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 64762U 26145.56830479 +.00000000 +00000-0 +61454-3 0 00001
2 64762 53.1585 244.8510 0001194 82.6034 277.5104 15.34401139 03
| Epoch (UTC): | 25 May 2026 13:38:21 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 244.8510° |
| argument of perigee: | 82.6034° |
| revolutions per day: | 15.34401139 |
| mean anomaly at epoch: | 277.5104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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