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 09023U 76069B 23083.66195063 .00000771 00000-0 25290-3 0 9990
2 09023 74.0439 168.3707 0017257 177.2572 182.8681 14.39960502447679
| Epoch (UTC): | 24 March 2023 15:53:12 |
| Eccentricity: | 0.0017257 |
| inclination: | 74.0439° |
| perigee height: | 746 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 168.3707° |
| argument of perigee: | 177.2572° |
| revolutions per day: | 14.39960502 |
| mean anomaly at epoch: | 182.8681° |
| orbit number at epoch: | 44767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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