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 46331U 26144.68746147 +.00000000 +00000-0 +75823-3 0 00008
2 46331 53.0376 325.2237 0007206 183.3185 176.7786 15.73161896 00
| Epoch (UTC): | 24 May 2026 16:29:56 |
| Eccentricity: | 0.0007206 |
| inclination: | 53.0376° |
| perigee height: | 345 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 325.2237° |
| argument of perigee: | 183.3185° |
| revolutions per day: | 15.73161896 |
| mean anomaly at epoch: | 176.7786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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