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 42759U 17034B 23081.80109334 .00011479 00000-0 60342-3 0 9994
2 42759 43.0171 235.3230 0011676 266.0806 198.5250 15.15620779318524
| Epoch (UTC): | 22 March 2023 19:13:34 |
| Eccentricity: | 0.0011676 |
| inclination: | 43.0171° |
| perigee height: | 511 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 235.3230° |
| argument of perigee: | 266.0806° |
| revolutions per day: | 15.15620779 |
| mean anomaly at epoch: | 198.5250° |
| orbit number at epoch: | 31852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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