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 46782U 26145.03479752 +.00000000 +00000-0 +63003-3 0 00000
2 46782 53.0409 259.7732 0006249 254.6917 105.3410 15.71110280 00
| Epoch (UTC): | 25 May 2026 00:50:06 |
| Eccentricity: | 0.0006249 |
| inclination: | 53.0409° |
| perigee height: | 352 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 259.7732° |
| argument of perigee: | 254.6917° |
| revolutions per day: | 15.71110280 |
| mean anomaly at epoch: | 105.3410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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