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 65983U 26145.33105505 +.00000000 +00000-0 +19437-3 0 00001
2 65983 81.3025 232.8290 0001219 119.3865 240.7414 13.84125667 09
| Epoch (UTC): | 25 May 2026 07:56:43 |
| Eccentricity: | 0.0001219 |
| inclination: | 81.3025° |
| perigee height: | 948 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 232.8290° |
| argument of perigee: | 119.3865° |
| revolutions per day: | 13.84125667 |
| mean anomaly at epoch: | 240.7414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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