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 66940U 26145.31648242 +.00000000 +00000-0 +68407-3 0 00004
2 66940 53.1610 2.1725 0001377 88.4294 271.6866 15.34406616 05
| Epoch (UTC): | 25 May 2026 07:35:44 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.1725° |
| argument of perigee: | 88.4294° |
| revolutions per day: | 15.34406616 |
| mean anomaly at epoch: | 271.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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