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 23279U 94061B 24311.29604674 .00017989 00000-0 99753-3 0 9992
2 23279 82.9666 54.8998 0648692 5.5580 355.2353 14.15941059502016
Epoch (UTC): | 06 November 2024 07:06:18 |
Eccentricity: | 0.0648692 |
inclination: | 82.9666° |
perigee height: | 371 km |
apogee height: | 1307 km |
right ascension of ascending node: | 54.8998° |
argument of perigee: | 5.5580° |
revolutions per day: | 14.15941059 |
mean anomaly at epoch: | 355.2353° |
orbit number at epoch: | 50201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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