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 24252.89531354 .00000753 00000-0 25934-3 0 9991
2 27386 98.2906 211.1099 0001213 87.7993 292.6006 14.38664338180544
| Epoch (UTC): | 08 September 2024 21:29:15 |
| Eccentricity: | 0.0001213 |
| inclination: | 98.2906° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 211.1099° |
| argument of perigee: | 87.7993° |
| revolutions per day: | 14.38664338 |
| mean anomaly at epoch: | 292.6006° |
| orbit number at epoch: | 18054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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