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 23463U 95002A 24357.65844875 .00000072 00000-0 61937-4 0 9991
2 23463 82.9274 56.3939 0038501 201.8706 269.7277 13.72671173498018
| Epoch (UTC): | 22 December 2024 15:48:09 |
| Eccentricity: | 0.0038501 |
| inclination: | 82.9274° |
| perigee height: | 961 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 56.3939° |
| argument of perigee: | 201.8706° |
| revolutions per day: | 13.72671173 |
| mean anomaly at epoch: | 269.7277° |
| orbit number at epoch: | 49801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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