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 41175U 26145.38218691 +.00000000 +00000-0 +00000-0 0 00007
2 41175 55.8130 101.8837 0004978 338.1073 21.8293 1.70473719 07
| Epoch (UTC): | 25 May 2026 09:10:20 |
| Eccentricity: | 0.0004978 |
| inclination: | 55.8130° |
| perigee height: | 23207 km |
| apogee height: | 23237 km |
| right ascension of ascending node: | 101.8837° |
| argument of perigee: | 338.1073° |
| revolutions per day: | 1.70473719 |
| mean anomaly at epoch: | 21.8293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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