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 04:14:27 |
| Eccentricity: | 0.0018130 |
| inclination: | 82.5142° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 255.5571° |
| argument of perigee: | 22.1541° |
| revolutions per day: | 14.85298501 |
| mean anomaly at epoch: | 93.7546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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