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 43678U 18084H 25140.62028847 .00002275 00000-0 19680-3 0 9991
2 43678 98.1019 315.9849 0007653 1.6362 358.4883 14.98238972357395
| Epoch (UTC): | 20 May 2025 14:53:12 |
| Eccentricity: | 0.0007653 |
| inclination: | 98.1019° |
| perigee height: | 567 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 315.9849° |
| argument of perigee: | 1.6362° |
| revolutions per day: | 14.98238972 |
| mean anomaly at epoch: | 358.4883° |
| orbit number at epoch: | 35739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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