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 65222U 26145.58335647 +.00000000 +00000-0 +29213-3 0 00009
2 65222 53.1595 155.2613 0001017 68.4973 70.3678 15.34385433 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.2613° |
| argument of perigee: | 68.4973° |
| revolutions per day: | 15.34385433 |
| mean anomaly at epoch: | 70.3678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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