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 20642U 90050E 23219.86063813 0.00006000 00000-0 54324-3 0 00
2 20642 63.3080 117.8805 0920789 63.0277 296.9723 13.47402790 01
| Epoch (UTC): | 07 August 2023 20:39:19 |
| Eccentricity: | 0.0920789 |
| inclination: | 63.3080° |
| perigee height: | 395 km |
| apogee height: | 1769 km |
| right ascension of ascending node: | 117.8805° |
| argument of perigee: | 63.0277° |
| revolutions per day: | 13.47402790 |
| mean anomaly at epoch: | 296.9723° |
| 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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