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 23340.80784571 .00014406 00000-0 15534-3 0 9994
2 48274 41.4692 184.6265 0007879 287.2847 72.7131 15.63347302148822
| Epoch (UTC): | 06 December 2023 19:23:17 |
| Eccentricity: | 0.0007879 |
| inclination: | 41.4692° |
| perigee height: | 372 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 184.6265° |
| argument of perigee: | 287.2847° |
| revolutions per day: | 15.63347302 |
| mean anomaly at epoch: | 72.7131° |
| orbit number at epoch: | 14882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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