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 12862U 77121AQ 24358.15674014 .00003797 00000-0 19631-2 0 9995
2 12862 66.2105 58.0026 0137763 161.3249 227.6413 14.11269118290432
| Epoch (UTC): | 23 December 2024 03:45:42 |
| Eccentricity: | 0.0137763 |
| inclination: | 66.2105° |
| perigee height: | 755 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 58.0026° |
| argument of perigee: | 161.3249° |
| revolutions per day: | 14.11269118 |
| mean anomaly at epoch: | 227.6413° |
| orbit number at epoch: | 29043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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