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 66511U 26145.40901837 +.00000000 +00000-0 +62994-3 0 00005
2 66511 43.0009 277.2883 0000565 263.5852 96.4936 15.27591297 06
| Epoch (UTC): | 25 May 2026 09:48:59 |
| Eccentricity: | 0.0000565 |
| inclination: | 43.0009° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 277.2883° |
| argument of perigee: | 263.5852° |
| revolutions per day: | 15.27591297 |
| mean anomaly at epoch: | 96.4936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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