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 59381U 26145.57575492 +.00000000 +00000-0 +13032-4 0 00004
2 59381 53.1618 260.6265 0000980 83.0823 277.0291 15.34383689 08
| Epoch (UTC): | 25 May 2026 13:49:05 |
| Eccentricity: | 0.0000980 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 260.6265° |
| argument of perigee: | 83.0823° |
| revolutions per day: | 15.34383689 |
| mean anomaly at epoch: | 277.0291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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