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 65325U 26145.56615433 +.00000000 +00000-0 +49558-3 0 00009
2 65325 53.1600 209.8960 0000846 78.9729 281.1367 15.30195805 07
| Epoch (UTC): | 25 May 2026 13:35:15 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1600° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.8960° |
| argument of perigee: | 78.9729° |
| revolutions per day: | 15.30195805 |
| mean anomaly at epoch: | 281.1367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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