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 65766U 26145.20267796 +.00000000 +00000-0 +53013-3 0 00005
2 65766 51.9003 57.2450 0000840 93.7042 266.4017 14.79929651 09
| Epoch (UTC): | 25 May 2026 04:51:51 |
| Eccentricity: | 0.0000840 |
| inclination: | 51.9003° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 57.2450° |
| argument of perigee: | 93.7042° |
| revolutions per day: | 14.79929651 |
| mean anomaly at epoch: | 266.4017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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