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): | 12 January 2026 06:47:34 |
| Eccentricity: | 0.0008111 |
| inclination: | 53.2311° |
| perigee height: | 452 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 44.8511° |
| argument of perigee: | 59.7575° |
| revolutions per day: | 15.36272397 |
| mean anomaly at epoch: | 300.4231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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