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,
1 32052U 26106.64948862 +.00000000 +00000-0 +89089-5 0 00006
2 32052 82.9786 251.2280 0039313 48.8032 311.6503 13.75161949 03
| Epoch (UTC): | 16 April 2026 15:35:15 |
| Eccentricity: | 0.0039313 |
| inclination: | 82.9786° |
| perigee height: | 952 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 251.2280° |
| argument of perigee: | 48.8032° |
| revolutions per day: | 13.75161949 |
| mean anomaly at epoch: | 311.6503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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