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 24357.91886311 .00000367 00000-0 13309-3 0 9990
2 27386 98.3106 312.7260 0001128 83.3985 344.8837 14.38792925195646
| Epoch (UTC): | 22 December 2024 22:03:09 |
| Eccentricity: | 0.0001128 |
| inclination: | 98.3106° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 312.7260° |
| argument of perigee: | 83.3985° |
| revolutions per day: | 14.38792925 |
| mean anomaly at epoch: | 344.8837° |
| orbit number at epoch: | 19564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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