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 65232U 26145.66244729 +.00000000 +00000-0 +10937-3 0 00002
2 65232 86.5001 21.1042 0001666 87.3777 272.7548 13.24411225 08
| Epoch (UTC): | 25 May 2026 15:53:55 |
| Eccentricity: | 0.0001666 |
| inclination: | 86.5001° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1042° |
| argument of perigee: | 87.3777° |
| revolutions per day: | 13.24411225 |
| mean anomaly at epoch: | 272.7548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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