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 62565U 26145.39571412 +.00000000 +00000-0 +17696-2 0 00008
2 62565 43.0011 37.7672 0001224 289.7949 70.2786 15.70904999 07
| Epoch (UTC): | 25 May 2026 09:29:49 |
| Eccentricity: | 0.0001224 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 37.7672° |
| argument of perigee: | 289.7949° |
| revolutions per day: | 15.70904999 |
| mean anomaly at epoch: | 70.2786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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