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 23087U 94023A 23156.92289063 .00000024 00000-0 37607-4 0 9997
2 23087 71.0533 122.8316 0007060 138.1487 222.0177 14.13966916502339
| Epoch (UTC): | 05 June 2023 22:08:57 |
| Eccentricity: | 0.0007060 |
| inclination: | 71.0533° |
| perigee height: | 841 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 122.8316° |
| argument of perigee: | 138.1487° |
| revolutions per day: | 14.13966916 |
| mean anomaly at epoch: | 222.0177° |
| orbit number at epoch: | 50233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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