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 59875U 26144.51710164 +.00000000 +00000-0 +13776-4 0 00007
2 59875 43.0008 177.4298 0001267 274.5534 85.5172 15.27579306 08
| Epoch (UTC): | 24 May 2026 12:24:37 |
| Eccentricity: | 0.0001267 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.4298° |
| argument of perigee: | 274.5534° |
| revolutions per day: | 15.27579306 |
| mean anomaly at epoch: | 85.5172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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