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 65310U 26145.63368606 +.00000000 +00000-0 +33482-4 0 00008
2 65310 50.0116 286.6745 0000606 98.6760 261.4181 13.29321980 07
| Epoch (UTC): | 25 May 2026 15:12:30 |
| Eccentricity: | 0.0000606 |
| inclination: | 50.0116° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.6745° |
| argument of perigee: | 98.6760° |
| revolutions per day: | 13.29321980 |
| mean anomaly at epoch: | 261.4181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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