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 30302U 99025ZP 24259.52608855 .00016510 00000-0 95101-2 0 9995
2 30302 98.5521 183.3370 0118594 330.0809 29.3617 14.05696127896682
| Epoch (UTC): | 15 September 2024 12:37:34 |
| Eccentricity: | 0.0118594 |
| inclination: | 98.5521° |
| perigee height: | 788 km |
| apogee height: | 960 km |
| right ascension of ascending node: | 183.3370° |
| argument of perigee: | 330.0809° |
| revolutions per day: | 14.05696127 |
| mean anomaly at epoch: | 29.3617° |
| orbit number at epoch: | 89668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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