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 09903U 77024A 24260.86179165 .00000104 00000-0 53091-4 0 9995
2 09903 81.2709 35.5079 0038797 10.5760 349.6217 14.08567393437688
| Epoch (UTC): | 16 September 2024 20:40:58 |
| Eccentricity: | 0.0038797 |
| inclination: | 81.2709° |
| perigee height: | 836 km |
| apogee height: | 892 km |
| right ascension of ascending node: | 35.5079° |
| argument of perigee: | 10.5760° |
| revolutions per day: | 14.08567393 |
| mean anomaly at epoch: | 349.6217° |
| orbit number at epoch: | 43768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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