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 25115.69687211 .00001244 00000-0 22518-3 0 9996
2 33066 48.4437 355.7264 0007225 14.2603 345.8512 14.72486701904948
| Epoch (UTC): | 25 April 2025 16:43:29 |
| Eccentricity: | 0.0007225 |
| inclination: | 48.4437° |
| perigee height: | 648 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 355.7264° |
| argument of perigee: | 14.2603° |
| revolutions per day: | 14.72486701 |
| mean anomaly at epoch: | 345.8512° |
| orbit number at epoch: | 90494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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