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 03:03:24 |
| Eccentricity: | 0.0011500 |
| inclination: | 41.4654° |
| perigee height: | 378 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 192.0458° |
| argument of perigee: | 268.5283° |
| revolutions per day: | 15.60438906 |
| mean anomaly at epoch: | 91.4238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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