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 23344.30136167 .00000020 00000-0 00000-0 0 9990
2 40186 26.1910 317.6103 7312342 222.6909 350.7767 1.88728078 81747
| Epoch (UTC): | 10 December 2023 07:13:57 |
| Eccentricity: | 0.7312342 |
| inclination: | 26.1910° |
| perigee height: | 1056 km |
| apogee height: | 41506 km |
| right ascension of ascending node: | 317.6103° |
| argument of perigee: | 222.6909° |
| revolutions per day: | 1.88728078 |
| mean anomaly at epoch: | 350.7767° |
| orbit number at epoch: | 8174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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