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 57829U 26145.53889264 +.00000000 +00000-0 +10626-3 0 00005
2 57829 43.0006 159.9836 0001181 275.5675 84.5042 15.27572981 05
| Epoch (UTC): | 25 May 2026 12:56:00 |
| Eccentricity: | 0.0001181 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 159.9836° |
| argument of perigee: | 275.5675° |
| revolutions per day: | 15.27572981 |
| mean anomaly at epoch: | 84.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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