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 27387U 02009B 23331.92972268 .00000290 00000-0 11423-3 0 9990
2 27387 98.7803 312.9368 0032360 359.7939 0.3227 14.36284618139465
| Epoch (UTC): | 27 November 2023 22:18:48 |
| Eccentricity: | 0.0032360 |
| inclination: | 98.7803° |
| perigee height: | 747 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 312.9368° |
| argument of perigee: | 359.7939° |
| revolutions per day: | 14.36284618 |
| mean anomaly at epoch: | 0.3227° |
| orbit number at epoch: | 13946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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