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 23153.42689040 .00021803 00000-0 57819-3 0 9995
2 47311 60.6797 115.2510 0014517 167.6205 192.5249 15.38251815132011
| Epoch (UTC): | 02 June 2023 10:14:43 |
| Eccentricity: | 0.0014517 |
| inclination: | 60.6797° |
| perigee height: | 441 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 115.2510° |
| argument of perigee: | 167.6205° |
| revolutions per day: | 15.38251815 |
| mean anomaly at epoch: | 192.5249° |
| orbit number at epoch: | 13201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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