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 65859U 26145.41687183 +.00000000 +00000-0 +91523-3 0 00005
2 65859 53.1605 297.7385 0000968 101.3040 258.8071 15.34414323 09
| Epoch (UTC): | 25 May 2026 10:00:17 |
| Eccentricity: | 0.0000968 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 297.7385° |
| argument of perigee: | 101.3040° |
| revolutions per day: | 15.34414323 |
| mean anomaly at epoch: | 258.8071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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