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 23339.66663251 .00000584 00000-0 81656-3 0 9993
2 00016 34.2618 98.1696 2020607 177.2225 184.1753 10.48990488591785
| Epoch (UTC): | 05 December 2023 15:59:57 |
| Eccentricity: | 0.2020607 |
| inclination: | 34.2618° |
| perigee height: | 655 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 98.1696° |
| argument of perigee: | 177.2225° |
| revolutions per day: | 10.48990488 |
| mean anomaly at epoch: | 184.1753° |
| orbit number at epoch: | 59178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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