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 62224U 26145.25448627 +.00000000 +00000-0 +11705-2 0 00001
2 62224 53.1568 84.0775 0001094 92.7758 267.3385 15.69765560 03
| Epoch (UTC): | 25 May 2026 06:06:27 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 84.0775° |
| argument of perigee: | 92.7758° |
| revolutions per day: | 15.69765560 |
| mean anomaly at epoch: | 267.3385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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