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 63961U 26145.37183645 +.00000000 +00000-0 +46615-3 0 00008
2 63961 42.9981 103.1762 0001128 266.8483 93.2239 15.27589703 04
| Epoch (UTC): | 25 May 2026 08:55:26 |
| Eccentricity: | 0.0001128 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1762° |
| argument of perigee: | 266.8483° |
| revolutions per day: | 15.27589703 |
| mean anomaly at epoch: | 93.2239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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