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 data is extracted from the following two-line orbital elements,
1 41847U 16066G 23088.17118878 .00002772 00000-0 41767-3 0 9991
2 41847 98.5109 157.0917 0361757 77.5255 286.6152 14.39447842335296
| Epoch (UTC): | 29 March 2023 04:06:30 |
| Eccentricity: | 0.0361757 |
| inclination: | 98.5109° |
| perigee height: | 502 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 157.0917° |
| argument of perigee: | 77.5255° |
| revolutions per day: | 14.39447842 |
| mean anomaly at epoch: | 286.6152° |
| orbit number at epoch: | 33529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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