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 18313U 26105.43315644 +.00000000 +00000-0 +19058-4 0 00000
2 18313 82.5607 351.7079 0008761 247.1850 112.8385 13.84304816 03
| Epoch (UTC): | 15 April 2026 10:23:44 |
| Eccentricity: | 0.0008761 |
| inclination: | 82.5607° |
| perigee height: | 942 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 351.7079° |
| argument of perigee: | 247.1850° |
| revolutions per day: | 13.84304816 |
| mean anomaly at epoch: | 112.8385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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