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 24259.94473146 .00000354 00000-0 22516-3 0 9990
2 09662 81.2728 63.7439 0051304 243.6638 115.9254 14.01154979437103
| Epoch (UTC): | 15 September 2024 22:40:24 |
| Eccentricity: | 0.0051304 |
| inclination: | 81.2728° |
| perigee height: | 852 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 63.7439° |
| argument of perigee: | 243.6638° |
| revolutions per day: | 14.01154979 |
| mean anomaly at epoch: | 115.9254° |
| orbit number at epoch: | 43710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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