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,
| Epoch (UTC): | 12 September 2023 15:20:31 |
| Eccentricity: | 0.0006472 |
| inclination: | 97.2621° |
| perigee height: | 226 km |
| apogee height: | 235 km |
| right ascension of ascending node: | 258.2074° |
| argument of perigee: | 205.1820° |
| revolutions per day: | 16.16004275 |
| mean anomaly at epoch: | 154.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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