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 39769U 14029D 25013.14604985 .00007661 00000-0 79458-3 0 9994
2 39769 97.7152 87.4252 0002859 223.8738 136.2253 14.90252744575874
Epoch (UTC): | 13 January 2025 03:30:18 |
Eccentricity: | 0.0002859 |
inclination: | 97.7152° |
perigee height: | 595 km |
apogee height: | 599 km |
right ascension of ascending node: | 87.4252° |
argument of perigee: | 223.8738° |
revolutions per day: | 14.90252744 |
mean anomaly at epoch: | 136.2253° |
orbit number at epoch: | 57587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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