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 24276.17438608 .00000803 00000-0 11123-2 0 9991
2 00016 34.2663 306.8035 2024711 9.5868 353.8019 10.49433821623455
| Epoch (UTC): | 02 October 2024 04:11:06 |
| Eccentricity: | 0.2024711 |
| inclination: | 34.2663° |
| perigee height: | 650 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 306.8035° |
| argument of perigee: | 9.5868° |
| revolutions per day: | 10.49433821 |
| mean anomaly at epoch: | 353.8019° |
| orbit number at epoch: | 62345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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