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 65834U 26145.26760302 +.00000000 +00000-0 +77687-3 0 00001
2 65834 53.1583 92.9433 0001116 88.0446 272.0683 15.30228143 09
| Epoch (UTC): | 25 May 2026 06:25:20 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 92.9433° |
| argument of perigee: | 88.0446° |
| revolutions per day: | 15.30228143 |
| mean anomaly at epoch: | 272.0683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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