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 63395U 26145.43850275 +.00000000 +00000-0 +43042-3 0 00007
2 63395 97.6886 39.3227 0005087 114.0626 246.1130 14.99804364 03
| Epoch (UTC): | 25 May 2026 10:31:26 |
| Eccentricity: | 0.0005087 |
| inclination: | 97.6886° |
| perigee height: | 564 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 39.3227° |
| argument of perigee: | 114.0626° |
| revolutions per day: | 14.99804364 |
| mean anomaly at epoch: | 246.1130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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