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): | 14 January 2026 20:38:50 |
| Eccentricity: | 0.0023421 |
| inclination: | 98.8136° |
| perigee height: | 845 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 359.4398° |
| argument of perigee: | 206.6546° |
| revolutions per day: | 14.09148237 |
| mean anomaly at epoch: | 214.3450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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