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 65461U 26145.04000486 +.00000000 +00000-0 +60380-3 0 00005
2 65461 53.1577 263.5210 0000818 89.1880 270.9216 15.34396465 05
| Epoch (UTC): | 25 May 2026 00:57:36 |
| Eccentricity: | 0.0000818 |
| inclination: | 53.1577° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 263.5210° |
| argument of perigee: | 89.1880° |
| revolutions per day: | 15.34396465 |
| mean anomaly at epoch: | 270.9216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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