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 13:23:46 |
| Eccentricity: | 0.0503587 |
| inclination: | 51.7613° |
| perigee height: | 490 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 153.4350° |
| argument of perigee: | 191.4652° |
| revolutions per day: | 14.11553653 |
| mean anomaly at epoch: | 167.4450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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