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 65484U 26144.61551706 +.00000000 +00000-0 +77787-3 0 00007
2 65484 53.1558 265.1056 0001324 88.9363 271.1792 15.34413390 00
| Epoch (UTC): | 24 May 2026 14:46:20 |
| Eccentricity: | 0.0001324 |
| inclination: | 53.1558° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 265.1056° |
| argument of perigee: | 88.9363° |
| revolutions per day: | 15.34413390 |
| mean anomaly at epoch: | 271.1792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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