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 39355U 10057V 17187.44534897 .00007319 00000-0 58422-1 0 9998
2 39355 20.3313 111.6722 7174179 349.2965 308.9022 2.27573484 45659
| Epoch (UTC): | 06 July 2017 10:41:18 |
| Eccentricity: | 0.7174179 |
| inclination: | 20.3313° |
| perigee height: | 521 km |
| apogee height: | 35552 km |
| right ascension of ascending node: | 111.6722° |
| argument of perigee: | 349.2965° |
| revolutions per day: | 2.27573484 |
| mean anomaly at epoch: | 308.9022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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