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 15055U 84062A 23083.54915074 .00000112 00000-0 10213-3 0 9991
2 15055 82.9567 230.1956 0028648 102.6773 330.0114 13.74381564943364
Epoch (UTC): | 24 March 2023 13:10:46 |
Eccentricity: | 0.0028648 |
inclination: | 82.9567° |
perigee height: | 963 km |
apogee height: | 1005 km |
right ascension of ascending node: | 230.1956° |
argument of perigee: | 102.6773° |
revolutions per day: | 13.74381564 |
mean anomaly at epoch: | 330.0114° |
orbit number at epoch: | 94336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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