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 57814U 26145.32873294 +.00000000 +00000-0 -11619-4 0 00007
2 57814 43.0008 161.8474 0001326 271.3214 88.7486 15.27585208 09
| Epoch (UTC): | 25 May 2026 07:53:22 |
| Eccentricity: | 0.0001326 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.8474° |
| argument of perigee: | 271.3214° |
| revolutions per day: | 15.27585208 |
| mean anomaly at epoch: | 88.7486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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