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 40958U 15057A 23083.72247301 .00001351 00000-0 21346-3 0 9995
2 40958 97.7125 121.8448 0019075 134.2076 226.0699 14.73750566401252
Epoch (UTC): | 24 March 2023 17:20:21 |
Eccentricity: | 0.0019075 |
inclination: | 97.7125° |
perigee height: | 636 km |
apogee height: | 662 km |
right ascension of ascending node: | 121.8448° |
argument of perigee: | 134.2076° |
revolutions per day: | 14.73750566 |
mean anomaly at epoch: | 226.0699° |
orbit number at epoch: | 40125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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