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 44265U 19029AG 20287.67823757 .29311092 12381-4 20466-2 0 9992
2 44265 52.9803 332.3076 0000578 316.8106 43.5401 16.40378467 77859
| Epoch (UTC): | 13 October 2020 16:16:39 |
| Eccentricity: | 0.0000578 |
| inclination: | 52.9803° |
| perigee height: | 164 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 332.3076° |
| argument of perigee: | 316.8106° |
| revolutions per day: | 16.40378467 |
| mean anomaly at epoch: | 43.5401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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