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 47311U 21002C 22178.56301048 .00005608 00000-0 22997-3 0 9999
2 47311 60.6857 324.1853 0018027 344.5364 15.5171 15.25442644 80008
| Epoch (UTC): | 27 June 2022 13:30:44 |
| Eccentricity: | 0.0018027 |
| inclination: | 60.6857° |
| perigee height: | 477 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 324.1853° |
| argument of perigee: | 344.5364° |
| revolutions per day: | 15.25442644 |
| mean anomaly at epoch: | 15.5171° |
| orbit number at epoch: | 8000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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