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 65417U 26145.51459156 +.00000000 +00000-0 +63181-3 0 00002
2 65417 53.1575 235.6987 0001894 87.3767 272.7450 15.30212718 08
| Epoch (UTC): | 25 May 2026 12:21:00 |
| Eccentricity: | 0.0001894 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.6987° |
| argument of perigee: | 87.3767° |
| revolutions per day: | 15.30212718 |
| mean anomaly at epoch: | 272.7450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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