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 20U 59007A 22022.76775283 .00000667 00000-0 27421-3 0 9994
2 20 33.3408 260.1165 1665298 126.8434 249.6727 11.56006765298262
| Epoch (UTC): | 22 January 2022 18:25:33 |
| Eccentricity: | 0.1665298 |
| inclination: | 33.3408° |
| perigee height: | 508 km |
| apogee height: | 3260 km |
| right ascension of ascending node: | 260.1165° |
| argument of perigee: | 126.8434° |
| revolutions per day: | 11.56006765 |
| mean anomaly at epoch: | 249.6727° |
| orbit number at epoch: | 29826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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