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 57225U 26144.88360249 +.00000000 +00000-0 +21646-4 0 00004
2 57225 43.0056 320.8194 0001595 271.3941 88.6728 15.27577552 00
| Epoch (UTC): | 24 May 2026 21:12:23 |
| Eccentricity: | 0.0001595 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.8194° |
| argument of perigee: | 271.3941° |
| revolutions per day: | 15.27577552 |
| mean anomaly at epoch: | 88.6728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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