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 40071U 14037C 22136.06025745 .00000746 00000-0 10183-3 0 9993
2 40071 98.4147 3.1828 0009552 64.7624 295.4591 14.81808337424546
| Epoch (UTC): | 16 May 2022 01:26:46 |
| Eccentricity: | 0.0009552 |
| inclination: | 98.4147° |
| perigee height: | 617 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 3.1828° |
| argument of perigee: | 64.7624° |
| revolutions per day: | 14.81808337 |
| mean anomaly at epoch: | 295.4591° |
| orbit number at epoch: | 42454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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