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 56371U 26145.52683845 +.00000000 +00000-0 +00000-0 0 00004
2 56371 2.7178 80.2121 0001812 31.5954 33.4616 1.00270930 07
| Epoch (UTC): | 25 May 2026 12:38:38 |
| Eccentricity: | 0.0001812 |
| inclination: | 2.7178° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 80.2121° |
| argument of perigee: | 31.5954° |
| revolutions per day: | 1.00270930 |
| mean anomaly at epoch: | 33.4616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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