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 57791U 26145.43111719 +.00000000 +00000-0 -16283-4 0 00002
2 57791 43.0049 121.0670 0001252 283.3371 76.7341 15.27572507 04
| Epoch (UTC): | 25 May 2026 10:20:48 |
| Eccentricity: | 0.0001252 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.0670° |
| argument of perigee: | 283.3371° |
| revolutions per day: | 15.27572507 |
| mean anomaly at epoch: | 76.7341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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