[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 24th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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
209/14:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
3
209/15:41:12
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
3
209/22:00:48
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
4
212/23:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
1
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
3
219/05:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
2
Coasting Arc #1 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2017/205/13:31:09
955
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2991796
49 A = 6784058
89 meter
Y = 5013533
49 meter E =
0010950
Z = -3466960
93 I = 51
44142
XDOT = -6145
545174 Wp = 75
60555
YDOT = 535
537262 meter/sec RA = 210
92216 deg
ZDOT = -4538
224737 TA = 145
15869
MA = 145
08695
Ha = 223
073 n
mi
Hp = 212
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9815605
29 X = 2952351
89
Y = 16448600
70 feet Y = 5046769
49 meter
Z = -11374543
73 Z = -3452523
50
XDOT = -20162
549784 XDOT = -6129
032986
YDOT = 1757
012015 feet/sec YDOT = 466
906242 meter/sec
ZDOT = -14889
188769 ZDOT = -4568
037065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1536084
89 X = 468198
68
Y = -19130438
67 feet Y = -5830957
71 meter
Z = -11311479
87 Z = -3447739
06
XDOT = 15939
988611 XDOT = 4858
508529
YDOT = 10143
239264 feet/sec YDOT = 3091
659328 meter/sec
ZDOT = -15021
016755 ZDOT = -4578
405907
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 17205
58829981
00016717 00000-0 10270-3 0 9002
2 25544 51
6359 211
8912 0006250 64
7846 295
3954 15
54209618 27561
Satellite: ISS
Catalog Number: 25544
Epoch time: 17205
58829981 = yrday
fracday
Element set: 900
Inclination: 51
6359 deg
RA of node: 211
8912 deg
Eccentricity:
0006250
Arg of perigee: 64
7846 deg
Mean anomaly: 295
3954 deg
Mean motion: 15
54209618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2756
Checksum: 337
Coasting Arc #2 (Orbit 2771)
---------------------------------------
Vector Time (GMT): 2017/206/13:31:09
955
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1500396
01 A = 6780173
20 meter
Y = -4772777
63 meter E =
0013558
Z = 4564994
78 I = 51
45731
XDOT = 7011
290856 Wp = 95
41450
YDOT = 713
670327 meter/sec RA = 205
92162 deg
ZDOT = 3041
541440 TA = 324
10115
MA = 324
19217
Ha = 222
970 n
mi
Hp = 212
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4922559
10 X = -1469088
05
Y = -15658719
26 feet Y = -4789381
23 meter
Z = 14977016
98 Z = 4557782
31
XDOT = 23002
922755 XDOT = 6988
015329
YDOT = 2341
438081 feet/sec YDOT = 791
945069 meter/sec
ZDOT = 9978
810499 ZDOT = 3075
542863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4764829
68 X = -1452320
09
Y = 15737108
37 feet Y = 4796670
63 meter
Z = 14945833
30 Z = 4555489
99
XDOT = -16396
618582 XDOT = -4997
689344
YDOT = -14612
442635 feet/sec YDOT = -4453
872515 meter/sec
ZDOT = 10128
986543 ZDOT = 3087
315098
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 17206
61707285
00016717 00000-0 10270-3 0 9010
2 25544 51
6360 206
7625 0005993 68
1081 292
0708 15
54242695 27720
Satellite: ISS
Catalog Number: 25544
Epoch time: 17206
61707285 = yrday
fracday
Element set: 901
Inclination: 51
6360 deg
RA of node: 206
7625 deg
Eccentricity:
0005993
Arg of perigee: 68
1081 deg
Mean anomaly: 292
0708 deg
Mean motion: 15
54242695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2772
Checksum: 314
Coasting Arc #3 (Orbit 2786)
---------------------------------------
Vector Time (GMT): 2017/207/13:31:09
955
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -218532
59 A = 6777614
31 meter
Y = 4353981
60 meter E =
0020187
Z = -5207378
27 I = 51
47945
XDOT = -7344
776274 Wp = 78
15400
YDOT = -1792
248354 meter/sec RA = 200
91195 deg
ZDOT = -1190
166068 TA = 180
38066
MA = 180
38220
Ha = 223
067 n
mi
Hp = 212
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -716970
43 X = -241909
32
Y = 14284716
55 feet Y = 4351407
24 meter
Z = -17084574
38 Z = -5208496
49
XDOT = -24097
035021 XDOT = -7318
407876
YDOT = -5880
079902 feet/sec YDOT = -1874
235170 meter/sec
ZDOT = -3904
744316 ZDOT = -1225
780012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8415843
79 X = 2565149
19
Y = -11556402
68 feet Y = -3522391
54 meter
Z = -17090142
94 Z = -5209075
57
XDOT = 15940
307911 XDOT = 4858
605851
YDOT = 17615
974635 feet/sec YDOT = 5369
349069 meter/sec
ZDOT = -4061
910825 ZDOT = -1238
070419
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 17207
58154537
00016717 00000-0 10270-3 0 9024
2 25544 51
6371 201
9529 0006169 71
3755 288
8067 15
54216768 27871
Satellite: ISS
Catalog Number: 25544
Epoch time: 17207
58154537 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 201
9529 deg
Eccentricity:
0006169
Arg of perigee: 71
3755 deg
Mean anomaly: 288
8067 deg
Mean motion: 15
54216768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2787
Checksum: 339
Coasting Arc #4 (Orbit 2802)
---------------------------------------
Vector Time (GMT): 2017/208/13:31:09
955
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1997955
40 A = 6777243
15 meter
Y = -3775321
62 meter E =
0009242
Z = 5254571
24 I = 51
50943
XDOT = 7147
547798 Wp = 70
52632
YDOT = 2684
882520 meter/sec RA = 195
90142 deg
ZDOT = -784
535326 TA = 27
00141
MA = 26
95336
Ha = 222
998 n
mi
Hp = 212
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6554971
77 X = 2014499
84
Y = -12386225
80 feet Y = -3752886
69 meter
Z = 17239406
94 Z = 5264316
66
XDOT = 23449
959966 XDOT = 7120
804341
YDOT = 8808
669684 feet/sec YDOT = 2764
661735 meter/sec
ZDOT = -2573
934797 ZDOT = -749
880241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12105911
11 X = -3689881
71
Y = 6951783
85 feet Y = 2118903
72 meter
Z = 17283026
75 Z = 5267866
55
XDOT = -14498
304790 XDOT = -4419
083300
YDOT = -19194
560734 feet/sec YDOT = -5850
502112 meter/sec
ZDOT = -2421
115681 ZDOT = -737
956059
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 17208
61031099
00016717 00000-0 10270-3 0 9037
2 25544 51
6373 196
8239 0006166 74
1686 286
0146 15
54224724 28032
Satellite: ISS
Catalog Number: 25544
Epoch time: 17208
61031099 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 196
8239 deg
Eccentricity:
0006166
Arg of perigee: 74
1686 deg
Mean anomaly: 286
0146 deg
Mean motion: 15
54224724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2803
Checksum: 313
Coasting Arc #5 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2017/209/13:31:09
955
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3677528
34 A = 6779377
09 meter
Y = 3144424
14 meter E =
0016809
Z = -4763939
31 I = 51
54810
XDOT = -6332
873433 Wp = 98
07567
YDOT = -3375
342808 meter/sec RA = 190
89591 deg
ZDOT = 2666
552809 TA = 198
30262
MA = 198
36318
Ha = 223
054 n
mi
Hp = 212
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12065381
68 X = -3689276
22
Y = 10316352
18 feet Y = 3103233
89 meter
Z = -15629722
14 Z = -4781831
87
XDOT = -20777
143809 XDOT = -6307
611426
YDOT = -11073
959344 feet/sec YDOT = -3446
020083 meter/sec
ZDOT = 8748
532837 ZDOT = 2635
851391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15596856
60 X = 4753921
89
Y = -2499108
44 feet Y = -761728
25 meter
Z = -15709274
10 Z = -4788186
75
XDOT = 11736
772129 XDOT = 3577
368145
YDOT = 19224
580326 feet/sec YDOT = 5859
652083 meter/sec
ZDOT = 8613
273384 ZDOT = 2625
325727
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 17209
57477547
00016717 00000-0 10270-3 0 9046
2 25544 51
6372 192
0156 0006099 77
2158 282
9676 15
54217997 28183
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
57477547 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 192
0156 deg
Eccentricity:
0006099
Arg of perigee: 77
2158 deg
Mean anomaly: 282
9676 deg
Mean motion: 15
54217997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 353
Coasting Arc #6 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3158791
04 A = 6780976
12 meter
Y = 4126369
98 meter E =
0014833
Z = -4371109
52 I = 51
55640
XDOT = -6684
111295 Wp = 73
20429
YDOT = 1501
512880 meter/sec RA = 190
67370 deg
ZDOT = -3418
282910 TA = 162
06812
MA = 162
01573
Ha = 223
050 n
mi
Hp = 212
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10363487
67 X = 3133646
55
Y = 13537959
25 feet Y = 4161553
18 meter
Z = -14340910
50 Z = -4355826
32
XDOT = -21929
499000 XDOT = -6683
800706
YDOT = 4926
223361 feet/sec YDOT = 1426
768380 meter/sec
ZDOT = -11214
838945 ZDOT = -3450
751065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7304935
99 X = -2226544
49
Y = -15467156
60 feet Y = -4714389
33 meter
Z = -14273924
06 Z = -4350692
05
XDOT = 21275
513529 XDOT = 6484
776524
YDOT = 417
634516 feet/sec YDOT = 127
295001 meter/sec
ZDOT = -11358
600657 ZDOT = -3462
101480
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 17209
63907315
00016717 00000-0 10270-3 0 9055
2 25544 51
6384 191
6949 0006168 77
3782 282
8060 15
54248344 28199
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
63907315 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 191
6949 deg
Eccentricity:
0006168
Arg of perigee: 77
3782 deg
Mean anomaly: 282
8060 deg
Mean motion: 15
54248344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 338
Coasting Arc #7 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS) : 887043
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -164402
61 A = 6777170
58 meter
Y = -4271491
87 meter E =
0008727
Z = 5251549
79 I = 51
54570
XDOT = 7595
246764 Wp = 93
28230
YDOT = 732
359198 meter/sec RA = 190
47372 deg
ZDOT = 831
774742 TA = 348
75392
MA = 348
77341
Ha = 222
924 n
mi
Hp = 212
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -539378
63 X = -142134
57
Y = -14014080
95 feet Y = -4273205
89 meter
Z = 17229494
05 Z = 5250805
22
XDOT = 24918
788597 XDOT = 7582
452537
YDOT = 2402
753274 feet/sec YDOT = 817
222863 meter/sec
ZDOT = 2728
919756 ZDOT = 868
638562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 879760
34 X = 268150
95
Y = 14000143
26 feet Y = 4267243
67 meter
Z = 17226806
73 Z = 5250730
69
XDOT = -23915
238102 XDOT = -7289
364574
YDOT = -2062
260270 feet/sec YDOT = -628
576930 meter/sec
ZDOT = 2891
800198 ZDOT = 881
420700
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 17209
70336944
00016717 00000-0 10270-3 0 9068
2 25544 51
6389 191
3754 0005947 77
7175 282
4643 15
54275533 28204
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
70336944 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 191
3754 deg
Eccentricity:
0005947
Arg of perigee: 77
7175 deg
Mean anomaly: 282
4643 deg
Mean motion: 15
54275533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 336
Coasting Arc #8 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3740166
72 A = 6779604
97 meter
Y = -3160952
13 meter E =
0013604
Z = 4679554
58 I = 51
56052
XDOT = 6331
416623 Wp = 70
49087
YDOT = 3289
848922 meter/sec RA = 189
12721 deg
ZDOT = -2827
044414 TA = 47
61924
MA = 47
50417
Ha = 222
853 n
mi
Hp = 212
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12270888
18 X = 3752504
63
Y = -10370577
86 feet Y = -3119058
12 meter
Z = 15352869
37 Z = 4697752
87
XDOT = 20772
364249 XDOT = 6307
890333
YDOT = 10793
467592 feet/sec YDOT = 3360
519616 meter/sec
ZDOT = -9275
080097 ZDOT = -2796
345821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11602008
64 X = 3536292
23
Y = 11001185
38 feet Y = 3353161
30 meter
Z = 15433777
74 Z = 4704215
45
XDOT = -7719
098559 XDOT = -2352
781241
YDOT = 21014
162386 feet/sec YDOT = 6405
116695 meter/sec
ZDOT = -9139
815318 ZDOT = -2785
815709
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 17209
96055868
00016717 00000-0 10270-3 0 9070
2 25544 51
6373 190
0905 0005845 79
4600 280
7211 15
54237503 28241
Satellite: ISS
Catalog Number: 25544
Epoch time: 17209
96055868 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 190
0905 deg
Eccentricity:
0005845
Arg of perigee: 79
4600 deg
Mean anomaly: 280
7211 deg
Mean motion: 15
54237503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 315
Coasting Arc #9 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5151203
25 A = 6783270
74 meter
Y = 2516569
48 meter E =
0011461
Z = -3635865
34 I = 51
60491
XDOT = -4965
439370 Wp = 92
06350
YDOT = -3843
606162 meter/sec RA = 184
13256 deg
ZDOT = 4386
118668 TA = 224
83087
MA = 224
92352
Ha = 222
968 n
mi
Hp = 212
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16900273
14 X = -5161300
27
Y = 8256461
55 feet Y = 2458908
84 meter
Z = -11928692
07 Z = -3660912
53
XDOT = -16290
811580 XDOT = -4943
395522
YDOT = -12610
256436 feet/sec YDOT = -3899
009909 meter/sec
ZDOT = 14390
153111 ZDOT = 4362
051797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10264862
96 X = -3128730
23
Y = -15676665
21 feet Y = -4778247
56 meter
Z = -12039802
35 Z = -3669731
76
XDOT = 9351
337777 XDOT = 2850
287754
YDOT = -17064
688755 feet/sec YDOT = -5201
317132 meter/sec
ZDOT = 14284
275118 ZDOT = 4353
847056
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 17210
92501846
00016717 00000-0 10270-3 0 9081
2 25544 51
6369 185
2808 0005997 83
9320 276
2516 15
54249962 28397
Satellite: ISS
Catalog Number: 25544
Epoch time: 17210
92501846 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 185
2808 deg
Eccentricity:
0005997
Arg of perigee: 83
9320 deg
Mean anomaly: 276
2516 deg
Mean motion: 15
54249962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 342
Coasting Arc #10 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6176391
53 A = 6786849
63 meter
Y = -1789416
47 meter E =
0019413
Z = 2145887
17 I = 51
64956
XDOT = 3171
988183 Wp = 102
74720
YDOT = 4306
036462 meter/sec RA = 179
15180 deg
ZDOT = -5501
282822 TA = 53
44662
MA = 53
26807
Ha = 222
852 n
mi
Hp = 212
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20263751
74 X = 6185518
64
Y = -5870788
93 feet Y = -1720296
89 meter
Z = 7040312
25 Z = 2175912
04
XDOT = 10406
785376 XDOT = 3150
323515
YDOT = 14127
416214 feet/sec YDOT = 4341
386817 meter/sec
ZDOT = -18048
828157 ZDOT = -5485
926903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8647515
25 X = 2635762
65
Y = 19194149
58 feet Y = 5850376
79 meter
Z = 7173346
23 Z = 2186435
93
XDOT = -11110
550565 XDOT = -3386
495812
YDOT = 11771
212770 feet/sec YDOT = 3587
865652 meter/sec
ZDOT = -17981
526108 ZDOT = -5480
769158
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 17211
95376870
00016717 00000-0 10270-3 0 9093
2 25544 51
6367 180
1511 0005862 85
9606 274
2216 15
54285682 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 17211
95376870 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 180
1511 deg
Eccentricity:
0005862
Arg of perigee: 85
9606 deg
Mean anomaly: 274
2216 deg
Mean motion: 15
54285682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 329
Coasting Arc #11 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6684664
64 A = 6788836
08 meter
Y = 1057271
71 meter E =
0015577
Z = -473503
42 I = 51
68767
XDOT = -1147
902905 Wp = 59
59578
YDOT = -4642
825593 meter/sec RA = 174
18121 deg
ZDOT = 5993
253125 TA = 295
30102
MA = 295
46232
Ha = 223
001 n
mi
Hp = 212
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21931314
44 X = -6693690
49
Y = 3468739
19 feet Y = 982468
80 meter
Z = -1553488
92 Z = -505997
08
XDOT = -3766
085645 XDOT = -1125
012344
YDOT = -15232
367432 feet/sec YDOT = -4655
534475 meter/sec
ZDOT = 19662
903953 ZDOT = 5987
732423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6872582
73 X = -2094763
22
Y = -21102479
04 feet Y = -6432035
61 meter
Z = -1697355
98 Z = -517354
10
XDOT = 12889
877216 XDOT = 3928
834575
YDOT = -5740
243064 feet/sec YDOT = -1749
626086 meter/sec
ZDOT = 19639
142583 ZDOT = 5986
010659
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 17212
91822225
00016717 00000-0 10270-3 0 9102
2 25544 51
6359 175
3423 0006101 92
3582 267
8269 15
54257915 28704
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
91822225 = yrday
fracday
Element set: 910
Inclination: 51
6359 deg
RA of node: 175
3423 deg
Eccentricity:
0006101
Arg of perigee: 92
3582 deg
Mean anomaly: 267
8269 deg
Mean motion: 15
54257915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 310
Coasting Arc #12 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2678566
65 A = 6779385
55 meter
Y = 4057418
41 meter E =
0017148
Z = -4740914
50 I = 51
65936
XDOT = -7004
169832 Wp = 103
90252
YDOT = -1429
201916 meter/sec RA = 173
89633 deg
ZDOT = 2738
431574 TA = 193
21008
MA = 193
25504
Ha = 223
049 n
mi
Hp = 212
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8787948
32 X = -2700709
84
Y = 13311740
18 feet Y = 4027341
24 meter
Z = -15554181
45 Z = -4753979
67
XDOT = -22979
559817 XDOT = -7000
969409
YDOT = -4688
982663 feet/sec YDOT = -1507
509519 meter/sec
ZDOT = 8984
355558 ZDOT = 2704
415468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15842533
32 X = -4828804
15
Y = -1275025
15 feet Y = -388627
67 meter
Z = -15612542
13 Z = -4758702
84
XDOT = -6975
752886 XDOT = -2126
209480
YDOT = -21324
765203 feet/sec YDOT = -6499
788434 meter/sec
ZDOT = 8834
105278 ZDOT = 2692
635289
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 17212
98251949
00016717 00000-0 10270-3 0 9119
2 25544 51
6374 175
0215 0006177 93
7769 266
4090 15
54256638 28711
Satellite: ISS
Catalog Number: 25544
Epoch time: 17212
98251949 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 175
0215 deg
Eccentricity:
0006177
Arg of perigee: 93
7769 deg
Mean anomaly: 266
4090 deg
Mean motion: 15
54256638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 334
Coasting Arc #13 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4253793
63 A = 6783173
08 meter
Y = -3786677
72 meter E =
0017787
Z = 3669532
42 I = 51
70448
XDOT = 5866
355214 Wp = 89
62930
YDOT = 2353
180463 meter/sec RA = 168
90778 deg
ZDOT = -4353
760755 TA = 46
72970
MA = 46
58143
Ha = 222
980 n
mi
Hp = 212
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13956015
84 X = 4277996
48
Y = -12423483
34 feet Y = -3738973
77 meter
Z = 12039148
37 Z = 3690254
45
XDOT = 19246
572224 XDOT = 5860
753580
YDOT = 7720
408343 feet/sec YDOT = 2418
750931 meter/sec
ZDOT = -14283
991978 ZDOT = -4325
277553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17646427
82 X = 5378631
20
Y = 5957207
64 feet Y = 1815756
89 meter
Z = 12131350
80 Z = 3697635
72
XDOT = 3243
407622 XDOT = 988
590643
YDOT = 19346
159608 feet/sec YDOT = 5896
709449 meter/sec
ZDOT = -14158
328068 ZDOT = -4315
458395
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 17214
01126319
00016717 00000-0 10270-3 0 9128
2 25544 51
6375 169
8909 0006148 97
7873 262
3978 15
54249035 28871
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
01126319 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 169
8909 deg
Eccentricity:
0006148
Arg of perigee: 97
7873 deg
Mean anomaly: 262
3978 deg
Mean motion: 15
54249035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 343
Coasting Arc #14 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5431698
43 A = 6786707
46 meter
Y = 3400253
60 meter E =
0010688
Z = -2237893
54 I = 51
74954
XDOT = -4276
388857 Wp = 73
31834
YDOT = -3251
183330 meter/sec RA = 163
93384 deg
ZDOT = 5464
175119 TA = 261
85784
MA = 261
97909
Ha = 222
994 n
mi
Hp = 212
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17820532
90 X = -5458446
80
Y = 11155687
67 feet Y = 3339363
23 meter
Z = -7342170
41 Z = -2264343
55
XDOT = -14030
147169 XDOT = -4266
257441
YDOT = -10666
611975 feet/sec YDOT = -3298
948482 meter/sec
ZDOT = 17927
083725 ZDOT = 5443
426384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18631018
47 X = -5678734
43
Y = -9652286
64 feet Y = -2942016
97 meter
Z = -7459674
26 Z = -2273708
72
XDOT = 1306
119596 XDOT = 398
105253
YDOT = -16243
904698 feet/sec YDOT = -4951
142152 meter/sec
ZDOT = 17835
749586 ZDOT = 5436
336474
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 17214
97570485
00016717 00000-0 10270-3 0 9131
2 25544 51
6387 165
0826 0006196 100
3813 259
8038 15
54274209 29025
Satellite: ISS
Catalog Number: 25544
Epoch time: 17214
97570485 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 165
0826 deg
Eccentricity:
0006196
Arg of perigee: 100
3813 deg
Mean anomaly: 259
8038 deg
Mean motion: 15
54274209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 320
Coasting Arc #15 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6158890
54 A = 6788755
18 meter
Y = -2792375
16 meter E =
0018754
Z = 503268
09 I = 51
78667
XDOT = 2382
041228 Wp = 121
76648
YDOT = 4144
746513 meter/sec RA = 158
96999 deg
ZDOT = -5999
609296 TA = 52
81339
MA = 52
64233
Ha = 222
972 n
mi
Hp = 212
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20206333
80 X = 6187213
28
Y = -9161335
84 feet Y = -2723343
93 meter
Z = 1651142
04 Z = 533254
31
XDOT = 7815
095891 XDOT = 2364
659320
YDOT = 13598
249714 feet/sec YDOT = 4171
287292 meter/sec
ZDOT = -19683
757532 ZDOT = -5988
080193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18359330
37 X = 5595923
90
Y = 12437998
26 feet Y = 3791101
87 meter
Z = 1784224
72 Z = 543831
69
XDOT = -6539
532349 XDOT = -1993
249460
YDOT = 12536
369314 feet/sec YDOT = 3821
085367 meter/sec
ZDOT = -19633
334451 ZDOT = -5984
240341
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 17216
00443901
00016717 00000-0 10270-3 0 9140
2 25544 51
6379 159
9529 0006117 104
5750 255
6082 15
54284109 29187
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
00443901 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 159
9529 deg
Eccentricity:
0006117
Arg of perigee: 104
5750 deg
Mean anomaly: 255
6082 deg
Mean motion: 15
54284109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 311
Coasting Arc #16 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 802029
16 A = 6777085
47 meter
Y = 4174557
15 meter E =
0020534
Z = -5295986
93 I = 51
75384
XDOT = -7265
855246 Wp = 98
05876
YDOT = 2297
394031 meter/sec RA = 158
24123 deg
ZDOT = 710
123062 TA = 178
72883
MA = 178
72360
Ha = 222
914 n
mi
Hp = 212
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2631329
25 X = 781013
51
Y = 13696053
66 feet Y = 4183408
80 meter
Z = -17375285
21 Z = -5292141
76
XDOT = -23838
107761 XDOT = -7294
454686
YDOT = 7537
381990 feet/sec YDOT = 2215
982348 meter/sec
ZDOT = 2329
800072 ZDOT = 674
758934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1420441
96 X = 432950
71
Y = 13894546
07 feet Y = 4235057
64 meter
Z = -17358866
60 Z = -5290982
54
XDOT = -23452
058021 XDOT = -7148
187285
YDOT = 5114
124349 feet/sec YDOT = 1558
785101 meter/sec
ZDOT = 2172
988176 ZDOT = 662
326796
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 17216
13302956
00016717 00000-0 10270-3 0 9159
2 25544 51
6398 159
3148 0005936 103
7973 256
3840 15
54273591 29201
Satellite: ISS
Catalog Number: 25544
Epoch time: 17216
13302956 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 159
3148 deg
Eccentricity:
0005936
Arg of perigee: 103
7973 deg
Mean anomaly: 256
3840 deg
Mean motion: 15
54273591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 324
Coasting Arc #17 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 953608
27 A = 6778996
80 meter
Y = -4697566
87 meter E =
0012176
Z = 4783910
08 I = 51
79190
XDOT = 7098
653278 Wp = 81
72284
YDOT = -1252
756196 meter/sec RA = 153
25097 deg
ZDOT = -2637
728229 TA = 34
25016
MA = 34
17169
Ha = 222
773 n
mi
Hp = 212
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3128636
04 X = 982829
31
Y = -15411964
79 feet Y = -4686739
86 meter
Z = 15695243
03 Z = 4788613
04
XDOT = 23289
544876 XDOT = 7124
946928
YDOT = -4110
092507 feet/sec YDOT = -1173
227065 meter/sec
ZDOT = -8653
964006 ZDOT = -2603
181935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4228715
14 X = 1288912
38
Y = -15124816
76 feet Y = -4610044
15 meter
Z = 15716728
74 Z = 4790458
92
XDOT = 22493
839822 XDOT = 6856
122378
YDOT = -2569
902544 feet/sec YDOT = -783
306295 meter/sec
ZDOT = -8500
897743 ZDOT = -2591
073632
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 17217
16175704
00016717 00000-0 10270-3 0 9163
2 25544 51
6408 154
1850 0005832 107
4212 252
7572 15
54325039 29362
Satellite: ISS
Catalog Number: 25544
Epoch time: 17217
16175704 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 154
1850 deg
Eccentricity:
0005832
Arg of perigee: 107
4212 deg
Mean anomaly: 252
7572 deg
Mean motion: 15
54325039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 299
Coasting Arc #18 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2521496
52 A = 6782675
25 meter
Y = 5048420
44 meter E =
0012035
Z = -3776003
36 I = 51
83248
XDOT = -6364
770632 Wp = 107
21684
YDOT =
198151 meter/sec RA = 148
27230 deg
ZDOT = 4258
187255 TA = 207
76375
MA = 207
82804
Ha = 222
835 n
mi
Hp = 212
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8272626
36 X = -2559420
26
Y = 16563059
19 feet Y = 5020011
48 meter
Z = -12388462
48 Z = -3788343
66
XDOT = -20881
793413 XDOT = -6384
983606
YDOT =
650101 feet/sec YDOT = -71
090254 meter/sec
ZDOT = 13970
430628 ZDOT = 4227
220655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9194493
04 X = -2802481
48
Y = 16026797
72 feet Y = 4884967
94 meter
Z = -12443806
97 Z = -3792872
36
XDOT = -19764
554868 XDOT = -6024
236324
YDOT = -617
679608 feet/sec YDOT = -188
268744 meter/sec
ZDOT = 13833
367056 ZDOT = 4216
410279
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 17218
12618579
00016717 00000-0 10270-3 0 9173
2 25544 51
6404 149
3769 0006032 110
2853 249
8949 15
54322268 29512
Satellite: ISS
Catalog Number: 25544
Epoch time: 17218
12618579 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 149
3769 deg
Eccentricity:
0006032
Arg of perigee: 110
2853 deg
Mean anomaly: 249
8949 deg
Mean motion: 15
54322268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 329
Coasting Arc #19 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819154
27 A = 6786444
47 meter
Y = -5101982
39 meter E =
0019754
Z = 2304669
05 I = 51
87242
XDOT = 5219
501296 Wp = 109
12451
YDOT = 1435
424759 meter/sec RA = 143
30619 deg
ZDOT = -5440
126798 TA = 45
26116
MA = 45
10054
Ha = 222
766 n
mi
Hp = 212
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12530033
70 X = 3864727
42
Y = -16738787
36 feet Y = -5059019
26 meter
Z = 7561250
17 Z = 2323331
48
XDOT = 17124
348084 XDOT = 5229
487004
YDOT = 4709
398814 feet/sec YDOT = 1493
848768 meter/sec
ZDOT = -17848
185032 ZDOT = -5414
748298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13209971
80 X = 4026399
40
Y = -16168427
03 feet Y = -4928136
56 meter
Z = 7644597
00 Z = 2330073
17
XDOT = 15836
213062 XDOT = 4826
877741
YDOT = 4504
244673 feet/sec YDOT = 1372
893776 meter/sec
ZDOT = -17736
047502 ZDOT = -5405
947279
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 17219
15490358
00016717 00000-0 10270-3 0 9181
2 25544 51
6405 144
2478 0005953 112
7017 247
4766 15
54330121 29679
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
15490358 = yrday
fracday
Element set: 918
Inclination: 51
6405 deg
RA of node: 144
2478 deg
Eccentricity:
0005953
Arg of perigee: 112
7017 deg
Mean anomaly: 247
4766 deg
Mean motion: 15
54330121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 314
Coasting Arc #20 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -46014
46 A = 6778795
22 meter
Y = -4740199
46 meter E =
0011941
Z = 4835898
70 I = 51
84916
XDOT = 6748
371195 Wp = 84
25664
YDOT = -2647
495972 meter/sec RA = 142
70355 deg
ZDOT = -2524
384524 TA = 30
49876
MA = 30
42937
Ha = 222
892 n
mi
Hp = 212
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -150966
09 X = -16494
82
Y = -15551835
51 feet Y = -4740549
11 meter
Z = 15865809
37 Z = 4835746
74
XDOT = 22140
325444 XDOT = 6789
736616
YDOT = -8686
010407 feet/sec YDOT = -2571
799739 meter/sec
ZDOT = -8282
101456 ZDOT = -2491
503306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10460651
44 X = -3188406
56
Y = -11508990
80 feet Y = -3507940
40 meter
Z = 15865818
22 Z = 4835901
39
XDOT = 10090
406696 XDOT = 3075
555961
YDOT = -20416
892294 feet/sec YDOT = -6223
068771 meter/sec
ZDOT = -8136
162448 ZDOT = -2479
902314
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 17219
28349288
00016717 00000-0 10270-3 0 9191
2 25544 51
6396 143
6074 0006157 111
8770 248
3038 15
54329823 29697
Satellite: ISS
Catalog Number: 25544
Epoch time: 17219
28349288 = yrday
fracday
Element set: 919
Inclination: 51
6396 deg
RA of node: 143
6074 deg
Eccentricity:
0006157
Arg of perigee: 111
8770 deg
Mean anomaly: 248
3038 deg
Mean motion: 15
54329823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 342
Coasting Arc #21 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 902274
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1446275
67 A = 6782477
38 meter
Y = 5400226
14 meter E =
0012327
Z = -3853819
90 I = 51
88775
XDOT = -6288
254996 Wp = 110
38967
YDOT = 1290
473982 meter/sec RA = 137
72799 deg
ZDOT = 4174
800706 TA = 203
44425
MA = 203
50050
Ha = 222
834 n
mi
Hp = 212
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4744998
93 X = -1487835
36
Y = 17717277
38 feet Y = 5383820
57 meter
Z = -12643766
07 Z = -3860946
20
XDOT = -20630
757862 XDOT = -6322
496776
YDOT = 4233
838525 feet/sec YDOT = 1219
962942 meter/sec
ZDOT = 13696
852709 ZDOT = 4144
171795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8479148
28 X = 2584444
40
Y = 16238917
13 feet Y = 4949621
94 meter
Z = -12676094
34 Z = -3863673
55
XDOT = -11286
444109 XDOT = -3440
108164
YDOT = 16462
056597 feet/sec YDOT = 5017
634851 meter/sec
ZDOT = 13561
063928 ZDOT = 4133
412285
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 17220
24791021
00016717 00000-0 10270-3 0 9207
2 25544 51
6407 138
7993 0006065 115
2830 244
8952 15
54311882 29847
Satellite: ISS
Catalog Number: 25544
Epoch time: 17220
24791021 = yrday
fracday
Element set: 920
Inclination: 51
6407 deg
RA of node: 138
7993 deg
Eccentricity:
0006065
Arg of perigee: 115
2830 deg
Mean anomaly: 244
8952 deg
Mean motion: 15
54311882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 308
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