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 33412U 08054A 24286.55211853 .00010438 00000-0 84959-3 0 9996
2 33412 97.8656 124.3507 0016866 178.9564 181.1697 14.99615347864869
Epoch (UTC): | 12 October 2024 13:15:03 |
Eccentricity: | 0.0016866 |
inclination: | 97.8656° |
perigee height: | 556 km |
apogee height: | 580 km |
right ascension of ascending node: | 124.3507° |
argument of perigee: | 178.9564° |
revolutions per day: | 14.99615347 |
mean anomaly at epoch: | 181.1697° |
orbit number at epoch: | 86486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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