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 23712U 95060A 23088.39180767 -.00000022 00000-0 00000-0 0 9992
2 23712 13.6354 12.2147 0002160 331.1480 224.1901 1.00274483 21095
| Epoch (UTC): | 29 March 2023 09:24:12 |
| Eccentricity: | 0.0002160 |
| inclination: | 13.6354° |
| perigee height: | 35776 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 12.2147° |
| argument of perigee: | 331.1480° |
| revolutions per day: | 1.00274483 |
| mean anomaly at epoch: | 224.1901° |
| orbit number at epoch: | 2109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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