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 66486U 26144.80769459 +.00000000 +00000-0 +92180-3 0 00001
2 66486 43.0000 280.5252 0001467 282.3986 77.6702 15.27580153 05
| Epoch (UTC): | 24 May 2026 19:23:04 |
| Eccentricity: | 0.0001467 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.5252° |
| argument of perigee: | 282.3986° |
| revolutions per day: | 15.27580153 |
| mean anomaly at epoch: | 77.6702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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