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 39714U 92093KE 24355.63670301 .00001210 00000-0 52084-3 0 9998
2 39714 71.0841 99.4664 0096586 271.2175 87.7889 14.24117131575193
| Epoch (UTC): | 20 December 2024 15:16:51 |
| Eccentricity: | 0.0096586 |
| inclination: | 71.0841° |
| perigee height: | 742 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 99.4664° |
| argument of perigee: | 271.2175° |
| revolutions per day: | 14.24117131 |
| mean anomaly at epoch: | 87.7889° |
| orbit number at epoch: | 57519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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