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 23233U 94057A 23081.48559775 .00000091 00000-0 68727-4 0 9996
2 23233 98.8421 135.8303 0011877 56.0946 304.1356 14.15755805474844
Epoch (UTC): | 22 March 2023 11:39:15 |
Eccentricity: | 0.0011877 |
inclination: | 98.8421° |
perigee height: | 831 km |
apogee height: | 848 km |
right ascension of ascending node: | 135.8303° |
argument of perigee: | 56.0946° |
revolutions per day: | 14.15755805 |
mean anomaly at epoch: | 304.1356° |
orbit number at epoch: | 47484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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