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 24280.95412922 .00000746 00000-0 26843-3 0 9991
2 27387 98.8080 273.5039 0032759 149.1034 211.2088 14.36497537184575
| Epoch (UTC): | 06 October 2024 22:53:56 |
| Eccentricity: | 0.0032759 |
| inclination: | 98.8080° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 273.5039° |
| argument of perigee: | 149.1034° |
| revolutions per day: | 14.36497537 |
| mean anomaly at epoch: | 211.2088° |
| orbit number at epoch: | 18457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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