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 24277.52651706 .00075288 00000-0 77856-3 0 9996
2 48274 41.4658 142.4379 0002867 103.3586 256.7574 15.63750249196042
| Epoch (UTC): | 03 October 2024 12:38:11 |
| Eccentricity: | 0.0002867 |
| inclination: | 41.4658° |
| perigee height: | 375 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 142.4379° |
| argument of perigee: | 103.3586° |
| revolutions per day: | 15.63750249 |
| mean anomaly at epoch: | 256.7574° |
| orbit number at epoch: | 19604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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