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 65411U 26145.51276993 +.00000000 +00000-0 +63078-3 0 00007
2 65411 53.1586 234.9875 0001475 87.0513 273.0657 15.31723976 00
| Epoch (UTC): | 25 May 2026 12:18:23 |
| Eccentricity: | 0.0001475 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 234.9875° |
| argument of perigee: | 87.0513° |
| revolutions per day: | 15.31723976 |
| mean anomaly at epoch: | 273.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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