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 59471U 26145.52078354 +.00000000 +00000-0 +18673-4 0 00000
2 59471 43.0027 317.1064 0000924 283.1211 76.9538 15.27574407 09
| Epoch (UTC): | 25 May 2026 12:29:55 |
| Eccentricity: | 0.0000924 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.1064° |
| argument of perigee: | 283.1211° |
| revolutions per day: | 15.27574407 |
| mean anomaly at epoch: | 76.9538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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