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 22023.93819806 .00000073 00000-0 37754-4 0 9990
2 27386 98.1688 11.9464 0001196 86.8513 304.8715 14.38070689 42764
| Epoch (UTC): | 23 January 2022 22:31:00 |
| Eccentricity: | 0.0001196 |
| inclination: | 98.1688° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 11.9464° |
| argument of perigee: | 86.8513° |
| revolutions per day: | 14.38070689 |
| mean anomaly at epoch: | 304.8715° |
| orbit number at epoch: | 4276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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