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 13618U 82102B 24284.61614578 .00000275 00000-0 26247-3 0 9998
2 13618 82.9666 320.7814 0031275 208.3210 266.7037 13.76957626108784
| Epoch (UTC): | 10 October 2024 14:47:14 |
| Eccentricity: | 0.0031275 |
| inclination: | 82.9666° |
| perigee height: | 952 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 320.7814° |
| argument of perigee: | 208.3210° |
| revolutions per day: | 13.76957626 |
| mean anomaly at epoch: | 266.7037° |
| orbit number at epoch: | 10878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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