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 27060U 01058F 21025.74277294 .00000006 00000-0 -23672-4 0 9992
2 27060 82.5413 20.1220 0009543 89.3037 270.9150 12.63003385879669
| Epoch (UTC): | 25 January 2021 17:49:35 |
| Eccentricity: | 0.0009543 |
| inclination: | 82.5413° |
| perigee height: | 1403 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 20.1220° |
| argument of perigee: | 89.3037° |
| revolutions per day: | 12.63003385 |
| mean anomaly at epoch: | 270.9150° |
| orbit number at epoch: | 87966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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