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 44250U 19029R 20259.91668981 .00384114 11978-4 11690-3 0 9993
2 44250 52.9869 115.1258 0009234 267.0021 304.7602 16.26094342 73363
| Epoch (UTC): | 15 September 2020 22:00:02 |
| Eccentricity: | 0.0009234 |
| inclination: | 52.9869° |
| perigee height: | 197 km |
| apogee height: | 209 km |
| right ascension of ascending node: | 115.1258° |
| argument of perigee: | 267.0021° |
| revolutions per day: | 16.26094342 |
| mean anomaly at epoch: | 304.7602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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