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 59940U 26145.35752866 +.00000000 +00000-0 +49034-5 0 00005
2 59940 43.0005 259.9280 0001083 275.2559 84.8169 15.27577904 06
| Epoch (UTC): | 25 May 2026 08:34:50 |
| Eccentricity: | 0.0001083 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.9280° |
| argument of perigee: | 275.2559° |
| revolutions per day: | 15.27577904 |
| mean anomaly at epoch: | 84.8169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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