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 66815U 26145.41542255 +.00000000 +00000-0 +54526-3 0 00000
2 66815 43.0016 41.0244 0001940 273.6092 86.4537 15.27596578 08
| Epoch (UTC): | 25 May 2026 09:58:12 |
| Eccentricity: | 0.0001940 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.0244° |
| argument of perigee: | 273.6092° |
| revolutions per day: | 15.27596578 |
| mean anomaly at epoch: | 86.4537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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