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 65229U 26145.60962181 +.00000000 +00000-0 +11350-3 0 00001
2 65229 86.5021 21.1962 0001704 84.7991 275.3337 13.24412897 00
| Epoch (UTC): | 25 May 2026 14:37:51 |
| Eccentricity: | 0.0001704 |
| inclination: | 86.5021° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1962° |
| argument of perigee: | 84.7991° |
| revolutions per day: | 13.24412897 |
| mean anomaly at epoch: | 275.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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