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 63255U 26145.67257145 +.00000000 +00000-0 +10699-3 0 00007
2 63255 97.6919 37.9994 0000711 346.7062 13.4140 14.95194010 09
| Epoch (UTC): | 25 May 2026 16:08:30 |
| Eccentricity: | 0.0000711 |
| inclination: | 97.6919° |
| perigee height: | 581 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 37.9994° |
| argument of perigee: | 346.7062° |
| revolutions per day: | 14.95194010 |
| mean anomaly at epoch: | 13.4140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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