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 57080U 26145.04081091 +.00000000 +00000-0 +13801-4 0 00001
2 57080 43.0058 25.2462 0001031 266.5006 93.5728 15.27575993 00
| Epoch (UTC): | 25 May 2026 00:58:46 |
| Eccentricity: | 0.0001031 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.2462° |
| argument of perigee: | 266.5006° |
| revolutions per day: | 15.27575993 |
| mean anomaly at epoch: | 93.5728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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