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 40928U 15051D 22363.79982108 .09201092 21690-5 85924-3 0 9992
2 40928 96.9993 28.5009 0003467 313.2323 142.4476 16.38834510408965
| Epoch (UTC): | 29 December 2022 19:11:44 |
| Eccentricity: | 0.0003467 |
| inclination: | 96.9993° |
| perigee height: | 166 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 28.5009° |
| argument of perigee: | 313.2323° |
| revolutions per day: | 16.38834510 |
| mean anomaly at epoch: | 142.4476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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