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 07682U 75016E 24357.87502907 .00000002 00000-0 12803-3 0 9990
2 07682 74.0008 160.7928 0021831 165.5529 307.3156 12.44735225834527
| Epoch (UTC): | 22 December 2024 21:00:02 |
| Eccentricity: | 0.0021831 |
| inclination: | 74.0008° |
| perigee height: | 1469 km |
| apogee height: | 1504 km |
| right ascension of ascending node: | 160.7928° |
| argument of perigee: | 165.5529° |
| revolutions per day: | 12.44735225 |
| mean anomaly at epoch: | 307.3156° |
| orbit number at epoch: | 83452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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