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 42765U 17036A 23083.66366701 .00079305 00000-0 18026-2 0 9995
2 42765 97.1554 123.6551 0007698 52.2590 307.9355 15.42687678320228
Epoch (UTC): | 24 March 2023 15:55:40 |
Eccentricity: | 0.0007698 |
inclination: | 97.1554° |
perigee height: | 433 km |
apogee height: | 443 km |
right ascension of ascending node: | 123.6551° |
argument of perigee: | 52.2590° |
revolutions per day: | 15.42687678 |
mean anomaly at epoch: | 307.9355° |
orbit number at epoch: | 32022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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