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 00:09:29 |
| Eccentricity: | 0.0004202 |
| inclination: | 97.3621° |
| perigee height: | 398 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 28.3789° |
| argument of perigee: | 191.3163° |
| revolutions per day: | 15.55458847 |
| mean anomaly at epoch: | 168.7997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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