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 66220U 26145.24320259 +.00000000 +00000-0 +69651-3 0 00004
2 66220 53.1584 234.0816 0001329 84.1673 275.9480 15.30216590 09
| Epoch (UTC): | 25 May 2026 05:50:12 |
| Eccentricity: | 0.0001329 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.0816° |
| argument of perigee: | 84.1673° |
| revolutions per day: | 15.30216590 |
| mean anomaly at epoch: | 275.9480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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