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 00082U 61004B 24255.32288620 .00002119 00000-0 17947-2 0 9993
2 00082 38.8540 230.1609 1165459 350.5005 7.5277 12.27002861997697
| Epoch (UTC): | 11 September 2024 07:44:57 |
| Eccentricity: | 0.1165459 |
| inclination: | 38.8540° |
| perigee height: | 637 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 230.1609° |
| argument of perigee: | 350.5005° |
| revolutions per day: | 12.27002861 |
| mean anomaly at epoch: | 7.5277° |
| orbit number at epoch: | 99769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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