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 66648U 26145.50977219 +.00000000 +00000-0 +99238-4 0 00006
2 66648 82.5036 184.6426 0009791 230.5569 129.4645 12.42917928 09
| Epoch (UTC): | 25 May 2026 12:14:04 |
| Eccentricity: | 0.0009791 |
| inclination: | 82.5036° |
| perigee height: | 1487 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 184.6426° |
| argument of perigee: | 230.5569° |
| revolutions per day: | 12.42917928 |
| mean anomaly at epoch: | 129.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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