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 65992U 26145.33310487 +.00000000 +00000-0 +15722-3 0 00001
2 65992 81.3032 233.4897 0001079 99.6895 260.4381 13.78090259 07
| Epoch (UTC): | 25 May 2026 07:59:40 |
| Eccentricity: | 0.0001079 |
| inclination: | 81.3032° |
| perigee height: | 970 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 233.4897° |
| argument of perigee: | 99.6895° |
| revolutions per day: | 13.78090259 |
| mean anomaly at epoch: | 260.4381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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