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 46342U 26145.33610781 +.00000000 +00000-0 +13210-2 0 00008
2 46342 53.1564 13.3660 0004261 136.8164 223.3174 15.36482133 04
| Epoch (UTC): | 25 May 2026 08:03:59 |
| Eccentricity: | 0.0004261 |
| inclination: | 53.1564° |
| perigee height: | 454 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 13.3660° |
| argument of perigee: | 136.8164° |
| revolutions per day: | 15.36482133 |
| mean anomaly at epoch: | 223.3174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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