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 65463U 26144.75611466 +.00000000 +00000-0 +48657-3 0 00003
2 65463 53.1583 264.5868 0000965 87.4143 272.6969 15.30206930 07
| Epoch (UTC): | 24 May 2026 18:08:48 |
| Eccentricity: | 0.0000965 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 264.5868° |
| argument of perigee: | 87.4143° |
| revolutions per day: | 15.30206930 |
| mean anomaly at epoch: | 272.6969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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