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 59462U 26145.53700559 +.00000000 +00000-0 +39788-4 0 00000
2 59462 43.0018 320.6913 0001063 288.0993 71.9743 15.27574109 09
| Epoch (UTC): | 25 May 2026 12:53:17 |
| Eccentricity: | 0.0001063 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.6913° |
| argument of perigee: | 288.0993° |
| revolutions per day: | 15.27574109 |
| mean anomaly at epoch: | 71.9743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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