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 28650U 05017B 25131.96106269 .00005667 00000-0 40325-3 0 9996
2 28650 98.0020 134.0866 0020100 314.7034 45.2553 15.04911711 86328
Epoch (UTC): | 11 May 2025 23:03:55 |
Eccentricity: | 0.0020100 |
inclination: | 98.0020° |
perigee height: | 538 km |
apogee height: | 566 km |
right ascension of ascending node: | 134.0866° |
argument of perigee: | 314.7034° |
revolutions per day: | 15.04911711 |
mean anomaly at epoch: | 45.2553° |
orbit number at epoch: | 8632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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