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 59334U 26145.38578819 +.00000000 +00000-0 -29875-4 0 00000
2 59334 43.0030 113.5075 0001293 268.7960 91.2743 15.27566337 02
| Epoch (UTC): | 25 May 2026 09:15:32 |
| Eccentricity: | 0.0001293 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.5075° |
| argument of perigee: | 268.7960° |
| revolutions per day: | 15.27566337 |
| mean anomaly at epoch: | 91.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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