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 44832U 19084J 20272.06303716 .11453400 23230-5 63587-3 0 9997
2 44832 96.9437 144.0914 0010614 231.8961 128.1384 16.41416157 46773
| Epoch (UTC): | 28 September 2020 01:30:46 |
| Eccentricity: | 0.0010614 |
| inclination: | 96.9437° |
| perigee height: | 155 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 144.0914° |
| argument of perigee: | 231.8961° |
| revolutions per day: | 16.41416157 |
| mean anomaly at epoch: | 128.1384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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