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 65856U 26145.45045016 +.00000000 +00000-0 +83952-3 0 00006
2 65856 53.1587 297.2375 0002140 76.8618 283.2623 15.34407706 02
| Epoch (UTC): | 25 May 2026 10:48:38 |
| Eccentricity: | 0.0002140 |
| inclination: | 53.1587° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.2375° |
| argument of perigee: | 76.8618° |
| revolutions per day: | 15.34407706 |
| mean anomaly at epoch: | 283.2623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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