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 13:49:06 |
| Eccentricity: | 0.0001363 |
| inclination: | 98.1294° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 23.8279° |
| argument of perigee: | 94.1307° |
| revolutions per day: | 14.63393490 |
| mean anomaly at epoch: | 266.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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