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 09662U 77002B 24287.43727167 .00000362 00000-0 22966-3 0 9998
2 09662 81.2778 37.4654 0052546 166.3802 193.8797 14.01172313440954
| Epoch (UTC): | 13 October 2024 10:29:40 |
| Eccentricity: | 0.0052546 |
| inclination: | 81.2778° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 37.4654° |
| argument of perigee: | 166.3802° |
| revolutions per day: | 14.01172313 |
| mean anomaly at epoch: | 193.8797° |
| orbit number at epoch: | 44095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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