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 00016U 58002A 24282.36354589 .00001418 00000-0 19641-2 0 9990
2 00016 34.2640 288.9015 2024378 35.7251 336.3246 10.49447353624100
| Epoch (UTC): | 08 October 2024 08:43:30 |
| Eccentricity: | 0.2024378 |
| inclination: | 34.2640° |
| perigee height: | 650 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 288.9015° |
| argument of perigee: | 35.7251° |
| revolutions per day: | 10.49447353 |
| mean anomaly at epoch: | 336.3246° |
| orbit number at epoch: | 62410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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