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 26098.87452806 +.00000000 +00000-0 +00000-0 0 00007
2 40186 25.7800 102.4895 7283269 224.1934 58.3871 1.88723004 09
| Epoch (UTC): | 08 April 2026 20:59:19 |
| Eccentricity: | 0.7283269 |
| inclination: | 25.7800° |
| perigee height: | 1136 km |
| apogee height: | 41427 km |
| right ascension of ascending node: | 102.4895° |
| argument of perigee: | 224.1934° |
| revolutions per day: | 1.88723004 |
| mean anomaly at epoch: | 58.3871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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