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 63325U 26145.51567538 +.00000000 +00000-0 +84469-3 0 00004
2 63325 43.0027 317.2625 0000744 278.9907 81.0861 15.27598083 02
| Epoch (UTC): | 25 May 2026 12:22:34 |
| Eccentricity: | 0.0000744 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.2625° |
| argument of perigee: | 278.9907° |
| revolutions per day: | 15.27598083 |
| mean anomaly at epoch: | 81.0861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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