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 27006U 01056F 22230.42316022 .00000000 00000-0 50755-4 0 9992
2 27006 99.5856 5.9639 0015469 92.2548 336.3081 13.70982017 35231
| Epoch (UTC): | 18 August 2022 10:09:21 |
| Eccentricity: | 0.0015469 |
| inclination: | 99.5856° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 5.9639° |
| argument of perigee: | 92.2548° |
| revolutions per day: | 13.70982017 |
| mean anomaly at epoch: | 336.3081° |
| orbit number at epoch: | 3523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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