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 31656U 99025CBN 24356.35792833 .00013129 00000-0 42475-2 0 9996
2 31656 99.1741 311.4623 0026831 24.8879 132.3352 14.38960555913145
Epoch (UTC): | 21 December 2024 08:35:25 |
Eccentricity: | 0.0026831 |
inclination: | 99.1741° |
perigee height: | 743 km |
apogee height: | 781 km |
right ascension of ascending node: | 311.4623° |
argument of perigee: | 24.8879° |
revolutions per day: | 14.38960555 |
mean anomaly at epoch: | 132.3352° |
orbit number at epoch: | 91314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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