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 24357.81767204 .00027672 00000-0 33233-3 0 9993
2 48274 41.4679 13.6319 0001982 252.7034 107.3587 15.60253132208597
| Epoch (UTC): | 22 December 2024 19:37:26 |
| Eccentricity: | 0.0001982 |
| inclination: | 41.4679° |
| perigee height: | 385 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 13.6319° |
| argument of perigee: | 252.7034° |
| revolutions per day: | 15.60253132 |
| mean anomaly at epoch: | 107.3587° |
| orbit number at epoch: | 20859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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