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 23088.69463160 .00002426 00000-0 32393-3 0 9991
2 23342 97.7862 131.3686 0001225 63.2626 296.8712 14.80449100529718
| Epoch (UTC): | 29 March 2023 16:40:16 |
| Eccentricity: | 0.0001225 |
| inclination: | 97.7862° |
| perigee height: | 627 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 131.3686° |
| argument of perigee: | 63.2626° |
| revolutions per day: | 14.80449100 |
| mean anomaly at epoch: | 296.8712° |
| orbit number at epoch: | 52971 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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