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 41862U 26144.64887476 +.00000000 +00000-0 +00000-0 0 00001
2 41862 55.4835 101.7326 0004640 315.3959 44.5266 1.70473997 06
| Epoch (UTC): | 24 May 2026 15:34:22 |
| Eccentricity: | 0.0004640 |
| inclination: | 55.4835° |
| perigee height: | 23208 km |
| apogee height: | 23236 km |
| right ascension of ascending node: | 101.7326° |
| argument of perigee: | 315.3959° |
| revolutions per day: | 1.70473997 |
| mean anomaly at epoch: | 44.5266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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