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 24292U 96050B 23080.55859740 .00000051 00000-0 00000+0 0 9990
2 24292 62.8141 230.0533 5518750 248.8182 58.6250 4.14707579402256
| Epoch (UTC): | 21 March 2023 13:24:22 |
| Eccentricity: | 0.5518750 |
| inclination: | 62.8141° |
| perigee height: | 955 km |
| apogee height: | 19017 km |
| right ascension of ascending node: | 230.0533° |
| argument of perigee: | 248.8182° |
| revolutions per day: | 4.14707579 |
| mean anomaly at epoch: | 58.6250° |
| orbit number at epoch: | 40225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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