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 43881U 18111F 25138.70802211 .00025069 00000-0 85676-3 0 9993
2 43881 97.6109 55.4252 0005463 334.8739 25.2235 15.30262659348447
Epoch (UTC): | 18 May 2025 16:59:33 |
Eccentricity: | 0.0005463 |
inclination: | 97.6109° |
perigee height: | 471 km |
apogee height: | 479 km |
right ascension of ascending node: | 55.4252° |
argument of perigee: | 334.8739° |
revolutions per day: | 15.30262659 |
mean anomaly at epoch: | 25.2235° |
orbit number at epoch: | 34844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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