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 22285U 92093B 23146.98980738 .00000175 00000-0 11467-3 0 9995
2 22285 71.0222 340.2115 0002672 38.3279 321.8033 14.15153882569480
| Epoch (UTC): | 26 May 2023 23:45:19 |
| Eccentricity: | 0.0002672 |
| inclination: | 71.0222° |
| perigee height: | 840 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 340.2115° |
| argument of perigee: | 38.3279° |
| revolutions per day: | 14.15153882 |
| mean anomaly at epoch: | 321.8033° |
| orbit number at epoch: | 56948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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