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 24255.57516520 .00000903 00000-0 37145-3 0 9993
2 26931 67.0499 108.3571 0007696 267.9798 92.0422 14.31365652198316
| Epoch (UTC): | 11 September 2024 13:48:14 |
| Eccentricity: | 0.0007696 |
| inclination: | 67.0499° |
| perigee height: | 781 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 108.3571° |
| argument of perigee: | 267.9798° |
| revolutions per day: | 14.31365652 |
| mean anomaly at epoch: | 92.0422° |
| orbit number at epoch: | 19831 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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