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 63682U 26145.49002161 +.00000000 +00000-0 +69848-3 0 00007
2 63682 42.9979 317.3501 0002762 281.5618 78.4923 15.27592388 08
| Epoch (UTC): | 25 May 2026 11:45:37 |
| Eccentricity: | 0.0002762 |
| inclination: | 42.9979° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 317.3501° |
| argument of perigee: | 281.5618° |
| revolutions per day: | 15.27592388 |
| mean anomaly at epoch: | 78.4923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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