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 65469U 26145.34674336 +.00000000 +00000-0 +67678-3 0 00004
2 65469 53.1578 261.8787 0001225 70.0655 290.0479 15.34413772 01
| Epoch (UTC): | 25 May 2026 08:19:18 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.1578° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.8787° |
| argument of perigee: | 70.0655° |
| revolutions per day: | 15.34413772 |
| mean anomaly at epoch: | 290.0479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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