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 23153.13482670 .00000298 00000-0 10294-3 0 9995
2 09023 74.0445 40.0611 0016832 25.2384 334.9590 14.40021579457671
| Epoch (UTC): | 02 June 2023 03:14:09 |
| Eccentricity: | 0.0016832 |
| inclination: | 74.0445° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 40.0611° |
| argument of perigee: | 25.2384° |
| revolutions per day: | 14.40021579 |
| mean anomaly at epoch: | 334.9590° |
| orbit number at epoch: | 45767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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