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 46052U 26145.35833029 +.00000000 +00000-0 +78517-3 0 00002
2 46052 53.1585 106.3261 0001988 122.3955 237.7260 15.79162073 06
| Epoch (UTC): | 25 May 2026 08:35:59 |
| Eccentricity: | 0.0001988 |
| inclination: | 53.1585° |
| perigee height: | 331 km |
| apogee height: | 334 km |
| right ascension of ascending node: | 106.3261° |
| argument of perigee: | 122.3955° |
| revolutions per day: | 15.79162073 |
| mean anomaly at epoch: | 237.7260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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