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 57892U 26145.28401395 +.00000000 +00000-0 +45721-4 0 00007
2 57892 43.0035 241.3632 0001167 270.9856 89.0862 15.27579115 07
| Epoch (UTC): | 25 May 2026 06:48:58 |
| Eccentricity: | 0.0001167 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.3632° |
| argument of perigee: | 270.9856° |
| revolutions per day: | 15.27579115 |
| mean anomaly at epoch: | 89.0862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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