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 45874U 20046B 22225.92368101 0.00008916 00000-0 59426-3 0 09
2 45874 53.9768 222.8698 0009709 165.9743 194.0353 15.06578744 07
| Epoch (UTC): | 13 August 2022 22:10:06 |
| Eccentricity: | 0.0009709 |
| inclination: | 53.9768° |
| perigee height: | 540 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 222.8698° |
| argument of perigee: | 165.9743° |
| revolutions per day: | 15.06578744 |
| mean anomaly at epoch: | 194.0353° |
| 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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