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 65634U 26145.46577795 +.00000000 +00000-0 +82913-3 0 00001
2 65634 53.1594 310.6126 0001513 91.9539 268.1636 15.30212279 02
| Epoch (UTC): | 25 May 2026 11:10:43 |
| Eccentricity: | 0.0001513 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6126° |
| argument of perigee: | 91.9539° |
| revolutions per day: | 15.30212279 |
| mean anomaly at epoch: | 268.1636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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