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): | 16 January 2026 06:18:05 |
| Eccentricity: | 0.0031030 |
| inclination: | 82.9353° |
| perigee height: | 965 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 266.8864° |
| argument of perigee: | 313.9390° |
| revolutions per day: | 13.73145958 |
| mean anomaly at epoch: | 167.3236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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