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 62225U 26145.53359113 +.00000000 +00000-0 +13882-2 0 00002
2 62225 53.1565 82.2473 0001505 69.9564 290.1616 15.69782162 02
| Epoch (UTC): | 25 May 2026 12:48:22 |
| Eccentricity: | 0.0001505 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 82.2473° |
| argument of perigee: | 69.9564° |
| revolutions per day: | 15.69782162 |
| mean anomaly at epoch: | 290.1616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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