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 66380U 26144.69088338 +.00000000 +00000-0 +44969-3 0 00003
2 66380 53.1585 223.0166 0001059 97.2351 262.8772 15.34402083 08
| Epoch (UTC): | 24 May 2026 16:34:52 |
| Eccentricity: | 0.0001059 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 223.0166° |
| argument of perigee: | 97.2351° |
| revolutions per day: | 15.34402083 |
| mean anomaly at epoch: | 262.8772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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