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 44881U 19093C 23336.86919720 .00001923 00000-0 24252-3 0 9999
2 44881 97.8487 52.3786 0013302 245.4993 114.4834 14.83044141213793
| Epoch (UTC): | 02 December 2023 20:51:38 |
| Eccentricity: | 0.0013302 |
| inclination: | 97.8487° |
| perigee height: | 610 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 52.3786° |
| argument of perigee: | 245.4993° |
| revolutions per day: | 14.83044141 |
| mean anomaly at epoch: | 114.4834° |
| orbit number at epoch: | 21379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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