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 22141.45762683 .00014871 00000-0 60257-3 0 9996
2 47311 60.6849 103.8394 0012375 302.1162 57.8725 15.24850497 74349
| Epoch (UTC): | 21 May 2022 10:58:58 |
| Eccentricity: | 0.0012375 |
| inclination: | 60.6849° |
| perigee height: | 483 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 103.8394° |
| argument of perigee: | 302.1162° |
| revolutions per day: | 15.24850497 |
| mean anomaly at epoch: | 57.8725° |
| orbit number at epoch: | 7434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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