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 65643U 26145.47000223 +.00000000 +00000-0 +11102-2 0 00000
2 65643 53.1591 309.2237 0000834 51.8568 308.2510 15.34423385 01
| Epoch (UTC): | 25 May 2026 11:16:48 |
| Eccentricity: | 0.0000834 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.2237° |
| argument of perigee: | 51.8568° |
| revolutions per day: | 15.34423385 |
| mean anomaly at epoch: | 308.2510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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