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 66484U 26145.53258204 +.00000000 +00000-0 +41856-3 0 00005
2 66484 43.0014 222.6199 0001480 276.7412 83.3271 15.27588532 05
| Epoch (UTC): | 25 May 2026 12:46:55 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.6199° |
| argument of perigee: | 276.7412° |
| revolutions per day: | 15.27588532 |
| mean anomaly at epoch: | 83.3271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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