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 23030.59652895 .00014274 00000-0 16911-3 0 9992
2 48274 41.4748 274.7802 0002259 87.2532 354.6676 15.60949113100311
| Epoch (UTC): | 30 January 2023 14:19:00 |
| Eccentricity: | 0.0002259 |
| inclination: | 41.4748° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 274.7802° |
| argument of perigee: | 87.2532° |
| revolutions per day: | 15.60949113 |
| mean anomaly at epoch: | 354.6676° |
| orbit number at epoch: | 10031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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