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 40424U 26145.36931720 +.00000000 +00000-0 +00000-0 0 00006
2 40424 0.0112 312.6708 0001900 67.8419 352.4193 1.00273196 08
| Epoch (UTC): | 25 May 2026 08:51:49 |
| Eccentricity: | 0.0001900 |
| inclination: | 0.0112° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 312.6708° |
| argument of perigee: | 67.8419° |
| revolutions per day: | 1.00273196 |
| mean anomaly at epoch: | 352.4193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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