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 31732U 99025CEF 24357.57343094 .00001050 00000-0 59583-3 0 9996
2 31732 98.6163 41.0464 0041043 178.2555 181.8767 14.11636668593181
| Epoch (UTC): | 22 December 2024 13:45:44 |
| Eccentricity: | 0.0041043 |
| inclination: | 98.6163° |
| perigee height: | 824 km |
| apogee height: | 883 km |
| right ascension of ascending node: | 41.0464° |
| argument of perigee: | 178.2555° |
| revolutions per day: | 14.11636668 |
| mean anomaly at epoch: | 181.8767° |
| orbit number at epoch: | 59318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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