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 57911U 26145.55198619 +.00000000 +00000-0 +51670-4 0 00001
2 57911 43.0013 239.9201 0001728 275.9559 84.1095 15.27571716 01
| Epoch (UTC): | 25 May 2026 13:14:51 |
| Eccentricity: | 0.0001728 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9201° |
| argument of perigee: | 275.9559° |
| revolutions per day: | 15.27571716 |
| mean anomaly at epoch: | 84.1095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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