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 65086U 26144.97043375 +.00000000 +00000-0 +60656-3 0 00009
2 65086 53.1591 32.7131 0001352 94.2630 265.8525 15.30190010 06
| Epoch (UTC): | 24 May 2026 23:17:25 |
| Eccentricity: | 0.0001352 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 32.7131° |
| argument of perigee: | 94.2630° |
| revolutions per day: | 15.30190010 |
| mean anomaly at epoch: | 265.8525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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