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 20401U 90001A 23334.81775000 -.00000252 00000-0 00000+0 0 9999
2 20401 12.8474 354.9442 0012224 284.6484 61.0384 0.99000515119678
| Epoch (UTC): | 30 November 2023 19:37:33 |
| Eccentricity: | 0.0012224 |
| inclination: | 12.8474° |
| perigee height: | 36094 km |
| apogee height: | 36198 km |
| right ascension of ascending node: | 354.9442° |
| argument of perigee: | 284.6484° |
| revolutions per day: | 0.99000515 |
| mean anomaly at epoch: | 61.0384° |
| orbit number at epoch: | 11967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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