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 66216U 26145.54139847 +.00000000 +00000-0 +46186-3 0 00001
2 66216 53.1574 233.1043 0001502 98.1935 261.9237 15.30207191 06
| Epoch (UTC): | 25 May 2026 12:59:36 |
| Eccentricity: | 0.0001502 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1043° |
| argument of perigee: | 98.1935° |
| revolutions per day: | 15.30207191 |
| mean anomaly at epoch: | 261.9237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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