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 66959U 26145.15879596 +.00000000 +00000-0 +45074-3 0 00009
2 66959 42.9991 311.4929 0000650 296.1163 63.9622 15.27580108 04
| Epoch (UTC): | 25 May 2026 03:48:39 |
| Eccentricity: | 0.0000650 |
| inclination: | 42.9991° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 311.4929° |
| argument of perigee: | 296.1163° |
| revolutions per day: | 15.27580108 |
| mean anomaly at epoch: | 63.9622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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