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 22626U 93024A 21016.72146950 .00000187 00000-0 17504-4 0 9997
2 22626 82.5207 246.8263 0020380 92.5466 267.8085 14.88071526500575
| Epoch (UTC): | 16 January 2021 17:18:54 |
| Eccentricity: | 0.0020380 |
| inclination: | 82.5207° |
| perigee height: | 590 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 246.8263° |
| argument of perigee: | 92.5466° |
| revolutions per day: | 14.88071526 |
| mean anomaly at epoch: | 267.8085° |
| orbit number at epoch: | 50057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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