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 63502U 26145.38044212 +.00000000 +00000-0 +18742-3 0 00006
2 63502 53.1588 143.5548 0001031 97.2789 262.8329 15.30188265 06
| Epoch (UTC): | 25 May 2026 09:07:50 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5548° |
| argument of perigee: | 97.2789° |
| revolutions per day: | 15.30188265 |
| mean anomaly at epoch: | 262.8329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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