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 24256.92336084 .00000669 00000-0 24261-3 0 9991
2 27387 98.8058 248.9340 0031465 220.2010 139.6848 14.36474106181097
| Epoch (UTC): | 12 September 2024 22:09:38 |
| Eccentricity: | 0.0031465 |
| inclination: | 98.8058° |
| perigee height: | 747 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 248.9340° |
| argument of perigee: | 220.2010° |
| revolutions per day: | 14.36474106 |
| mean anomaly at epoch: | 139.6848° |
| orbit number at epoch: | 18109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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