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 44236U 19029B 20222.55316459 +.30875389 +12472-4 +17311-2 0 9994
2 44236 052.9807 260.6619 0004178 316.6235 043.5158 16.42066597069218
| Epoch (UTC): | 09 August 2020 13:16:33 |
| Eccentricity: | 0.0004178 |
| inclination: | 52.9807° |
| perigee height: | 157 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 260.6619° |
| argument of perigee: | 316.6235° |
| revolutions per day: | 16.42066597 |
| mean anomaly at epoch: | 43.5158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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