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 26932U 01043D 24357.97096701 .00000242 00000-0 12311-3 0 9999
2 26932 67.0543 210.8421 0008518 262.6218 97.3916 14.31010844213070
| Epoch (UTC): | 22 December 2024 23:18:11 |
| Eccentricity: | 0.0008518 |
| inclination: | 67.0543° |
| perigee height: | 782 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 210.8421° |
| argument of perigee: | 262.6218° |
| revolutions per day: | 14.31010844 |
| mean anomaly at epoch: | 97.3916° |
| orbit number at epoch: | 21307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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