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 66181U 26145.58258433 +.00000000 +00000-0 +39580-3 0 00009
2 66181 53.1580 248.2916 0001238 86.8879 273.2263 15.30199195 06
| Epoch (UTC): | 25 May 2026 13:58:55 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2916° |
| argument of perigee: | 86.8879° |
| revolutions per day: | 15.30199195 |
| mean anomaly at epoch: | 273.2263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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