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 59312U 26145.46152346 +.00000000 +00000-0 +58837-4 0 00007
2 59312 43.0015 164.2275 0001382 271.7130 88.3563 15.27580316 08
| Epoch (UTC): | 25 May 2026 11:04:35 |
| Eccentricity: | 0.0001382 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.2275° |
| argument of perigee: | 271.7130° |
| revolutions per day: | 15.27580316 |
| mean anomaly at epoch: | 88.3563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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