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 23337.81959417 .00010411 00000-0 66184-3 0 9994
2 22 50.2792 269.0155 0121088 66.8259 294.5395 15.03433081414784
| Epoch (UTC): | 03 December 2023 19:40:12 |
| Eccentricity: | 0.0121088 |
| inclination: | 50.2792° |
| perigee height: | 472 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 269.0155° |
| argument of perigee: | 66.8259° |
| revolutions per day: | 15.03433081 |
| mean anomaly at epoch: | 294.5395° |
| orbit number at epoch: | 41478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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