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 33066U 08031G 25108.77530169 .00001356 00000-0 24274-3 0 9991
2 33066 48.4438 28.2523 0007481 345.0003 15.0686 14.72465458903923
| Epoch (UTC): | 18 April 2025 18:36:26 |
| Eccentricity: | 0.0007481 |
| inclination: | 48.4438° |
| perigee height: | 648 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 28.2523° |
| argument of perigee: | 345.0003° |
| revolutions per day: | 14.72465458 |
| mean anomaly at epoch: | 15.0686° |
| orbit number at epoch: | 90392 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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