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 40553U 15020B 23088.47753628 .00000022 00000-0 85079-4 0 9995
2 40553 82.4919 44.3030 0016016 35.4360 324.7776 12.42892191362715
| Epoch (UTC): | 29 March 2023 11:27:39 |
| Eccentricity: | 0.0016016 |
| inclination: | 82.4919° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 44.3030° |
| argument of perigee: | 35.4360° |
| revolutions per day: | 12.42892191 |
| mean anomaly at epoch: | 324.7776° |
| orbit number at epoch: | 36271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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