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 64613U 26145.50646402 +.00000000 +00000-0 +71540-3 0 00008
2 64613 53.1583 338.5854 0001800 82.0187 278.1018 15.30207965 03
| Epoch (UTC): | 25 May 2026 12:09:18 |
| Eccentricity: | 0.0001800 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5854° |
| argument of perigee: | 82.0187° |
| revolutions per day: | 15.30207965 |
| mean anomaly at epoch: | 278.1018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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