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 57477U 26145.01976825 +.00000000 +00000-0 +38696-3 0 00004
2 57477 43.0008 264.7815 0001721 267.8347 92.2308 15.27588313 05
| Epoch (UTC): | 25 May 2026 00:28:27 |
| Eccentricity: | 0.0001721 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 264.7815° |
| argument of perigee: | 267.8347° |
| revolutions per day: | 15.27588313 |
| mean anomaly at epoch: | 92.2308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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