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 57780U 26145.42726301 +.00000000 +00000-0 +38574-4 0 00004
2 57780 43.0022 121.0337 0001182 272.2852 87.7865 15.27580541 06
| Epoch (UTC): | 25 May 2026 10:15:15 |
| Eccentricity: | 0.0001182 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.0337° |
| argument of perigee: | 272.2852° |
| revolutions per day: | 15.27580541 |
| mean anomaly at epoch: | 87.7865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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