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 66373U 26145.53085863 +.00000000 +00000-0 +22876-3 0 00002
2 66373 53.1574 233.1276 0001194 75.3101 284.8032 15.30197271 01
| Epoch (UTC): | 25 May 2026 12:44:26 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1276° |
| argument of perigee: | 75.3101° |
| revolutions per day: | 15.30197271 |
| mean anomaly at epoch: | 284.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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