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 65205U 26145.40695505 +.00000000 +00000-0 +49897-3 0 00003
2 65205 53.1589 155.8607 0001003 82.5493 277.5624 15.34410316 09
| Epoch (UTC): | 25 May 2026 09:46:00 |
| Eccentricity: | 0.0001003 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.8607° |
| argument of perigee: | 82.5493° |
| revolutions per day: | 15.34410316 |
| mean anomaly at epoch: | 277.5624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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