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 is defined by the following mean orbital elements,
1 27391U 02012A 18068.91646861 +.07233816 -11624-5 +29177-3 0 9990
2 27391 088.9490 280.8971 0006346 277.5506 193.5554 16.43427109218648
| Epoch (UTC): | 09 March 2018 21:59:42 |
| Eccentricity: | 0.0006346 |
| inclination: | 88.9490° |
| perigee height: | 152 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 280.8971° |
| argument of perigee: | 277.5506° |
| revolutions per day: | 16.43427109 |
| mean anomaly at epoch: | 193.5554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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