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 41459U 16025D 23266.77034071 .00048595 00000-0 11645-2 0 9995
2 41459 98.1742 118.5088 0094486 113.9734 247.1437 15.36658261408009
| Epoch (UTC): | 23 September 2023 18:29:17 |
| Eccentricity: | 0.0094486 |
| inclination: | 98.1742° |
| perigee height: | 391 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 118.5088° |
| argument of perigee: | 113.9734° |
| revolutions per day: | 15.36658261 |
| mean anomaly at epoch: | 247.1437° |
| orbit number at epoch: | 40800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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