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 62569U 26145.21891027 +.00000000 +00000-0 +85692-3 0 00002
2 62569 43.0002 220.6529 0001488 274.9401 85.1280 15.27597519 08
| Epoch (UTC): | 25 May 2026 05:15:13 |
| Eccentricity: | 0.0001488 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 220.6529° |
| argument of perigee: | 274.9401° |
| revolutions per day: | 15.27597519 |
| mean anomaly at epoch: | 85.1280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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