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 65347U 26145.46008501 +.00000000 +00000-0 +52539-3 0 00007
2 65347 53.1584 209.9431 0001065 85.3849 274.7274 15.31705099 03
| Epoch (UTC): | 25 May 2026 11:02:31 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.9431° |
| argument of perigee: | 85.3849° |
| revolutions per day: | 15.31705099 |
| mean anomaly at epoch: | 274.7274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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