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 22176.73036342 .00008038 00000-0 38783-3 0 9997
2 47497 97.4360 235.6806 0007926 235.1003 124.9487 15.18922542 78548
| Epoch (UTC): | 25 June 2022 17:31:43 |
| Eccentricity: | 0.0007926 |
| inclination: | 97.4360° |
| perigee height: | 503 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 235.6806° |
| argument of perigee: | 235.1003° |
| revolutions per day: | 15.18922542 |
| mean anomaly at epoch: | 124.9487° |
| orbit number at epoch: | 7854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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