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 23705U 26156.89642987 +.00000000 +00000-0 -72882-4 0 00005
2 23705 71.0217 355.0652 0013281 335.6559 24.3935 14.15505590 05
| Epoch (UTC): | 05 June 2026 21:30:51 |
| Eccentricity: | 0.0013281 |
| inclination: | 71.0217° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 355.0652° |
| argument of perigee: | 335.6559° |
| revolutions per day: | 14.15505590 |
| mean anomaly at epoch: | 24.3935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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