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 00694U 63047A 24280.82392578 .00004822 00000-0 59235-3 0 9992
2 00694 30.3556 208.8530 0561333 197.7664 160.2549 14.08680626 58304
| Epoch (UTC): | 06 October 2024 19:46:27 |
| Eccentricity: | 0.0561333 |
| inclination: | 30.3556° |
| perigee height: | 457 km |
| apogee height: | 1270 km |
| right ascension of ascending node: | 208.8530° |
| argument of perigee: | 197.7664° |
| revolutions per day: | 14.08680626 |
| mean anomaly at epoch: | 160.2549° |
| orbit number at epoch: | 5830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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