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 is defined by the following mean orbital elements,
1 05707U 26065.64639588 +.00000000 +00000-0 +12428-3 0 00000
2 05707 74.0284 326.5877 0024329 335.0588 24.9390 14.40452142 00
| Epoch (UTC): | 06 March 2026 15:30:48 |
| Eccentricity: | 0.0024329 |
| inclination: | 74.0284° |
| perigee height: | 740 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 326.5877° |
| argument of perigee: | 335.0588° |
| revolutions per day: | 14.40452142 |
| mean anomaly at epoch: | 24.9390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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