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 63365U 26145.45601351 +.00000000 +00000-0 +64846-3 0 00000
2 63365 53.1605 53.6973 0001227 88.6691 271.4453 15.35425140 04
| Epoch (UTC): | 25 May 2026 10:56:39 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.1605° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 53.6973° |
| argument of perigee: | 88.6691° |
| revolutions per day: | 15.35425140 |
| mean anomaly at epoch: | 271.4453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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