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 57332U 26145.49432605 +.00000000 +00000-0 +29993-4 0 00000
2 57332 43.0021 178.5691 0001519 271.0703 88.9975 15.27577916 01
| Epoch (UTC): | 25 May 2026 11:51:49 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.5691° |
| argument of perigee: | 271.0703° |
| revolutions per day: | 15.27577916 |
| mean anomaly at epoch: | 88.9975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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