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 28163U 04005A 16107.17649683 .99999999 80343-5 50846-3 0 9999
2 28163 62.8606 306.2093 0183577 253.9848 222.5544 16.31216773 90564
| Epoch (UTC): | 16 April 2016 04:14:09 |
| Eccentricity: | 0.0183577 |
| inclination: | 62.8606° |
| perigee height: | 69 km |
| apogee height: | 310 km |
| right ascension of ascending node: | 306.2093° |
| argument of perigee: | 253.9848° |
| revolutions per day: | 16.31216773 |
| mean anomaly at epoch: | 222.5544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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