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): | 13 January 2026 21:17:27 |
| Eccentricity: | 0.6966659 |
| inclination: | 27.9834° |
| perigee height: | 310 km |
| apogee height: | 31031 km |
| right ascension of ascending node: | 193.3854° |
| argument of perigee: | 168.4178° |
| revolutions per day: | 2.65175640 |
| mean anomaly at epoch: | 225.2283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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