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 44909U 19096E 23340.22247906 .00000016 00000-0 12668-4 0 9999
2 44909 82.5225 233.6224 0217979 144.5092 217.0737 12.79724306184162
| Epoch (UTC): | 06 December 2023 05:20:22 |
| Eccentricity: | 0.0217979 |
| inclination: | 82.5225° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 233.6224° |
| argument of perigee: | 144.5092° |
| revolutions per day: | 12.79724306 |
| mean anomaly at epoch: | 217.0737° |
| orbit number at epoch: | 18416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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