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 59680U 24085D 24358.18582669 .00022176 00000-0 84477-3 0 9995
2 59680 97.3842 69.4745 0011258 132.6851 227.5338 15.26673208 35009
| Epoch (UTC): | 23 December 2024 04:27:35 |
| Eccentricity: | 0.0011258 |
| inclination: | 97.3842° |
| perigee height: | 478 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 69.4745° |
| argument of perigee: | 132.6851° |
| revolutions per day: | 15.26673208 |
| mean anomaly at epoch: | 227.5338° |
| orbit number at epoch: | 3500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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