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 data is extracted from the following two-line orbital elements,
1 15766U 81053KB 25163.21261688 .00004035 00000-0 12084-2 0 9992
2 15766 82.9358 241.9551 0004041 274.8309 85.2424 14.42673069 61296
| Epoch (UTC): | 12 June 2025 05:06:10 |
| Eccentricity: | 0.0004041 |
| inclination: | 82.9358° |
| perigee height: | 747 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 241.9551° |
| argument of perigee: | 274.8309° |
| revolutions per day: | 14.42673069 |
| mean anomaly at epoch: | 85.2424° |
| orbit number at epoch: | 6129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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