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 63327U 26145.50750292 +.00000000 +00000-0 +61362-3 0 00003
2 63327 43.0012 309.4197 0001279 267.8345 92.2360 15.27590493 07
| Epoch (UTC): | 25 May 2026 12:10:48 |
| Eccentricity: | 0.0001279 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.4197° |
| argument of perigee: | 267.8345° |
| revolutions per day: | 15.27590493 |
| mean anomaly at epoch: | 92.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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