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 42818U 26145.40235705 +.00000000 +00000-0 +00000-0 0 00000
2 42818 0.0177 317.5716 0002260 105.1717 290.6102 1.00269983 00
| Epoch (UTC): | 25 May 2026 09:39:23 |
| Eccentricity: | 0.0002260 |
| inclination: | 0.0177° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 317.5716° |
| argument of perigee: | 105.1717° |
| revolutions per day: | 1.00269983 |
| mean anomaly at epoch: | 290.6102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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