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): | 12 January 2026 11:53:46 |
| Eccentricity: | 0.5328802 |
| inclination: | 49.4023° |
| perigee height: | 330 km |
| apogee height: | 15636 km |
| right ascension of ascending node: | 194.2265° |
| argument of perigee: | 173.9968° |
| revolutions per day: | 5.04427444 |
| mean anomaly at epoch: | 196.7424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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