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 65345U 26145.33925191 +.00000000 +00000-0 +32980-3 0 00002
2 65345 53.1571 210.6051 0000897 35.3855 324.7206 15.31710326 08
| Epoch (UTC): | 25 May 2026 08:08:31 |
| Eccentricity: | 0.0000897 |
| inclination: | 53.1571° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.6051° |
| argument of perigee: | 35.3855° |
| revolutions per day: | 15.31710326 |
| mean anomaly at epoch: | 324.7206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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