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 65883U 26144.81497128 +.00000000 +00000-0 +70820-3 0 00000
2 65883 53.1589 16.7515 0000869 22.8288 337.2753 15.34401581 03
| Epoch (UTC): | 24 May 2026 19:33:33 |
| Eccentricity: | 0.0000869 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 16.7515° |
| argument of perigee: | 22.8288° |
| revolutions per day: | 15.34401581 |
| mean anomaly at epoch: | 337.2753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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