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 23859U 96024C 24357.78746322 .00000486 00000-0 36113-3 0 9993
2 23859 99.0745 297.4063 0086880 145.9168 276.6839 13.98002103460680
| Epoch (UTC): | 22 December 2024 18:53:56 |
| Eccentricity: | 0.0086880 |
| inclination: | 99.0745° |
| perigee height: | 837 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 297.4063° |
| argument of perigee: | 145.9168° |
| revolutions per day: | 13.98002103 |
| mean anomaly at epoch: | 276.6839° |
| orbit number at epoch: | 46068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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