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 40080U 26142.66583565 +.00000000 +00000-0 +00000-0 0 00004
2 40080 0.0504 346.1892 0004018 52.7384 321.1003 5.00115771 05
| Epoch (UTC): | 22 May 2026 15:58:48 |
| Eccentricity: | 0.0004018 |
| inclination: | 0.0504° |
| perigee height: | 8060 km |
| apogee height: | 8072 km |
| right ascension of ascending node: | 346.1892° |
| argument of perigee: | 52.7384° |
| revolutions per day: | 5.00115771 |
| mean anomaly at epoch: | 321.1003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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