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 19:23:02 |
| Eccentricity: | 0.0033178 |
| inclination: | 82.9441° |
| perigee height: | 952 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 282.7110° |
| argument of perigee: | 342.0094° |
| revolutions per day: | 13.76595922 |
| mean anomaly at epoch: | 17.9886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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