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 34910U 93036ADF 24357.84792137 .00000942 00000-0 98196-3 0 9991
2 34910 73.8760 301.1404 0468595 120.5441 277.2360 13.36963174769649
Epoch (UTC): | 22 December 2024 20:21:00 |
Eccentricity: | 0.0468595 |
inclination: | 73.8760° |
perigee height: | 769 km |
apogee height: | 1472 km |
right ascension of ascending node: | 301.1404° |
argument of perigee: | 120.5441° |
revolutions per day: | 13.36963174 |
mean anomaly at epoch: | 277.2360° |
orbit number at epoch: | 76964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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