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 63776U 26145.55139735 +.00000000 +00000-0 +41838-3 0 00005
2 63776 42.9991 338.7645 0001027 277.7894 82.2841 15.27591423 09
| Epoch (UTC): | 25 May 2026 13:14:00 |
| Eccentricity: | 0.0001027 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.7645° |
| argument of perigee: | 277.7894° |
| revolutions per day: | 15.27591423 |
| mean anomaly at epoch: | 82.2841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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