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 66232U 26145.42764134 +.00000000 +00000-0 +23028-3 0 00009
2 66232 53.1586 233.8020 0001481 86.3335 273.7835 15.30178880 05
| Epoch (UTC): | 25 May 2026 10:15:48 |
| Eccentricity: | 0.0001481 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.8020° |
| argument of perigee: | 86.3335° |
| revolutions per day: | 15.30178880 |
| mean anomaly at epoch: | 273.7835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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