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 40922U 15050C 24337.18876181 .00000041 00000-0 22361-3 0 9999
2 40922 82.4887 68.3398 0016729 180.2653 179.8420 12.42892474417065
Epoch (UTC): | 02 December 2024 04:31:49 |
Eccentricity: | 0.0016729 |
inclination: | 82.4887° |
perigee height: | 1481 km |
apogee height: | 1507 km |
right ascension of ascending node: | 68.3398° |
argument of perigee: | 180.2653° |
revolutions per day: | 12.42892474 |
mean anomaly at epoch: | 179.8420° |
orbit number at epoch: | 41706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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