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 65641U 26145.47841802 +.00000000 +00000-0 +11746-2 0 00008
2 65641 53.1595 309.2791 0001538 91.5479 268.5700 15.34423376 01
| Epoch (UTC): | 25 May 2026 11:28:55 |
| Eccentricity: | 0.0001538 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.2791° |
| argument of perigee: | 91.5479° |
| revolutions per day: | 15.34423376 |
| mean anomaly at epoch: | 268.5700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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