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 65890U 26145.64769838 +.00000000 +00000-0 +88972-3 0 00007
2 65890 53.1597 14.1218 0001130 82.5972 277.5157 15.30212282 05
| Epoch (UTC): | 25 May 2026 15:32:41 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 14.1218° |
| argument of perigee: | 82.5972° |
| revolutions per day: | 15.30212282 |
| mean anomaly at epoch: | 277.5157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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