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 31979U 99025CPG 24353.98687253 .00006002 00000-0 56379-2 0 9999
2 31979 99.3788 90.6100 0274839 131.8581 230.6375 13.66280145867206
| Epoch (UTC): | 18 December 2024 23:41:05 |
| Eccentricity: | 0.0274839 |
| inclination: | 99.3788° |
| perigee height: | 810 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 90.6100° |
| argument of perigee: | 131.8581° |
| revolutions per day: | 13.66280145 |
| mean anomaly at epoch: | 230.6375° |
| orbit number at epoch: | 86720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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