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 24259.44345125 .00034709 00000-0 35803-3 0 9991
2 48274 41.4676 252.8421 0002134 154.7859 205.3085 15.64081428193216
Epoch (UTC): | 15 September 2024 10:38:34 |
Eccentricity: | 0.0002134 |
inclination: | 41.4676° |
perigee height: | 374 km |
apogee height: | 377 km |
right ascension of ascending node: | 252.8421° |
argument of perigee: | 154.7859° |
revolutions per day: | 15.64081428 |
mean anomaly at epoch: | 205.3085° |
orbit number at epoch: | 19321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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