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 23080.10851009 .00045113 00000-0 48476-3 0 9999
2 48274 41.4747 333.1338 0002267 201.5337 305.0231 15.62949389108050
| Epoch (UTC): | 21 March 2023 02:36:15 |
| Eccentricity: | 0.0002267 |
| inclination: | 41.4747° |
| perigee height: | 377 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 333.1338° |
| argument of perigee: | 201.5337° |
| revolutions per day: | 15.62949389 |
| mean anomaly at epoch: | 305.0231° |
| orbit number at epoch: | 10805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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