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 21015.51856972 .00000014 00000-0 18009-4 0 9996
2 27386 98.1413 17.4512 0001207 86.3584 23.8003 14.38008754989099
| Epoch (UTC): | 15 January 2021 12:26:44 |
| Eccentricity: | 0.0001207 |
| inclination: | 98.1413° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 17.4512° |
| argument of perigee: | 86.3584° |
| revolutions per day: | 14.38008754 |
| mean anomaly at epoch: | 23.8003° |
| orbit number at epoch: | 98909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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