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 15:21:06 |
| Eccentricity: | 0.0014870 |
| inclination: | 82.5213° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 272.6833° |
| argument of perigee: | 266.7668° |
| revolutions per day: | 14.82085932 |
| mean anomaly at epoch: | 93.1845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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