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 23342U 94074A 24281.85710758 .00006076 00000-0 75519-3 0 9995
2 23342 97.7197 311.5006 0001092 71.9163 288.2170 14.82907373612350
| Epoch (UTC): | 07 October 2024 20:34:14 |
| Eccentricity: | 0.0001092 |
| inclination: | 97.7197° |
| perigee height: | 619 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 311.5006° |
| argument of perigee: | 71.9163° |
| revolutions per day: | 14.82907373 |
| mean anomaly at epoch: | 288.2170° |
| orbit number at epoch: | 61235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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