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 65580U 26145.43543544 +.00000000 +00000-0 +78166-4 0 00009
2 65580 81.3054 31.9393 0006413 252.8411 107.2044 13.83148067 01
| Epoch (UTC): | 25 May 2026 10:27:01 |
| Eccentricity: | 0.0006413 |
| inclination: | 81.3054° |
| perigee height: | 948 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 31.9393° |
| argument of perigee: | 252.8411° |
| revolutions per day: | 13.83148067 |
| mean anomaly at epoch: | 107.2044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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