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): | 24 June 2025 15:28:47 |
| Eccentricity: | 0.4787562 |
| inclination: | 41.1455° |
| perigee height: | 55213 km |
| apogee height: | 168354 km |
| right ascension of ascending node: | 10.1728° |
| argument of perigee: | 78.3758° |
| revolutions per day: | 0.21373703 |
| mean anomaly at epoch: | 359.6018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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