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 43495U 18052A 25217.01969766 0.00000000 00000-0 00000-0 0 05
2 43495 97.3598 332.5626 0004091 298.0302 61.9696 15.25982691 08
| Epoch (UTC): | 05 August 2025 00:28:21 |
| Eccentricity: | 0.0004091 |
| inclination: | 97.3598° |
| perigee height: | 485 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 332.5626° |
| argument of perigee: | 298.0302° |
| revolutions per day: | 15.25982691 |
| mean anomaly at epoch: | 61.9696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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