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 24278.51624493 .00000774 00000-0 27794-3 0 9995
2 27387 98.8079 271.0112 0032644 156.1454 204.1252 14.36494291184191
| Epoch (UTC): | 04 October 2024 12:23:23 |
| Eccentricity: | 0.0032644 |
| inclination: | 98.8079° |
| perigee height: | 747 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 271.0112° |
| argument of perigee: | 156.1454° |
| revolutions per day: | 14.36494291 |
| mean anomaly at epoch: | 204.1252° |
| orbit number at epoch: | 18419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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