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 40186U 26137.42763068 +.00000000 +00000-0 +00000-0 0 00007
2 40186 25.7799 93.1765 7286376 240.0185 331.0659 1.88721897 08
| Epoch (UTC): | 17 May 2026 10:15:47 |
| Eccentricity: | 0.7286376 |
| inclination: | 25.7799° |
| perigee height: | 1128 km |
| apogee height: | 41436 km |
| right ascension of ascending node: | 93.1765° |
| argument of perigee: | 240.0185° |
| revolutions per day: | 1.88721897 |
| mean anomaly at epoch: | 331.0659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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