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 23339.59407754 .00016084 00000-0 17321-3 0 9993
2 48274 41.4693 192.0405 0007923 279.7862 80.2083 15.63309633148639
Epoch (UTC): | 05 December 2023 14:15:28 |
Eccentricity: | 0.0007923 |
inclination: | 41.4693° |
perigee height: | 373 km |
apogee height: | 383 km |
right ascension of ascending node: | 192.0405° |
argument of perigee: | 279.7862° |
revolutions per day: | 15.63309633 |
mean anomaly at epoch: | 80.2083° |
orbit number at epoch: | 14863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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