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 41332U 16009A 23180.88490118 .09259703 24311-5 33772-3 0 9998
2 41332 97.1856 267.0062 0014944 268.6625 91.2964 16.42740294414628
| Epoch (UTC): | 29 June 2023 21:14:15 |
| Eccentricity: | 0.0014944 |
| inclination: | 97.1856° |
| perigee height: | 149 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 267.0062° |
| argument of perigee: | 268.6625° |
| revolutions per day: | 16.42740294 |
| mean anomaly at epoch: | 91.2964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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