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 53062U 26145.39841875 +.00000000 +00000-0 -11839-3 0 00008
2 53062 97.4466 325.3869 0001103 80.0965 280.0386 15.05664097 03
| Epoch (UTC): | 25 May 2026 09:33:43 |
| Eccentricity: | 0.0001103 |
| inclination: | 97.4466° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3869° |
| argument of perigee: | 80.0965° |
| revolutions per day: | 15.05664097 |
| mean anomaly at epoch: | 280.0386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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