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 66883U 26145.40386056 +.00000000 +00000-0 +91038-3 0 00008
2 66883 53.1617 27.5447 0001224 82.1952 277.9190 15.34416912 02
| Epoch (UTC): | 25 May 2026 09:41:33 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1617° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 27.5447° |
| argument of perigee: | 82.1952° |
| revolutions per day: | 15.34416912 |
| mean anomaly at epoch: | 277.9190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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