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 03:53:54 |
| Eccentricity: | 0.0016986 |
| inclination: | 62.7823° |
| perigee height: | 545 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 75.8348° |
| argument of perigee: | 328.8332° |
| revolutions per day: | 15.03263302 |
| mean anomaly at epoch: | 31.1758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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