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 17:03:00 |
| Eccentricity: | 0.0218266 |
| inclination: | 82.5198° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 81.0359° |
| argument of perigee: | 140.7046° |
| revolutions per day: | 12.79746501 |
| mean anomaly at epoch: | 221.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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