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 44819U 19082A 24358.17937931 .00001147 00000-0 15476-3 0 9997
2 44819 97.8187 7.6624 0002835 118.9747 241.1750 14.80992051274044
| Epoch (UTC): | 23 December 2024 04:18:18 |
| Eccentricity: | 0.0002835 |
| inclination: | 97.8187° |
| perigee height: | 624 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 7.6624° |
| argument of perigee: | 118.9747° |
| revolutions per day: | 14.80992051 |
| mean anomaly at epoch: | 241.1750° |
| orbit number at epoch: | 27404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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