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 47497U 21006CN 22278.42875918 .00028677 00000-0 12651-2 0 9992
2 47497 97.4249 335.8836 0007018 242.0240 118.0286 15.21711094 93991
| Epoch (UTC): | 05 October 2022 10:17:24 |
| Eccentricity: | 0.0007018 |
| inclination: | 97.4249° |
| perigee height: | 496 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 335.8836° |
| argument of perigee: | 242.0240° |
| revolutions per day: | 15.21711094 |
| mean anomaly at epoch: | 118.0286° |
| orbit number at epoch: | 9399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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