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 65508U 26145.60111219 +.00000000 +00000-0 +17328-3 0 00000
2 65508 53.1593 273.1821 0001116 83.5932 276.5198 15.34393348 06
| Epoch (UTC): | 25 May 2026 14:25:36 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.1821° |
| argument of perigee: | 83.5932° |
| revolutions per day: | 15.34393348 |
| mean anomaly at epoch: | 276.5198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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