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 63495U 26145.37938509 +.00000000 +00000-0 +41217-3 0 00000
2 63495 53.1584 143.5522 0001251 87.9580 272.1564 15.30207350 06
| Epoch (UTC): | 25 May 2026 09:06:18 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5522° |
| argument of perigee: | 87.9580° |
| revolutions per day: | 15.30207350 |
| mean anomaly at epoch: | 272.1564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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