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 46375U 26145.37555801 +.00000000 +00000-0 +72823-3 0 00005
2 46375 53.0233 272.7731 0003995 236.8789 123.1843 15.68003065 07
| Epoch (UTC): | 25 May 2026 09:00:48 |
| Eccentricity: | 0.0003995 |
| inclination: | 53.0233° |
| perigee height: | 362 km |
| apogee height: | 367 km |
| right ascension of ascending node: | 272.7731° |
| argument of perigee: | 236.8789° |
| revolutions per day: | 15.68003065 |
| mean anomaly at epoch: | 123.1843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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