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 42390U 00055SJ 24357.65900217 .00005337 00000-0 22841-2 0 9996
2 42390 98.6597 67.2474 0014502 319.7787 40.2319 14.25252782457113
Epoch (UTC): | 22 December 2024 15:48:57 |
Eccentricity: | 0.0014502 |
inclination: | 98.6597° |
perigee height: | 797 km |
apogee height: | 818 km |
right ascension of ascending node: | 67.2474° |
argument of perigee: | 319.7787° |
revolutions per day: | 14.25252782 |
mean anomaly at epoch: | 40.2319° |
orbit number at epoch: | 45711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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