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 05:46:24 |
| Eccentricity: | 0.0010944 |
| inclination: | 82.5557° |
| perigee height: | 941 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 62.4706° |
| argument of perigee: | 135.1355° |
| revolutions per day: | 13.84299894 |
| mean anomaly at epoch: | 225.0692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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