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 06:33:14 |
| Eccentricity: | 0.0007763 |
| inclination: | 51.6333° |
| perigee height: | 413 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 336.4632° |
| argument of perigee: | 20.7339° |
| revolutions per day: | 15.49304898 |
| mean anomaly at epoch: | 339.3964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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