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): | 15 January 2026 15:37:08 |
| Eccentricity: | 0.6665638 |
| inclination: | 6.7833° |
| perigee height: | 303 km |
| apogee height: | 27018 km |
| right ascension of ascending node: | 164.0966° |
| argument of perigee: | 173.9205° |
| revolutions per day: | 3.06055682 |
| mean anomaly at epoch: | 202.4581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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