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 65625U 26145.46790062 +.00000000 +00000-0 +48026-3 0 00002
2 65625 53.1592 309.2138 0001231 83.9120 276.2023 15.34403707 03
| Epoch (UTC): | 25 May 2026 11:13:46 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.2138° |
| argument of perigee: | 83.9120° |
| revolutions per day: | 15.34403707 |
| mean anomaly at epoch: | 276.2023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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