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 41861U 26143.32954110 +.00000000 +00000-0 +00000-0 0 00004
2 41861 55.4841 101.7765 0005510 308.1575 51.7536 1.70474331 03
| Epoch (UTC): | 23 May 2026 07:54:32 |
| Eccentricity: | 0.0005510 |
| inclination: | 55.4841° |
| perigee height: | 23206 km |
| apogee height: | 23238 km |
| right ascension of ascending node: | 101.7765° |
| argument of perigee: | 308.1575° |
| revolutions per day: | 1.70474331 |
| mean anomaly at epoch: | 51.7536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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