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 25134.70694748 .00028637 00000-0 32254-3 0 9991
2 48274 41.4645 224.1214 0006452 270.7948 89.2152 15.61886175230922
Epoch (UTC): | 14 May 2025 16:58:00 |
Eccentricity: | 0.0006452 |
inclination: | 41.4645° |
perigee height: | 378 km |
apogee height: | 386 km |
right ascension of ascending node: | 224.1214° |
argument of perigee: | 270.7948° |
revolutions per day: | 15.61886175 |
mean anomaly at epoch: | 89.2152° |
orbit number at epoch: | 23092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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