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 41759U 16056A 22244.78142178 0.00005800 00000-0 29082-3 0 06
2 41759 141.7144 16.6800 0009224 346.3093 13.3079 15.16439381 00
| Epoch (UTC): | 01 September 2022 18:45:14 |
| Eccentricity: | 0.0009224 |
| inclination: | 141.7144° |
| perigee height: | 510 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 16.6800° |
| argument of perigee: | 346.3093° |
| revolutions per day: | 15.16439381 |
| mean anomaly at epoch: | 13.3079° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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