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 64902U 26145.57722041 +.00000000 +00000-0 +15623-3 0 00000
2 64902 97.4328 224.4945 0001123 132.8826 227.2504 15.20196173 00
| Epoch (UTC): | 25 May 2026 13:51:11 |
| Eccentricity: | 0.0001123 |
| inclination: | 97.4328° |
| perigee height: | 504 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 224.4945° |
| argument of perigee: | 132.8826° |
| revolutions per day: | 15.20196173 |
| mean anomaly at epoch: | 227.2504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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