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 20692U 90050D 23078.12919733 0.00004618 00000-0 53289-3 0 00
2 20692 63.3184 128.6771 0897626 65.6753 295.1403 13.45531668 04
| Epoch (UTC): | 19 March 2023 03:06:02 |
| Eccentricity: | 0.0897626 |
| inclination: | 63.3184° |
| perigee height: | 418 km |
| apogee height: | 1759 km |
| right ascension of ascending node: | 128.6771° |
| argument of perigee: | 65.6753° |
| revolutions per day: | 13.45531668 |
| mean anomaly at epoch: | 295.1403° |
| 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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