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 46347U 26145.58335647 +.00000000 +00000-0 +66610-3 0 00008
2 46347 53.0308 257.0595 0005627 336.2721 239.5942 15.82237171 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005627 |
| inclination: | 53.0308° |
| perigee height: | 320 km |
| apogee height: | 328 km |
| right ascension of ascending node: | 257.0595° |
| argument of perigee: | 336.2721° |
| revolutions per day: | 15.82237171 |
| mean anomaly at epoch: | 239.5942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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