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 23156.56982910 .00004296 00000-0 19624-3 0 9995
2 39679 51.6117 107.2649 0154423 109.3575 252.4165 15.12822571502483
| Epoch (UTC): | 05 June 2023 13:40:33 |
| Eccentricity: | 0.0154423 |
| inclination: | 51.6117° |
| perigee height: | 421 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 107.2649° |
| argument of perigee: | 109.3575° |
| revolutions per day: | 15.12822571 |
| mean anomaly at epoch: | 252.4165° |
| orbit number at epoch: | 50248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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