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 23081.42320602 .00045285 00000-0 48433-3 0 9998
2 48274 41.4744 325.1062 0002293 214.5968 139.1991 15.63067838108257
| Epoch (UTC): | 22 March 2023 10:09:25 |
| Eccentricity: | 0.0002293 |
| inclination: | 41.4744° |
| perigee height: | 377 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 325.1062° |
| argument of perigee: | 214.5968° |
| revolutions per day: | 15.63067838 |
| mean anomaly at epoch: | 139.1991° |
| orbit number at epoch: | 10825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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