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 22U 59009A 23026.79669797 .00007247 00000-0 51734-3 0 9993
2 22 50.2822 301.8350 0130075 307.1029 51.8089 14.98886838368060
| Epoch (UTC): | 26 January 2023 19:07:14 |
| Eccentricity: | 0.0130075 |
| inclination: | 50.2822° |
| perigee height: | 480 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 301.8350° |
| argument of perigee: | 307.1029° |
| revolutions per day: | 14.98886838 |
| mean anomaly at epoch: | 51.8089° |
| orbit number at epoch: | 36806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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