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 24287.49200962 .00008225 00000-0 66078-3 0 9995
2 20692 63.2997 52.8679 0903383 73.0685 296.7297 13.54721792 21511
| Epoch (UTC): | 13 October 2024 11:48:29 |
| Eccentricity: | 0.0903383 |
| inclination: | 63.2997° |
| perigee height: | 383 km |
| apogee height: | 1726 km |
| right ascension of ascending node: | 52.8679° |
| argument of perigee: | 73.0685° |
| revolutions per day: | 13.54721792 |
| mean anomaly at epoch: | 296.7297° |
| orbit number at epoch: | 2151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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