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 62855U 26145.23295183 +.00000000 +00000-0 +90983-3 0 00002
2 62855 53.1594 133.7519 0002222 94.3320 265.7934 15.30226107 06
| Epoch (UTC): | 25 May 2026 05:35:27 |
| Eccentricity: | 0.0002222 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 133.7519° |
| argument of perigee: | 94.3320° |
| revolutions per day: | 15.30226107 |
| mean anomaly at epoch: | 265.7934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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