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 30309U 99025ZW 24263.42794133 .00000765 00000-0 60274-3 0 9990
2 30309 99.2870 314.4785 0092993 330.7741 28.8234 13.92956612897871
| Epoch (UTC): | 19 September 2024 10:16:14 |
| Eccentricity: | 0.0092993 |
| inclination: | 99.2870° |
| perigee height: | 850 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 314.4785° |
| argument of perigee: | 330.7741° |
| revolutions per day: | 13.92956612 |
| mean anomaly at epoch: | 28.8234° |
| orbit number at epoch: | 89787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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