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 66313U 26144.82916425 +.00000000 +00000-0 +00000-0 0 00006
2 66313 20.0901 352.1461 0004308 102.0511 258.0129 5.31203760 04
| Epoch (UTC): | 24 May 2026 19:53:59 |
| Eccentricity: | 0.0004308 |
| inclination: | 20.0901° |
| perigee height: | 7491 km |
| apogee height: | 7503 km |
| right ascension of ascending node: | 352.1461° |
| argument of perigee: | 102.0511° |
| revolutions per day: | 5.31203760 |
| mean anomaly at epoch: | 258.0129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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