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 23083.62613854 .00000665 00000-0 23228-3 0 9995
2 27386 98.2225 57.1445 0001413 87.1854 351.0148 14.38294213103805
| Epoch (UTC): | 24 March 2023 15:01:38 |
| Eccentricity: | 0.0001413 |
| inclination: | 98.2225° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 57.1445° |
| argument of perigee: | 87.1854° |
| revolutions per day: | 14.38294213 |
| mean anomaly at epoch: | 351.0148° |
| orbit number at epoch: | 10380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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