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 13149U 82037B 24357.89957036 .00000552 00000-0 19757-3 0 9990
2 13149 74.0411 258.7401 0012519 155.2468 204.9289 14.36307299231276
Epoch (UTC): | 22 December 2024 21:35:22 |
Eccentricity: | 0.0012519 |
inclination: | 74.0411° |
perigee height: | 762 km |
apogee height: | 779 km |
right ascension of ascending node: | 258.7401° |
argument of perigee: | 155.2468° |
revolutions per day: | 14.36307299 |
mean anomaly at epoch: | 204.9289° |
orbit number at epoch: | 23127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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