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 23087.56312900 .00045398 00000-0 47396-3 0 9993
2 48274 41.4746 287.5962 0004282 253.2299 142.3725 15.63674601109227
| Epoch (UTC): | 28 March 2023 13:30:54 |
| Eccentricity: | 0.0004282 |
| inclination: | 41.4746° |
| perigee height: | 374 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 287.5962° |
| argument of perigee: | 253.2299° |
| revolutions per day: | 15.63674601 |
| mean anomaly at epoch: | 142.3725° |
| orbit number at epoch: | 10922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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