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 65408U 26145.23539218 +.00000000 +00000-0 +46149-3 0 00004
2 65408 53.1584 236.8086 0001259 91.3520 268.7625 15.30209339 02
| Epoch (UTC): | 25 May 2026 05:38:57 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 236.8086° |
| argument of perigee: | 91.3520° |
| revolutions per day: | 15.30209339 |
| mean anomaly at epoch: | 268.7625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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