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 39095U 73086HH 24354.73256625 .00000035 00000-0 68039-3 0 9991
2 39095 102.4987 356.9594 0058077 135.2180 225.3585 12.30923337510455
Epoch (UTC): | 19 December 2024 17:34:53 |
Eccentricity: | 0.0058077 |
inclination: | 102.4987° |
perigee height: | 1499 km |
apogee height: | 1591 km |
right ascension of ascending node: | 356.9594° |
argument of perigee: | 135.2180° |
revolutions per day: | 12.30923337 |
mean anomaly at epoch: | 225.3585° |
orbit number at epoch: | 51045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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