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 25693U 99021A 23082.80440485 .00001059 00000-0 15263-3 0 9999
2 25693 64.5542 114.1358 0016951 212.9839 147.0210 14.81510021291978
Epoch (UTC): | 23 March 2023 19:18:20 |
Eccentricity: | 0.0016951 |
inclination: | 64.5542° |
perigee height: | 612 km |
apogee height: | 636 km |
right ascension of ascending node: | 114.1358° |
argument of perigee: | 212.9839° |
revolutions per day: | 14.81510021 |
mean anomaly at epoch: | 147.0210° |
orbit number at epoch: | 29197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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