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 57254U 26145.45667299 +.00000000 +00000-0 +27212-4 0 00000
2 57254 43.0017 306.0760 0001207 257.4830 102.5887 15.27577056 07
| Epoch (UTC): | 25 May 2026 10:57:36 |
| Eccentricity: | 0.0001207 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.0760° |
| argument of perigee: | 257.4830° |
| revolutions per day: | 15.27577056 |
| mean anomaly at epoch: | 102.5887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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