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 23279U 94061B 25196.80108965 .00006865 00000-0 36623-3 0 9991
2 23279 82.9594 213.1804 0620665 323.4315 32.5950 14.22600252537662
Epoch (UTC): | 15 July 2025 19:13:34 |
Eccentricity: | 0.0620665 |
inclination: | 82.9594° |
perigee height: | 370 km |
apogee height: | 1263 km |
right ascension of ascending node: | 213.1804° |
argument of perigee: | 323.4315° |
revolutions per day: | 14.22600252 |
mean anomaly at epoch: | 32.5950° |
orbit number at epoch: | 53766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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