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 23271.85880307 .00013216 00000-0 83911-3 0 9995
2 33493 98.2426 293.8130 0016932 62.6976 297.5972 15.08898674799369
Epoch (UTC): | 28 September 2023 20:36:40 |
Eccentricity: | 0.0016932 |
inclination: | 98.2426° |
perigee height: | 528 km |
apogee height: | 551 km |
right ascension of ascending node: | 293.8130° |
argument of perigee: | 62.6976° |
revolutions per day: | 15.08898674 |
mean anomaly at epoch: | 297.5972° |
orbit number at epoch: | 79936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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