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 65685U 26145.58335647 +.00000000 +00000-0 +12366-2 0 00002
2 65685 53.1602 348.6529 0000976 96.6859 287.7687 15.33547178 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000976 |
| inclination: | 53.1602° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 348.6529° |
| argument of perigee: | 96.6859° |
| revolutions per day: | 15.33547178 |
| mean anomaly at epoch: | 287.7687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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