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 40374U 26140.58994198 +.00000000 +00000-0 +00000-0 0 00007
2 40374 4.4687 43.3969 0051040 179.4752 212.2735 1.00273172 03
| Epoch (UTC): | 20 May 2026 14:09:30 |
| Eccentricity: | 0.0051040 |
| inclination: | 4.4687° |
| perigee height: | 35571 km |
| apogee height: | 36001 km |
| right ascension of ascending node: | 43.3969° |
| argument of perigee: | 179.4752° |
| revolutions per day: | 1.00273172 |
| mean anomaly at epoch: | 212.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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