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 43495U 18052A 25105.93774724 0.00000000 00000-0 00000-0 0 00
2 43495 97.3686 223.1159 0001457 311.0613 48.9386 15.25981064 00
| Epoch (UTC): | 15 April 2025 22:30:21 |
| Eccentricity: | 0.0001457 |
| inclination: | 97.3686° |
| perigee height: | 487 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 223.1159° |
| argument of perigee: | 311.0613° |
| revolutions per day: | 15.25981064 |
| mean anomaly at epoch: | 48.9386° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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