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 25940U 99057A 23082.88960055 .00000592 00000-0 22033-3 0 9995
2 25940 98.7479 49.2266 0003970 236.1612 123.9195 14.35820000227931
Epoch (UTC): | 23 March 2023 21:21:01 |
Eccentricity: | 0.0003970 |
inclination: | 98.7479° |
perigee height: | 769 km |
apogee height: | 775 km |
right ascension of ascending node: | 49.2266° |
argument of perigee: | 236.1612° |
revolutions per day: | 14.35820000 |
mean anomaly at epoch: | 123.9195° |
orbit number at epoch: | 22793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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