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 66111U 26145.32778539 +.00000000 +00000-0 +67267-3 0 00001
2 66111 53.1569 108.2203 0001211 94.8292 265.2847 15.30215299 02
| Epoch (UTC): | 25 May 2026 07:52:00 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1569° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.2203° |
| argument of perigee: | 94.8292° |
| revolutions per day: | 15.30215299 |
| mean anomaly at epoch: | 265.2847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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