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 20066U 89046A 23087.76577373 .00000035 00000-0 00000-0 0 9994
2 20066 13.7891 349.4224 0002616 105.4188 71.6478 0.98817595 14207
| Epoch (UTC): | 28 March 2023 18:22:42 |
| Eccentricity: | 0.0002616 |
| inclination: | 13.7891° |
| perigee height: | 36188 km |
| apogee height: | 36210 km |
| right ascension of ascending node: | 349.4224° |
| argument of perigee: | 105.4188° |
| revolutions per day: | 0.98817595 |
| mean anomaly at epoch: | 71.6478° |
| orbit number at epoch: | 1420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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