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 23156.81680596 .00000300 00000-0 10338-3 0 9993
2 09023 74.0444 33.2608 0016977 17.3927 342.7806 14.40024139458207
| Epoch (UTC): | 05 June 2023 19:36:12 |
| Eccentricity: | 0.0016977 |
| inclination: | 74.0444° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 33.2608° |
| argument of perigee: | 17.3927° |
| revolutions per day: | 14.40024139 |
| mean anomaly at epoch: | 342.7806° |
| orbit number at epoch: | 45820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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