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 23151.88434161 .00000271 00000-0 94251-4 0 9994
2 09023 74.0446 42.3707 0016787 27.8498 332.3552 14.40020625457497
| Epoch (UTC): | 31 May 2023 21:13:27 |
| Eccentricity: | 0.0016787 |
| inclination: | 74.0446° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 42.3707° |
| argument of perigee: | 27.8498° |
| revolutions per day: | 14.40020625 |
| mean anomaly at epoch: | 332.3552° |
| orbit number at epoch: | 45749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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