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 65779U 26145.01357524 +.00000000 +00000-0 -84939-4 0 00000
2 65779 51.9034 45.6360 0000783 104.3793 255.7257 14.79930676 02
| Epoch (UTC): | 25 May 2026 00:19:32 |
| Eccentricity: | 0.0000783 |
| inclination: | 51.9034° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 45.6360° |
| argument of perigee: | 104.3793° |
| revolutions per day: | 14.79930676 |
| mean anomaly at epoch: | 255.7257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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