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 63855U 26145.32762948 +.00000000 +00000-0 +34293-3 0 00003
2 63855 42.9987 5.0112 0000291 82.0071 278.0814 15.27589806 08
| Epoch (UTC): | 25 May 2026 07:51:47 |
| Eccentricity: | 0.0000291 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 5.0112° |
| argument of perigee: | 82.0071° |
| revolutions per day: | 15.27589806 |
| mean anomaly at epoch: | 278.0814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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