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 31569U 99025BZL 24355.56594308 .00004186 00000-0 29235-2 0 9990
2 31569 102.6225 18.0502 0181316 135.6640 13.9376 13.91813327887993
Epoch (UTC): | 20 December 2024 13:34:57 |
Eccentricity: | 0.0181316 |
inclination: | 102.6225° |
perigee height: | 790 km |
apogee height: | 1054 km |
right ascension of ascending node: | 18.0502° |
argument of perigee: | 135.6640° |
revolutions per day: | 13.91813327 |
mean anomaly at epoch: | 13.9376° |
orbit number at epoch: | 88799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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