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 65631U 26145.61079813 +.00000000 +00000-0 +38602-3 0 00009
2 65631 53.1583 308.6848 0001062 85.6632 274.4491 15.34398555 03
| Epoch (UTC): | 25 May 2026 14:39:32 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 308.6848° |
| argument of perigee: | 85.6632° |
| revolutions per day: | 15.34398555 |
| mean anomaly at epoch: | 274.4491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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