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 23335.52037395 .00000380 00000-0 13802-3 0 9995
2 27386 98.2555 298.8505 0001298 84.2290 27.8341 14.38458011140010
| Epoch (UTC): | 01 December 2023 12:29:20 |
| Eccentricity: | 0.0001298 |
| inclination: | 98.2555° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 298.8505° |
| argument of perigee: | 84.2290° |
| revolutions per day: | 14.38458011 |
| mean anomaly at epoch: | 27.8341° |
| orbit number at epoch: | 14001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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