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 00:18:56 |
| Eccentricity: | 0.0005676 |
| inclination: | 70.9398° |
| perigee height: | 845 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 316.0207° |
| argument of perigee: | 339.0159° |
| revolutions per day: | 14.12910074 |
| mean anomaly at epoch: | 21.0728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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