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 66274U 26145.38697413 +.00000000 +00000-0 +22297-3 0 00002
2 66274 53.1591 195.3841 0000970 94.2513 265.8598 15.30200115 03
| Epoch (UTC): | 25 May 2026 09:17:14 |
| Eccentricity: | 0.0000970 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 195.3841° |
| argument of perigee: | 94.2513° |
| revolutions per day: | 15.30200115 |
| mean anomaly at epoch: | 265.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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