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 65341U 26145.55138352 +.00000000 +00000-0 +26853-3 0 00009
2 65341 53.1576 209.7958 0000947 86.7680 273.3430 15.30199152 01
| Epoch (UTC): | 25 May 2026 13:13:59 |
| Eccentricity: | 0.0000947 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.7958° |
| argument of perigee: | 86.7680° |
| revolutions per day: | 15.30199152 |
| mean anomaly at epoch: | 273.3430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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