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 05:02:54 |
| Eccentricity: | 0.0606480 |
| inclination: | 82.9581° |
| perigee height: | 367 km |
| apogee height: | 1238 km |
| right ascension of ascending node: | 64.1544° |
| argument of perigee: | 120.2654° |
| revolutions per day: | 14.26678152 |
| mean anomaly at epoch: | 245.9992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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