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 62863U 26145.34259161 +.00000000 +00000-0 +71109-3 0 00008
2 62863 53.1589 133.7343 0001224 88.5161 271.5980 15.30202810 04
| Epoch (UTC): | 25 May 2026 08:13:19 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.7343° |
| argument of perigee: | 88.5161° |
| revolutions per day: | 15.30202810 |
| mean anomaly at epoch: | 271.5980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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