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 22225.58576917 .00000052 00000-0 30674-4 0 9999
2 27386 98.1876 204.0258 0001391 85.4417 28.4947 14.38144460 71671
| Epoch (UTC): | 13 August 2022 14:03:30 |
| Eccentricity: | 0.0001391 |
| inclination: | 98.1876° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 204.0258° |
| argument of perigee: | 85.4417° |
| revolutions per day: | 14.38144460 |
| mean anomaly at epoch: | 28.4947° |
| orbit number at epoch: | 7167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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