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 41874U 16062F 23114.55433276 .12197930 12307-4 16020-2 0 9995
2 41874 51.6210 259.1691 0008863 292.1780 67.8303 16.34669829358106
| Epoch (UTC): | 24 April 2023 13:18:14 |
| Eccentricity: | 0.0008863 |
| inclination: | 51.6210° |
| perigee height: | 174 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 259.1691° |
| argument of perigee: | 292.1780° |
| revolutions per day: | 16.34669829 |
| mean anomaly at epoch: | 67.8303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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