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 33493U 09002B 23086.90705992 .00015458 00000-0 11041-2 0 9995
2 33493 98.2509 95.8303 0015567 323.2625 36.7531 15.04506751771512
Epoch (UTC): | 27 March 2023 21:46:09 |
Eccentricity: | 0.0015567 |
inclination: | 98.2509° |
perigee height: | 542 km |
apogee height: | 564 km |
right ascension of ascending node: | 95.8303° |
argument of perigee: | 323.2625° |
revolutions per day: | 15.04506751 |
mean anomaly at epoch: | 36.7531° |
orbit number at epoch: | 77151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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