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 12165U 78026E 24357.92138659 .00000223 00000-0 14853-3 0 9993
2 12165 99.0482 18.9355 0042619 295.7207 137.7444 14.10883548 43508
| Epoch (UTC): | 22 December 2024 22:06:47 |
| Eccentricity: | 0.0042619 |
| inclination: | 99.0482° |
| perigee height: | 825 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 18.9355° |
| argument of perigee: | 295.7207° |
| revolutions per day: | 14.10883548 |
| mean anomaly at epoch: | 137.7444° |
| orbit number at epoch: | 4350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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