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 65220U 26145.31444766 +.00000000 +00000-0 +99116-3 0 00000
2 65220 53.1586 155.9942 0001214 87.0295 273.0847 15.34398372 05
| Epoch (UTC): | 25 May 2026 07:32:48 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.9942° |
| argument of perigee: | 87.0295° |
| revolutions per day: | 15.34398372 |
| mean anomaly at epoch: | 273.0847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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