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 65986U 26141.78240876 +.00000000 +00000-0 +49105-4 0 00006
2 65986 81.3024 236.7175 0000944 126.6852 233.4389 13.78997230 03
| Epoch (UTC): | 21 May 2026 18:46:40 |
| Eccentricity: | 0.0000944 |
| inclination: | 81.3024° |
| perigee height: | 967 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 236.7175° |
| argument of perigee: | 126.6852° |
| revolutions per day: | 13.78997230 |
| mean anomaly at epoch: | 233.4389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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