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 is defined by the following mean orbital elements,
1 51080U 22002DA 24138.97473861 .01172231 64229-3 32625-2 0 9996
2 51080 97.4039 222.9048 0007866 241.8685 118.1795 15.93809903130740
| Epoch (UTC): | 17 May 2024 23:23:37 |
| Eccentricity: | 0.0007866 |
| inclination: | 97.4039° |
| perigee height: | 286 km |
| apogee height: | 297 km |
| right ascension of ascending node: | 222.9048° |
| argument of perigee: | 241.8685° |
| revolutions per day: | 15.93809903 |
| mean anomaly at epoch: | 118.1795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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