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 25568U 98072B 24250.87487417 .00000416 00000-0 43422-3 0 9990
2 25568 82.9510 202.0649 0026609 87.7127 333.1923 13.72915895289408
| Epoch (UTC): | 06 September 2024 20:59:49 |
| Eccentricity: | 0.0026609 |
| inclination: | 82.9510° |
| perigee height: | 969 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 202.0649° |
| argument of perigee: | 87.7127° |
| revolutions per day: | 13.72915895 |
| mean anomaly at epoch: | 333.1923° |
| orbit number at epoch: | 28940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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