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 26948U 01046A 24121.83638540 0.00000000 00000-0 00000-0 0 00
2 26948 12.9159 33.2875 0003624 194.0815 165.9197 1.00270000 07
| Epoch (UTC): | 30 April 2024 20:04:23 |
| Eccentricity: | 0.0003624 |
| inclination: | 12.9159° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 33.2875° |
| argument of perigee: | 194.0815° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 165.9197° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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