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 66941U 26145.02437575 +.00000000 +00000-0 +64895-3 0 00005
2 66941 53.1585 3.1936 0000992 83.8847 276.2269 15.34398180 01
| Epoch (UTC): | 25 May 2026 00:35:06 |
| Eccentricity: | 0.0000992 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.1936° |
| argument of perigee: | 83.8847° |
| revolutions per day: | 15.34398180 |
| mean anomaly at epoch: | 276.2269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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