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 24277U 96046A 23344.64625601 .00000113 00000-0 62065-4 0 9991
2 24277 98.9174 6.1773 0000209 267.5539 92.5618 14.29809898424452
Epoch (UTC): | 10 December 2023 15:30:36 |
Eccentricity: | 0.0000209 |
inclination: | 98.9174° |
perigee height: | 792 km |
apogee height: | 792 km |
right ascension of ascending node: | 6.1773° |
argument of perigee: | 267.5539° |
revolutions per day: | 14.29809898 |
mean anomaly at epoch: | 92.5618° |
orbit number at epoch: | 42445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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