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 65772U 26145.47819373 +.00000000 +00000-0 +24546-3 0 00004
2 65772 51.9008 51.0394 0001025 88.3145 271.7935 14.79936258 09
| Epoch (UTC): | 25 May 2026 11:28:35 |
| Eccentricity: | 0.0001025 |
| inclination: | 51.9008° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 51.0394° |
| argument of perigee: | 88.3145° |
| revolutions per day: | 14.79936258 |
| mean anomaly at epoch: | 271.7935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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