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 65825U 26145.13538289 +.00000000 +00000-0 +85814-3 0 00005
2 65825 53.1590 92.8343 0001230 89.2213 270.8931 15.34406907 00
| Epoch (UTC): | 25 May 2026 03:14:57 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 92.8343° |
| argument of perigee: | 89.2213° |
| revolutions per day: | 15.34406907 |
| mean anomaly at epoch: | 270.8931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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