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 62231U 26145.48560374 +.00000000 +00000-0 +62111-3 0 00006
2 62231 53.1592 223.1029 0001087 55.9022 304.2082 15.30213938 03
| Epoch (UTC): | 25 May 2026 11:39:16 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.1029° |
| argument of perigee: | 55.9022° |
| revolutions per day: | 15.30213938 |
| mean anomaly at epoch: | 304.2082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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