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 24308.44252077 .00069292 00000-0 80311-3 0 9998
2 48274 41.4673 313.5295 0006134 330.2512 29.7977 15.60835941200881
Epoch (UTC): | 03 November 2024 10:37:13 |
Eccentricity: | 0.0006134 |
inclination: | 41.4673° |
perigee height: | 381 km |
apogee height: | 389 km |
right ascension of ascending node: | 313.5295° |
argument of perigee: | 330.2512° |
revolutions per day: | 15.60835941 |
mean anomaly at epoch: | 29.7977° |
orbit number at epoch: | 20088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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