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 53740U 26145.38709896 +.00000000 +00000-0 +47797-4 0 00008
2 53740 53.2116 279.7037 0001642 85.9407 274.1773 15.08834128 01
| Epoch (UTC): | 25 May 2026 09:17:25 |
| Eccentricity: | 0.0001642 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.7037° |
| argument of perigee: | 85.9407° |
| revolutions per day: | 15.08834128 |
| mean anomaly at epoch: | 274.1773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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