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 23191U 94046A 24143.02786439 .18726165 43003-5 37353-3 0 9997
2 23191 69.8337 212.9228 0016708 210.6795 213.0509 16.45617662487487
| Epoch (UTC): | 22 May 2024 00:40:07 |
| Eccentricity: | 0.0016708 |
| inclination: | 69.8337° |
| perigee height: | 140 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 212.9228° |
| argument of perigee: | 210.6795° |
| revolutions per day: | 16.45617662 |
| mean anomaly at epoch: | 213.0509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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