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 65952U 26144.66374469 +.00000000 +00000-0 +45221-3 0 00009
2 65952 51.8999 27.1229 0000948 90.1349 269.9722 14.79927228 08
| Epoch (UTC): | 24 May 2026 15:55:47 |
| Eccentricity: | 0.0000948 |
| inclination: | 51.8999° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 27.1229° |
| argument of perigee: | 90.1349° |
| revolutions per day: | 14.79927228 |
| mean anomaly at epoch: | 269.9722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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