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 65640U 26145.44905282 +.00000000 +00000-0 +70596-3 0 00006
2 65640 53.1603 309.8065 0001294 63.6532 296.4604 15.34400446 05
| Epoch (UTC): | 25 May 2026 10:46:38 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.8065° |
| argument of perigee: | 63.6532° |
| revolutions per day: | 15.34400446 |
| mean anomaly at epoch: | 296.4604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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