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 41314U 98067HQ 17164.58972946 +.11750698 +12645-4 +18149-3 0 9997
2 41314 051.6052 348.7173 0009415 280.9513 079.0457 16.47784496078591
| Epoch (UTC): | 13 June 2017 14:09:12 |
| Eccentricity: | 0.0009415 |
| inclination: | 51.6052° |
| perigee height: | 139 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 348.7173° |
| argument of perigee: | 280.9513° |
| revolutions per day: | 16.47784496 |
| mean anomaly at epoch: | 79.0457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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