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): | 14 January 2026 05:09:31 |
| Eccentricity: | 0.0010364 |
| inclination: | 82.4687° |
| perigee height: | 527 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 101.0856° |
| argument of perigee: | 156.4625° |
| revolutions per day: | 15.10806754 |
| mean anomaly at epoch: | 203.7081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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