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 25724U 99023A 24284.54602045 .00000080 00000-0 60970-3 0 9992
2 25724 28.2342 13.8122 2129747 334.0779 16.6618 9.37506663 14665
| Epoch (UTC): | 10 October 2024 13:06:16 |
| Eccentricity: | 0.2129747 |
| inclination: | 28.2342° |
| perigee height: | 1099 km |
| apogee height: | 5146 km |
| right ascension of ascending node: | 13.8122° |
| argument of perigee: | 334.0779° |
| revolutions per day: | 9.37506663 |
| mean anomaly at epoch: | 16.6618° |
| orbit number at epoch: | 1466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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