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 57716U 26145.42014539 +.00000000 +00000-0 +10602-3 0 00007
2 57716 43.0019 44.8935 0001205 276.1886 83.8829 15.27573289 01
| Epoch (UTC): | 25 May 2026 10:05:00 |
| Eccentricity: | 0.0001205 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.8935° |
| argument of perigee: | 276.1886° |
| revolutions per day: | 15.27573289 |
| mean anomaly at epoch: | 83.8829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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