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 54342U 22151CM 24357.95173360 .00000381 00000-0 24364-3 0 9998
2 54342 98.8153 354.2598 0052868 78.6792 282.0312 14.08559661108088
| Epoch (UTC): | 22 December 2024 22:50:29 |
| Eccentricity: | 0.0052868 |
| inclination: | 98.8153° |
| perigee height: | 826 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 354.2598° |
| argument of perigee: | 78.6792° |
| revolutions per day: | 14.08559661 |
| mean anomaly at epoch: | 282.0312° |
| orbit number at epoch: | 10808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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