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 23093U 94024B 23150.92628674 .00000025 00000-0 10109-4 0 9993
2 23093 82.9443 297.3556 0010856 37.9335 322.2586 13.77976503930521
Epoch (UTC): | 30 May 2023 22:13:51 |
Eccentricity: | 0.0010856 |
inclination: | 82.9443° |
perigee height: | 963 km |
apogee height: | 979 km |
right ascension of ascending node: | 297.3556° |
argument of perigee: | 37.9335° |
revolutions per day: | 13.77976503 |
mean anomaly at epoch: | 322.2586° |
orbit number at epoch: | 93052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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