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 66545U 26145.75126499 +.00000000 +00000-0 +38286-3 0 00000
2 66545 51.7987 284.4923 0008980 177.4117 182.6907 15.15424158 09
| Epoch (UTC): | 25 May 2026 18:01:49 |
| Eccentricity: | 0.0008980 |
| inclination: | 51.7987° |
| perigee height: | 513 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 284.4923° |
| argument of perigee: | 177.4117° |
| revolutions per day: | 15.15424158 |
| mean anomaly at epoch: | 182.6907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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