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 22019.13863219 .00016969 00000-0 20045-3 0 9998
2 48274 41.4703 47.0617 0002478 101.6881 8.1721 15.60918958 41463
| Epoch (UTC): | 19 January 2022 03:19:37 |
| Eccentricity: | 0.0002478 |
| inclination: | 41.4703° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 47.0617° |
| argument of perigee: | 101.6881° |
| revolutions per day: | 15.60918958 |
| mean anomaly at epoch: | 8.1721° |
| orbit number at epoch: | 4146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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