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): | 16 January 2026 05:56:05 |
| Eccentricity: | 0.0014886 |
| inclination: | 82.5211° |
| perigee height: | 612 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 272.1154° |
| argument of perigee: | 264.5451° |
| revolutions per day: | 14.82086529 |
| mean anomaly at epoch: | 95.4066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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