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 24280.84495645 .00006432 00000-0 79935-3 0 9990
2 23342 97.7196 310.5231 0001105 70.0620 290.0713 14.82894923612205
| Epoch (UTC): | 06 October 2024 20:16:44 |
| Eccentricity: | 0.0001105 |
| inclination: | 97.7196° |
| perigee height: | 619 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 310.5231° |
| argument of perigee: | 70.0620° |
| revolutions per day: | 14.82894923 |
| mean anomaly at epoch: | 290.0713° |
| orbit number at epoch: | 61220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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