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 26931U 01043C 24340.81665389 .00000640 00000-0 27142-3 0 9997
2 26931 67.0510 248.0629 0006919 260.9089 99.1230 14.31530110210671
| Epoch (UTC): | 05 December 2024 19:35:58 |
| Eccentricity: | 0.0006919 |
| inclination: | 67.0510° |
| perigee height: | 781 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 248.0629° |
| argument of perigee: | 260.9089° |
| revolutions per day: | 14.31530110 |
| mean anomaly at epoch: | 99.1230° |
| orbit number at epoch: | 21067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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