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 19:12:24 |
| Eccentricity: | 0.0188814 |
| inclination: | 28.2455° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 186.5475° |
| argument of perigee: | 116.4304° |
| revolutions per day: | 13.53157884 |
| mean anomaly at epoch: | 245.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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