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 24594U 94029YW 24357.88373133 .00006673 00000-0 14948-2 0 9995
2 24594 81.4622 152.8461 0471325 69.1478 295.9489 14.05115303431651
Epoch (UTC): | 22 December 2024 21:12:34 |
Eccentricity: | 0.0471325 |
inclination: | 81.4622° |
perigee height: | 534 km |
apogee height: | 1218 km |
right ascension of ascending node: | 152.8461° |
argument of perigee: | 69.1478° |
revolutions per day: | 14.05115303 |
mean anomaly at epoch: | 295.9489° |
orbit number at epoch: | 43165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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