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 32956U 26145.63565314 +.00000000 +00000-0 -24666-3 0 00007
2 32956 82.5093 11.8162 0021263 6.8621 353.2746 12.43069542 06
| Epoch (UTC): | 25 May 2026 15:15:20 |
| Eccentricity: | 0.0021263 |
| inclination: | 82.5093° |
| perigee height: | 1477 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 11.8162° |
| argument of perigee: | 6.8621° |
| revolutions per day: | 12.43069542 |
| mean anomaly at epoch: | 353.2746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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