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 23264.09170862 .00021188 00000-0 23264-3 0 9996
2 48274 41.4739 292.4333 0007952 69.5766 290.5927 15.62664098136824
Epoch (UTC): | 21 September 2023 02:12:03 |
Eccentricity: | 0.0007952 |
inclination: | 41.4739° |
perigee height: | 374 km |
apogee height: | 385 km |
right ascension of ascending node: | 292.4333° |
argument of perigee: | 69.5766° |
revolutions per day: | 15.62664098 |
mean anomaly at epoch: | 290.5927° |
orbit number at epoch: | 13682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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