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 63580U 26145.54860421 +.00000000 +00000-0 +61053-3 0 00001
2 63580 42.9999 247.7540 0001128 270.8798 89.1924 15.27593375 08
| Epoch (UTC): | 25 May 2026 13:09:59 |
| Eccentricity: | 0.0001128 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.7540° |
| argument of perigee: | 270.8798° |
| revolutions per day: | 15.27593375 |
| mean anomaly at epoch: | 89.1924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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