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 24309.78613135 .00059818 00000-0 69008-3 0 9995
2 48274 41.4675 305.3521 0005838 338.9497 21.1101 15.61009831201092
Epoch (UTC): | 04 November 2024 18:52:01 |
Eccentricity: | 0.0005838 |
inclination: | 41.4675° |
perigee height: | 381 km |
apogee height: | 388 km |
right ascension of ascending node: | 305.3521° |
argument of perigee: | 338.9497° |
revolutions per day: | 15.61009831 |
mean anomaly at epoch: | 21.1101° |
orbit number at epoch: | 20109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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