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 39679U 14021B 23154.19169203 .00005728 00000-0 25607-3 0 9993
2 39679 51.6113 118.4097 0154526 101.0162 260.8234 15.12799103502120
| Epoch (UTC): | 03 June 2023 04:36:02 |
| Eccentricity: | 0.0154526 |
| inclination: | 51.6113° |
| perigee height: | 421 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 118.4097° |
| argument of perigee: | 101.0162° |
| revolutions per day: | 15.12799103 |
| mean anomaly at epoch: | 260.8234° |
| orbit number at epoch: | 50212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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