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 31914U 99025CLR 24357.98509619 .00001327 00000-0 25784-3 0 9993
2 31914 99.0583 185.5204 0185684 61.3219 300.6504 14.54727051929232
| Epoch (UTC): | 22 December 2024 23:38:32 |
| Eccentricity: | 0.0185684 |
| inclination: | 99.0583° |
| perigee height: | 578 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 185.5204° |
| argument of perigee: | 61.3219° |
| revolutions per day: | 14.54727051 |
| mean anomaly at epoch: | 300.6504° |
| orbit number at epoch: | 92923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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