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 24280.71726317 .00000511 00000-0 28700-3 0 9999
2 22285 71.0247 13.6273 0004198 346.7421 13.3591 14.15310923639721
| Epoch (UTC): | 06 October 2024 17:12:51 |
| Eccentricity: | 0.0004198 |
| inclination: | 71.0247° |
| perigee height: | 838 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 13.6273° |
| argument of perigee: | 346.7421° |
| revolutions per day: | 14.15310923 |
| mean anomaly at epoch: | 13.3591° |
| orbit number at epoch: | 63972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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