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 43476U 18047A 22267.57995368 +.00002486 00000-0 +10005-3 0 07
2 43476 88.9951 25.0514 0013405 343.8327 118.1099 15.24757182241521
| Epoch (UTC): | 24 September 2022 13:55:07 |
| Eccentricity: | 0.0013405 |
| inclination: | 88.9951° |
| perigee height: | 482 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 25.0514° |
| argument of perigee: | 343.8327° |
| revolutions per day: | 15.24757182 |
| mean anomaly at epoch: | 118.1099° |
| orbit number at epoch: | 24152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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