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 115U 60002D 23265.48495133 .00003513 00000-0 40966-3 0 9990
2 115 48.1646 294.1483 0031574 110.5896 249.8409 14.87002232390073
| Epoch (UTC): | 22 September 2023 11:38:19 |
| Eccentricity: | 0.0031574 |
| inclination: | 48.1646° |
| perigee height: | 585 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 294.1483° |
| argument of perigee: | 110.5896° |
| revolutions per day: | 14.87002232 |
| mean anomaly at epoch: | 249.8409° |
| orbit number at epoch: | 39007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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