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 39762U 14028B 23088.17094753 .00000049 00000-0 28504-3 0 9994
2 39762 82.4485 126.5999 0021772 114.7175 245.6169 12.42885212401492
| Epoch (UTC): | 29 March 2023 04:06:09 |
| Eccentricity: | 0.0021772 |
| inclination: | 82.4485° |
| perigee height: | 1477 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 126.5999° |
| argument of perigee: | 114.7175° |
| revolutions per day: | 12.42885212 |
| mean anomaly at epoch: | 245.6169° |
| orbit number at epoch: | 40149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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