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 22179.76143388 .00001338 00000-0 11744-3 0 9993
2 00022 50.2812 220.7278 0134635 213.7814 145.4501 14.97111208581323
| Epoch (UTC): | 28 June 2022 18:16:27 |
| Eccentricity: | 0.0134635 |
| inclination: | 50.2812° |
| perigee height: | 482 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 220.7278° |
| argument of perigee: | 213.7814° |
| revolutions per day: | 14.97111208 |
| mean anomaly at epoch: | 145.4501° |
| orbit number at epoch: | 58132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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