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 65831U 26145.12065600 +.00000000 +00000-0 +81173-3 0 00007
2 65831 53.1607 92.7421 0000996 73.7391 286.3721 15.34398048 00
| Epoch (UTC): | 25 May 2026 02:53:44 |
| Eccentricity: | 0.0000996 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.7421° |
| argument of perigee: | 73.7391° |
| revolutions per day: | 15.34398048 |
| mean anomaly at epoch: | 286.3721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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