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 63564U 26145.41127788 +.00000000 +00000-0 +50739-3 0 00000
2 63564 43.0010 197.1213 0001422 267.3170 92.7519 15.27612138 02
| Epoch (UTC): | 25 May 2026 09:52:14 |
| Eccentricity: | 0.0001422 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.1213° |
| argument of perigee: | 267.3170° |
| revolutions per day: | 15.27612138 |
| mean anomaly at epoch: | 92.7519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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