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 23153.56348974 -.00000095 00000-0 -24427-4 0 9991
2 22285 71.0222 326.4178 0003046 20.0504 340.0738 14.15155120570091
| Epoch (UTC): | 02 June 2023 13:31:25 |
| Eccentricity: | 0.0003046 |
| inclination: | 71.0222° |
| perigee height: | 839 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 326.4178° |
| argument of perigee: | 20.0504° |
| revolutions per day: | 14.15155120 |
| mean anomaly at epoch: | 340.0738° |
| orbit number at epoch: | 57009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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