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): | 11 January 2026 04:44:03 |
| Eccentricity: | 0.0113890 |
| inclination: | 69.9603° |
| perigee height: | 905 km |
| apogee height: | 1073 km |
| right ascension of ascending node: | 191.2361° |
| argument of perigee: | 155.9686° |
| revolutions per day: | 13.72881222 |
| mean anomaly at epoch: | 204.6783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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