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 data is extracted from the following two-line orbital elements,
1 40186U 11077K 25138.44516074 .00000070 00000-0 00000-0 0 9992
2 40186 24.8466 185.5865 7359285 84.4433 0.8718 1.88712866 91667
| Epoch (UTC): | 18 May 2025 10:41:01 |
| Eccentricity: | 0.7359285 |
| inclination: | 24.8466° |
| perigee height: | 926 km |
| apogee height: | 41639 km |
| right ascension of ascending node: | 185.5865° |
| argument of perigee: | 84.4433° |
| revolutions per day: | 1.88712866 |
| mean anomaly at epoch: | 0.8718° |
| orbit number at epoch: | 9166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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