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 63406U 26145.37442894 +.00000000 +00000-0 +85604-3 0 00007
2 63406 43.0018 30.0506 0000807 271.4397 88.6362 15.27591159 07
| Epoch (UTC): | 25 May 2026 08:59:10 |
| Eccentricity: | 0.0000807 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.0506° |
| argument of perigee: | 271.4397° |
| revolutions per day: | 15.27591159 |
| mean anomaly at epoch: | 88.6362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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