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 03:59:40 |
| Eccentricity: | 0.0001226 |
| inclination: | 97.8843° |
| perigee height: | 578 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 205.7923° |
| argument of perigee: | 74.8462° |
| revolutions per day: | 14.96050391 |
| mean anomaly at epoch: | 285.2894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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