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 03978U 65082SE 24280.88980656 .00004951 00000-0 82592-3 0 9992
2 03978 32.5668 353.8955 0035134 157.2089 203.0133 14.68530657355881
| Epoch (UTC): | 06 October 2024 21:21:19 |
| Eccentricity: | 0.0035134 |
| inclination: | 32.5668° |
| perigee height: | 641 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 353.8955° |
| argument of perigee: | 157.2089° |
| revolutions per day: | 14.68530657 |
| mean anomaly at epoch: | 203.0133° |
| orbit number at epoch: | 35588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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