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 65493U 26144.82781691 +.00000000 +00000-0 +84058-3 0 00007
2 65493 53.1602 276.1816 0001268 86.3941 273.7207 15.34386064 03
| Epoch (UTC): | 24 May 2026 19:52:03 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 276.1816° |
| argument of perigee: | 86.3941° |
| revolutions per day: | 15.34386064 |
| mean anomaly at epoch: | 273.7207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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