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 00022U 59009A 23331.90367072 .00012273 00000-0 77909-3 0 9993
2 00022 50.2798 297.1287 0121452 43.8373 317.2140 15.03272265658938
| Epoch (UTC): | 27 November 2023 21:41:17 |
| Eccentricity: | 0.0121452 |
| inclination: | 50.2798° |
| perigee height: | 472 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 297.1287° |
| argument of perigee: | 43.8373° |
| revolutions per day: | 15.03272265 |
| mean anomaly at epoch: | 317.2140° |
| orbit number at epoch: | 65893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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