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 65051U 26145.62065536 +.00000000 +00000-0 +82722-4 0 00006
2 65051 50.0053 346.3980 0000476 45.3471 314.7440 13.29324041 08
| Epoch (UTC): | 25 May 2026 14:53:44 |
| Eccentricity: | 0.0000476 |
| inclination: | 50.0053° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.3980° |
| argument of perigee: | 45.3471° |
| revolutions per day: | 13.29324041 |
| mean anomaly at epoch: | 314.7440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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