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 02680U 67014A 24357.31149819 .00000910 00000-0 38929-3 0 9995
2 02680 39.4425 348.5189 0708126 193.3794 164.7232 13.40532843803204
| Epoch (UTC): | 22 December 2024 07:28:33 |
| Eccentricity: | 0.0708126 |
| inclination: | 39.4425° |
| perigee height: | 577 km |
| apogee height: | 1637 km |
| right ascension of ascending node: | 348.5189° |
| argument of perigee: | 193.3794° |
| revolutions per day: | 13.40532843 |
| mean anomaly at epoch: | 164.7232° |
| orbit number at epoch: | 80320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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