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 41844U 16066D 23312.33604464 .16428040 26725-5 21414-3 0 9998
2 41844 97.3344 339.0456 0008282 230.7301 129.3269 16.49213338390294
| Epoch (UTC): | 08 November 2023 08:03:54 |
| Eccentricity: | 0.0008282 |
| inclination: | 97.3344° |
| perigee height: | 136 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 339.0456° |
| argument of perigee: | 230.7301° |
| revolutions per day: | 16.49213338 |
| mean anomaly at epoch: | 129.3269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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