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 22143.25652788 .00032716 00000-0 39518-3 0 9999
2 48274 41.4737 10.4933 0002146 33.7275 117.5942 15.60037951 60870
| Epoch (UTC): | 23 May 2022 06:09:24 |
| Eccentricity: | 0.0002146 |
| inclination: | 41.4737° |
| perigee height: | 386 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 10.4933° |
| argument of perigee: | 33.7275° |
| revolutions per day: | 15.60037951 |
| mean anomaly at epoch: | 117.5942° |
| orbit number at epoch: | 6087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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