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 41860U 26144.72200713 +.00000000 +00000-0 +00000-0 0 00001
2 41860 55.4828 101.7300 0004738 349.6187 10.3311 1.70473926 03
| Epoch (UTC): | 24 May 2026 17:19:41 |
| Eccentricity: | 0.0004738 |
| inclination: | 55.4828° |
| perigee height: | 23208 km |
| apogee height: | 23236 km |
| right ascension of ascending node: | 101.7300° |
| argument of perigee: | 349.6187° |
| revolutions per day: | 1.70473926 |
| mean anomaly at epoch: | 10.3311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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