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 63771U 26145.54837784 +.00000000 +00000-0 +69131-3 0 00004
2 63771 43.0026 331.0422 0000352 290.8440 69.2374 15.27590305 01
| Epoch (UTC): | 25 May 2026 13:09:39 |
| Eccentricity: | 0.0000352 |
| inclination: | 43.0026° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 331.0422° |
| argument of perigee: | 290.8440° |
| revolutions per day: | 15.27590305 |
| mean anomaly at epoch: | 69.2374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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