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 65343U 26145.44608110 +.00000000 +00000-0 +58938-3 0 00002
2 65343 53.1585 210.5565 0001500 87.1000 273.0172 15.30211020 03
| Epoch (UTC): | 25 May 2026 10:42:21 |
| Eccentricity: | 0.0001500 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5565° |
| argument of perigee: | 87.1000° |
| revolutions per day: | 15.30211020 |
| mean anomaly at epoch: | 273.0172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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