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 51081U 22002DB 24142.74938976 .04589662 24556-5 17292-2 0 9997
2 51081 97.3942 227.5617 0013335 270.9952 88.9811 16.24120762131382
| Epoch (UTC): | 21 May 2024 17:59:07 |
| Eccentricity: | 0.0013335 |
| inclination: | 97.3942° |
| perigee height: | 199 km |
| apogee height: | 217 km |
| right ascension of ascending node: | 227.5617° |
| argument of perigee: | 270.9952° |
| revolutions per day: | 16.24120762 |
| mean anomaly at epoch: | 88.9811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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