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 22276U 92089B 23032.52252869 .00002663 00000-0 24269-3 0 9999
2 22276 20.2860 120.4268 0061346 145.3808 215.0629 14.85991322607610
| Epoch (UTC): | 01 February 2023 12:32:26 |
| Eccentricity: | 0.0061346 |
| inclination: | 20.2860° |
| perigee height: | 567 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 120.4268° |
| argument of perigee: | 145.3808° |
| revolutions per day: | 14.85991322 |
| mean anomaly at epoch: | 215.0629° |
| orbit number at epoch: | 60761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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