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 05:42:21 |
| Eccentricity: | 0.0036340 |
| inclination: | 71.1064° |
| perigee height: | 793 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 198.5396° |
| argument of perigee: | 210.3991° |
| revolutions per day: | 14.21962499 |
| mean anomaly at epoch: | 322.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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