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 66965U 26145.47672639 +.00000000 +00000-0 +58606-3 0 00005
2 66965 42.9950 309.5787 0000334 315.2231 44.8594 15.27597298 08
| Epoch (UTC): | 25 May 2026 11:26:29 |
| Eccentricity: | 0.0000334 |
| inclination: | 42.9950° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 309.5787° |
| argument of perigee: | 315.2231° |
| revolutions per day: | 15.27597298 |
| mean anomaly at epoch: | 44.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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