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): | 14 January 2026 01:23:57 |
| Eccentricity: | 0.0099403 |
| inclination: | 51.6066° |
| perigee height: | 386 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 243.4353° |
| argument of perigee: | 263.4676° |
| revolutions per day: | 15.37506630 |
| mean anomaly at epoch: | 95.4983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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