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 47500U 21006CR 22183.86487952 .00006985 00000-0 36357-3 0 9995
2 47500 97.4457 243.0360 0009580 213.4893 146.5736 15.16296960 79603
| Epoch (UTC): | 02 July 2022 20:45:25 |
| Eccentricity: | 0.0009580 |
| inclination: | 97.4457° |
| perigee height: | 510 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 243.0360° |
| argument of perigee: | 213.4893° |
| revolutions per day: | 15.16296960 |
| mean anomaly at epoch: | 146.5736° |
| orbit number at epoch: | 7960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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