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 23264.90002470 .00000253 00000-0 96486-4 0 9993
2 27386 98.2421 230.9817 0001212 87.1635 299.5185 14.38408790129869
| Epoch (UTC): | 21 September 2023 21:36:02 |
| Eccentricity: | 0.0001212 |
| inclination: | 98.2421° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 230.9817° |
| argument of perigee: | 87.1635° |
| revolutions per day: | 14.38408790 |
| mean anomaly at epoch: | 299.5185° |
| orbit number at epoch: | 12986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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