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 63563U 26145.42797370 +.00000000 +00000-0 +42922-3 0 00005
2 63563 43.0000 197.2443 0001772 276.3124 83.7526 15.27588958 03
| Epoch (UTC): | 25 May 2026 10:16:16 |
| Eccentricity: | 0.0001772 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.2443° |
| argument of perigee: | 276.3124° |
| revolutions per day: | 15.27588958 |
| mean anomaly at epoch: | 83.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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