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 24280.91098389 .00041445 00000-0 42651-3 0 9998
2 48274 41.4653 121.7420 0003023 140.8528 219.2531 15.64075493196578
Epoch (UTC): | 06 October 2024 21:51:49 |
Eccentricity: | 0.0003023 |
inclination: | 41.4653° |
perigee height: | 374 km |
apogee height: | 378 km |
right ascension of ascending node: | 121.7420° |
argument of perigee: | 140.8528° |
revolutions per day: | 15.64075493 |
mean anomaly at epoch: | 219.2531° |
orbit number at epoch: | 19657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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