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 45859U 20043A 24358.11607392 .00000804 00000-0 15748-3 0 9991
2 45859 98.1956 4.1374 0131511 116.3300 245.1476 14.60192164237876
| Epoch (UTC): | 23 December 2024 02:47:08 |
| Eccentricity: | 0.0131511 |
| inclination: | 98.1956° |
| perigee height: | 599 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 4.1374° |
| argument of perigee: | 116.3300° |
| revolutions per day: | 14.60192164 |
| mean anomaly at epoch: | 245.1476° |
| orbit number at epoch: | 23787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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