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 65774U 26145.64830969 +.00000000 +00000-0 +91958-5 0 00002
2 65774 51.9043 17.8180 0000978 125.7128 234.3925 14.79938043 04
| Epoch (UTC): | 25 May 2026 15:33:33 |
| Eccentricity: | 0.0000978 |
| inclination: | 51.9043° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 17.8180° |
| argument of perigee: | 125.7128° |
| revolutions per day: | 14.79938043 |
| mean anomaly at epoch: | 234.3925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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