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 22148.53886938 .00011951 00000-0 48399-3 0 9991
2 47311 60.6867 77.1955 0012779 313.6456 46.3571 15.25029387 75425
| Epoch (UTC): | 28 May 2022 12:55:58 |
| Eccentricity: | 0.0012779 |
| inclination: | 60.6867° |
| perigee height: | 482 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 77.1955° |
| argument of perigee: | 313.6456° |
| revolutions per day: | 15.25029387 |
| mean anomaly at epoch: | 46.3571° |
| orbit number at epoch: | 7542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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