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): | 13 January 2026 12:38:53 |
| Eccentricity: | 0.0005395 |
| inclination: | 98.4073° |
| perigee height: | 685 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 278.6303° |
| argument of perigee: | 1.9272° |
| revolutions per day: | 14.61371260 |
| mean anomaly at epoch: | 358.1949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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