View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39497U 13076E 18145.87910812 +.00000024 +00000-0 +10000-3 0 9994
2 39497 082.4851 204.2054 0018160 044.4871 315.7667 12.42675850200123
| Epoch (UTC): | 25 May 2018 21:05:54 |
| Eccentricity: | 0.0018160 |
| inclination: | 82.4851° |
| perigee height: | 1481 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 204.2054° |
| argument of perigee: | 44.4871° |
| revolutions per day: | 12.42675850 |
| mean anomaly at epoch: | 315.7667° |
| orbit number at epoch: | 20012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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