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 55131U 26145.80054603 +.00000000 +00000-0 +00000-0 0 00002
2 55131 3.6623 78.5887 0004180 274.9945 340.7496 1.00090820 06
| Epoch (UTC): | 25 May 2026 19:12:47 |
| Eccentricity: | 0.0004180 |
| inclination: | 3.6623° |
| perigee height: | 35820 km |
| apogee height: | 35855 km |
| right ascension of ascending node: | 78.5887° |
| argument of perigee: | 274.9945° |
| revolutions per day: | 1.00090820 |
| mean anomaly at epoch: | 340.7496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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