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 65476U 26144.84842220 +.00000000 +00000-0 +85170-3 0 00002
2 65476 53.1576 263.7424 0001504 80.5062 279.6109 15.31721572 04
| Epoch (UTC): | 24 May 2026 20:21:43 |
| Eccentricity: | 0.0001504 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 263.7424° |
| argument of perigee: | 80.5062° |
| revolutions per day: | 15.31721572 |
| mean anomaly at epoch: | 279.6109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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