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 66266U 26145.42907314 +.00000000 +00000-0 +32546-3 0 00000
2 66266 53.1582 194.9428 0001098 93.3866 266.7261 15.30202919 04
| Epoch (UTC): | 25 May 2026 10:17:51 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.9428° |
| argument of perigee: | 93.3866° |
| revolutions per day: | 15.30202919 |
| mean anomaly at epoch: | 266.7261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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