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 14:32:53 |
| Eccentricity: | 0.0031481 |
| inclination: | 98.8164° |
| perigee height: | 747 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 30.1526° |
| argument of perigee: | 215.0077° |
| revolutions per day: | 14.36753601 |
| mean anomaly at epoch: | 144.9039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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