
2 25544 51
6410 153
0413 0002037 110
9223 249
2148 15
54919986 13243
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29538133 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 153
0413 deg
Eccentricity:
0002037
Arg of perigee: 110
9223 deg
Mean anomaly: 249
2148 deg
Mean motion: 15
54919986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 285
Coasting Arc #15 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -873445
45 A = 6778012
88 meter
Y = 4889854
71 meter E =
0012157
Z = -4623654
25 I = 51
82779
XDOT = -6857
859309 Wp = 110
65491
YDOT = 1614
406513 meter/sec RA = 147
16159 deg
ZDOT = 3005
062934 TA = 189
27129
MA = 189
29376
Ha = 220
413 n
mi
Hp = 212
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2865634
66 X = -905600
59
Y = 16042830
40 feet Y = 4879907
40 meter
Z = -15169469
32 Z = -4627975
36
XDOT = -22499
538415 XDOT = -6889
999502
YDOT = 5296
609295 feet/sec YDOT = 1537
537682 meter/sec
ZDOT = 9859
130361 ZDOT = 2971
671359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10023736
01 X = 3055234
74
Y = 12826225
19 feet Y = 3909433
44 meter
Z = -15189132
05 Z = -4629647
45
XDOT = -10297
495194 XDOT = -3138
676535
YDOT = 19541
380092 feet/sec YDOT = 5956
212652 meter/sec
ZDOT = 9713
029114 ZDOT = 2960
531274
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 16223
25942410
00016717 00000-0 10270-3 0 9143
2 25544 51
6424 148
2305 0001821 112
5213 247
6133 15
54899461 13398
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
25942410 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 148
2305 deg
Eccentricity:
0001821
Arg of perigee: 112
5213 deg
Mean anomaly: 247
6133 deg
Mean motion: 15
54899461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 285
Coasting Arc #16 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5605437
41 A = 6780967
47 meter
Y = -95255
82 meter E =
0007624
Z = -3821764
68 I = 51
83822
XDOT = -2764
701392 Wp = 84
90767
YDOT = 5777
740654 meter/sec RA = 146
63457 deg
ZDOT = -4205
587313 TA = 140
84887
MA = 140
79368
Ha = 220
443 n
mi
Hp = 212
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18390542
69 X = 5624650
31
Y = -312519
11 feet Y = -32464
70 meter
Z = -12538598
02 Z = -3794488
42
XDOT = -9070
542624 XDOT = -2808
675306
YDOT = 18955
842040 feet/sec YDOT = 5746
577986 meter/sec
ZDOT = -13797
858639 ZDOT = -4219
124313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -123396
89 X = -37611
37
Y = -18473445
92 feet Y = -5630706
32 meter
Z = -12419449
99 Z = -3785448
36
XDOT = 17513
974072 XDOT = 5338
259297
YDOT = 9184
913464 feet/sec YDOT = 2799
561624 meter/sec
ZDOT = -13857
917305 ZDOT = -4223
893195
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 16223
38796391
00016717 00000-0 10270-3 0 9153
2 25544 51
6399 147
5883 0001858 110
4645 249
6707 15
54915020 13410
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
38796391 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 147
5883 deg
Eccentricity:
0001858
Arg of perigee: 110
4645 deg
Mean anomaly: 249
6707 deg
Mean motion: 15
54915020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 327
Coasting Arc #17 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4464092
84 A = 6776859
58 meter
Y = -1379827
02 meter E =
0008511
Z = 4903756
52 I = 51
85098
XDOT = 4395
146887 Wp = 120
13278
YDOT = -5833
219216 meter/sec RA = 141
65219 deg
ZDOT = 2352
511892 TA = 306
88250
MA = 306
96048
Ha = 220
418 n
mi
Hp = 212
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14645973
87 X = -4472151
63
Y = -4526991
54 feet Y = -1429792
54 meter
Z = 16088440
02 Z = 4882051
67
XDOT = 14419
773250 XDOT = 4448
621364
YDOT = -19137
858320 feet/sec YDOT = -5783
770745 meter/sec
ZDOT = 7718
214868 ZDOT = 2373
992146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4423612
64 X = -1348317
13
Y = 14780538
64 feet Y = 4505108
18 meter
Z = 15993856
14 Z = 4874927
35
XDOT = -18158
069726 XDOT = -5534
579653
YDOT = -13914
568246 feet/sec YDOT = -4241
160401 meter/sec
ZDOT = 7812
992890 ZDOT = 2381
400233
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 16224
41627296
00016717 00000-0 10270-3 0 9166
2 25544 51
6397 142
4569 0001656 115
2689 244
8636 15
54942429 13578
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
41627296 = yrday
fracday
Element set: 916
Inclination: 51
6397 deg
RA of node: 142
4569 deg
Eccentricity:
0001656
Arg of perigee: 115
2689 deg
Mean anomaly: 244
8636 deg
Mean motion: 15
54942429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 338
Coasting Arc #18 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3004679
59 A = 6775095
04 meter
Y = 2923884
74 meter E =
0016382
Z = -5336196
69 I = 51
86943
XDOT = -5481
832939 Wp = 91
64689
YDOT = 5344
649643 meter/sec RA = 136
66031 deg
ZDOT = -159
046725 TA = 176
84528
MA = 176
83493
Ha = 220
341 n
mi
Hp = 212
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9857872
67 X = 2997681
38
Y = 9592797
71 feet Y = 2957445
99 meter
Z = -17507207
00 Z = -5321617
81
XDOT = -17985
016204 XDOT = -5540
418169
YDOT = 17534
939772 feet/sec YDOT = 5283
020554 meter/sec
ZDOT = -521
806841 ZDOT = -185
818116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9348098
55 X = 2849300
44
Y = -10199102
36 feet Y = -3108686
40 meter
Z = -17443998
48 Z = -5316930
74
XDOT = 17219
456482 XDOT = 5248
490336
YDOT = 16871
729780 feet/sec YDOT = 5142
503237 meter/sec
ZDOT = -639
637382 ZDOT = -194
961474
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 16225
38031344
00016717 00000-0 10270-3 0 9177
2 25544 51
6396 137
6452 0001701 116
7524 243
3803 15
54910646 13722
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
38031344 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 137
6452 deg
Eccentricity:
0001701
Arg of perigee: 116
7524 deg
Mean anomaly: 243
3803 deg
Mean motion: 15
54910646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 293
Coasting Arc #19 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1399975
58 A = 6776376
08 meter
Y = -4336714
93 meter E =
0006820
Z = 5010471
92 I = 51
89801
XDOT = 6001
101938 Wp = 69
12070
YDOT = -4317
796360 meter/sec RA = 131
67029 deg
ZDOT = -2055
794686 TA = 40
80935
MA = 40
75829
Ha = 220
343 n
mi
Hp = 212
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4593095
72 X = -1375715
74
Y = -14228067
35 feet Y = -4352234
83 meter
Z = 16438556
18 Z = 5003730
12
XDOT = 19688
654652 XDOT = 6058
924673
YDOT = -14165
998558 feet/sec YDOT = -4250
364687 meter/sec
ZDOT = -6744
733222 ZDOT = -2026
502778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14020379
76 X = -4273411
75
Y = 5282740
88 feet Y = 1610179
42 meter
Z = 16409818
97 Z = 5001712
82
XDOT = -14584
130684 XDOT = -4445
243033
YDOT = -18107
607553 feet/sec YDOT = -5519
198782 meter/sec
ZDOT = -6616
040202 ZDOT = -2016
569053
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 16226
40861976
00016717 00000-0 10270-3 0 9184
2 25544 51
6408 132
5135 0001631 120
4829 239
6485 15
54924596 13880
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
40861976 = yrday
fracday
Element set: 918
Inclination: 51
6408 deg
RA of node: 132
5135 deg
Eccentricity:
0001631
Arg of perigee: 120
4829 deg
Mean anomaly: 239
6485 deg
Mean motion: 15
54924596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 328
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