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 57476U 26145.34284882 +.00000000 +00000-0 +55722-4 0 00004
2 57476 43.0027 262.9103 0001612 270.3397 89.7270 15.27574554 09
| Epoch (UTC): | 25 May 2026 08:13:42 |
| Eccentricity: | 0.0001612 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.9103° |
| argument of perigee: | 270.3397° |
| revolutions per day: | 15.27574554 |
| mean anomaly at epoch: | 89.7270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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