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 08305U 74089BN 24357.57663646 -.00000058 00000-0 -13542-3 0 9991
2 08305 101.4997 226.4122 0092531 190.7030 199.0460 12.35163429258211
| Epoch (UTC): | 22 December 2024 13:50:21 |
| Eccentricity: | 0.0092531 |
| inclination: | 101.4997° |
| perigee height: | 1454 km |
| apogee height: | 1600 km |
| right ascension of ascending node: | 226.4122° |
| argument of perigee: | 190.7030° |
| revolutions per day: | 12.35163429 |
| mean anomaly at epoch: | 199.0460° |
| orbit number at epoch: | 25821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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