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 65976U 26144.65708125 +.00000000 +00000-0 -61941-2 0 00001
2 65976 81.2981 233.6607 0001231 189.4690 170.6443 13.83052566 09
| Epoch (UTC): | 24 May 2026 15:46:11 |
| Eccentricity: | 0.0001231 |
| inclination: | 81.2981° |
| perigee height: | 952 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 233.6607° |
| argument of perigee: | 189.4690° |
| revolutions per day: | 13.83052566 |
| mean anomaly at epoch: | 170.6443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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