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 25132.59679063 .00031277 00000-0 35353-3 0 9996
2 48274 41.4647 236.9826 0006448 258.5063 101.5052 15.61760286230595
Epoch (UTC): | 12 May 2025 14:19:22 |
Eccentricity: | 0.0006448 |
inclination: | 41.4647° |
perigee height: | 378 km |
apogee height: | 387 km |
right ascension of ascending node: | 236.9826° |
argument of perigee: | 258.5063° |
revolutions per day: | 15.61760286 |
mean anomaly at epoch: | 101.5052° |
orbit number at epoch: | 23059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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