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 48274U 21035A 24261.35892625 .00061152 00000-0 62232-3 0 9994
2 48274 41.4675 241.1258 0002629 170.8533 189.2355 15.64228168193518
Epoch (UTC): | 17 September 2024 08:36:51 |
Eccentricity: | 0.0002629 |
inclination: | 41.4675° |
perigee height: | 373 km |
apogee height: | 377 km |
right ascension of ascending node: | 241.1258° |
argument of perigee: | 170.8533° |
revolutions per day: | 15.64228168 |
mean anomaly at epoch: | 189.2355° |
orbit number at epoch: | 19351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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