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): | 23 June 2025 20:20:07 |
| Eccentricity: | 0.4654312 |
| inclination: | 34.3846° |
| perigee height: | 56995 km |
| apogee height: | 167350 km |
| right ascension of ascending node: | 12.5797° |
| argument of perigee: | 106.2819° |
| revolutions per day: | 0.21268519 |
| mean anomaly at epoch: | 358.6899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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