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 48274U 21035A 24315.61305263 .00054641 00000-0 66946-3 0 9991
2 48274 41.4666 269.9513 0009445 303.7585 56.2353 15.59436420202009
Epoch (UTC): | 10 November 2024 14:42:47 |
Eccentricity: | 0.0009445 |
inclination: | 41.4666° |
perigee height: | 383 km |
apogee height: | 395 km |
right ascension of ascending node: | 269.9513° |
argument of perigee: | 303.7585° |
revolutions per day: | 15.59436420 |
mean anomaly at epoch: | 56.2353° |
orbit number at epoch: | 20200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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