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 1328U 65032A 25109.19908842 .00000045 00000-0 19211-3 0 9994
2 1328 41.1865 31.4006 0246105 261.1108 96.1710 13.38882733931937
| Epoch (UTC): | 19 April 2025 04:46:41 |
| Eccentricity: | 0.0246105 |
| inclination: | 41.1865° |
| perigee height: | 929 km |
| apogee height: | 1298 km |
| right ascension of ascending node: | 31.4006° |
| argument of perigee: | 261.1108° |
| revolutions per day: | 13.38882733 |
| mean anomaly at epoch: | 96.1710° |
| orbit number at epoch: | 93193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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