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 23789U 96009C 21026.24890978 .00000028 00000-0 95002-4 0 9991
2 23789 82.5813 136.2705 0004908 192.7723 167.3245 12.62614444149347
| Epoch (UTC): | 26 January 2021 05:58:25 |
| Eccentricity: | 0.0004908 |
| inclination: | 82.5813° |
| perigee height: | 1408 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 136.2705° |
| argument of perigee: | 192.7723° |
| revolutions per day: | 12.62614444 |
| mean anomaly at epoch: | 167.3245° |
| orbit number at epoch: | 14934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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