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 57424U 26145.63894932 +.00000000 +00000-0 +29686-3 0 00001
2 57424 97.2708 214.2077 0007555 183.3491 176.7703 15.34458107 00
| Epoch (UTC): | 25 May 2026 15:20:05 |
| Eccentricity: | 0.0007555 |
| inclination: | 97.2708° |
| perigee height: | 457 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 214.2077° |
| argument of perigee: | 183.3491° |
| revolutions per day: | 15.34458107 |
| mean anomaly at epoch: | 176.7703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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