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 66085U 26145.27815124 +.00000000 +00000-0 +97857-3 0 00005
2 66085 53.1587 249.7921 0002640 86.0805 274.0498 15.30228624 06
| Epoch (UTC): | 25 May 2026 06:40:32 |
| Eccentricity: | 0.0002640 |
| inclination: | 53.1587° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 249.7921° |
| argument of perigee: | 86.0805° |
| revolutions per day: | 15.30228624 |
| mean anomaly at epoch: | 274.0498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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