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 26045.94846536 +.00000000 +00000-0 +52465-4 0 00008
2 23705 71.0196 227.9983 0011717 164.6403 195.5078 14.15495655 04
| Epoch (UTC): | 14 February 2026 22:45:47 |
| Eccentricity: | 0.0011717 |
| inclination: | 71.0196° |
| perigee height: | 832 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 227.9983° |
| argument of perigee: | 164.6403° |
| revolutions per day: | 14.15495655 |
| mean anomaly at epoch: | 195.5078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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