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 65582U 26145.38357427 +.00000000 +00000-0 +18360-3 0 00007
2 65582 81.3064 31.8883 0007040 252.1675 107.8714 13.83941740 08
| Epoch (UTC): | 25 May 2026 09:12:20 |
| Eccentricity: | 0.0007040 |
| inclination: | 81.3064° |
| perigee height: | 945 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 31.8883° |
| argument of perigee: | 252.1675° |
| revolutions per day: | 13.83941740 |
| mean anomaly at epoch: | 107.8714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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