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 65375U 26145.47590856 +.00000000 +00000-0 +49280-3 0 00007
2 65375 53.1585 171.3553 0001089 82.7227 277.3897 15.30193668 01
| Epoch (UTC): | 25 May 2026 11:25:18 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3553° |
| argument of perigee: | 82.7227° |
| revolutions per day: | 15.30193668 |
| mean anomaly at epoch: | 277.3897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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