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 65622U 26144.94009500 +.00000000 +00000-0 +62107-3 0 00007
2 65622 53.1594 313.0307 0000828 79.2565 280.8529 15.30206750 02
| Epoch (UTC): | 24 May 2026 22:33:44 |
| Eccentricity: | 0.0000828 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0307° |
| argument of perigee: | 79.2565° |
| revolutions per day: | 15.30206750 |
| mean anomaly at epoch: | 280.8529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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