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 33410U 08053C 24282.57248027 .00033133 00000-0 17265-2 0 9996
2 33410 97.8692 319.5293 0103954 220.5094 138.8365 15.11266329871130
Epoch (UTC): | 08 October 2024 13:44:22 |
Eccentricity: | 0.0103954 |
inclination: | 97.8692° |
perigee height: | 460 km |
apogee height: | 604 km |
right ascension of ascending node: | 319.5293° |
argument of perigee: | 220.5094° |
revolutions per day: | 15.11266329 |
mean anomaly at epoch: | 138.8365° |
orbit number at epoch: | 87113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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