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 66271U 26145.51338345 +.00000000 +00000-0 +32469-3 0 00002
2 66271 53.1589 194.7552 0001157 76.8611 283.2519 15.30201581 07
| Epoch (UTC): | 25 May 2026 12:19:16 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.7552° |
| argument of perigee: | 76.8611° |
| revolutions per day: | 15.30201581 |
| mean anomaly at epoch: | 283.2519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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