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 66762U 26145.62487980 +.00000000 +00000-0 +18282-3 0 00006
2 66762 97.4206 218.7844 0012442 124.7917 235.4486 15.11317594 04
| Epoch (UTC): | 25 May 2026 14:59:49 |
| Eccentricity: | 0.0012442 |
| inclination: | 97.4206° |
| perigee height: | 524 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.7844° |
| argument of perigee: | 124.7917° |
| revolutions per day: | 15.11317594 |
| mean anomaly at epoch: | 235.4486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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