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 23084.00446904 .00049839 00000-0 52693-3 0 9991
2 48274 41.4695 309.3480 0002891 248.4940 250.3843 15.63327567108665
| Epoch (UTC): | 25 March 2023 00:06:26 |
| Eccentricity: | 0.0002891 |
| inclination: | 41.4695° |
| perigee height: | 376 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 309.3480° |
| argument of perigee: | 248.4940° |
| revolutions per day: | 15.63327567 |
| mean anomaly at epoch: | 250.3843° |
| orbit number at epoch: | 10866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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