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 02:52:23 |
| Eccentricity: | 0.0025423 |
| inclination: | 81.1462° |
| perigee height: | 476 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 257.4830° |
| argument of perigee: | 353.5807° |
| revolutions per day: | 15.24025532 |
| mean anomaly at epoch: | 6.5096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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