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 57226U 26145.45796910 +.00000000 +00000-0 -62591-4 0 00002
2 57226 43.0063 317.3907 0001737 266.6234 93.4419 15.27558448 06
| Epoch (UTC): | 25 May 2026 10:59:28 |
| Eccentricity: | 0.0001737 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.3907° |
| argument of perigee: | 266.6234° |
| revolutions per day: | 15.27558448 |
| mean anomaly at epoch: | 93.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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