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 24726U 97006B 24260.66942101 .00000056 00000-0 25463-3 0 9990
2 24726 82.5997 309.1905 0006417 97.4912 262.6907 12.61372712269977
| Epoch (UTC): | 16 September 2024 16:03:57 |
| Eccentricity: | 0.0006417 |
| inclination: | 82.5997° |
| perigee height: | 1412 km |
| apogee height: | 1422 km |
| right ascension of ascending node: | 309.1905° |
| argument of perigee: | 97.4912° |
| revolutions per day: | 12.61372712 |
| mean anomaly at epoch: | 262.6907° |
| orbit number at epoch: | 26997 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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