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 23027.15314976 .00016771 00000-0 19867-3 0 9992
2 48274 41.4750 295.7370 0002594 49.1184 98.3854 15.60851686 99773
| Epoch (UTC): | 27 January 2023 03:40:32 |
| Eccentricity: | 0.0002594 |
| inclination: | 41.4750° |
| perigee height: | 383 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 295.7370° |
| argument of perigee: | 49.1184° |
| revolutions per day: | 15.60851686 |
| mean anomaly at epoch: | 98.3854° |
| orbit number at epoch: | 9977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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