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 27386U 02009A 23036.53424872 .00000261 00000-0 99594-4 0 9995
2 27386 98.2142 12.0739 0001228 89.6473 20.1800 14.38235461 97033
| Epoch (UTC): | 05 February 2023 12:49:19 |
| Eccentricity: | 0.0001228 |
| inclination: | 98.2142° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 12.0739° |
| argument of perigee: | 89.6473° |
| revolutions per day: | 14.38235461 |
| mean anomaly at epoch: | 20.1800° |
| orbit number at epoch: | 9703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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