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 66006U 26145.32136056 +.00000000 +00000-0 +32749-3 0 00003
2 66006 53.1577 107.5791 0001283 91.5123 268.6025 15.30208115 08
| Epoch (UTC): | 25 May 2026 07:42:45 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.5791° |
| argument of perigee: | 91.5123° |
| revolutions per day: | 15.30208115 |
| mean anomaly at epoch: | 268.6025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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