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 24305U 96052B 23088.45195839 .00000136 00000-0 12906-3 0 9992
2 24305 82.9368 230.3599 0028836 286.1953 73.6030 13.73888877331729
Epoch (UTC): | 29 March 2023 10:50:49 |
Eccentricity: | 0.0028836 |
inclination: | 82.9368° |
perigee height: | 964 km |
apogee height: | 1007 km |
right ascension of ascending node: | 230.3599° |
argument of perigee: | 286.1953° |
revolutions per day: | 13.73888877 |
mean anomaly at epoch: | 73.6030° |
orbit number at epoch: | 33172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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