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 22331.84321808 .00003315 00000-0 25302-3 0 9999
2 00022 50.2805 224.5692 0132388 77.0339 284.5355 14.98066857604118
| Epoch (UTC): | 27 November 2022 20:14:14 |
| Eccentricity: | 0.0132388 |
| inclination: | 50.2805° |
| perigee height: | 481 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 224.5692° |
| argument of perigee: | 77.0339° |
| revolutions per day: | 14.98066857 |
| mean anomaly at epoch: | 284.5355° |
| orbit number at epoch: | 60411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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