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 65495U 26145.08121012 +.00000000 +00000-0 +47249-3 0 00004
2 65495 53.1591 276.3343 0001008 86.1365 273.9751 15.30203822 01
| Epoch (UTC): | 25 May 2026 01:56:56 |
| Eccentricity: | 0.0001008 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 276.3343° |
| argument of perigee: | 86.1365° |
| revolutions per day: | 15.30203822 |
| mean anomaly at epoch: | 273.9751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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