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 24278.10128860 .00092913 00000-0 95447-3 0 9991
2 48274 41.4657 138.9234 0002849 109.8770 250.2376 15.63840714196133
| Epoch (UTC): | 04 October 2024 02:25:51 |
| Eccentricity: | 0.0002849 |
| inclination: | 41.4657° |
| perigee height: | 374 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 138.9234° |
| argument of perigee: | 109.8770° |
| revolutions per day: | 15.63840714 |
| mean anomaly at epoch: | 250.2376° |
| orbit number at epoch: | 19613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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